COLOMBIA A320

LAN COLOMBIA AIRLINES

MINIMUM EQUIPMENT LIST
Issue date 27 February 2015

This document is based on MMEL rev date: 02 DEC 14

EASA Project N 0010002556-001 Approval date: 31 OCT 14

Applicable to the following aircrafts:

CC-BAF CC-BAG CC-BAN CC-BAO CC-BAR CC-BAS CC-BAT CC-BAU CC-BAV
CC-BAX CC-BAZ CC-BFA CC-BFB CC-BFC CC-BFD CC-BFE CC-BFG CC-BFH

The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its
contents must be maintained. It must not be used for any purpose other than that for which it is supplied, nor may
information contained in it be disclosed to unauthorized persons. It must not be reproduced in whole or in part
without permission in writing from the owners of the copyright.

AIRBUS 2005. All Rights Reserved.

AIRBUS S.A.S
CUSTOMER SERVICES DIRECTORATE
31707 BLAGNAC CEDEX
FRANCE

REFERENCE: LAN COLOMBIA A320 FLEET MEL ISSUE DATE: 27 FEB 15

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 COLOMBIA

LAN COLOMBIA AIRLINES

MINIMUM EQUIPMENT LIST

The content of this document is the property of Airbus. It is supplied in confidence and commercial
security on its contents must be maintained. It must not be used for any purpose other than that for
which it is supplied, nor may information contained in it be disclosed to unauthorized persons. It must
not be reproduced in whole or in part without permission in writing from the owners of the copyright.
AIRBUS 2005. All rights reserved.

AIRBUS S.A.S
CUSTOMER SERVICES DIRECTORATE
31707 BLAGNAC CEDEX
FRANCE

REFERENCE: LAN COLOMBIA FLEET MEL ISSUE DATE: 27 FEB 15

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 TRANSMITTAL LETTER

COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Issue date: 27 FEB 15

This is the LAN COLOMBIA AIRLINES MINIMUM EQUIPMENT LIST at issue date 27 FEB 15 for
the COLOMBIA and replacing last issue dated 12 DEC 14

No comment

LAN COLOMBIA FLEET TRL P 1/2

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COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET TRL P 2/2

MEL 27 FEB 15
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COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Please incorporate this revision as follow:

Localization Insert
Remove
Subsection Title Rev. Date
PLP-LESS
ALL 27 FEB 15
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
PLP-LEDU
ALL 27 FEB 15
LIST OF EFFECTIVE DOCUMENTARY UNITS
HOW-PLP-TOC
ALL 27 FEB 15
TABLE OF CONTENTS
HOW-PLP-SOH
ALL 27 FEB 15
SUMMARY OF HIGHLIGHTS
HOW
ALL 27 FEB 15
How to Use
ME-PLP-TOC
ALL 27 FEB 15
TABLE OF CONTENTS
ME-PLP-SOH
ALL 27 FEB 15
SUMMARY OF HIGHLIGHTS
ME-21
ALL 27 FEB 15
Air Conditioning
ME-23
ALL 27 FEB 15
Communications
ME-24
ALL 27 FEB 15
Electrical Power
ME-26
ALL 27 FEB 15
Fire Protection
ME-27
ALL 27 FEB 15
Flight Controls
ME-28
ALL 27 FEB 15
Fuel
ME-30
ALL 27 FEB 15
Ice and Rain Protection
ME-31
ALL 27 FEB 15
Indicating/Recording Systems
ME-32
ALL 27 FEB 15
Landing Gear
ME-34
ALL 27 FEB 15
Navigation
ME-36
ALL 27 FEB 15
Pneumatic
ME-47
ALL 27 FEB 15
Inert Gas System
Continued on the following page

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LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

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Subsection Title Rev. Date
ME-70
ALL 27 FEB 15
Engine
MI-PLP-TOC
ALL 27 FEB 15
TABLE OF CONTENTS
MI-PLP-SOH
ALL 27 FEB 15
SUMMARY OF HIGHLIGHTS
MI-00-01
ALL 27 FEB 15
Approval Reference
MI-00-08
ALL 27 FEB 15
ECAM and MAINTENANCE STATUS
MI-21-00
ALL 27 FEB 15
MAINTENANCE Messages on the STATUS SD page
MI-21-01-03
ALL 27 FEB 15
CARGO VENT Overhead Panel
MI-21-28
ALL 27 FEB 15
Cargo Compartment Ventilation
MI-21-51
ALL 27 FEB 15
Pack Flow Control
MI-21-52
ALL 27 FEB 15
Air Cooling System
MI-21-63
ALL 27 FEB 15
Cockpit and Cabin Temperature Control
MI-22-70
ALL 27 FEB 15
Flight Management System (FMS)
MI-22-81-01
ALL 27 FEB 15
Auto Flight Control Panel (FCU)
MI-22-81-03
ALL 27 FEB 15
FCU Channel
MI-22-83
ALL 27 FEB 15
Flight Management and Guidance Computer (FMGC)
MI-23-10
ALL 27 FEB 15
Speech Communication
MI-23-73-01
ALL 27 FEB 15
Cabin Intercommunication Data System (CIDS)
MI-23-73-03
ALL 27 FEB 15
DEU B
MI-23-73-10
ALL 27 FEB 15
Smoke Detection Function
MI-23-74
ALL 27 FEB 15
Cabin Crew Panel
Continued on the following page

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LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

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Subsection Title Rev. Date
MI-24-01-01
ALL 27 FEB 15
ELEC Overhead Panel
MI-24-22
ALL 27 FEB 15
AC Main Generation
MI-24-26
ALL 27 FEB 15
Galley and Commercial Supply System
MI-24-32
ALL 27 FEB 15
DC Main Generation (TR 1, TR 2)
MI-26-00
ALL 27 FEB 15
MAINTENANCE Message on the STATUS SD page
MI-26-13
ALL 27 FEB 15
APU Fire and Overheat Detection
MI-26-16
ALL 27 FEB 15
Cargo Compartment Smoke Detection
MI-26-17
ALL 27 FEB 15
Lavatory Smoke Detection
MI-27-07
ALL 27 FEB 15
Indications on SD pages
MI-27-64
ALL 27 FEB 15
Spoiler Hydraulic Actuation
MI-27-94
ALL 27 FEB 15
SEC System (Spoiler and Elevator Computer)
MI-28-07-05
ALL 27 FEB 15
Fuel Flow Indication on the FUEL SD page
MI-28-07-06
ALL 27 FEB 15
Fuel Used Indication on the FUEL SD page
MI-28-21
ALL 27 FEB 15
Main Fuel Pump System
MI-28-25
ALL 27 FEB 15
Refuel/Defuel System
MI-29-01-01
ALL 27 FEB 15
HYD Overhead Panel
MI-29-10
ALL 27 FEB 15
Main Hydraulic Power
MI-30-00
ALL 27 FEB 15
MAINTENANCE Message on the STATUS SD page
MI-30-21
ALL 27 FEB 15
Engine Air Intake Ice Protection
MI-30-81
ALL 27 FEB 15
Ice Detection
Continued on the following page

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LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

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Subsection Title Rev. Date
MI-31-00
ALL 27 FEB 15
MAINTENANCE Message on the STATUS SD page
MI-31-07
ALL 27 FEB 15
Indications on the System Display (SD)
MI-31-62
ALL 27 FEB 15
Display Management Computer (DMC)
MI-32-07
ALL 27 FEB 15
Indications on the WHEEL SD page
MI-32-09
ALL 27 FEB 15
ECAM Alerts
MI-32-44
ALL 27 FEB 15
Alternate Braking
MI-33-10
ALL 27 FEB 15
Cockpit General Illumination
MI-33-51
ALL 27 FEB 15
Cabin Emergency Lighting
MI-34-00
ALL 27 FEB 15
MAINTENANCE Messages on the STATUS SD page
MI-34-01-01
ALL 27 FEB 15
ADIRS Overhead Panel
MI-34-05
ALL 27 FEB 15
Indications on the Primary Flight Display (PFD)
MI-34-10
ALL 27 FEB 15
Air Data/Inertial Reference System (ADIRS)
MI-34-22
ALL 27 FEB 15
Attitude and Heading Standby Data
MI-34-23
ALL 27 FEB 15
Integrated Standby Instrument System (ISIS)
MI-34-40
ALL 27 FEB 15
GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar
MI-35-01-01
ALL 27 FEB 15
OXYGEN Overhead Panel
MI-35-30
ALL 27 FEB 15
Portable Oxygen
MI-36-00
ALL 27 FEB 15
MAINTENANCE Message on the STATUS SD Page
MI-36-11
ALL 27 FEB 15
Engine Bleed Air Supply System
MI-36-12
ALL 27 FEB 15
APU Bleed Air Supply and Crossbleed Systems
Continued on the following page

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MINIMUM EQUIPMENT LIST

Continued from the previous page

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Subsection Title Rev. Date
MI-36-22
ALL 27 FEB 15
Leak Detection Loop
MI-47-00
ALL 27 FEB 15
MAINTENANCE Message on the STATUS SD Page
MI-47-10
ALL 27 FEB 15
Generation/Storage
MI-49-10
ALL 27 FEB 15
Power Plant
MI-52-33
ALL 27 FEB 15
Bulk Cargo Compartment Door
MI-52-51
ALL 27 FEB 15
Reinforced Cockpit Door (CDLS)
MI-56-10
ALL 27 FEB 15
Cockpit
MI-70-00
ALL 27 FEB 15
MAINTENANCE Messages on the STATUS SD page
MI-73-07
ALL 27 FEB 15
Indications on the ENGINE SD page
MI-73-08
ALL 27 FEB 15
Indications on the EWD
MI-73-09
ALL 27 FEB 15
ECAM Alert
MI-73-10
ALL 27 FEB 15
Distribution
MI-74-07
ALL 27 FEB 15
Indications on the ENGINE SD page
MI-74-09
ALL 27 FEB 15
ECAM Alert
MI-74-31
ALL 27 FEB 15
Ignition Starting and Continuous Relight
MI-77-07-02
ALL 27 FEB 15
Indications on the ENGINE SD page
MI-78-08
ALL 27 FEB 15
Indications on the EWD
MI-78-30
ALL 27 FEB 15
Thrust Reversers
MI-79-07
ALL 27 FEB 15
Indications on the ENGINE SD page
MI-79-09
ALL 27 FEB 15
ECAM Alerts
Continued on the following page

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LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

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Subsection Title Rev. Date
MI-79-20
ALL 27 FEB 15
Distribution
MI-79-40
ALL 27 FEB 15
IDG Oil Cooling System
MI-80-11
ALL 27 FEB 15
Pneumatic Starter and Valve System
MO-PLP-TOC
ALL 27 FEB 15
TABLE OF CONTENTS
MO-PLP-SOH
ALL 27 FEB 15
SUMMARY OF HIGHLIGHTS
MO-21-23
ALL 27 FEB 15
Lavatory And Galley Ventilation
MO-21-28
ALL 27 FEB 15
Cargo Compartment Ventilation
MO-21-31
ALL 27 FEB 15
Pressure Control and Monitoring
MO-21-51
ALL 27 FEB 15
Flow Control and Indicating
MO-21-63
ALL 27 FEB 15
Cockpit and Cabin Temperature Control
MO-22-60
ALL 27 FEB 15
Flight Augmentation (FAC)
MO-22-70
ALL 27 FEB 15
Flight Management System (FMS)
MO-23-74
ALL 27 FEB 15
Cabin Crew Panel
MO-24-22
ALL 27 FEB 15
AC Main Generation
MO-24-26
ALL 27 FEB 15
Galley and Commercial Supply System
MO-26-12
ALL 27 FEB 15
Engine Fire and Overheat Detection
MO-26-13
ALL 27 FEB 15
APU Fire and Overheat Detection
MO-27-64
ALL 27 FEB 15
Spoiler Hydraulic Actuation
MO-29-09
ALL 27 FEB 15
ECAM Alerts
MO-30-31
ALL 27 FEB 15
Probe Ice Protection
Continued on the following page

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LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

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Subsection Title Rev. Date
MO-30-81
ALL 27 FEB 15
Ice Detection
MO-31-07
ALL 27 FEB 15
Indications on the System Display (SD)
MO-31-62
ALL 27 FEB 15
Display Management Computer (DMC)
MO-32-09
ALL 27 FEB 15
ECAM Alerts
MO-32-32
ALL 27 FEB 15
Proximity Detector System
MO-32-42
ALL 27 FEB 15
Normal Braking
MO-32-51
ALL 27 FEB 15
Steering
MO-34-01-01
ALL 27 FEB 15
ADIRS Overhead Panel
MO-34-10
ALL 27 FEB 15
Air Data/Inertial Reference System (ADIRS)
MO-34-23
ALL 27 FEB 15
Integrated Standby Instrument System (ISIS)
MO-34-40
ALL 27 FEB 15
GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar
MO-35-01-01
ALL 27 FEB 15
OXYGEN Overhead Panel
MO-35-20
ALL 27 FEB 15
Passenger Oxygen
MO-36-11
ALL 27 FEB 15
Engine Bleed Air Supply System
MO-36-12
ALL 27 FEB 15
APU Bleed Air Supply and Crossbleed Systems
MO-36-22
ALL 27 FEB 15
Leak Detection Loop
MO-49-10
ALL 27 FEB 15
Power Plant
MO-73-20
ALL 27 FEB 15
Controlling
MO-74-07
ALL 27 FEB 15
Indications on the ENGINE SD page
MO-74-31
ALL 27 FEB 15
Ignition Starting and Continuous Relight
Continued on the following page

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LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

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Subsection Title Rev. Date
MO-78-30
ALL 27 FEB 15
Thrust Reversers
MO-79-09
ALL 27 FEB 15
ECAM Alerts

LAN COLOMBIA FLEET FI P 8/8

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PRELIMINARY PAGES
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 PRELIMINARY PAGES
TABLE OF CONTENTS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

HOW How to Use

ME MEL Entries

MI MEL Items

MO MEL Operational Procedures

NEF NEF Non-Essential Equipment & Furnishings

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LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS
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MINIMUM EQUIPMENT LIST

M Localization DU Title DU identification DU date

No Temporary Documentary Unit

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AIRCRAFT ALLOCATION TABLE
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

This table gives, for each delivered aircraft, the cross reference between:
- The Manufacturing Serial Number (MSN).
- The Fleet Serial Number (FSN) of the aircraft as known by AIRBUS S.A.S.
- The registration number of the aircraft as known by AIRBUS S.A.S.
- The aircraft model.
(1)
M MSN FSN Registration Number Model
4516 CC-BAF 320-232
4546 CC-BAG 320-232
4758 CC-BAN 320-214
4767 CC-BAO 320-214
4892 CC-BAR 320-214
4896 CC-BAS 320-214
4921 CC-BAT 320-214
4943 CC-BAU 320-214
4972 CC-BAV 320-214
5178 CC-BAX 320-214
5229 CC-BAZ 320-214
5234 CC-BFA 320-214
5263 CC-BFB 320-214
5316 CC-BFC 320-214
5324 CC-BFD 320-214
5364 CC-BFE 320-214
5443 CC-BFG 320-214
5453 CC-BFH 320-214
(1) Evolution code : N=New, R=Revised

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MINIMUM EQUIPMENT LIST

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LIST OF MODIFICATIONS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

(1)
M MODIFICATION Linked SB Incorp. Date Title
P10383 29 MAR 10 INDICATING/RECORDING SYSTEMS - FLIGHT
WARNING COMPUTER (FWC) - INSTALL FWC
STANDARD H2-F5
Applicable to: ALL
K10494 29 MAR 10 AIRBORNE AUXILIARY POWER - GENERAL - INSTALL
APIC APS3200 APU AS STANDARD (REPLACES
HONEYWELL GTCP36-300)
Applicable to: ALL
J1735 29 MAR 10 LANDING GEAR-POSITION AND WARNING-
INTRODUCE LGCIU STD -4D
Applicable to: ALL
P9594 29 MAR 10 PNEUMATIC - LEAK DETECTION - ACTIVATE PYLON
LEAK DETECTION MONITORING
Applicable to: ALL
J2879 07 JUN 11 INERT GAS SYSTEM - CERTIFY FUEL TANK
INERTING SYSTEM AND ACTIVATE MONITORING
Applicable to: MSN 5178-5453
K1806 29 MAR 10 ELECTRICAL POWER-AC/DC ESSENTIAL POWER
DISTRIBUTION-PROVIDE PROVISIONS FOR ETOPS-
Applicable to: ALL
P11146 19 JUL 11 LANDING GEAR - PARKING/ULTIMATE EMERGENCY
BRAKING ACTIVATE PARKING BRAKE MONITORING
FUNCTION ON SA A/C
Applicable to: ALL
P11632 19 JUL 11 INDICATING/RECORDING SYSTEM - SDAC -
ACTIVATETRAN SPONDER MONITORING BY PIN
PROGRAMMING
Applicable to: MSN 4516-4758, 4892-5263
P3379 29 MAR 10 INDICATING/RECORDING SYSTEMS - GENERAL-
DEFINE CPIP3
Applicable to: ALL
J0071 29 MAR 10 WINGS-WING TIP FENCES-INTRODUCE WING TIPS
INCLUDING FENCES-
Applicable to: ALL
P9873 11 JAN 11 POWER PLANT - GENERAL - INTRODUCE
CFM56-5BX/3 ENGINE (SAC) "TECH INSERTION
PROGRAM"
Applicable to: MSN 4758-5453
K0052 29 MAR 10 INDICATING/RECORDING SYSTEMS - INSTALL AN
AIRCRAFT INTEGRATED DATA SYSTEM -
Applicable to: ALL
Continued on the following page

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LIST OF MODIFICATIONS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

(1)
M MODIFICATION Linked SB Incorp. Date Title
J2963 29 MAR 10 WINGS - MAIN STRUCTURE - REDUCE THE
QUANTITY OF MAGNETIC LEVEL INDICATORS
Applicable to: ALL
P7754 29 MAR 10 NAVIGATION - DDRMI - REPLACE THALES DDRMI
P/N 63543-150-3 BY P/N 63543-150-4.
Applicable to: ALL
P10098 24-1120 03 29 MAR 10 ELECTRICAL POWER - AC ESSENTIAL GENERATION
SWITCHING - INSTALL AUTO SWITCHING SYSTEM
FOR AC AND DC ESS BUS
Applicable to: ALL
K7755 25-1305 06 29 MAR 10 EQUIPMENT FURNISHINGS-CURTAINS AND
PARTITIONS-MODIFIED INTRUSION AND
PENETRATION RESISTANT COCKPIT DOOR
Applicable to: ALL
K0024 29 MAR 10 DOORS- BULK CARGO COMPARTMENT- INSTALL AN
ADDITIONAL DOOR AT FR 60/62-
Applicable to: ALL
P10777 29 MAR 10 AUTO FLIGHT - FAC (FLIGHT AUGMENTATION
COMPUTER) - INTRODUCE FAC SOFTWARE
STANDARD "BAM0620"
Applicable to: MSN 4516-4758, 4892-5364
P2798 29 MAR 10 NAVIGATION - VOR/MARKER - MODIFY VOR
ANTENNA FAIRING
Applicable to: ALL
K0036 29 MAR 10 FIRE PROTECTION - AFT CARGO COMPARTMENT -
INSTALL SMOKE DETECTION SYSTEM -
Applicable to: ALL
K0037 29 MAR 10 FIRE PROTECTION - CARGO COMPARTMENT FIRE
EXTINGUISHING - INSTALL A SINGLE SHOT SYSTEM
-
Applicable to: ALL
K0035 29 MAR 10 FIRE PROTECTION - FWD CARGO COMPARTMENT -
INSTALL SMOKE DETECTION SYSTEM -
Applicable to: ALL
P9196 06 MAY 14 NAVIGATION - STANDBY DATA: INTEGRATED
STANDBY INSTRUMENT SYSTEM (ISIS) - INSTALL
ISIS STD WB01
Applicable to: ALL
P7125 29 MAR 10 INDICATING RECORDING SYSTEM-FWC-
INTRODUCE FWC STANDARD H2 F1
Applicable to: ALL
Continued on the following page

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LIST OF MODIFICATIONS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

(1)
M MODIFICATION Linked SB Incorp. Date Title
P1362 29 MAR 10 EQUIPMENT/FURNISHINGS - COCKPIT - ADD A
FIFTH STRAP ON 4TH OCCUPANT SEAT SHOULDER
HARNESS -
Applicable to: ALL
P4287 29 MAR 10 INDICATING/RECORDING SYSTEMS - FWC -
DEFINE OEB REMINDER WITHIN FWC STD -E1 AND
SUBSEQUENT
Applicable to: ALL
P8671 29 MAR 10 INDICATING/RECORDING SYSTEMS-ELECTRONIC
INSTRUMENT SYSTEM(EIS)- INSTALL DISPLAY
MANAGEMENT COMPUTER SOFTWARE EIS2 S4-2
Applicable to: ALL
K3680 29 MAR 10 APU - STORAGE AND DISTRIBUTION - MODIFY APU
COMMON LUBRICATION SYSTEM
Applicable to: ALL
K3737 29 MAR 10 AIR CONDITIONING - AIR COOLING SYSTEM -
INTRODUCE MODIFIED RAM AIR INLET
Applicable to: ALL
K3681 29 MAR 10 APU - CONTROL AND MONITORING - MODIFY ECB
FORCOMMON LUBRICATION SYSTEM APU/GEN
Applicable to: ALL
P5638 29 MAR 10 NAVIGATION-STANDBY DATA : ALTITUDE AND
HEADING - INSTALL INTEGRATED STANDBY
INSTRUMENT SYSTEM (ISIS)
Applicable to: ALL
K2770 29 MAR 10 AIRBORNE AUXILIARY POWER - CONTROL AND
MONITORING - INTRODUCE ECB P/N 304640-3
Applicable to: ALL
P3524 29 MAR 10 ELECTRICAL POWER - AC AUXILIARY GENERATION
(APU GENERATOR) - INTRODUCE MODIFIED
GENERATOR
Applicable to: ALL
K0402 29 MAR 10 ICE AND RAIN PROTECTION - DRAIN MAST
ICE PROTECTION - INSTALL TEMPERATURE
REGULATED HEATING SYSTEM
Applicable to: ALL
P7005 29 MAR 10 LANDING GEAR - NORMAL BRAKING - INTRODUCE
STD 9 BSCU (TWIN VERSION)
Applicable to: ALL
Continued on the following page

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COLOMBIA
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MINIMUM EQUIPMENT LIST

Continued from the previous page

(1)
M MODIFICATION Linked SB Incorp. Date Title
P10801 02 JUL 13 AUTO-FLIGHT-FLIGHT MANAGEMENT AND
GUIDANCE COMPUTER (FMGC)-INSTALL FMGC
HONEYWELL H2C13 ON CFM A/C
Applicable to: MSN 4758-5453
K3682 29 MAR 10 AIRBORNE AUXILIARY POWER - MODIFY WIRING
FOR COMMON LUBRICATION SYSTEM APU/GEN
Applicable to: ALL
P9126 22-1203 01 29 MAR 10 AUTOFLIGHT - FMGC - INSTALL FMGC IAE/PW STD
P1I10 (WITH FMS2 HONEYWELL) ON A/C FITTED
WITH IAE OR PW POWERPLANTS
Applicable to: MSN 4516-4546
P3924 29 MAR 10 LANDING GEAR - MLG - MESSIER - INTRODUCE
BRAKES P/N C202253
Applicable to: ALL
J0376 29 MAR 10 LANDING GEAR - MLG - MINOR IMPROVEMENTS
INTRODUCED FROM A/C 44 -
Applicable to: ALL
P6146 29 MAR 10 INDICATING/RECORDING SYSTEM - FWC -
INTRODUCE "F/CTL FLAP LVR NOT ZERO" RED
WARNING
Applicable to: MSN 4516-5263
K8400 29 MAR 10 COMMUNICATIONS-CIDS-INTRODUCE ENHANCED
CIDS (A318 VERSION) AND RELATED SYSTEMS ON
SINGLE AISLE FAMILY
Applicable to: ALL
P11807 13 AUG 14 INDICATING/RECORDING SYSTEM - ELECTRONIC
INSTRUMENT SYSTEM (EIS) - INSTALL NEW EIS2
SOFTWARE S9
Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453
P8799 34-1352 01 29 MAR 10 NAVIGATION- GPWS - USE LATERAL GPS POSITION
WITH AUTOMATIC DESELECTION
Applicable to: ALL
P5121 19 JUL 12 INDICATING/RECORDING SYSTEMS - DATA
LOADING SYSTEMS -INSTALL A MULTIPURPOSE
DISC DRIVE UNIT IN A COCKPIT
Applicable to: MSN 4516-4972
P5518 32-1232 01 29 MAR 10 LANDING GEAR-NORMAL BRAKING- INTRODUCE
32-1336 01 STD 8 BSCU (TWIN VERSION)
Applicable to: ALL
K6461 29 MAR 10 LIGHTS-EMERGENCY LIGHTING-INTRODUCE LED
EXIT SIGNS
Applicable to: ALL
Continued on the following page

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(1)
M MODIFICATION Linked SB Incorp. Date Title
J1617 29 MAR 10 FLIGHT CONTROLS-GENERAL- DELETION OF L.A.F.
FEATURE FROM A320 A/C (SERIAL SOLUTION)
Applicable to: ALL
K4913 29 MAR 10 HYDRAULIC POWER - AUXILIARY HYDRAULIC
POWER - INSTALL A319 RAM AIR TURBINE ON A320
Applicable to: ALL
P12367 11 APR 12 ENGINE FUEL AND CONTROL- FADEC SYSTEM-
INSTALL ECU SOFTWARE STANDARD 5BS ON
CFM56-5B ENGINES
Applicable to: MSN 5178-5453
P9522 29 MAR 10 AUTO-FLIGHT-MULTIPURPOSE CONTROL AND
DISPLAY UNIT(MCDU) - ACTIVATE BACK-UP NAV
FUNCTION
Applicable to: ALL
P12877 06 MAY 14 ENGINE FUEL AND CONTROL- FADEC SYSTEM-
INTRODUCE NEW ECU SOFTWARE 5BS2 ON
CFM56-5B ENGINES
Applicable to: MSN 5178-5453
P4885 29 MAR 10 NAVIGATION - GPWS - ACTIVATE ENHANCED
FUNCTIONS OF THE EGPWS
Applicable to: ALL
P5253 29 MAR 10 NAVIGATION - ADIRS - REPLACE ADIRS CDU BY
MSU (MODE SELECTOR UNIT)
Applicable to: ALL
P10443 19 JUL 11 FLIGHT CONTROL - ELAC SYSTEM - INTRODUCE
ELAC "L93" SOFTWARE STANDARD
Applicable to: MSN 4516-4758, 4892-5364
P10402 17 NOV 10 COMMUNICATIONS - AUDIO MANAGEMENT -
MODIFY AMU POWER SUPPLY TO COPE WITH DC
ESSENTIAL BUS LOSS
Applicable to: ALL
J0739 29 MAR 10 LANDING GEAR-MLG-INTRODUCE TORQUE LINK
APEX DAMPER
Applicable to: ALL
P11819 02 OCT 12 INDICATING/RECORDING SYSTEMS - FLIGHT
WARNING COMPUTER (FWC) - INSTALL FWC
STANDARD H2-F6
Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453
K6443 29 MAR 10 AIR CONDITIONING-AIR COOLING- INSTALL A NEW
ECS
Applicable to: ALL
Continued on the following page

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(1)
M MODIFICATION Linked SB Incorp. Date Title
P1631 29 MAR 10 NAVIGATION - MODIFY GPWC WARNING -
Applicable to: ALL
K1522 11 JAN 11 COMMUNICATIONS - INSTALL PA IN USE
INDICATORS LIGHT
Applicable to: MSN 4758-5453
P9655 29 MAR 10 LANDING GEAR - NORMAL BRAKING - INSTALL
BSCU SOFTWARE STD "L4.9"
Applicable to: ALL
K3901 29 MAR 10 COMMUNICATIONS-CIDS-INTRODUCE MODIFIED
DIRECTOR POWER SUPPLY PRINCIPLE
Applicable to: ALL
P5451 29 MAR 10 ELECTRICAL POWER - GENERAL - AC-DC MAIN
DISTRIBUTION - INSTALL AC-DC SHEDDABLE
BUSBARS
Applicable to: ALL
P6125 34-1249 02 29 MAR 10 NAVIGATION-ADIRU-INSTALL HONEYWELL ADIR U 4
MCU AD11 (NEW HARD)
Applicable to: ALL
P7268 34-1252 00 29 MAR 10 NAVIGATION-ADIRU-RESTORE RVSM 3 CIRCUIT
CAPABILITIES (SERIAL SOLUTION)
Applicable to: ALL
P2650 29 MAR 10 ICE AND RAIN PROTECTION - ICE DETECTION -
INSTALL DUAL ADVISORY ICE DETECTION SYSTEM
Applicable to: ALL
P10439 11 JAN 11 AUTO-FLIGHT - FMGC - INSTALL FMGC HNWL STD
P1C12 ON CFM A/C
Applicable to: MSN 4758-5453
J3240 18 DEC 12 FUEL - QUANTITY INDICATING - ACTIVATE FUEL
LEAK DETECTION WARNING SYSTEM
Applicable to: MSN 5364-5453
P4801 29 MAR 10 ELECTRICAL POWER-GENERAL-DEFINE NEW
ELECTRICAL GENERATION CONCEPT FOR SINGLE
AISLE A/C
Applicable to: ALL
P3957 11 JAN 11 HYDRAULIC POWER-GENERAL-INTRODUCE AN
HYDRAULIC SHUT-OFF VALVE ON THE CFM T/R
SYSTEM
Applicable to: MSN 4758-5453
P7175 29 MAR 10 ELECTRICAL POWER - GENERAL - INSTALL A
COMMERCIAL SHEDDING PUSH-BUTTON SWITCH IN
COCKPIT
Applicable to: ALL
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(1)
M MODIFICATION Linked SB Incorp. Date Title
P3956 29 MAR 10 HYDRAULIC POWER-GENERAL-INTRODUCE AN
HYDRAULIC SHUT-OFF VALVE ON THE IAE T/R
SYSTEM
Applicable to: MSN 4516-4546
P4808 29 MAR 10 LANDING GEAR-WHEELS AND BRAKES- INTRODUCE
BSCU COMMON STD
Applicable to: ALL
J2765 19 JUL 12 WING - MAIN STRUCTURE - TOP SKIN PANEL NO. 2 -
REMOVE MANUAL REFUEL APERTURE
Applicable to: ALL
K4574 17 NOV 10 AIR CONDITIONING-FLOW CONTROL AND
INDICATING INTRODUCE MODIFIED AIR
CONDITIONING FLOW CONTROL
Applicable to: ALL
P6538 29 MAR 10 INDICATING/RECORDING SYSTEMS-FWC TO
COMPLY WITH EM2 BSCS WARNING/ECAM
INDICATIONS
Applicable to: ALL
P13023 18 DEC 12 INDICATING RECORDING SYSTEMS-FWC-
INTRODUCE FWC STANDARD H2-F7
Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453
K9473 29 MAR 10 AIR CONDITIONING - PRESSURE CONTROL AND
MONITORING - INSTALL RPCU AND WIRING
PROVISIONS FOR RPWS
Applicable to: ALL
P10300 17 NOV 10 ELECTRICAL POWER - AC MAIN GENERATION -
INSTALL EEPGS GCU SOFTWARE STANDARD "5.2"
Applicable to: ALL
P4151 29 MAR 10 INDICATING/RECORDING SYSTEM - INSTALL A
PORTABLE DATA LOADER CONNECTOR AND DISK
STOWAGE
Applicable to: ALL
P1063 29 MAR 10 AUTO FLIGHT - IMPROVE SEGREGATION OF AUTO
PILOT DISCONNECT CIRCUIT -
Applicable to: ALL
K2450 49-1029 27 29 MAR 10 AIRBORNE AUXILIARY POWER UNIT - INTRODUCE
APIC APS-3200
Applicable to: ALL
P6319 17 NOV 10 COMMUNICATIONS - AUDIO MANAGEMENT -
INSTALL TEAM DIGITAL AMU P/N 4031-SA-01
Applicable to: ALL
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(1)
M MODIFICATION Linked SB Incorp. Date Title
P10653 07 NOV 13 INDICATING/RECORDING SYSTEMS - FLIGHT
WARNING COMPUTER (FWC) - INSTALL FWC
STANDARD H2-F3P
Applicable to: ALL
P4149 29 MAR 10 ENGINE FUEL AND CONTROL-CONTROLLING-
INTRODUCE E.E.C. SOFTWARE SCN 10A ON IAE
V2500-A5
Applicable to: MSN 4516-4546
P0661 29 MAR 10 EQUIPMENT/FURNISHINGS-COCKPIT-ADD A FIFTH
STRAP ON 3RD OCCUPANT SHOULDER HARNESS-
Applicable to: ALL
P8341 11 JAN 11 NACELLES / PYLONS - PYLONS - IMPROVE
AERODYNAMIC SHAPE OF CFM PYLON
Applicable to: MSN 4758-5453
P6801 31-1231 01 29 MAR 10 INDICATING/RECORDING SYSTEMS - FWC - INSTALL
FWC STANDARD H2E4
Applicable to: ALL
J3283 18 DEC 12 WINGS-GENERAL-CERTIFY SHARKLET
INSTALLATION FOR A320/A319/A318
Applicable to: MSN 5453
P2316 29 MAR 10 AUTO FLIGHT - ACTIVATE WINDSHEAR FUNCTION
Applicable to: ALL
P12126 13 AUG 14 AUTO FLIGHT - FLIGHT AUGMENTATION COMPUTER
(FAC) - INSTALL FAC 622 (SHARKLET PROJECT)
Applicable to: MSN 5443-5453
J0012 29 MAR 10 LIGHTS - NAVIGATION LIGHTS - INSTALL A SECOND
NAVIGATION LIGHT SYSTEM -
Applicable to: ALL
P0197 29 MAR 10 COMMUNICATIONS - HF SYSTEM - INSTALL A
SINGLE SYSTEM
Applicable to: ALL
P5429 11 JAN 11 ENGINE FUEL AND CONTROL-FADEC SYSTEM-
CFM56-5B-SAC-INTRODUCE ECU SOFTWARE 5BI
Applicable to: MSN 4758-5453
K8905 29 MAR 10 EQUIPMENT/FURNISHINGS-CURTAINS AND
PARTITIONS-INSTALL DEADBOLT ON CENTER
LATCH OF REINFORCED COCKPIT DOOR
Applicable to: ALL
P7945 17 NOV 10 ELECTRICAL POWER - AC MAIN GENERATION-
INSTALL NEW GCU SOFTWARE STD 5.1 ON SA A/C
EQUIPPED WITH ENHANCED EPGS
Applicable to: ALL
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(1)
M MODIFICATION Linked SB Incorp. Date Title
22-1359 00 07 JUN 12 AUTO-FLIGHT-FLIGHT MANAGEMENT AND
GUIDANCE COMPUTER (FMGC)-INSTALL FMGC
HONEYWELL H2C13 ON CFM A/C
Applicable to: MSN 4758, 4892-4972
P4576 29 MAR 10 LANDING GEAR-ALTERNATE BRAKING- INTRODUCE
MODIFIED ALTERNATE BRAKING SYSTEM
Applicable to: ALL
K9995 29 MAR 10 AIR CONDITIONING - PRESSURE CONTROL AND
MONITORING - REMOVE RESIDUAL PRESSURE
CONTROL UNTI (RPCU) (ANTI MOD TO 34673)
Applicable to: MSN 4516-4546
J0006 29 MAR 10 FUEL- INSTALL A CENTRE TANK SYSTEM-
Applicable to: ALL
P4170 29 MAR 10 FLIGHT CONTROLS - FCDC SYSTEM - PROVIDE
A VISUAL INDICATION FOR SIMULTANEOUS SIDE
STICK ACTION
Applicable to: ALL
P6954 29 MAR 10 AUTO-FLIGHT - FLIGHT AUGMENTATION COMPUTER
(FAC) - INTRODUCE FAC SOFTWARE "BAM0616"
Applicable to: ALL
P8257 27-1149 02 29 MAR 10 FLIGHT CONTROLS - SEC SYSTEM - INSTALL
SPOILER AND ELEVATOR COMPUTER SOFTWARE
FOR A318 EIS (BAM0511)
Applicable to: ALL
P4023 29 MAR 10 GENERAL - SYSTEM PROVISION FOR HIGH
ALTITUDE OPERATION UP TO 14100 FT
Applicable to: ALL
P9107 31-1267 03 29 MAR 10 INDICATING/RECORDING SYSTEMS - FLIGHT
31-1300 02 WARNING COMPUTER (FWC) - INSTALL FWC
STANDARD H2F3
Applicable to: ALL
P4977 29 MAR 10 INDICATING/RECORDING SYSTEMS - FWC -
PROVIDE NEW SYNTHETIC VOICE "DUAL INPUT"
Applicable to: ALL
P8757 07 JUN 12 ENGINE FUEL AND CONTROL - GENERAL
INTRODUCE HMU P13 ON CFM56-5A/5B ENGINES
Applicable to: MSN 4758-5453
K1498 29 MAR 10 HYDRAULIC POWER-BLUE SYTEM ACCUMULATOR-
RELOCATE CONNECTOR
Applicable to: ALL
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M MODIFICATION Linked SB Incorp. Date Title
P9824 31-1276 01 29 MAR 10 INDICATING/RECORDING SYSTEMS-ELECTRONIC
INSTRUMENT SYSTEM(EIS)-INSTALL DISPLAY
MANAGEMENT COMPUTER SOFTWARE EIS2 S7
Applicable to: ALL
P2493 29 MAR 10 EQUIPMENT/FURNISHINGS - COCKPIT SEATS -
INTRODUCE TYPE A340 SEATS
Applicable to: ALL
P11620 24 JAN 12 INDICATING/RECORDING SYSTEMS - FWC -
ACQUISITION/INTERFACE ACTIVATE MONITORING
OF ATC/XPDR
Applicable to: ALL
P0033 06 MAY 14 COMMUNICATIONS - HF SYSTEM - INSTALL SYSTEM
PROVISION FOR A SINGLE SYSTEM -
Applicable to: ALL
P4502 29 MAR 10 INFORMATION SYSTEM - AIR TRAFFIC AND
INFORMATION SYSTEM (ATIMS) - INSTALL ATSU
COMPUTER FOR ACARS
Applicable to: ALL
P8863 11 APR 12 INDICATING/RECORDING SYSTEM FWC
ACQUISITION INTERFACE CONNECT FWC TO RPWS
TO PREVENT DOOR OPENING WITH RESIDUAL
CABIN PRESSURE
Applicable to: ALL
J2361 18 DEC 12 FUEL-QUANTITY INDICATION-REMOVE FUEL LEAK
DETECTION FUNCTION ASSOCIATED WITH FQIC
13-9 (ANTI-MOD FOR MOD 32650)
Applicable to: MSN 5364-5453
J2360 29 MAR 10 FUEL - QUANTITY INDICATION - INTRODUCE FUEL
LEAK DETECTION
Applicable to: MSN 5364-5453
K2962 29 MAR 10 HYDRAULIC POWER-BLUE MAIN HYDRAULIC
POWER-IMPROVE MAINTENANCE STATUS OF BLUE
HYDRAULIC RESERVOIR
Applicable to: ALL
P6578 29 MAR 10 INDICATING RECORDING SYSTEMS- EIS-INSTALL
DMC, DU AND DISKETTES FOR EIS2
Applicable to: ALL
P10891 32-1350 00 29 MAR 10 LANDING GEAR - NORMAL BRAKING - INSTALL
BSCU SOFTWARE STD "L4.9 B" (EM2)
Applicable to: ALL
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(1)
M MODIFICATION Linked SB Incorp. Date Title
P7092 19 JUL 11 INDICATING/RECORDING SYSTEM - EIS - ACTIVATE
FUEL FLOW/DELTA ISA FUNCTION BY PIN
PROGRAMMING ON DMC
Applicable to: ALL
P11484 19 JUL 11 FLIGHT CONTROLS - FCDC SYSTEM - INTRODUCE
FCDC STANDARD 58
Applicable to: MSN 4546-4758, 4892-5364
P8340 29 MAR 10 NACELLES / PYLONS - PYLONS - IMPROVE
AERODYNAMIC SHAPE OF IAE PYLON
Applicable to: MSN 4516-4546
J2832 28-1159 00 29 MAR 10 FUEL - MAIN FUEL PUMP SYSTEM - INSPECT AND
ADMINISTER CORRECT TORQUE AND SCREW
LOCKING ON FIXING BOLTS
Applicable to: ALL
P0159 29 MAR 10 EQUIPMENT/FURNISHINGS - ADD A FIFTH STRAP TO
FLIGHT CREW SHOULDER HARNESS -
Applicable to: ALL
K4160 29 MAR 10 DOORS-CARGO COMPARTMENT FWD/AFT-
INTRODUCE MODIFIED ACTUATOR FITTING AND
ATTACHMENT
Applicable to: ALL
P8303 29 MAR 10 NAVIGATION - DDRMI - REMOVE DDRMI
VOR/ADF/DME INDICATORS
Applicable to: ALL
K7790 29 MAR 10 DOORS-PASSENGER COMPARTMENT FIXED
INTERIOR DOORS-INSTALL ELECTRICAL COCKPIT
DOOR RELEASE SYSTEM
Applicable to: ALL
P10762 13 AUG 14 AUTO FLIGHT - FMGC - INSTALL FMGC HWL H2C12
(RELEASE 1A) ON CFM A/C
Applicable to: MSN 4758-4767, 4972-5178, 5234, 5443-5453
K5446 29 MAR 10 INDICATING/RECORDING SYSTEMS-CFDS-
INTRODUCE A COMBINED FDIU/DMU
Applicable to: MSN 4516-4758, 4892-5453
P10763 13 AUG 14 AUTO FLIGHT - FMGC - INSTALL FMGC HWL H2I11
(RELEASE 1A) ON IAE AND PW A/C
Applicable to: MSN 4516-4546
K0070 21-1047 05 29 MAR 10 AIR CONDITIONING - CARGO COMPARTMENT
- VENTILATION - INSTALL SYSTEM IN AFT
COMPARTMENT -
Applicable to: ALL
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(1)
M MODIFICATION Linked SB Incorp. Date Title
P0053 29 MAR 10 EQUIPMENT/FURNISHINGS - FLIGHT
COMPARTMENT - INSTALL SLIDING TABLES AT
PILOT'S STATION -
Applicable to: ALL
P5794 19 JUL 12 INDICATING RECORDING SYS-DATA LOADING
-INTRODUCE A MULTIPURPOSE DISK DRIVE UNIT
P/N AC68A200 IN THE COCKPIT
Applicable to: MSN 4516-4972
K0064 29 MAR 10 LIGHTS - EXTERIOR LIGHTS - INSTALL
SYNCHRONIZED STROBE LIGHTS
Applicable to: ALL
P5706 31-1257 01 29 MAR 10 INDICATING RECORDING SYSTEM-FWC-
INTRODUCE FWC STANDARD H2/E3P
Applicable to: ALL
J1764 19 JUL 11 FUEL-QUANTITY INDICATING-INTRODUCE MODIFIED
PRE-SELECTOR UNITS P/N 0203
Applicable to: ALL
J1570 29 MAR 10 CROSS FEED VALVE P/N-2
Applicable to: ALL
P1970 29 MAR 10 COMMUNICATIONS - INSTALL HF1 FOR ETOPS
Applicable to: ALL
J0937 29 MAR 10 LANDING GEAR - MAIN LANDING GEAR (TWIN
WHEELS) - INTRODUCE A NEW STANDARD TORQUE
LINKS DAMPER AND ABEX PIN.
Applicable to: ALL
P4539 29 MAR 10 AUTOFLIGHT-FLIGHT CONTROL UNIT- (FCU)
INTRODUCE SEXTANT MODULAR FCU
Applicable to: ALL
P0040 29 MAR 10 EQUIPMENT/FURNISHINGS - FLIGHT
COMPARTMENT - INSTALL A 4TH OCCUPANT SEAT -
Applicable to: ALL
P0143 29 MAR 10 COMMUNICATIONS - RADIO MANAGEMENT -
INSTALL A 3RD RMP -
Applicable to: ALL
P3365 29 MAR 10 ICE AND RAIN PROTECTION-ICE DETECTION-
PROVIDE ICE DETECTOR ILLUMINATION
Applicable to: ALL
K2335 29 MAR 10 FIRE PROTECTION - LAVATORY SMOKE
DETECTION - INTRODUCE AMBIENT SYSTEM
Applicable to: ALL
(1) Evolution code : N=New, R=Revised, E=Effectivity

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Revision Manager.................................................................................................................................................... A
Foreword.................................................................................................................................................................. B
Questions and Suggestions.................................................................................................................................... C
MEL Contents.......................................................................................................................................................... D
How to get the MMEL updated?............................................................................................................................. E
Documentary Unit (DU)........................................................................................................................................... F
MEL Revision Management.................................................................................................................................... G
Optional Equipment (If Installed) .................................................................................................................. H
Removal of Item........................................................................................................................................................I
How to Use the MEL Entries Section? ...................................................................................................................J
How to Use the MMEL Items Section? ................................................................................................................. K
How to Use the MEL Operational Procedures Section?......................................................................................... L
Landing Capabilities ( CAT 2, CAT 3 SINGLE, CAT 3 DUAL) ............................................................................. M
Required Navigation Performance (RNP)............................................................................................................... N
Reduced Vertical Separation Minimum (RVSM).....................................................................................................O
Futur Air Navigation System (FANS)...................................................................................................................... P
Abbreviations........................................................................................................................................................... Q

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Localization Toc ID Reason

Title Index
HOW A 1 Update according to MMEL Rev. 02-12-2014
Revision Manager

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REVISION MANAGER
Ident.: HOW-20800653.9001001 / 27 FEB 15
Applicable to: ALL

This DU contains the name of the person in charge of MEL custumization as the name of the person
in charge of performing the final crosscheck in order to deliver the document to the Aeronautical
Authority for approval.
1
AIRBUS A320
DATE CUSTOMIZED CROSSCHECKED
MAY 18/11 A.MART E.LPEZ LIBARDI
JUL 29/11 A.MART E.LPEZ LIBARDI
SEP 12/11 A.MART E.LPEZ LIBARDI
NOV 02/11 A. MART E.LPEZ LIBARDI
AGO 01/11 N. PATINO J.C RODRIGUEZ
NOV 18/11 N. PATINO J.C RODRIGUEZ
ENE 13/12 N.PATINO J.C RODRIGUEZ
SEP 01/12 N.PATINO J.C RODRIGUEZ
FEB 01/13 N.PATINO J.C RODRIGUEZ
MAY 13/13 N.PATINO J.C RODRIGUEZ
NOV 05/13 N.PATINO J.C RODRIGUEZ
APR 02/14 L. DELGADO J. TORRES
JUN 20/14 L. FELIZZOLA L. DELGADO
JUL 18/14 L. FELIZZOLA L. DELGADO
OCT 10/14 C. SIMBAQUEBA L. FELIZZOLA
DIC 12/14 C. SIMBAQUEBA L. FELIZZOLA
FEB 27/15 C. SIMBAQUEBA L. FELIZZOLA

AIRBUS A319
DATE CUSTOMIZED CROSSCHECKED
MAY 25/11 A.MART E.LPEZ LIBARDI
SEP 12/11 A.MART E.LPEZ LIBARDI
DEC 12/11 A.MART E.LPEZ LIBARDI
FEB 24/12 A.MART E.LPEZ LIBARDI
MAY 31/12 A.MART E.LPEZ LIBARDI
AUG 17/12 A.MART E.LPEZ LIBARDI
NOV 27/12 A.MART E.LPEZ LIBARDI
FEB 14/13 A.MART E.LPEZ LIBARDI
APR 22/13 A.MART E.LPEZ LIBARDI

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AIRBUS A319/A320
DATE CUSTOMIZED CROSSCHECKED
AUG 01/13 A.MART E.LPEZ LIBARDI

FOREWORD
Ident.: HOW-00012802.0001001 / 12 SEP 11
Applicable to: ALL

This Master Minimum Equipment List ( MMEL ) is a reference manual published in English. It
is approved by the European Aviation Safety Agency ( EASA ). This MMEL must be used as a
reference by the Operator to develop its MEL .
This MMEL takes into account the specific configuration of each aircraft of the Operator's fleet. The
aircraft validity is managed at Documentary Unit (DU) level. Refer to HOW Documentary Unit (DU)
This MMEL is produced in XML format and can be published in PDF format and in electronic format
for electronic consultation on EFB .
Airbus also proposes a set of tools to create and publish the Operators MEL based on this MMEL .

QUESTIONS AND SUGGESTIONS

Ident.: HOW-00012803.0001001 / 18 JUL 14
Applicable to: ALL

For any questions or comments related to this manual, the Operators Flight Operations Management
may contact the Airbus Flight Operations & Training support department.

MEL CONTENTS
Ident.: HOW-00012804.0001001 / 10 OCT 14
Applicable to: ALL

This MEL has four sections:

How to Use (HOW) : This section contains general information and describes the organization
of the manual.
MEL Entries (ME) : This section lists all the ECAM alerts and indicates the associated
MEL item (if any) to apply for dispatching the aircraft. This section is a
user-friendly entry point for the flight crew and the maintenance personnel
when an ECAM alert reports a system failure.
MEL Items (MI) : This section is approved by the Aeronautical Authorities and lists all the
MEL items with the associated dispatch conditions.

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MEL Operational : This section gives the operational procedures that are associated with the
Procedures (MO) MEL items.
NEF(Non-Essential : This section list are all items installed on the aircraft as part of the original
Equipment & type certification, supplemental type certificate, or other form of alteration
Furnishings) that have no effect on the safe operation of flight and would not be
required by the applicable certification rules or operational rules.
Note: The MEL Maintenance Procedures are published in the AMM.

HOW TO GET THE MMEL UPDATED?

Ident.: HOW-00012805.0001001 / 17 SEP 10
Applicable to: ALL

Airbus provides the Operator with an MMEL which reflects the aircraft configuration at delivery, and
the necessary revisions to reflect configuration changes due to Airbus approved modifications.
The Operator must inform Airbus without delay of the effective changes to the aircraft delivery
configuration made through Airbus Service Bulletin (SB). This permits Airbus to provide the Operator
with the MMEL revisions/updates.
The Operator must timely report any SB embodiment to the following address:
E.MAIL : sb.reporting@airbus.com
Airbus will not provide revisions, and will not take responsibility for any effect on the MMEL:
Due to modifications installed by third parties without an Airbus SB, and/or
Due to modifications installed through an Airbus SB, if Airbus is not informed of the SB
embodiment.

DOCUMENTARY UNIT (DU)

Ident.: HOW-00012806.0001001 / 12 SEP 11
Applicable to: ALL

This MEL is made of Documentary Units (DU). The DUs contain the technical data.
In the MEL, a DU can be:
An ECAM alert,
An MEL item,
An MEL operational procedure.
The List of Effective Documentary Units (LEDU) lists all the DUs that constitute this MEL.
The DUs are arranged into sections and subsections (also called PSL). The List of Effective
Sections/Subsections (LESS) lists all the subsections that constitute this MEL. The subsections
contain the DUs.

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DU IDENTIFICATION STRIP
In the PDF format, below the title of the DU, the grey identification strip indicates for each DU:
The DU identification (Ident.). Each DU is identified by its unique identification number. This DU
identification is used to cross-refer to the LEDU.
The DU date. For approved DUs (MEL items DU), this date corresponds to the approval date by
the Aeronautical Authority of the MEL revision. For non-approved DUs, this date corresponds to
the date of release of the DU by Airbus.
The "Applicable to" field that lists the aircraft to which the DU applies.
Note: 0012-0220 means that the DU applies to all MSNs (listed in the AAT) from MSN 0012
up to and including MSN 0220.

In the electronic format, the same information is available by selecting the DOC REF option in
the INFO drop down list. The electronic format also displays the Criteria field that indicates the
aircraft configuration to which the DU applies.
LIST OF EFFECTIVE DOCUMENTARY UNITS (LEDU)
For each DU, the LEDU indicates the following information:
The M field that may indicate the following Evolution Code:
The E letter indicates an aircraft validity change of the DU. The list of aircraft to which the
DU applies has changed compared to the previous MEL revision, by addition or deletion of
one or several aircraft.
The N letter indicates a new DU added by this MEL revision.
The R letter indicates a revised DU. The content of the DU is updated by this MEL revision.
The "Localization" field that is the identification of the subsection that contains the DU. In the
PDF format, this cross-refers to the page footer, which permits the user to localize the DU within
the manual.
The DU title.
The DU identification (Ident.). Each DU is identified by its unique identification number. This DU
identification is used to cross-refer to the LEDU.
The DU date. For approved DUs (MEL items DU), this date corresponds to the approval date by
the Aeronautical Authority of the MEL revision. For non-approved DUs, this date corresponds to
the date of release of the DU by Airbus.
The criteria: This field indicates the aircraft configuration to which the DU applies.
The "Applicable to" field that lists the aircraft to which the DU applies.
Note: 0012-0220 means that the DU applies to all MSNs (listed in the AAT) from MSN 0012
up to and including MSN 0220.

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MEL REVISION MANAGEMENT

Ident.: HOW-00012807.0001001 / 12 SEP 11
Applicable to: ALL

MEL REVISION CYCLE

The MEL revision adds, updates, or deletes information. The Operator determines the revision
cycle. For urgent update, Airbus issues an immediate revision regardless of the revision cycle.
MEL ISSUE DATE
An issue date identifies each MEL revision.
The issue date appears:
In the Transmittal Letter for the PDF format, and
In the LIBRARY panel of the OPS LIBRARY Browser for the electronic consultation.
Note: The issue date is different from the Aeronautical Authority approval date. The
Aeronautical Authority approval date appears in the MEL Approval Reference of the MEL
Preamble. The applicability date of this MEL is based on the issue date and not on the
Aeronautical Authority approval date ( Refer to MI-00-01 Approval Reference ).
MEL REVISION CONTENTS
Each MEL revision contains the following information that is useful to update the MEL and to
identify the changes that the revision has inserted:
The Transmittal Letter (in PDF format only),
The List of Effective Sections/Subsections ( LESS ) (in PDF format only),
The Filling Instructions (in PDF format only),
The List of Effective Documentary Units ( LEDU ),
The Summary of Highlights ( SOH ).
Each MEL revision also contains:
An Aircraft Allocation Table ( AAT ),
A List of Modifications ( LOM ).
When there is a change within a DU, the MEL revision updates the whole subsection that contains
the DU.
TRANSMITTAL LETTER
The Transmittal Letter is a way of communication between Airbus and the Operators. The
Transmittal Letter also specifies the issue date of the MEL revision.
The Transmittal Letter only exists in the PDF format.

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PDF PAGE HEADER AND FOOTER

In the PDF format, the header of the page contains the subsection title whereas the footer
contains:
The subsection identification,
The subsection issue date. The subsection issue date corresponds to the issue date of the
latest MEL revision that has revised the subsection.
The page number within this subsection and the total number of pages within this subsection.
The Table of Contents ( TOC ) indexing.
This TOC indexing uses the TOC indexes. Each TOC entry has an alphabetical index that
identifies this TOC entry within its subsection. The manual user can easily find a TOC entry
content within the manual thanks to this alphabetical index and the subsection identification. Both
are indicated in the TOC and both cross-refer to the PDF page footer.
In the PDF page footer, the TOC indexing is of the following type:
B : The PDF page contains the whole "B" TOC entry content.
B to D : The PDF page contains the whole "B", "C" and "D" TOC entries contents.
B : The "B" TOC entry content starts on this PDF page and continues on the
following PDF page.
B : The "B" TOC entry content starts on a previous PDF page and finishes on this
PDF page.
B : The "B" TOC entry content starts on a previous PDF page and continues on the
following PDF page.
B to D : The PDF page contains the whole "B" and "C" TOC entries contents but the "D"
TOC entry content starts on this PDF page and continues on the following PDF
page.
B to D : The PDF page contains the whole "C" and "D" TOC entries contents but the
"B" TOC entry content starts on a previous PDF page and finishes on this PDF
page.
B to D : The PDF page contains the whole "C" TOC entry content but the "B" TOC entry
content starts on a previous PDF page and finishes on this PDF page and the
"D" TOC entry content starts on this PDF page and continues on the following
PDF page.
Note: 1. The indexes follow the alphabetical order: A, B, C, ..., Z, AA, AB, AC, ..., AZ, BA,
BB,BC, ...
2. For each subsection, the index starts again from A.
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS ( LESS )
The manual is organized by sections and subsections (also called PSL ). The subsections contain
the DUs.

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The LESS lists all the subsections that constitute this MEL . The LESS only exists in the PDF
format.
When there is a change within a DU, the MEL revision updates the whole subsection that contains
the DU. This subsection gets a new date that corresponds to the issue date of the MEL revision.
Note: Each subsection has its own date that corresponds to the issue date of the latest MEL
revision that has revised the subsection. Therefore subsections of a same manual might
have different dates.
For each subsection, the LESS indicates:
The subsection identification (also referred to as localization),
The subsection title,
The subsection issue date. The subsection issue date corresponds the issue date of the latest
MEL revision that has revised the subsection.
The "M" field that may indicate the following Evolution Code:
The E letter indicates only an aircraft validity change of one or several DUs of this
subsection compared to the previous MEL revision. No DU content of this subsection has
changed compared to the previous MEL revision.
The M letter indicates a subsection that has moved compared to the previous MEL revision.
The N letter indicates a new subsection added by this MEL revision.
The R letter indicates a revised subsection. The content of one or several DUs of this
subsection is updated by this MEL revision.
Each PDF page footer indicates the subsection identification and the subsection issue date for
cross-reference with the LESS . Therefore the manual holder can use the LESS to ensure that the
MEL is up-to-date and that no page is missing.
FILLING INSTRUCTIONS
The Filling Instructions enable the manual holder:
To update the paper MEL when a new MEL revision is available, and
To quickly identify the subsections that the new MEL revision has revised.
The Filling Instructions notify the manual holder to remove a subsection, to add a new subsection
or to update an existing subsection.
For each revised subsection, the Filling Instructions also indicate:
The subsection identification (also referred to as localization),
The subsection title,
The new issue date of the subsection.
After incorporating the new revision with the Filling Instructions, the manual organization must
correspond to the LESS .
The Filling Instructions only exist in the PDF format.

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Each PDF page footer indicates the subsection identification and the subsection issue date for
cross-reference with the Filling Instructions. Therefore the manual holder can use the Filling
Instructions to update the paper MEL and to identify the latest revised subsections.
HIGHLIGHTS AND REVISION MARKS
In the PDF format, a vertical bar in the margin of the DU identifies the modified part. Each vertical
bar has a numerical index that refers to the associated reason of the change in the Summary of
Highlights ( SOH ).
The SOH lists all the changes and associated reasons of the change (if necessary) that the
revision has inserted.
In electronic consultation, the vertical bar is available by selecting the REV MARKS option in the
INFO drop down list. The user can display the associated reason of the change by clicking on the
bar.
AIRCRAFT ALLOCATION TABLE ( AAT )
The AAT indicates the list of aircraft that are taken into account in this MEL . For each aircraft, the
AAT indicates the following information:
The MSN number,
The Fleet Serial Number ( FSN ) of the aircraft as known by Airbus,
The registration number of the aircraft as known by Airbus,
The aircraft model.
The M field may indicate the following Evolution Code:
The N letter indicates a new aircraft added by this MEL revision,
The R letter indicates a change of the FSN or registration number or aircraft model.
LIST OF MODIFICATIONS ( LOM )
The LOM lists the criteria (Modification Proposals ( MP ) and Service Bulletins ( SB )) which the
installation on the aircraft affects the MEL .
Note: Each MP has one or more associated MOD s. The MP / MOD correlation is available in
AirN@v / Engineering.
The LOM also indicates:
The title of the criteria,
The date of incorporation of the criteria in the MEL ,

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The list of aircraft that have the criteria,

The M field that may indicate the following Evolution Code:
The E letter indicates an aircraft validity change of the criteria. The list of aircraft to which
the criteria applies has changed compared to the previous MEL revision, by addition or
deletion of one or several aircraft.
The N letter indicates new criteria added by this MEL revision,
The R letter indicates a change in the criteria title or associated SB .

OPTIONAL EQUIPMENT (IF INSTALLED)

Ident.: HOW-00012808.0001001 / 17 SEP 10
Applicable to: ALL

The (If Installed) symbol indicates that a paragraph is applicable only if the aircraft has the
related equipment.
When a DU title has the (If Installed) symbol , this indicates that the DU might not apply to all the
aircraft listed in the DU validity.
The Operator is responsible for:
Managing the aircraft validity for the DU in the MEL and removing the (If Installed) symbol , or
Removing the DU from the MEL if the DU does not apply to the Operators fleet.

REMOVAL OF ITEM
Ident.: HOW-00012809.0001001 / 17 SEP 10
Applicable to: ALL

When operating under MEL , it is not permitted to remove the item from its place in the aircraft,
unless the associated dispatch condition clearly authorizes the Operator to do it.
Note: The (If Installed) symbol does not mean that the Operator can remove the item. This
symbol indicates that the configuration of some aircraft of the Operator's fleet might not
include this item. Refer to HOW Optional Equipment (If Installed) .

HOW TO USE THE MEL ENTRIES SECTION?

Ident.: HOW-00012810.0001001 / 12 SEP 11
Applicable to: ALL

This section lists all the ECAM alerts. The ECAM monitors the condition of some systems. In the
case of malfunction of one or more systems, the ECAM provides the flight crew with an associated
ECAM alert. Refer to MI-00-08 ECAM and MAINTENANCE STATUS .
For each ECAM alert, this section indicates the associated MEL item (if any) to be applied for the
dispatch.

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When an ECAM alert reports a system failure, the flight crew and the maintenance personnel should
refer to this section as a user-friendly entry point in the MEL .
AIRCRAFT STATUS COLUMN
An ECAM alert may cover one or several failure modes of the monitored system.
For each failure mode, the AIRCRAFT STATUS column may indicate the following status:
NIL : When there is only one failure mode, the AIRCRAFT STATUS column
indicates NIL .
When there are several failure modes, the AIRCRAFT STATUS column
might give a short description of each failure mode and/or a simple way
to identify each failure mode. If the MEL does not give this information,
the column displays NIL .
Actual alert : This indicates that the monitored system is inoperative. The failure mode
is the failure of the monitored system.
False alert : This indicates that the monitoring system is inoperative. The failure
mode is the failure of the monitoring system. The monitored system
remains fully operative.
The Operator is responsible for identifying the failure mode.
CONDITION OF DISPATCH COLUMN
For each failure mode, the CONDITION OF DISPATCH column gives the applicable MEL item(s)
for dispatch. But the flight crew is responsible for checking that the condition of the aircraft
systems/components complies with the MEL requirements. If not, the dispatch of the
aircraft is not permitted.
The CONDITION OF DISPATCH column may also give the following alternate possibilities:
NO DISPATCH : It is not permitted to dispatch the aircraft when the ECAM displays this
alert.
Not related to MEL : The ECAM alert does not report a system failure but a reversible
abnormal condition such as the state of a system or an aircraft
configuration or an external condition. This condition is not a system
failure and is not related to MEL . The MEL shall not be used.
This is not a NO-GO situation. The corrective action to revert to normal
condition is immediate, obvious or well known by flight crew and/or
maintenance personnel.

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HOW TO USE THE MMEL ITEMS SECTION?

Ident.: HOW-00012811.0001001 / 10 OCT 14
Applicable to: ALL

This section lists the equipment, components, systems or functions that are safety-related and that
are temporarily permitted to be inoperative at departure provided that the Operator complies with the
associated MMEL requirements.
Note: One single computer may include several functions. The corresponding MMEL item is
either:
The computer: The MMEL does not consider the loss of a single function. In this case,
when one function is inoperative, the Operator must consider that the computer is
inoperative.
Each function separately. In this case, if several functions are inoperative, the Operator
must apply all the related MMEL items.
ITEM NUMBERING
A code of three pairs of digits or four pairs of digits identifies each MMEL item.
The three first digits of this numbering system follow the ATA Spec 2200.
For practical reasons, the second pair of digits also follows the below Airbus organization:
00 refers to maintenance messages on the STATUS SD page ,
01 refers to items located on the overhead panels,
05 refers to indications on the PFD ,
06 refers to indications on the ND ,
07 refers to indications on the SD pages,
08 refers to indications on the EWD ,
09 refers to ECAM alerts,
10 to 95 follows the ATA Spec 2200 (first digit only).
The last pair of digits is the item rank. The item rank complies with the following Airbus
organization rules:
Item ranks from 01 to 49 are for Airbus MMEL items.
For items on the overhead panels:
Item ranks from 01 to 29 refer to lights,
Item ranks from 31 to 49 refer to pushbutton switches and selectors.
Item ranks from 50 to 99 are for Operator's MEL items.

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DISPATCH CONDITIONS
The dispatch conditions indicate (for each applicable item) the suitable conditions, limitations
(placards, operational procedures, maintenance procedures) necessary to ensure that an
acceptable level of safety is maintained.
Some MMEL items may have several dispatch conditions. Each dispatch condition offers a
different option to dispatch the aircraft.
A reference identifies each dispatch condition.
EXAMPLE
Dispatch condition reference 27-10-01C:
27-10-01 corresponds to the item number,
The letter "C" identifies the dispatch condition within the item 27-10-01.
Note: If an Operator receives only the dispatch conditions 27-10-01B and
27-10-01D, this means that the dispatch conditions 27-10-01A and
27-10-01C do not apply to the Operators fleet (this does not mean
that the dispatch conditions 27-10-01A and 27-10-01C are missing
from the MMEL ).

The dispatch condition reference is used:

To identify the open MEL items in the logbook,
To refer to the associated operational procedure (if any),
To refer to the associated maintenance procedure (if any),
To provide the Operators engineering and maintenance personnel with a unique reference at
fleet level for each option of dispatch for tracking and reporting purposes.
When an MMEL item has several dispatch conditions, the Operator must select and apply
only one dispatch condition at a time. An optional operational title is provided for each of the
dispatch condition reference. The aim of an operational title is to help the Operator to better
understand the operational differences between multiple dispatch conditions. In the frame of the
MEL customization, this operational title may be modified at Operators convenience provided that
the customized operational title still ensure the correct identification, the content and the intent
of the associated dispatch condition. When necessary, the Operator may successively apply
other dispatch conditions of the same item provided that the Operator complies with the MMEL
requirements and provided that the starting point of the repair interval countdown is not modified.
PROVISO
Each dispatch condition has one or several requirements, called provisos. Provisos are numbered
1), 2), 3)...
The Operator must comply with all the provisos of the selected dispatch condition.

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REPAIR INTERVAL
Each dispatch condition has an associated repair interval. The preamble of this MMEL defines the
repair interval categories. Refer to MI-00-05 Repair Interval .
A dash symbol replaces the repair interval in the following cases:
For items indicated As required by regulations. The MMEL does not specify the repair interval
because the repair interval depends on local regulations. The Operator must set a repair interval
in its MEL .
For items that refer to another manual (Weight and Balance, CDL ). The MMEL is not the
appropriate manual for this item.
For NO-GO items.
NBR INSTALLED
Each dispatch condition has a number installed that specifies the quantity of equipment,
components, systems or functions installed on the aircraft.
This quantity corresponds to the aircraft type certified configuration and, therefore required for
all flight conditions, unless otherwise indicated in the number required in conjunction with the
provisos of the dispatch condition.
A dash symbol indicates that a variable quantity is installed. When possible, the Operator may
replace the dash symbol by the quantity installed on the aircraft.
NBR REQUIRED
Each dispatch condition has a number required that specifies the minimum quantity of
equipment, components, systems or functions that must be operative for dispatch in accordance
with the provisos of the dispatch condition.
A dash symbol indicates that a variable quantity is required for dispatch. When possible, the
Operator may replace the dash symbol by the quantity required. For items indicated As required
by regulations, the dash symbol indicates that the MMEL does not specify the number required
because the number required depends on local regulations. The Operator must set a number
required in its MEL .
PLACARD
In the PDF format, the "YES" in the "Placard" column indicates the request for a placard. In the
electronic format, the "PLACARD" symbol indicates the request for a placard.
The control(s), and/or indicator(s) related to inoperative equipment, component, system or function
should be clearly placarded.
However, the absence of placard request in the MMEL does not prevent the Operator from
placarding.

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The Operator should determine:

The placard wording and location unless the MMEL dispatch condition requires a specific
wording and location.
The personnel (maintenance and/or flight crew) authorized to placard items.
OPERATIONAL AND MAINTENANCE PROCEDURES
The dispatch condition may require an operational or maintenance procedure to ensure an
acceptable level of safety.
The (o) symbol identifies an operational procedure.
The (m) symbol identifies a maintenance procedure.
The (o)(m) symbol means that the dispatch condition requires both an operational procedure and a
maintenance procedure.
The Operator is responsible to ensure that all operational and maintenance procedures are
appropriately performed regardless of who performs the procedures.
OPERATIONAL PROCEDURE
The (o) symbol indicates that the dispatch condition requires a specific operational procedure to
permit operation of the aircraft with the inoperative item.
Purpose of the operational procedure may be:
To require the flight crew or cabin crew to perform action(s),
To provide limitations or performance penalties,
To provide useful information to the crew.
The flight crew must read the content of the operational procedure before each flight.
The operational procedure must be applied before each flight. However, the dispatch condition
might specify a different periodicity. In this case this operational procedure must be applied
before the first MMEL dispatch and must be repeated at the defined periodicity.
The operational procedures are split and organized into specific flight phases. The flight crew
has to apply the part of the operational procedure related to the relevant flight phase.
Qualified flight crew or qualified cabin crew usually performs the operational procedures.
However other qualified personnel can also perform the operational procedures. But the flight
crew must read the content of the operational procedure before each flight.
MAINTENANCE PROCEDURE
The (m) symbol indicates that the dispatch condition requires a specific maintenance procedure
to permit operation of the aircraft with the inoperative item.
Purpose of the maintenance procedure may be:
To deactivate a system,
To check a system.

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The maintenance procedure is normally a one-time action that must be applied before the first
MMEL dispatch. However the dispatch condition may specify a periodicity for repetitive actions.
In this case the maintenance procedure must be applied before the first MMEL dispatch and
must be repeated at the defined periodicity.
Qualified maintenance personnel usually perform the maintenance procedures. However other
qualified and authorized personnel can also perform some actions if approved by the Operators
National Authority. But only qualified maintenance personnel can perform procedures that
require specialized knowledge or skill, or that require the use of tools or test equipment.
The MMEL maintenance procedures are published in the AMM . The MMEL item number must
be used to find the associated task in the AMM via the Deac/Reac Task by CDL / MMEL ...
function of AirN@v (in the AMM menu of AirN@v).
Note: 1. The MMEL item indicates the associated AMM task reference. However using the
AMM task reference is not the recommended method to find the task in the AMM .
The MMEL item number must be used instead with the above AirN@v function.
2. The MMEL item might indicate Refer to AMM task instead of the AMM task
reference. This indicates that the MMEL item is associated with several AMM tasks.
The above AirN@v function shall be used to find the applicable AMM task.
NOTES
There are three levels of notes:
Notes at the level of the item: these notes appear below the item title and before the first
dispatch condition of this item. These notes apply to all the dispatch conditions of the item.
Notes at the level of the dispatch condition: these notes appear at the end of the dispatch
condition. These notes apply only to this dispatch condition.
Notes at the level of the proviso: these notes appear within a proviso. These notes apply only to
this proviso.
REFERENCES
The references assist the Operator in complying with MMEL requirements. However, as indicated
in the preamble of this MMEL ( Refer to MI-00-03 Criteria for Dispatch ), the Operator is still
responsible for determining the applicable interrelationships and associated requirements.

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References are used in the following cases:

To permit the aircraft dispatch, another item has to be considered inoperative, or
Another source of information has to be reviewed and associated restrictions, and/or
procedures must be applied (e.g. Refer to FCOM , or Refer to Weight and Balance Manual),
or
To redirect to the applicable MMEL item. In that case, the referred relevant MMEL item must
be entered and the associated dispatch conditions must be applied, including the respective (o)
and (m) procedures if any.

HOW TO USE THE MEL OPERATIONAL PROCEDURES SECTION?

Ident.: HOW-00012818.0001001 / 10 OCT 14
Applicable to: ALL

This section lists the operational procedures associated with the MEL items. The dispatch conditions
may require an operational procedure to permit the dispatch of the aircraft.
The operational procedures are split and organized into specific flight phases. The flight crew has to
apply the part of the operational procedure related to the relevant flight phase.
The operational procedures may also have the following parts:
General Information : This part includes all information that the pilots must know due to
MEL condition.
Flight : This part groups all the limitations due to MELcondition that the pilots
Preparation/Limitation must consider for the route selection and flight preparation. This part
also includes aircraft performance penalties that should be used if no
performance software is available with the current failure case.
Procedure to be : The Operator has to develop its own operational procedure in the
developed in the MEL.
Operator's MEL

LANDING CAPABILITIES ( CAT 2, CAT 3 SINGLE, CAT 3 DUAL)

Ident.: HOW-00012812.0001001 / 31 MAY 12
Applicable to: ALL

When the landing capability of the aircraft is impacted by an inoperative item, it is shown with double
asterisk ( ** ) and the QRH (Refer to QRH/ Required Equipment for CAT2 and CAT3) shows the CAT
degradation. The associated MEL operational procedure provides the maximum landing capability.
The required equipment by certification for CAT 2, CAT 3 SINGLE and CAT 3 DUAL are listed in the
Flight ManualRefer to AFM/NORM-22-PA Required Equipment for CAT II and CAT III Approach and
Landing and the QRH (Refer to QRH/ Required Equipment for CAT2 and CAT3).

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The equipment to be operative to get CAT 2, CAT 3 SINGLE, or CAT 3 DUAL capability displayed on
the FMAs are listed in theQRH (Refer to QRH/ Required Equipment for CAT2 and CAT3).

REQUIRED NAVIGATION PERFORMANCE (RNP)

Ident.: HOW-00012813.0001001 / 12 SEP 11
Applicable to: ALL

The MEL does not include the minimum equipment required for RNP operations.
The minimum equipment/functions required to begin RNP operations are listed in the FCOM (Refer
to FCOM/PRO-SPO-51).

REDUCED VERTICAL SEPARATION MINIMUM (RVSM)

Ident.: HOW-00012814.0001001 / 12 SEP 11
Applicable to: ALL

When the RVSM capability of the aircraft is impacted by an inoperative item, the associated MEL
operational procedure provides the RVSM limitations.
The minimum equipment/functions required to begin RVSM operations are listed in the Flight
ManualRefer to AFM/NORM-34 Reduced Vertical Separation Minimum (RVSM) and FCOM (Refer to
FCOM/PRO-SPO-50 Reduced Vertical Separation Minimum (RVSM)).

FUTUR AIR NAVIGATION SYSTEM (FANS)

Ident.: HOW-00012815.0001001 / 23 MAR 11
Applicable to: ALL

The MEL does not include the minimum equipment required for FANS operations.
The minimum equipment/functions required to begin FANS operations are listed in the Airbus booklet
Getting to grips with FANS.

ABBREVIATIONS
Ident.: HOW-00012817.0001001 / 10 OCT 14
Applicable to: ALL

A
Abbreviation Term
A/C Aircraft
A/THR Autothrust
AAP Additional Attendant Panel
AAT Aircraft Allocation Table
ABCU Alternate Braking Control Unit
AC Alternating Current
Continued on the following page

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Abbreviation Term
ACARS ARINC Communication Addressing and Reporting System
ACFT Aircraft
ACMS Aircraft Condition Monitoring System
ACOC Air Cooled Oil Cooler
ACP Audio Control Panel
ACT Additional Center Tank
ADF Automatic Direction Finder
ADIRS Air Data Inertial Reference System
ADIRU Air Data Inertial Reference Unit
ADR Air Data Reference
ADS-B Automatic Dependent Surveillance Broadcast
AEVC Avionic Equipment Ventilation Controller
AGL Above Ground Level
AIP Attendant Indication Panel
ALT Altitude
AMM Aircraft Maintenance Manual
AOA Angle of Attack
AOC Airline Operational Control
AP Autopilot
APU Auxiliary Power Unit
ARPT Airport
ATA Air Transport Association
ATC Air Traffic Control
ATSAW Airborne Traffic Situational Awareness
ATSU Air Traffic Service Unit
ATT Attitude
AUTO Automatic
AVNCS Avionics

B
Abbreviation Term
B/UP Backup
BAT Battery
BCL Battery Charge Limiter
BMC Bleed Air Monitoring Computer
BSCU Braking Steering Control Unit
BTMU Brake Temperature Monitoring Unit

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C
Abbreviation Term
C/B Circuit Breaker
CAM Cabin Assignment Module
CAPT Captain
CAT Category
CCD Cursor Control Device
CDL Configuration Deviation List
CDLS Cockpit Door Locking System
CDSS Cockpit Door Surveillance System
CDU Control Display Unit
CFDIU Centralized Fault Data Interface Unit
CFDS Centralized Fault Display System
CG Center of Gravity
CIDS Cabin Intercommunication Data System
CL Climb
CLB Climb
COND Conditioning
CONF Configuration
CPC Cabin Pressure Controller
CTL Control
CTR Center
CVR Cockpit Voice Recorder

D
Abbreviation Term
DAC Double Annular Combustor
DAR Digital AIDS Recorder
DC Direct Current
DDRMI Digital Distance and Radio Magnetic Indicator
DEU Decoder / Encoder Unit
DFDR Digital Flight Data Recorder
DLRB Data Loading Routing Box
DMC Display Management Computer
DME Distance Measuring Equipment
DMU Data Management Unit
DU Display Unit

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E
Abbreviation Term
EASA European Aviation Safety Agency
ECAM Electronic Centralized Aircraft Monitoring
ECAS Emergency Cockpit Alerting System
ECP ECAM Control Panel
ECU Engine Control Unit
EEC Engine Electronic Controller
EFB Electronic Flight Bag
EFIS Electronic Flight Instrument System
EGT Exhaust Gas Temperature
EHS Enhanced Surveillance System
EIU Engine Interface Unit
ELAC Elevator Aileron Computer
ELEC Electric
ELT Emergency Locator Transmitter
EMCD Electronic Magnetic Chip Detector
ENG Engine
EPR Engine Pressure Ratio
ESS Essential
ETOPS Extended Range Twin Engined Aircraft Operations
EVMU Engine Vibration Monitoring Unit
EWD Engine Warning Display
EWDU Engine Warning Display Unit

F
Abbreviation Term
F/O First Officer
FAC Flight Augmentation Computer
FADEC Full Authority Digital Engine Control
FANS Future Air Navigation System
FAP Flight/Forward Attendant Panel
FCDC Flight Control Data Concentrator
FCOM Flight Crew Operating Manual
FCU Flight Control Unit
FD Flight Director
FDIMU Flight Data Interface and Management Unit
FDIU Flight Data Interface Unit
FL Flight Level
FLS FMS Landing System
FMA Flight Mode Annunciator
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Abbreviation Term
FMGC Flight Management Guidance Computer
FMS Flight Management System
FOB Fuel on Board
FQI Fuel Quantity Indication
FQIC Fuel Quantity Indication Computer
FSN Fleet Serial Number
FU Fuel Used
FWC Flight Warning Computer
FWD Forward

G
Abbreviation Term
G/S Glideslope
GAPCU Ground and Auxiliary Power Control Unit Unit
GCU Generator Control Unit
GEN Generator
GLS GNSS Landing System
GND Ground
GNSS Global Navigation Satellite System
GPCU Ground Power Control Unit
GPS Global Positioning System
GPU Ground Power Unit
GPWS Ground Proximity Warning System
GW Gross Weight

H
Abbreviation Term
HF High Frequency
HP High Pressure
HUD Head Up Display
HYD Hydraulics

I
Abbreviation Term
IAS Indicated Airspeed
IDG Integrated Drive Generator
IFE In-Flight Entertainment
IFR Instrument Flight Rules
ILS Instrument Landing System
IP Intermediate Pressure
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Abbreviation Term
IR Inertial Reference
IRS Inertial Reference System
ISA International Standard Atmosphere
ISB Inspection Service Bulletin
ISIS Integrated Standby Instrument System

J
Abbreviation Term
JAA Joint Aviation Authorities

L
Abbreviation Term
L/G Landing Gear
LAF Load Alleviation Function
LED Light Emitting Diode
LEDU List of Effective Documentary Units
LESS List of Effective Sections/Subsections
LGCIU Landing Gear Control Interface Unit
LH Left Hand
LOM List of Modifications
LP Low Pressure
LVDT Linear Variable Differential Transformer
LVR CLB Lever Climb

M
Abbreviation Term
MAN Manual
MCDU Multipurpose Control and Display Unit
MCT Maximum Continuous Thrust
MDDU Multipurpose Disk Drive Unit
MEL Minimum Equipment List
MES Main Engine Start
MLS Microwave Landing System
MMEL Master Minimum Equipment List
MMI Manual Magnetic Indicator
MMO Maximum Operating Mach
MMR Multi Mode Receiver
MOD Modification
MP Modification Proposal
MSN Manufacturer Serial Number
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Abbreviation Term
MTO Maximum Take-Off
MTOW Maximum Takeoff Weight

N
Abbreviation Term
NAV Navigation
ND Navigation Display
NDU Navigation Display Unit
NEF Non-Essential Equipment and Furnishings
NWS Nose Wheel Steering

O
Abbreviation Term
OANS On-board Airport Navigation System
OAT Outside Air Temperature
OEB Operations Engineering Bulletin
OEI One Engine Inoperative
OP CLB Open Climb

P
Abbreviation Term
P/N Part Number
PAX Passenger
PCU Power Control Unit
PDF Portable Document Format
PF Pilot Flying
PFD Primary Flight Display
PFDU Primary Flight Display Unit
PHC Probes Heat Computer
PNF Pilot Non Flying
PRV Pressure Regulation Valve
PSL Product Structure Level
PTP Programming and Test Panel
PTU Power Transfer Unit (Hydraulic)
PVI Paravisual Indicator
PWR Power

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Q
Abbreviation Term
QAR Quick Access Recorder
QCCU Quantity Calculation Control Unit
QNH Sea Level Atmospheric Pressure
QRH Quick Reference Handbook

R
Abbreviation Term
RA Radio Altitude
RAT Ram Air Turbine
RH Right Hand
RMI Radio Magnetic Indicator
RMP Radio Management Panel
RNP Required Navigation Performance
ROP Runway Overrun Protection
ROW Runway Overrun Warning
RTO Rejected Takeoff
RTOW Regulatory Takeoff Weight
RVSM Reduced Vertical Separation Minimum

S
Abbreviation Term
SAC Single Annular Combustor
SAT Static Air Temperature
SATCOM Satellite Communication
SB Service Bulletin
SD System Display
SDAC System Data Acquisition Concentrator
SDCU Smoke Detection Control Unit
SDF Smoke Detection Function
SDU System Display Unit
SEC Spoiler Elevator Computer
SFCC Slat/Flap Control Computer
SFCS Slat/Flap Control System
SOH Summary of Highlights
STBY Standby

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T
Abbreviation Term
T/O Takeoff
TAS True Air Speed
TAT Total Air Temperature
TAWS Terrain Awareness and Warning System
TCA Throttle Control Assy
TCAS Traffic Alert and Collision Avoidance System
TCC Turbine Case Cooling
TLC Takeoff and Landing Chart Computation Program
TOC Table of Contents
TOGA Takeoff/Go Around
TOW Takeoff Weight
TPIC Tire Pressure Indicating Computer
TR Transformer Rectifier Unit

U
Abbreviation Term
UTC Universal Coordinated Time

V
Abbreviation Term
V1 Critical Engine Failure Speed
V2 Takeoff Safety Speed
VAPP Approach Speed
VENT Ventilation
VFE Maximum Speed for each Flap Configuration
VFR Visual Flight Rules
VHF Very High Frequency
VLE Max Landing Gear Extended Speed
VMC Visual Meteorological Conditions
VMCA Minimum Control Speed in Flight
VMCG Minimum Control Speed on Ground
VMO Maximum Operating Speed
VMU Minimum Unstick Speed
VOR VHF Omnidirectional Range
VR Rotation Speed
VS Reference Stalling Speed
VSB Vender Service Bulletin

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W
Abbreviation Term
WBS Weight and Balance System
WTB Wing Tip Brake

X
Abbreviation Term
XML Extensible Mark-up Language

Z
Abbreviation Term
ZFW Zero Fuel Weight

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ME-21 Air Conditioning

AIR AFT CRG VENT FAULT.................................................................................................................................. A
AIR COND CTL 1(2)-A(B)....................................................................................................................................... B
AIR PACK 1(2) FAULT........................................................................................................................................... C
AIR PACK 1+2 FAULT............................................................................................................................................D
AIR PACK 1(2) OFF................................................................................................................................................E
AIR PACK 1(2) OVHT............................................................................................................................................. F
AIR PACK 1(2) REGUL FAULT..............................................................................................................................G
CAB PR EXCESS CAB ALT...................................................................................................................................H
CAB PR EXCESS RESIDUAL PR........................................................................................................................... I
CAB PR LDG ELEV FAULT.................................................................................................................................... J
CAB PR LO DIFF PR..............................................................................................................................................K
CAB PR OFV NOT OPEN.......................................................................................................................................L
CAB PR SAFETY VALVE OPEN........................................................................................................................... M
CAB PR SYS 1(2) FAULT...................................................................................................................................... N
CAB PR SYS 1+2 FAULT...................................................................................................................................... O
COND AFT CAB DUCT OVHT............................................................................................................................... P
COND AFT CRG ISOL VALVE.............................................................................................................................. Q
COND CKPT DUCT OVHT.....................................................................................................................................R
COND FWD CAB DUCT OVHT..............................................................................................................................S
COND HOT AIR FAULT..........................................................................................................................................T
COND L+R CAB FAN FAULT.................................................................................................................................U
COND LAV+GALLEY FAN FAULT......................................................................................................................... V
COND TRIM AIR SYS FAULT............................................................................................................................... W
VENT AVNCS SYS FAULT.....................................................................................................................................X
VENT BLOWER FAULT.......................................................................................................................................... Y
VENT EXTRACT FAULT......................................................................................................................................... Z
VENT SKIN VALVE FAULT..................................................................................................................................AA

ME-22 Auto Flight

AUTO FLT A/THR LIMITED....................................................................................................................................A
AUTO FLT A/THR OFF...........................................................................................................................................B
AUTO FLT AP OFF.................................................................................................................................................C
AUTO FLT FAC 1 FAULT.......................................................................................................................................D
AUTO FLT FAC 2 FAULT.......................................................................................................................................E
AUTO FLT FAC 1+2 FAULT................................................................................................................................... F
AUTO FLT FCU 1(2) FAULT.................................................................................................................................. G
AUTO FLT FCU 1+2 FAULT.................................................................................................................................. H
AUTO FLT REAC W/S DET FAULT........................................................................................................................ I
AUTO FLT RUD TRIM 1(2) FAULT.........................................................................................................................J
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AUTO FLT RUD TRIM SYS....................................................................................................................................K
AUTO FLT RUD TRV LIM 1(2)............................................................................................................................... L
AUTO FLT RUD TRV LIM SYS............................................................................................................................. M
AUTO FLT YAW DAMPER 1(2)............................................................................................................................. N
AUTO FLT YAW DAMPER SYS............................................................................................................................ O
WINDSHEAR DET FAULT...................................................................................................................................... P

ME-23 Communications
COM ACARS FAULT.............................................................................................................................................. A
COM CIDS 1+2 FAULT...........................................................................................................................................B
COM HF 1(2) DATA FAULT................................................................................................................................... C
COM HF 1(2) EMITTING........................................................................................................................................ D
COM SINGLE PTT STUCK.....................................................................................................................................E
COM VHF 3 DATA FAULT......................................................................................................................................F
COM VHF 1(2)(3) EMITTING................................................................................................................................. G

ME-24 Electrical Power

C/B TRIPPED.......................................................................................................................................................... A
ELEC AC BUS 1 FAULT.........................................................................................................................................B
ELEC AC BUS 2 FAULT.........................................................................................................................................C
ELEC AC ESS BUS ALTN......................................................................................................................................D
ELEC AC ESS BUS FAULT....................................................................................................................................E
ELEC AC ESS BUS SHED..................................................................................................................................... F
ELEC APU GEN FAULT.........................................................................................................................................G
ELEC APU GEN OVERLOAD.................................................................................................................................H
ELEC BAT 1(2) FAULT............................................................................................................................................ I
ELEC BAT 1(2) OFF................................................................................................................................................J
ELEC BCL 1(2) FAULT........................................................................................................................................... K
ELEC DC BAT BUS FAULT.................................................................................................................................... L
ELEC DC BUS 1 FAULT........................................................................................................................................M
ELEC DC BUS 2 FAULT........................................................................................................................................ N
ELEC DC BUS 1+2 FAULT.................................................................................................................................... O
ELEC DC EMER CONFIG...................................................................................................................................... P
ELEC DC ESS BUS FAULT................................................................................................................................... Q
ELEC DC ESS BUS SHED.....................................................................................................................................R
ELEC EMER CONFIG.............................................................................................................................................S
ELEC EMER GEN 1 LINE OFF.............................................................................................................................. T
ELEC ESS BUSSES ON BAT................................................................................................................................ U
ELEC GEN 1(2) FAULT.......................................................................................................................................... V
ELEC GEN 1(2) OFF............................................................................................................................................. W
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ELEC GEN 1(2)OVERLOAD................................................................................................................................... X
ELEC IDG 1(2) DISCONNECTED.......................................................................................................................... Y
ELEC IDG 1(2) OIL LO PR..................................................................................................................................... Z
ELEC IDG 1(2) OIL OVHT....................................................................................................................................AA
ELEC STATIC INV FAULT................................................................................................................................... AB
ELEC TR 1(2) FAULT...........................................................................................................................................AC

ME-26 Fire Protection

APU FIRE ...............................................................................................................................................................A
APU FIRE DET FAULT........................................................................................................................................... B
APU FIRE LOOP A(B) FAULT................................................................................................................................C
AVIONICS SMOKE ................................................................................................................................................ D
ENG 1(2) FIRE .......................................................................................................................................................E
ENG 1(2) FIRE DET FAULT................................................................................................................................... F
ENG 1(2) FIRE LOOP A FAULT............................................................................................................................ G
ENG 1(2) FIRE LOOP B FAULT............................................................................................................................ H
SMOKE AFT CARGO SMOKE.................................................................................................................................I
SMOKE AFT CRG BTL FAULT...............................................................................................................................J
SMOKE AFT CRG DET FAULT..............................................................................................................................K
SMOKE FWD CARGO SMOKE.............................................................................................................................. L
SMOKE FWD CRG BTL FAULT............................................................................................................................ M
SMOKE FWD CRG DET FAULT............................................................................................................................ N
SMOKE DET FAULT...............................................................................................................................................O
SMOKE LAVATORY DET FAULT...........................................................................................................................P
SMOKE LAVATORY SMOKE................................................................................................................................. Q

ME-27 Flight Controls

CONFIG L(R) SIDESTICK FAULT.......................................................................................................................... A
CONFIG PITCH TRIM NOT IN T.O. RANGE......................................................................................................... B
CONFIG RUD TRIM NOT IN T.O. RANGE............................................................................................................C
CONFIG SLATS(FLAPS) NOT IN T.O. CONFIG....................................................................................................D
CONFIG SPEED BRK NOT RETRACTED............................................................................................................. E
F/CTL AIL SERVO FAULT...................................................................................................................................... F
F/CTL ALTN LAW................................................................................................................................................... G
F/CTL DIRECT LAW............................................................................................................................................... H
F/CTL ELAC 1 FAULT..............................................................................................................................................I
F/CTL ELAC 1 PITCH FAULT................................................................................................................................. J
F/CTL ELAC 2 FAULT............................................................................................................................................ K
F/CTL ELAC 2 PITCH FAULT.................................................................................................................................L
F/CTL ELEV SERVO FAULT..................................................................................................................................M
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F/CTL FCDC 1 FAULT............................................................................................................................................N
F/CTL FCDC 2 FAULT........................................................................................................................................... O
F/CTL FCDC 1+2 FAULT........................................................................................................................................P
F/CTL FLAP ATTACH SENSOR............................................................................................................................ Q
F/CTL FLAP LVR NOT ZERO................................................................................................................................ R
F/CTL FLAP SYS 1 FAULT.................................................................................................................................... S
F/CTL FLAP SYS 2 FAULT.....................................................................................................................................T
F/CTL FLAP TIP BRK FAULT................................................................................................................................ U
F/CTL FLAPS(SLATS) FAULT................................................................................................................................ V
F/CTL FLAPS(SLATS) LOCKED............................................................................................................................W
F/CTL GND SPLR FAULT...................................................................................................................................... X
F/CTL GND SPLR (1+2)(3+4) FAULT.................................................................................................................... Y
F/CTL GND SPLR 5 FAULT................................................................................................................................... Z
F/CTL GND SPLR NOT ARMED..........................................................................................................................AA
F/CTL L(R) AIL FAULT......................................................................................................................................... AB
F/CTL L(R) ELEV FAULT..................................................................................................................................... AC
F/CTL L+R ELEV FAULT..................................................................................................................................... AD
F/CTL L(R) SIDESTICK FAULT............................................................................................................................AE
F/CTL PITCH TRIM/MCDU/CG DISAGREE......................................................................................................... AF
F/CTL SEC 1 FAULT............................................................................................................................................AG
F/CTL SEC 2 FAULT............................................................................................................................................AH
F/CTL SEC 3 FAULT............................................................................................................................................. AI
F/CTL SIDESTICK PRIORITY...............................................................................................................................AJ
F/CTL SLAT SYS 1 FAULT.................................................................................................................................. AK
F/CTL SLAT SYS 2 FAULT.................................................................................................................................. AL
F/CTL SLAT TIP BRK FAULT..............................................................................................................................AM
F/CTL SPD BRK DISAGREE............................................................................................................................... AN
F/CTL SPD BRK FAULT...................................................................................................................................... AO
F/CTL SPD BRK STILL OUT................................................................................................................................AP
F/CTL SPD BRK 2(3+4) FAULT...........................................................................................................................AQ
F/CTL SPLR FAULT............................................................................................................................................. AR
F/CTL STABILIZER JAM...................................................................................................................................... AS

ME-28 Fuel
FUEL APU LP VALVE FAULT................................................................................................................................ A
FUEL AUTO FEED FAULT..................................................................................................................................... B
FUEL CTR TK PUMP 1(2) LO PR......................................................................................................................... C
FUEL CTR TK PUMPS LO PR...............................................................................................................................D
FUEL CTR TK PUMPS OFF...................................................................................................................................E
FUEL ENG 1(2) LP VALVE OPEN......................................................................................................................... F
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FUEL FQI CH 1(2) FAULT..................................................................................................................................... G
FUEL F.USED/FOB DISAGREE............................................................................................................................. H
FUEL L(R) INNER(OUTER) TK HI TEMP................................................................................................................I
FUEL L(R) INNER(OUTER) TK LO TEMP..............................................................................................................J
FUEL L(R) OUTER XFR CLOSED......................................................................................................................... K
FUEL L(R) OUTER XFR OPEN.............................................................................................................................. L
FUEL L(R) TK PUMP 1(2) LO PR......................................................................................................................... M
FUEL L(R) TK PUMP 1+2 LO PR.......................................................................................................................... N
FUEL L(R) WING TK LO LVL................................................................................................................................ O
FUEL L+R WING TK LO LVL................................................................................................................................. P
FUEL L(R) XFR VALVE CLOSED..........................................................................................................................Q
FUEL L(R) XFR VALVE OPEN...............................................................................................................................R
FUEL X FEED VALVE FAULT................................................................................................................................S

ME-29 Hydraulic Power

HYD B ELEC PUMP LO PR................................................................................................................................... A
HYD B ELEC PUMP OVHT.................................................................................................................................... B
HYD B RSVR LO AIR PR.......................................................................................................................................C
HYD B RSVR LO LVL............................................................................................................................................ D
HYD B RSVR OVHT............................................................................................................................................... E
HYD B SYS LO PR................................................................................................................................................. F
HYD B+G SYS LO PR............................................................................................................................................G
HYD B+Y SYS LO PR............................................................................................................................................ H
HYD G ENG 1 PUMP LO PR.................................................................................................................................. I
HYD G RSVR LO AIR PR....................................................................................................................................... J
HYD G RSVR LO LVL............................................................................................................................................ K
HYD G RSVR OVHT............................................................................................................................................... L
HYD G SYS LO PR................................................................................................................................................M
HYD G+Y SYS LO PR............................................................................................................................................N
HYD PTU FAULT.................................................................................................................................................... O
HYD RAT FAULT.................................................................................................................................................... P
HYD Y ELEC PUMP LO PR...................................................................................................................................Q
HYD Y ELEC PUMP OVHT.................................................................................................................................... R
HYD Y ENG 2 PUMP LO PR................................................................................................................................. S
HYD Y RSVR LO AIR PR....................................................................................................................................... T
HYD Y RSVR LO LVL............................................................................................................................................ U
HYD Y RSVR OVHT............................................................................................................................................... V
HYD Y SYS LO PR................................................................................................................................................W
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ME-30 Ice and Rain Protection
ANTI ICE ALL PITOT.............................................................................................................................................. A
ANTI ICE CAPT(F/O)(STBY) AOA..........................................................................................................................B
ANTI ICE CAPT(F/O)(STBY) L(R) STAT................................................................................................................C
ANTI ICE CAPT(F/O)(STBY) PITOT.......................................................................................................................D
ANTI ICE CAPT+F/O PITOT...................................................................................................................................E
ANTI ICE CAPT+STBY PITOT................................................................................................................................F
ANTI ICE CAPT(F/O)(STBY) PROBES.................................................................................................................. G
ANTI ICE CAPT(F/O) TAT...................................................................................................................................... H
ANTI ICE DETECT FAULT.......................................................................................................................................I
ANTI ICE ENG 1(2) VALVE CLSD..........................................................................................................................J
ANTI ICE ENG 1(2) VALVE OPEN.........................................................................................................................K
ANTI ICE F/O+STBY PITOT................................................................................................................................... L
ANTI ICE ICE DETECTED..................................................................................................................................... M
ANTI ICE L(R) WINDOW........................................................................................................................................ N
ANTI ICE L(R) WINDSHIELD................................................................................................................................. O
ANTI ICE L+R WINDSHIELD..................................................................................................................................P
SEVERE ICE DETECTED...................................................................................................................................... Q
WING ANTI ICE L(R) HI PR...................................................................................................................................R
WING ANTI ICE L(R) VALVE OPEN...................................................................................................................... S
WING ANTI ICE OPEN ON GND........................................................................................................................... T
WING ANTI ICE SYS FAULT................................................................................................................................. U

ME-31 Indicating/Recording Systems

EIS DMC 1 FAULT..................................................................................................................................................A
EIS DMC 2 FAULT..................................................................................................................................................B
EIS DMC 3 FAULT..................................................................................................................................................C
EIS DMC/FWC COM FAULT.................................................................................................................................. D
FWS FWC 1 FAULT................................................................................................................................................E
FWS FWC 2 FAULT................................................................................................................................................F
FWS FWC 1+2 FAULT........................................................................................................................................... G
FWS OEB/FWC DISCREPANCY............................................................................................................................H
FWS SDAC 1 FAULT............................................................................................................................................... I
FWS SDAC 2 FAULT.............................................................................................................................................. J
FWS SDAC 1+2 FAULT..........................................................................................................................................K
RECORDER DFDR FAULT..................................................................................................................................... L
RECORDER SYS FAULT.......................................................................................................................................M
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ME-32 Landing Gear
BRAKES ALTN BRK FAULT...................................................................................................................................A
BRAKES ALTN L(R) RELEASED........................................................................................................................... B
BRAKES A/SKID N/WS FAULT.............................................................................................................................. C
BRAKES A/SKID N/WS OFF.................................................................................................................................. D
BRAKES AUTO BRK FAULT..................................................................................................................................E
BRAKES BRK Y ACCU LO PR.............................................................................................................................. F
BRAKES SYS 1 FAULT..........................................................................................................................................G
BRAKES SYS 2 FAULT..........................................................................................................................................H
BRAKES HOT........................................................................................................................................................... I
BRAKES NORM BRK FAULT..................................................................................................................................J
BRAKES NORM+ALT FAULT................................................................................................................................. K
BRAKES PARK BRK FAULT...................................................................................................................................L
BRAKES PARK BRK LO PR..................................................................................................................................M
BRAKES PARK BRK ON........................................................................................................................................N
BRAKES RELEASED..............................................................................................................................................O
BRAKES-N/WS MINOR FAULT.............................................................................................................................. P
CONFIG PARK BRK ON........................................................................................................................................ Q
L/G DOORS NOT CLOSED....................................................................................................................................R
L/G GEAR NOT DOWN.......................................................................................................................................... S
L/G GEAR NOT DOWNLOCKED............................................................................................................................T
L/G GEAR NOT UPLOCKED..................................................................................................................................U
L/G GEAR UPLOCK FAULT................................................................................................................................... V
L/G LGCIU 1 FAULT.............................................................................................................................................. W
L/G LGCIU 2 FAULT............................................................................................................................................... X
L/G LGCIU 1+2 FAULT........................................................................................................................................... Y
L/G SHOCK ABSORBER FAULT............................................................................................................................Z
L/G SYS DISAGREE.............................................................................................................................................AA
WHEEL HYD SEL FAULT.................................................................................................................................... AB
WHEEL N/W STRG FAULT..................................................................................................................................AC

ME-34 Navigation
NAV ADR 1 FAULT.................................................................................................................................................A
NAV ADR 2 FAULT.................................................................................................................................................B
NAV ADR 3 FAULT.................................................................................................................................................C
NAV ADR(1+2)(1+3)(2+3) FAULT...........................................................................................................................D
NAV ADR 1+2+3 FAULT.........................................................................................................................................E
NAV ALTI DISCREPANCY......................................................................................................................................F
NAV ATC/XPDR 1(2)(1+2) FAULT......................................................................................................................... G
NAV ATC/XPDR STBY........................................................................................................................................... H
Continued on the following page

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Continued from the previous page

NAV ADR DISAGREE.............................................................................................................................................. I
NAV ATT DISCREPANCY....................................................................................................................................... J
NAV BARO REF DISCREPANCY...........................................................................................................................K
NAV CAPT(F/O)(STBY) AOA FAULT......................................................................................................................L
NAV FM/GPS POS DISAGREE............................................................................................................................. M
NAV GPS 1(2) FAULT............................................................................................................................................ N
NAV GPWS FAULT................................................................................................................................................ O
NAV GPWS TERR DET FAULT............................................................................................................................. P
NAV HDG DISCREPANCY.....................................................................................................................................Q
NAV IAS DISCREPANCY....................................................................................................................................... R
NAV ILS 1(2)(1+2) FAULT...................................................................................................................................... S
NAV IR DISAGREE................................................................................................................................................. T
NAV IR NOT ALIGNED...........................................................................................................................................U
NAV IR 1 FAULT.....................................................................................................................................................V
NAV IR 2 FAULT....................................................................................................................................................W
NAV IR 3 FAULT.....................................................................................................................................................X
NAV IR 1+2(1+3)(2+3) FAULT................................................................................................................................Y
NAV LS TUNING DISAGREE................................................................................................................................. Z
NAV PRED W/S DET FAULT...............................................................................................................................AA
NAV RA DEGRADED........................................................................................................................................... AB
NAV RA 1(2) FAULT............................................................................................................................................ AC
NAV TCAS FAULT................................................................................................................................................AD
NAV TCAS STANDBY.......................................................................................................................................... AE
OVERSPEED ....................................................................................................................................................... AF

ME-36 Pneumatic
AIR APU BLEED FAULT.........................................................................................................................................A
AIR APU BLEED LEAK...........................................................................................................................................B
AIR BLEED 1(2) OFF..............................................................................................................................................C
AIR ENG HP VALVE FAULT.................................................................................................................................. D
AIR ENG 1(2) BLEED ABNORM PR...................................................................................................................... E
AIR ENG 1(2) BLEED FAULT.................................................................................................................................F
AIR ENG 1(2) BLEED HI TEMP.............................................................................................................................G
AIR ENG 1(2) BLEED LEAK...................................................................................................................................H
AIR ENG 1(2)(1+2) BLEED LO TEMP..................................................................................................................... I
AIR ENG 1(2) BLEED NOT CLSD.......................................................................................................................... J
Continued on the following page

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Continued from the previous page

AIR ENG 1(2) LEAK DET FAULT...........................................................................................................................K
AIR L(R) WING LEAK..............................................................................................................................................L
AIR L(R) WING LEAK DET FAULT........................................................................................................................M
AIR X BLEED FAULT............................................................................................................................................. N
BLEED MONITORING FAULT................................................................................................................................O
BLEED MONIT SYS 1(2) FAULT............................................................................................................................P

ME-46 Information Systems

DATA LINK ATC FAULT......................................................................................................................................... A
DATA LINK ATSU FAULT.......................................................................................................................................B
DATA LINK COMPANY FAULT.............................................................................................................................. C

ME-47 Inert Gas System

FUEL INERTING SYS FAULT................................................................................................................................ A

ME-49 Airborne Auxiliary Power

APU AUTO(EMER) SHUT DOWN.......................................................................................................................... A

ME-52 Doors
DOOR AFT(BULK)(FWD) CARGO..........................................................................................................................A
DOOR L(R) AFT AVIONICS....................................................................................................................................B
DOOR L(R) AFT CABIN......................................................................................................................................... C
DOOR L(R) AFT EMER EXIT.................................................................................................................................D
DOOR L(R) FWD AVIONICS.................................................................................................................................. E
DOOR L(R) FWD CABIN........................................................................................................................................ F
DOOR L(R) FWD EMER EXIT............................................................................................................................... G

ME-70 Engine
ENG COMPRESSOR VANE................................................................................................................................... A
ENG DUAL FAILURE.............................................................................................................................................. B
ENG THR LEVERS NOT SET................................................................................................................................C
ENG REV SET........................................................................................................................................................ D
ENG SAT ABOVE FLEX TEMP..............................................................................................................................E
ENG THRUST LOCKED..........................................................................................................................................F
ENG TYPE DISAGREE.......................................................................................................................................... G
ENG VIB SYS FAULT.............................................................................................................................................H
ENG 1(2) A/C FADEC SUPPLY...............................................................................................................................I
ENG 1(2) AIR EXCHANGR FAULT AIR VALVE CLOSED..................................................................................... J
ENG 1(2) AIR EXCHANGR FAULT AIR VALVE OPEN......................................................................................... K
ENG 1(2) BEARING 4 OIL SYS HI PRESS............................................................................................................L
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Continued from the previous page

ENG 1(2) BEARING 4 OIL SYS SCAVENGE VALVE FAULT...............................................................................M
ENG 1(2) BLEED STATUS FAULT........................................................................................................................ N
ENG 1(2) COMPRESSOR VANE........................................................................................................................... O
ENG 1(2) CTL VALVE FAULT................................................................................................................................ P
ENG 1(2) EGT(FF)(N1)(N2) DISCREPANCY.........................................................................................................Q
ENG 1(2) EGT(EPR)(FF)(N1)(N2) DISCREPANCY............................................................................................... R
ENG 1(2) EGT EXCEEDED DURING AIR START................................................................................................ S
ENG 1(2) EIU FAULT..............................................................................................................................................T
ENG 1(2) EPR MODE FAULT................................................................................................................................ U
ENG 1(2) FADEC A(B) FAULT............................................................................................................................... V
ENG 1(2) FADEC ALTERNATOR..........................................................................................................................W
ENG 1(2) FADEC FAULT........................................................................................................................................X
ENG 1(2) FADEC HI TEMP.................................................................................................................................... Y
ENG 1(2) FADEC OVHT......................................................................................................................................... Z
ENG 1(2) FADEC PLUG FAULT.......................................................................................................................... AA
ENG 1(2) FAIL...................................................................................................................................................... AB
ENG 1(2) FUEL CTL FAULT................................................................................................................................AC
ENG 1(2) FUEL FILTER CLOG........................................................................................................................... AD
ENG 1(2) FUEL HEAT SYS................................................................................................................................. AE
ENG 1(2) FUEL RETURN VALVE........................................................................................................................AF
ENG 1(2) FUEL VALVE FAULT...........................................................................................................................AG
ENG 1(2) HOT FUEL............................................................................................................................................AH
ENG 1(2) HP FUEL VALVE................................................................................................................................... AI
ENG 1(2) IGN A(B) FAULT................................................................................................................................... AJ
ENG 1(2) IGN A+B FAULT...................................................................................................................................AK
ENG 1(2) LOW N1................................................................................................................................................ AL
ENG 1(2) N1(N2)(EGT) OVER LIMIT.................................................................................................................. AM
ENG 1(2) OIL FILTER CLOG...............................................................................................................................AN
ENG 1(2) OIL HI TEMP........................................................................................................................................AO
ENG 1(2) OIL LO PR............................................................................................................................................AP
ENG 1(2) OIL LO TEMP...................................................................................................................................... AQ
ENG 1(2) ONE TLA FAULT................................................................................................................................. AR
ENG 1(2) OVSPD PROT FAULT..........................................................................................................................AS
ENG 1(2) PROBES FAULT...................................................................................................................................AT
ENG 1(2) REV INHIBITED................................................................................................................................... AU
ENG 1(2) REV ISOL FAULT................................................................................................................................ AV
ENG 1(2) REV PRESSURIZED...........................................................................................................................AW
ENG 1(2) REV SWITCH FAULT.......................................................................................................................... AX
ENG 1(2) REVERSE UNLOCKED........................................................................................................................AY
ENG 1(2) REVERSER FAULT..............................................................................................................................AZ
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Continued from the previous page

ENG 1(2) SENSOR FAULT.................................................................................................................................. BA
ENG 1(2) SHUT DOWN........................................................................................................................................BB
ENG 1(2) STALL...................................................................................................................................................BC
ENG 1(2) START FAULT..................................................................................................................................... BD
ENG 1(2) START VALVE FAULT.........................................................................................................................BE
ENG 1(2) SYSTEM FAULT...................................................................................................................................BF
ENG 1(2) THR LEVER ABV IDLE....................................................................................................................... BG
ENG 1(2) THR LEVER DISAGREE......................................................................................................................BH
ENG 1(2) THR LEVER FAULT.............................................................................................................................. BI

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Localization Toc ID Reason

Title Index
ME-36 N 2 Addition of an aircraft status to give the information that item
AIR X BLEED FAULT 36-12-04 is applicable when the crossbleed valve automatic
control is affected.
ME-36 N 3 Addition of the dispatch assessment referring to Item
AIR X BLEED FAULT 36-12-05 when the manual control of the crossbleed valve is
affected.
ME-23 E 1 Effectivity update: The information now also applies to MSN 4516,
COM SINGLE PTT STUCK 4767, 4972, 5178, 5234.
ME-27 Z 1 Effectivity update: The information now also applies to MSN 4516,
F/CTL GND SPLR 5 FAULT 4972, 5178, 5234.
ME-27 AA 2 Effectivity update: The information now also applies to MSN 4516,
F/CTL GND SPLR NOT ARMED 4767, 4972, 5178, 5234.
ME-27 AF 3 Effectivity update: The information now also applies to MSN 4516,
F/CTL PITCH TRIM/MCDU/CG 4767, 4972, 5178, 5234.
DISAGREE
ME-28 K 1 Effectivity update: The information now also applies to MSN 4516,
FUEL L(R) OUTER XFR CLOSED 4767, 4972, 5178, 5234.
ME-28 L 2 Effectivity update: The information now also applies to MSN 4516,
FUEL L(R) OUTER XFR OPEN 4767, 4972, 5178, 5234.
ME-28 Q 3 Effectivity update: The information no longer applies to MSN 4516,
FUEL L(R) XFR VALVE CLOSED 4767, 4972, 5178, 5234.
ME-28 R 4 Effectivity update: The information no longer applies to MSN 4516,
FUEL L(R) XFR VALVE OPEN 4767, 4972, 5178, 5234.
ME-31 D 1 Effectivity update: The information now also applies to MSN 4516,
EIS DMC/FWC COM FAULT 4767, 4972, 5178, 5234.
ME-32 L 1 Effectivity update: The information no longer applies to MSN 4516,
BRAKES PARK BRK FAULT 4767, 4972, 5178, 5234.
ME-32 L 2 Effectivity update: The information now also applies to MSN 4516,
BRAKES PARK BRK FAULT 4767, 4972, 5178, 5234.
ME-32 Y 3 Effectivity update: The information now also applies to MSN 4516,
L/G LGCIU 1+2 FAULT 4767, 4972, 5178, 5234.
ME-34 K 1 Effectivity update: The information now also applies to MSN 4516,
NAV BARO REF DISCREPANCY 4767, 4972, 5178, 5234.
ME-36 G 1 Effectivity update: The information now also applies to MSN 4516,
AIR ENG 1(2) BLEED HI TEMP 4767, 4972, 5178, 5234.
ME-47 A 1 Effectivity update: The information now also applies to MSN 5178,
FUEL INERTING SYS FAULT 5234.
ME-70 E 1 Effectivity update: The information now also applies to MSN 5178,
ENG SAT ABOVE FLEX TEMP 5234.
ME-70 AU 2 Effectivity update: The information now also applies to MSN 5178,
ENG 1(2) REV INHIBITED 5234. The information no longer applies to MSN 4546.

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LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: AIR AFT CRG VENT FAULT

Ident.: ME-21-00007457.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 21-28-03 AFT Cargo
Extraction Fan

ECAM Alert: AIR COND CTL 1(2)-A(B)

Ident.: ME-21-00007680.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 21-63-04 Air Conditioning
System Controller Channel (COND CTL
1(2)-A(B))

ECAM Alert: AIR PACK 1(2) FAULT

Ident.: ME-21-00007683.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 21-52-01 Air Conditioning
Pack

ECAM Alert: AIR PACK 1+2 FAULT

Ident.: ME-21-00008959.0001001 / 10 OCT 14
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 215201H Air
Conditioning Pack

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LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: AIR PACK 1(2) OFF

Ident.: ME-21-00007685.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 21-52-01 Air Conditioning
Pack

ECAM Alert: AIR PACK 1(2) OVHT

Ident.: ME-21-00007684.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 21-52-01 Air Conditioning
Pack

ECAM Alert: AIR PACK 1(2) REGUL FAULT

Ident.: ME-21-00007687.0002001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

If pack outlet temperature is affected Refer to Item 21-07-01-01 Pack Outlet
Temperature Indication on the BLEED
SD page
............................................................................................................. ................................................................................
If pack compressor outlet temperature is affected Refer to Item 21-07-01-03 Pack
Compressor Outlet Temperature
Indication on the BLEED SD page
............................................................................................................. ................................................................................
If pack flow sensor is affected Refer to Item 21-51-03 Pack Flow
Sensor
............................................................................................................. ................................................................................
If pack flow control valve is affected Refer to Item 21-52-01 Air Conditioning
Pack
............................................................................................................. ................................................................................
If pack ram air inlet is affected Refer to Item 21-52-02 Air Conditioning
Pack Ram Air Inlet Flap
............................................................................................................. ................................................................................
If turbine bypass valve is affected Refer to Item 21-61-01 Pack Turbine
Bypass Valve

LAN COLOMBIA FLEET ME-21 P 2/8

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COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: CAB PR EXCESS CAB ALT

Ident.: ME-21-00007713.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: CAB PR EXCESS RESIDUAL PR

Ident.: ME-21-00007714.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Apply ECAM procedure

ECAM Alert: CAB PR LDG ELEV FAULT

Ident.: ME-21-00007715.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 21-31-04 Landing
Elevation Selection AUTO Function

ECAM Alert: CAB PR LO DIFF PR

Ident.: ME-21-00007716.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: CAB PR OFV NOT OPEN

Ident.: ME-21-00007717.0002001 / 04 OCT 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

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LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: CAB PR SAFETY VALVE OPEN

Ident.: ME-21-00007718.0001001 / 12 SEP 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert Refer to FCOM/PRO-SPO-20-FLIGHT
WITHOUT CABIN PRESSURIZATION
............................................................................................................. ................................................................................
False alert Refer to Item 21-09-03 CAB PR SAFETY
VALVE OPEN Alert

ECAM Alert: CAB PR SYS 1(2) FAULT

Ident.: ME-21-00007719.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 21-31-01 Automatic Cabin
Pressure Control System (CPC, Outflow
Valve AUTO Channel)

ECAM Alert: CAB PR SYS 1+2 FAULT

Ident.: ME-21-00007720.0001001 / 12 SEP 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to FCOM/PRO-SPO-20 Flight
Without Cabin Pressurization

ECAM Alert: COND AFT CAB DUCT OVHT

Ident.: ME-21-00007703.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 21-63-02 Cockpit and
Cabin Trim Air Valve

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LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: COND AFT CRG ISOL VALVE

Ident.: ME-21-00007692.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 21-28-04 AFT Cargo
Isolation Valve

ECAM Alert: COND CKPT DUCT OVHT

Ident.: ME-21-00007697.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 21-63-02 Cockpit and
Cabin Trim Air Valve

ECAM Alert: COND FWD CAB DUCT OVHT

Ident.: ME-21-00007698.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 21-63-02 Cockpit and
Cabin Trim Air Valve

ECAM Alert: COND HOT AIR FAULT

Ident.: ME-21-00007707.0003001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 21-63-03 Hot Air Pressure
Regulating Valve

LAN COLOMBIA FLEET ME-21 P 5/8

MEL Q to T 27 FEB 15
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21 - AIR CONDITIONING
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: COND L+R CAB FAN FAULT

Ident.: ME-21-00007708.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: COND LAV+GALLEY FAN FAULT

Ident.: ME-21-00007709.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 21-23-01 Lavatory and
Galley Extraction Fan

ECAM Alert: COND TRIM AIR SYS FAULT

Ident.: ME-21-00007710.0003001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

If the trim air valves are closed Not related to MEL
............................................................................................................. ................................................................................
If associated with the AFT CAB TRIM VALVE subtitle Refer to Item 21-63-02 Cockpit and
Cabin Trim Air Valve
............................................................................................................. ................................................................................
If associated with the FWD CAB TRIM VALVE subtitle Refer to Item 21-63-02 Cockpit and
Cabin Trim Air Valve
............................................................................................................. ................................................................................
If associated with the CKPT TRIM VALVE subtitle Refer to Item 21-63-02 Cockpit and
Cabin Trim Air Valve
............................................................................................................. ................................................................................
If associated with the TRIM AIR HI PR subtitle Refer to Item 21-63-02 Cockpit and
Cabin Trim Air Valve

LAN COLOMBIA FLEET ME-21 P 6/8

MEL U to W 27 FEB 15
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COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: VENT AVNCS SYS FAULT

Ident.: ME-21-00007721.0001001 / 10 OCT 14
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

If the VENT SKIN VALVE FAULT alert is displayed on Refer to Item 21-26-04 Avionics Skin Air
the EWD due to the Avionics Skin Air Outlet valve. Outlet Valve
............................................................................................................. ................................................................................
If the VENT SKIN VALVE FAULT alert is displayed on Refer to Item 21-26-05 Avionics Skin Air
the EWD due to the Avionics Skin Air Inlet valve. Inlet Valve
............................................................................................................. ................................................................................
NIL Refer to Item 21-26-03 Avionics Skin
Exchanger Inlet Bypass Valve
or
Refer to Item 21-26-07 Avionics Skin
Exchanger Outlet Bypass Valve
or
Refer to Item 21-26-08 Avionics Air
Conditioning Inlet Valve
or
Refer to Item 21-26-06 Avionics Skin
Exchanger Isolation Valve
or
Refer to Item 21-26-10 Avionics
Equipment Ventilation Computer (AEVC)

ECAM Alert: VENT BLOWER FAULT

Ident.: ME-21-00007722.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert Refer to Item 21-26-01 Avionics Blower
Fan
............................................................................................................. ................................................................................
False alert Refer to Item 21-09-01 VENT BLOWER
FAULT Alert

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LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: VENT EXTRACT FAULT

Ident.: ME-21-00007723.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert Refer to Item 21-26-02 Avionics Extract
Fan
............................................................................................................. ................................................................................
False alert Refer to Item 21-09-02 VENT EXTRACT
FAULT Alert

ECAM Alert: VENT SKIN VALVE FAULT

Ident.: ME-21-00007725.0001001 / 12 SEP 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Outlet valve determined faulty on the CAB PRESS SD Refer to Item 21-26-04 Avionics Skin Air
page Outlet Valve
............................................................................................................. ................................................................................
Inlet valve determined faulty on the CAB PRESS SD Refer to Item 21-26-05 Avionics Skin Air
page Inlet Valve

LAN COLOMBIA FLEET ME-21 P 8/8

MEL Z to AA 27 FEB 15
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22 - AUTO FLIGHT
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: AUTO FLT A/THR LIMITED

Ident.: ME-22-00007837.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: AUTO FLT A/THR OFF

Ident.: ME-22-00007838.0001001 / 10 OCT 14
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 22-30-01 Autothrust
(A/THR)

ECAM Alert: AUTO FLT AP OFF

Ident.: ME-22-00007840.0001001 / 18 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert Refer to Item 22-10-01 Autopilot (AP)
............................................................................................................. ................................................................................
False alert Refer to Item 22-10-06 AP
Disengagement Warning

ECAM Alert: AUTO FLT FAC 1 FAULT

Ident.: ME-22-00007841.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 22-60-01 FAC 1

LAN COLOMBIA FLEET ME-22 P 1/4

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COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: AUTO FLT FAC 2 FAULT

Ident.: ME-22-00007842.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 22-60-02 FAC 2

ECAM Alert: AUTO FLT FAC 1+2 FAULT

Ident.: ME-22-00007843.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: AUTO FLT FCU 1(2) FAULT

Ident.: ME-22-00007844.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 22-81-03-01 FCU Channel

ECAM Alert: AUTO FLT FCU 1+2 FAULT

Ident.: ME-22-00007847.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: AUTO FLT REAC W/S DET FAULT

Ident.: ME-22-00007849.0001001 / 18 MAY 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 22-60-03 Reactive
Windshear Detection Function

LAN COLOMBIA FLEET ME-22 P 2/4

MEL E to I 10 OCT 14
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COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: AUTO FLT RUD TRIM 1(2) FAULT

Ident.: ME-22-00007855.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-22-01 Rudder Trim
System

ECAM Alert: AUTO FLT RUD TRIM SYS

Ident.: ME-22-00007856.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: AUTO FLT RUD TRV LIM 1(2)

Ident.: ME-22-00007857.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-23-01 Rudder Travel
Limiter System (Including Rudder and
Pedals Travel Limiter Units)

ECAM Alert: AUTO FLT RUD TRV LIM SYS

Ident.: ME-22-00007858.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-22 P 3/4

MEL J to M 10 OCT 14
 MEL ENTRIES
22 - AUTO FLIGHT
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: AUTO FLT YAW DAMPER 1(2)

Ident.: ME-22-00007859.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 22-60-04 Yaw Damper
System

ECAM Alert: AUTO FLT YAW DAMPER SYS

Ident.: ME-22-00007860.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: WINDSHEAR DET FAULT

Ident.: ME-22-00007861.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 22-60-03 Reactive
Windshear Detection Function

LAN COLOMBIA FLEET ME-22 P 4/4

MEL N to P 10 OCT 14
 MEL ENTRIES
23 - COMMUNICATIONS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: COM ACARS FAULT

Ident.: ME-23-00007862.0002001 / 18 MAY 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 46-21-01 Air Traffic Service
Unit (ATSU)

ECAM Alert: COM CIDS 1+2 FAULT

Ident.: ME-23-00007864.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: COM HF 1(2) DATA FAULT

Ident.: ME-23-00007867.0004001 / 18 MAY 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 23-10-01 HF System

ECAM Alert: COM HF 1(2) EMITTING

Ident.: ME-23-00007865.0002001 / 14 FEB 13
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

If hand microphone PTT pb is jammed in the transmitting Refer to Item 23-51-03 Hand Microphone
position
............................................................................................................. ................................................................................
If sidestick PTT pb is jammed in the transmitting position Refer to Item 23-51-06 Sidestick Radio
selector
............................................................................................................. ................................................................................
If a transmission Key on one ACP is jammed in the Refer to Item 23-52-05 ACP
transmitting position Transmission Key
............................................................................................................. ................................................................................
False alert Refer to Item 23-09-01 COM HF 1(2)
EMITTING Alert

LAN COLOMBIA FLEET ME-23 P 1/2

MEL A to D 27 FEB 15
 MEL ENTRIES
23 - COMMUNICATIONS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: COM SINGLE PTT STUCK

Ident.: ME-23-00014763.0002001 / 27 FEB 15
1 Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

If hand microphone PTT pb is jammed in the transmitting Refer to Item 23-51-03 Hand Microphone
position
............................................................................................................. ................................................................................
If sidestick PTT pb is jammed in the transmitting position Refer to Item 23-51-06 Sidestick Radio
selector
............................................................................................................. ................................................................................
If a transmission Key on one ACP is jammed in the Refer to Item 23-52-05 ACP
transmitting position Transmission Key

ECAM Alert: COM VHF 3 DATA FAULT

Ident.: ME-23-00007872.0004001 / 18 MAY 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 23-10-02 VHF System

ECAM Alert: COM VHF 1(2)(3) EMITTING

Ident.: ME-23-00007871.0001001 / 14 FEB 13
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

If hand microphone PTT pb is jammed in the transmitting Refer to Item 23-51-03 Hand Microphone
position
............................................................................................................. ................................................................................
If sidestick PTT pb is jammed in the transmitting position Refer to Item 23-51-06 Sidestick Radio
selector
............................................................................................................. ................................................................................
If a transmission Key on one ACP is jammed in the Refer to Item 23-52-05 ACP
transmitting position Transmission Key
............................................................................................................. ................................................................................
False alert Refer to Item 23-09-02 COM VHF 1(2)(3)
EMITTING Alert

LAN COLOMBIA FLEET ME-23 P 2/2

MEL E to G 27 FEB 15
 MEL ENTRIES
24 - ELECTRICAL POWER
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: C/B TRIPPED

Ident.: ME-24-00007881.0001001 / 18 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert Refer to affected systems
............................................................................................................. ................................................................................
False alert Refer to Item 24-09-02 C/B TRIPPED
Alert

ECAM Alert: ELEC AC BUS 1 FAULT

Ident.: ME-24-00007873.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ELEC AC BUS 2 FAULT

Ident.: ME-24-00007874.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ELEC AC ESS BUS ALTN

Ident.: ME-24-00010320.0003001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ELEC AC ESS BUS FAULT

Ident.: ME-24-00007875.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-24 P 1/8

MEL A to E 27 FEB 15
 MEL ENTRIES
24 - ELECTRICAL POWER
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ELEC AC ESS BUS SHED

Ident.: ME-24-00007876.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 24-09-01 ELEC AC ESS
BUS SHED Alert

ECAM Alert: ELEC APU GEN FAULT

Ident.: ME-24-00007877.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 24-23-01 AC Auxiliary
Generation (APU Generator, GCU
or GAPCU Auxiliary Power Control
function, Line Contactor)

ECAM Alert: ELEC APU GEN OVERLOAD

Ident.: ME-24-00013870.0001001 / 12 SEP 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 24-26-01 Galley Automatic
Load Shed System

ECAM Alert: ELEC BAT 1(2) FAULT

Ident.: ME-24-00007878.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-24 P 2/8

MEL F to I 27 FEB 15
 MEL ENTRIES
24 - ELECTRICAL POWER
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ELEC BAT 1(2) OFF

Ident.: ME-24-00007879.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: ELEC BCL 1(2) FAULT

Ident.: ME-24-00007880.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 24-38-02 Battery Charger
Limiter (BCL)

ECAM Alert: ELEC DC BAT BUS FAULT

Ident.: ME-24-00007883.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ELEC DC BUS 1 FAULT

Ident.: ME-24-00007886.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ELEC DC BUS 2 FAULT

Ident.: ME-24-00007887.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-24 P 3/8

MEL J to N 27 FEB 15
 MEL ENTRIES
24 - ELECTRICAL POWER
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ELEC DC BUS 1+2 FAULT

Ident.: ME-24-00007884.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ELEC DC EMER CONFIG

Ident.: ME-24-00007888.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ELEC DC ESS BUS FAULT

Ident.: ME-24-00007889.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ELEC DC ESS BUS SHED

Ident.: ME-24-00007891.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ELEC EMER CONFIG

Ident.: ME-24-00007892.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-24 P 4/8

MEL O to S 27 FEB 15
 MEL ENTRIES
24 - ELECTRICAL POWER
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ELEC EMER GEN 1 LINE OFF

Ident.: ME-24-00007894.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: ELEC ESS BUSSES ON BAT

Ident.: ME-24-00007895.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ELEC GEN 1(2) FAULT

Ident.: ME-24-00007905.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 24-22-01 AC Main
Generation (IDG, GCU, Line Contactor)

ECAM Alert: ELEC GEN 1(2) OFF

Ident.: ME-24-00007906.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: ELEC GEN 1(2)OVERLOAD

Ident.: ME-24-00007907.0001001 / 31 MAY 12
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 24-26-01 Galley Automatic
Load Shed System

LAN COLOMBIA FLEET ME-24 P 5/8

MEL T to X 27 FEB 15
 MEL ENTRIES
24 - ELECTRICAL POWER
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ELEC IDG 1(2) DISCONNECTED

Ident.: ME-24-00010319.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 24-22-01 AC Main
Generation (IDG, GCU, Line Contactor)

ECAM Alert: ELEC IDG 1(2) OIL LO PR

Ident.: ME-24-00007908.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 24-22-01 AC Main
Generation (IDG, GCU, Line Contactor)

ECAM Alert: ELEC IDG 1(2) OIL OVHT

Ident.: ME-24-00007909.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 24-22-01 AC Main
Generation (IDG, GCU, Line Contactor)

ECAM Alert: ELEC STATIC INV FAULT

Ident.: ME-24-00007910.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-24 P 6/8

MEL Y to AB 27 FEB 15
 MEL ENTRIES
24 - ELECTRICAL POWER
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ELEC TR 1(2) FAULT

Ident.: ME-24-00007911.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 24-32-01 DC Main
Generation (TR 1, TR 2)

LAN COLOMBIA FLEET ME-24 P 7/8

MEL AC 27 FEB 15
 MEL ENTRIES
24 - ELECTRICAL POWER
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET ME-24 P 8/8

MEL 27 FEB 15
 MEL ENTRIES
26 - FIRE PROTECTION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: APU FIRE

Ident.: ME-26-00007941.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 49-10-01 Power Plant
(APU)

ECAM Alert: APU FIRE DET FAULT

Ident.: ME-26-00007939.0001001 / 12 SEP 12
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 26-13-01 APU Fire
Detection Loop

ECAM Alert: APU FIRE LOOP A(B) FAULT

Ident.: ME-26-00007940.0001001 / 12 SEP 12
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 26-13-01 APU Fire
Detection Loop

ECAM Alert: AVIONICS SMOKE

Ident.: ME-26-00007920.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 26-15-01 Avionics Smoke
Detection System

LAN COLOMBIA FLEET ME-26 P 1/6

MEL A to D 27 FEB 15
 MEL ENTRIES
26 - FIRE PROTECTION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ENG 1(2) FIRE

Ident.: ME-26-00007938.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) FIRE DET FAULT

Ident.: ME-26-00007935.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) FIRE LOOP A FAULT

Ident.: ME-26-00007936.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

If engine 1 is affected Refer to Item 26-12-01 Engine Fire
Detection Loop A on the Engine 1
............................................................................................................. ................................................................................
If engine 2 is affected Refer to Item 26-12-02 Engine Fire
Detection Loop A on the Engine 2

ECAM Alert: ENG 1(2) FIRE LOOP B FAULT

Ident.: ME-26-00007937.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

If engine 1 is affected Refer to Item 26-12-03 Engine Fire
Detection Loop B on the Engine 1
............................................................................................................. ................................................................................
If engine 2 is affected Refer to Item 26-12-04 Engine Fire
Detection Loop B on the Engine 2

LAN COLOMBIA FLEET ME-26 P 2/6

MEL E to H 27 FEB 15
 MEL ENTRIES
26 - FIRE PROTECTION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: SMOKE AFT CARGO SMOKE

Ident.: ME-26-00007914.0001001 / 12 SEP 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: SMOKE AFT CRG BTL FAULT

Ident.: ME-26-00007916.0019001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

If the SMOKE FWD CRG BTL FAULT alert is not Refer to Item 26-23-02 Squib of the
displayed on the EWD Cargo Bottle 1
............................................................................................................. ................................................................................
If the SMOKE FWD CRG BTL FAULT alert is displayed Refer to Item 26-23-01 Cargo Agent
on the EWD Bottle

ECAM Alert: SMOKE AFT CRG DET FAULT

Ident.: ME-26-00007919.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 26-16-02 Smoke Detector
in the AFT and the BULK Cargo
Compartments

ECAM Alert: SMOKE FWD CARGO SMOKE

Ident.: ME-26-00007922.0001001 / 12 SEP 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-26 P 3/6

MEL I to L 27 FEB 15
 MEL ENTRIES
26 - FIRE PROTECTION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: SMOKE FWD CRG BTL FAULT

Ident.: ME-26-00007923.0019001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

If the SMOKE AFT CRG BTL FAULT alert is not Refer to Item 26-23-02 Squib of the
displayed on the EWD Cargo Bottle 1
............................................................................................................. ................................................................................
If the SMOKE AFT CRG BTL FAULT alert is displayed Refer to Item 26-23-01 Cargo Agent
on the EWD Bottle

ECAM Alert: SMOKE FWD CRG DET FAULT

Ident.: ME-26-00007925.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 26-16-01 Smoke Detector
in the FWD Cargo Compartment

ECAM Alert: SMOKE DET FAULT

Ident.: ME-26-00007926.0004001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 23-73-10-01 Smoke
Detection Function (CIDS-SDF)

ECAM Alert: SMOKE LAVATORY DET FAULT

Ident.: ME-26-00007928.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 26-17-01 Lavatory Smoke
Detection System

LAN COLOMBIA FLEET ME-26 P 4/6

MEL M to P 27 FEB 15
 MEL ENTRIES
26 - FIRE PROTECTION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: SMOKE LAVATORY SMOKE

Ident.: ME-26-00007930.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 26-17-01 Lavatory Smoke
Detection System

LAN COLOMBIA FLEET ME-26 P 5/6

MEL Q 27 FEB 15
 MEL ENTRIES
26 - FIRE PROTECTION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET ME-26 P 6/6

MEL 27 FEB 15
 MEL ENTRIES
27 - FLIGHT CONTROLS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: CONFIG L(R) SIDESTICK FAULT

Ident.: ME-27-00007983.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: CONFIG PITCH TRIM NOT IN T.O. RANGE

Ident.: ME-27-00007984.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: CONFIG RUD TRIM NOT IN T.O. RANGE

Ident.: ME-27-00007985.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: CONFIG SLATS(FLAPS) NOT IN T.O. CONFIG.

Ident.: ME-27-00007986.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: CONFIG SPEED BRK NOT RETRACTED

Ident.: ME-27-00007987.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-27 P 1/12

MEL A to E 27 FEB 15
 MEL ENTRIES
27 - FLIGHT CONTROLS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: F/CTL AIL SERVO FAULT

Ident.: ME-27-00007942.0001001 / 17 SEP 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-14-01 Left Aileron Blue
Servo-Control (Controlled by ELAC 1)
or
Refer to Item 27-14-02 Left Aileron
Green Servo-Control (Controlled by
ELAC 2)
or
Refer to Item 27-14-03 Right Aileron
Green Servo-Control (Controlled by
ELAC 1)
or
Refer to Item 27-14-04 Right Aileron
Blue Servo-Control (Controlled by ELAC
2)

ECAM Alert: F/CTL ALTN LAW

Ident.: ME-27-00007943.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: F/CTL DIRECT LAW

Ident.: ME-27-00007944.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-27 P 2/12

MEL F to H 27 FEB 15
 MEL ENTRIES
27 - FLIGHT CONTROLS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: F/CTL ELAC 1 FAULT

Ident.: ME-27-00007946.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-93-01 ELAC 1

ECAM Alert: F/CTL ELAC 1 PITCH FAULT

Ident.: ME-27-00007945.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-93-01 ELAC 1

ECAM Alert: F/CTL ELAC 2 FAULT

Ident.: ME-27-00007948.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: F/CTL ELAC 2 PITCH FAULT

Ident.: ME-27-00007947.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: F/CTL ELEV SERVO FAULT

Ident.: ME-27-00007949.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

If the servo-control is affected. NO DISPATCH
............................................................................................................. ................................................................................
If the servo-control position transducer is affected. Refer to Item 27-34-02 Elevator
Servo-Control Position Transducer

LAN COLOMBIA FLEET ME-27 P 3/12

MEL I to M 27 FEB 15
 MEL ENTRIES
27 - FLIGHT CONTROLS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: F/CTL FCDC 1 FAULT

Ident.: ME-27-00007950.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: F/CTL FCDC 2 FAULT

Ident.: ME-27-00007951.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-95-02 FCDC 2

ECAM Alert: F/CTL FCDC 1+2 FAULT

Ident.: ME-27-00007952.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: F/CTL FLAP ATTACH SENSOR

Ident.: ME-27-00007953.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: F/CTL FLAP LVR NOT ZERO

Ident.: ME-27-00007954.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

LAN COLOMBIA FLEET ME-27 P 4/12

MEL N to R 27 FEB 15
 MEL ENTRIES
27 - FLIGHT CONTROLS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: F/CTL FLAP SYS 1 FAULT

Ident.: ME-27-00007955.0001001 / 20 JUN 14
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH
............................................................................................................. ................................................................................
If the maintenance check confirms that the F/CTL FLAP Refer to Item 27-54-01 Flap Hydraulic
SYS 1 FAULT alert is displayed on the EWD due to a Motor
flap motor failure

ECAM Alert: F/CTL FLAP SYS 2 FAULT

Ident.: ME-27-00007956.0001001 / 20 JUN 14
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-51-01 SFCC Flap
Channel
............................................................................................................. ................................................................................
If the maintenance check confirms that the F/CTL FLAP Refer to Item 27-54-01 Flap Hydraulic
SYS 2 FAULT alert is displayed on the EWD due to a Motor
flap motor failure.

ECAM Alert: F/CTL FLAP TIP BRK FAULT

Ident.: ME-27-00007957.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-51-03 Flap Wing Tip
Brakes Solenoid

ECAM Alert: F/CTL FLAPS(SLATS) FAULT

Ident.: ME-27-00007958.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-27 P 5/12

MEL S to V 27 FEB 15
 MEL ENTRIES
27 - FLIGHT CONTROLS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: F/CTL FLAPS(SLATS) LOCKED

Ident.: ME-27-00007959.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: F/CTL GND SPLR FAULT

Ident.: ME-27-00007961.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

If the braking system is affected Refer to Item 32-42-06 Tachometer
............................................................................................................. ................................................................................
If the braking system is not affected Refer to Item 27-92-02 Ground Spoiler
Control System

ECAM Alert: F/CTL GND SPLR (1+2)(3+4) FAULT

Ident.: ME-27-00007960.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-92-02 Ground Spoiler
Control System

ECAM Alert: F/CTL GND SPLR 5 FAULT

Ident.: ME-27-00014417.0001001 / 27 FEB 15
1 Applicable to: MSN 4516-4758, 4972-5178, 5234

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-92-02 Ground Spoiler
Control System

LAN COLOMBIA FLEET ME-27 P 6/12

MEL W to Z 27 FEB 15
 MEL ENTRIES
27 - FLIGHT CONTROLS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: F/CTL GND SPLR NOT ARMED

Ident.: ME-27-00014419.0001001 / 27 FEB 15
2 Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

Ground spoilers are not armed while on approach below Not related to MEL
500 ft (150 m) AGL with the landing gears down.

ECAM Alert: F/CTL L(R) AIL FAULT

Ident.: ME-27-00007964.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: F/CTL L(R) ELEV FAULT

Ident.: ME-27-00007965.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: F/CTL L+R ELEV FAULT

Ident.: ME-27-00007963.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: F/CTL L(R) SIDESTICK FAULT

Ident.: ME-27-00007966.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-27 P 7/12

MEL AA to AE 27 FEB 15
 MEL ENTRIES
27 - FLIGHT CONTROLS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: F/CTL PITCH TRIM/MCDU/CG DISAGREE

Ident.: ME-27-00014418.0001001 / 27 FEB 15
3 Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: F/CTL SEC 1 FAULT

Ident.: ME-27-00007967.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-94-01 SEC 1

ECAM Alert: F/CTL SEC 2 FAULT

Ident.: ME-27-00007968.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-94-02 SEC 2

ECAM Alert: F/CTL SEC 3 FAULT

Ident.: ME-27-00007969.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-94-03 SEC 3

ECAM Alert: F/CTL SIDESTICK PRIORITY

Ident.: ME-27-00007970.0001001 / 19 OCT 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to FCOM/ F/CTL SIDESTICK
PRIORITY

LAN COLOMBIA FLEET ME-27 P 8/12

MEL AF to AJ 27 FEB 15
 MEL ENTRIES
27 - FLIGHT CONTROLS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: F/CTL SLAT SYS 1 FAULT

Ident.: ME-27-00007971.0001001 / 20 JUN 14
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH
............................................................................................................. ................................................................................
If the maintenance check confirms the F/CTL SLAT SYS Refer to Item 27-84-01 Slats Hydraulic
1 FAULT alert is displayed on the EWD due to a slat Motor
motor failure.

ECAM Alert: F/CTL SLAT SYS 2 FAULT

Ident.: ME-27-00007972.0001001 / 20 JUN 14
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-51-02 SFCC Slat
Channel
............................................................................................................. ................................................................................
If the maintenance check confirms the F/CTL SLAT SYS Refer to Item 27-84-01 Slats Hydraulic
2 FAULT alert is displayed on the EWD due to a slat Motor
motor failure.

ECAM Alert: F/CTL SLAT TIP BRK FAULT

Ident.: ME-27-00007973.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-81-01 Slat Wing Tip
Brakes Solenoid

ECAM Alert: F/CTL SPD BRK DISAGREE

Ident.: ME-27-00007976.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-92-01 Speedbrake
Control System

LAN COLOMBIA FLEET ME-27 P 9/12

MEL AK to AN 27 FEB 15
 MEL ENTRIES
27 - FLIGHT CONTROLS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: F/CTL SPD BRK FAULT

Ident.: ME-27-00007977.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-92-01 Speedbrake
Control System

ECAM Alert: F/CTL SPD BRK STILL OUT

Ident.: ME-27-00007978.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: F/CTL SPD BRK 2(3+4) FAULT

Ident.: ME-27-00007975.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-92-01 Speedbrake
Control System

LAN COLOMBIA FLEET ME-27 P 10/12

MEL AO to AQ 27 FEB 15
 MEL ENTRIES
27 - FLIGHT CONTROLS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: F/CTL SPLR FAULT

Ident.: ME-27-00007979.0001001 / 31 MAY 12
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 27-64-01 Spoiler 5
or
Refer to Item 27-64-02 Spoiler 1 or 3
or
Refer to Item 27-64-03 Spoiler 2 or 4
or
Refer to Item 27-64-04 Spoilers 1 and 2
or
Refer to Item 27-64-05 Spoilers 3 and 4

ECAM Alert: F/CTL STABILIZER JAM

Ident.: ME-27-00007980.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-27 P 11/12

MEL AR to AS 27 FEB 15
 MEL ENTRIES
27 - FLIGHT CONTROLS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET ME-27 P 12/12

MEL 27 FEB 15
 MEL ENTRIES
28 - FUEL
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: FUEL APU LP VALVE FAULT

Ident.: ME-28-00007992.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 28-29-01 APU LP Fuel
Valve

ECAM Alert: FUEL AUTO FEED FAULT

Ident.: ME-28-00007993.0002001 / 10 OCT 14
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 28-20-01 Automatic Fuel
Feed System

ECAM Alert: FUEL CTR TK PUMP 1(2) LO PR

Ident.: ME-28-00007995.0003001 / 10 OCT 14
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 28-21-02 Center Tank
Pump/Transfer Valve

ECAM Alert: FUEL CTR TK PUMPS LO PR

Ident.: ME-28-00007996.0003001 / 10 OCT 14
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 28-21-02 Center Tank
Pump/Transfer Valve

LAN COLOMBIA FLEET ME-28 P 1/6

MEL A to D 27 FEB 15
 MEL ENTRIES
28 - FUEL
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: FUEL CTR TK PUMPS OFF

Ident.: ME-28-00007997.0002001 / 10 OCT 14
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: FUEL ENG 1(2) LP VALVE OPEN

Ident.: ME-28-00007998.0001001 / 12 SEP 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 28-07-04-01 Engine LP
Fuel Valve Indication on the FUEL SD
page

ECAM Alert: FUEL FQI CH 1(2) FAULT

Ident.: ME-28-00008000.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 28-50-01 Fuel Quantity
Indicating Computer (FQIC) Channel

ECAM Alert: FUEL F.USED/FOB DISAGREE

Ident.: ME-28-00008001.0001001 / 27 FEB 15
Applicable to: MSN 5364-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

LAN COLOMBIA FLEET ME-28 P 2/6

MEL E to H 27 FEB 15
 MEL ENTRIES
28 - FUEL
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: FUEL L(R) INNER(OUTER) TK HI TEMP

Ident.: ME-28-00008003.0001001 / 10 OCT 14
Applicable to: MSN 4758-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert Dispatch possible only if delay T.O is
not displayed on ECAM .
............................................................................................................. ................................................................................
False alert Refer to Item 28-09-01 FUEL L(R)
INNER(OUTER)/WING TK HI TEMP
Alert

ECAM Alert: FUEL L(R) INNER(OUTER) TK HI TEMP

Ident.: ME-28-00008003.0002001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 28-09-01 FUEL L(R)
INNER(OUTER)/WING TK HI TEMP
Alert

ECAM Alert: FUEL L(R) INNER(OUTER) TK LO TEMP

Ident.: ME-28-00008004.0001001 / 10 OCT 14
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 28-09-02 FUEL L(R)
INNER(OUTER)/WING TK LO TEMP
Alert

LAN COLOMBIA FLEET ME-28 P 3/6

MEL I to J 27 FEB 15
 MEL ENTRIES
28 - FUEL
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: FUEL L(R) OUTER XFR CLOSED

Ident.: ME-28-00014884.0006001 / 27 FEB 15
1 Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 28-15-01 LH Wing Transfer
Valve
or
Refer to Item 28-15-02 RH Wing
Transfer Valve

ECAM Alert: FUEL L(R) OUTER XFR OPEN

Ident.: ME-28-00014885.0006001 / 27 FEB 15
2 Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 28-15-01 LH Wing Transfer
Valve
or
Refer to Item 28-15-02 RH Wing
Transfer Valve

ECAM Alert: FUEL L(R) TK PUMP 1(2) LO PR

Ident.: ME-28-00008006.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 28-21-01 Wing Tank Pump

ECAM Alert: FUEL L(R) TK PUMP 1+2 LO PR

Ident.: ME-28-00008005.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-28 P 4/6

MEL K to N 27 FEB 15
 MEL ENTRIES
28 - FUEL
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: FUEL L(R) WING TK LO LVL

Ident.: ME-28-00008007.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 28-46-04 Low Level
Detection System in the Inner/Wing Tank

ECAM Alert: FUEL L+R WING TK LO LVL

Ident.: ME-28-00008002.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: FUEL L(R) XFR VALVE CLOSED

Ident.: ME-28-00008009.0001001 / 27 FEB 15
3 Applicable to: MSN 4892-4943, 5229, 5263-5364

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 28-15-01 LH Wing Transfer
Valve
or
Refer to Item 28-15-02 RH Wing
Transfer Valve

LAN COLOMBIA FLEET ME-28 P 5/6

MEL O to Q 27 FEB 15
 MEL ENTRIES
28 - FUEL
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: FUEL L(R) XFR VALVE OPEN

Ident.: ME-28-00008010.0001001 / 27 FEB 15
4 Applicable to: MSN 4892-4943, 5229, 5263-5364

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 28-15-01 LH Wing Transfer
Valve
or
Refer to Item 28-15-02 RH Wing
Transfer Valve

ECAM Alert: FUEL X FEED VALVE FAULT

Ident.: ME-28-00008012.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-28 P 6/6

MEL R to S 27 FEB 15
 MEL ENTRIES
29 - HYDRAULIC POWER
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: HYD B ELEC PUMP LO PR

Ident.: ME-29-00008021.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-01 HYD B(Y) ELEC
PUMP LO PR Alert

ECAM Alert: HYD B ELEC PUMP OVHT

Ident.: ME-29-00008022.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-02 HYD B(Y) ELEC
PUMP OVHT Alert

ECAM Alert: HYD B RSVR LO AIR PR

Ident.: ME-29-00008023.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-04 HYD G(B)(Y)
RSVR LO AIR PR Alert

ECAM Alert: HYD B RSVR LO LVL

Ident.: ME-29-00008025.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-05 HYD G(B)(Y)
RSVR LO LVL Alert

LAN COLOMBIA FLEET ME-29 P 1/6

MEL A to D 05 NOV 13
 MEL ENTRIES
29 - HYDRAULIC POWER
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: HYD B RSVR OVHT

Ident.: ME-29-00008026.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-06 HYD G(B)(Y)
RSVR OVHT Alert

ECAM Alert: HYD B SYS LO PR

Ident.: ME-29-00008027.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-09 HYD G(B)(Y)(B
+G)(G+Y)(B+Y) SYS LO PR Alert

ECAM Alert: HYD B+G SYS LO PR

Ident.: ME-29-00008028.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-09 HYD G(B)(Y)(B
+G)(G+Y)(B+Y) SYS LO PR Alert

ECAM Alert: HYD B+Y SYS LO PR

Ident.: ME-29-00008029.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-09 HYD G(B)(Y)(B
+G)(G+Y)(B+Y) SYS LO PR Alert

LAN COLOMBIA FLEET ME-29 P 2/6

MEL E to H 05 NOV 13
 MEL ENTRIES
29 - HYDRAULIC POWER
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: HYD G ENG 1 PUMP LO PR

Ident.: ME-29-00008030.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-03 HYD G(Y) ENG
1(2) PUMP LO PR Alert

ECAM Alert: HYD G RSVR LO AIR PR

Ident.: ME-29-00008032.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-04 HYD G(B)(Y)
RSVR LO AIR PR Alert

ECAM Alert: HYD G RSVR LO LVL

Ident.: ME-29-00008033.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-05 HYD G(B)(Y)
RSVR LO LVL Alert

ECAM Alert: HYD G RSVR OVHT

Ident.: ME-29-00008035.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-06 HYD G(B)(Y)
RSVR OVHT Alert

LAN COLOMBIA FLEET ME-29 P 3/6

MEL I to L 05 NOV 13
 MEL ENTRIES
29 - HYDRAULIC POWER
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: HYD G SYS LO PR

Ident.: ME-29-00008036.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-09 HYD G(B)(Y)(B
+G)(G+Y)(B+Y) SYS LO PR Alert

ECAM Alert: HYD G+Y SYS LO PR

Ident.: ME-29-00008037.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-09 HYD G(B)(Y)(B
+G)(G+Y)(B+Y) SYS LO PR Alert

ECAM Alert: HYD PTU FAULT

Ident.: ME-29-00008038.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-07 HYD PTU FAULT
Alert

ECAM Alert: HYD RAT FAULT

Ident.: ME-29-00008039.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-08 HYD RAT FAULT
Alert

LAN COLOMBIA FLEET ME-29 P 4/6

MEL M to P 05 NOV 13
 MEL ENTRIES
29 - HYDRAULIC POWER
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: HYD Y ELEC PUMP LO PR

Ident.: ME-29-00008040.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert Refer to Item 29-24-01 Yellow System
Electric Pump
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-01 HYD B(Y) ELEC
PUMP LO PR Alert

ECAM Alert: HYD Y ELEC PUMP OVHT

Ident.: ME-29-00008041.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert Refer to Item 29-24-01 Yellow System
Electric Pump
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-02 HYD B(Y) ELEC
PUMP OVHT Alert

ECAM Alert: HYD Y ENG 2 PUMP LO PR

Ident.: ME-29-00008043.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-03 HYD G(Y) ENG
1(2) PUMP LO PR Alert

ECAM Alert: HYD Y RSVR LO AIR PR

Ident.: ME-29-00008044.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
Continued on the following page

LAN COLOMBIA FLEET ME-29 P 5/6

MEL Q to T 05 NOV 13
 MEL ENTRIES
29 - HYDRAULIC POWER
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

AIRCRAFT STATUS CONDITION OF DISPATCH
False alert Refer to Item 29-09-04 HYD G(B)(Y)
RSVR LO AIR PR Alert

ECAM Alert: HYD Y RSVR LO LVL

Ident.: ME-29-00008045.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-05 HYD G(B)(Y)
RSVR LO LVL Alert

ECAM Alert: HYD Y RSVR OVHT

Ident.: ME-29-00008046.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-06 HYD G(B)(Y)
RSVR OVHT Alert

ECAM Alert: HYD Y SYS LO PR

Ident.: ME-29-00008047.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 29-09-09 HYD G(B)(Y)(B
+G)(G+Y)(B+Y) SYS LO PR Alert

LAN COLOMBIA FLEET ME-29 P 6/6

MEL T to W 05 NOV 13
 MEL ENTRIES
30 - ICE AND RAIN PROTECTION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ANTI ICE ALL PITOT

Ident.: ME-30-00008053.0002001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ANTI ICE CAPT(F/O)(STBY) AOA

Ident.: ME-30-00008054.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 30-31-04 Angle of Attack
(AOA) Probe Heating

ECAM Alert: ANTI ICE CAPT(F/O)(STBY) L(R) STAT

Ident.: ME-30-00008056.0001001 / 31 MAY 12
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 30-31-03 Static Ports
Heater

ECAM Alert: ANTI ICE CAPT(F/O)(STBY) PITOT

Ident.: ME-30-00008058.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 30-31-02 Pitot Heater

ECAM Alert: ANTI ICE CAPT+F/O PITOT

Ident.: ME-30-00008059.0002001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-30 P 1/6

MEL A to E 27 FEB 15
 MEL ENTRIES
30 - ICE AND RAIN PROTECTION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ANTI ICE CAPT+STBY PITOT

Ident.: ME-30-00008060.0002001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ANTI ICE CAPT(F/O)(STBY) PROBES

Ident.: ME-30-00008062.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 30-31-01 Probe Heat
Computer (PHC)

ECAM Alert: ANTI ICE CAPT(F/O) TAT

Ident.: ME-30-00008064.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 30-31-05 TAT Probe
Heating

ECAM Alert: ANTI ICE DETECT FAULT

Ident.: ME-30-00008065.0002001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 30-81-01 Ice Detection
System

LAN COLOMBIA FLEET ME-30 P 2/6

MEL F to I 27 FEB 15
 MEL ENTRIES
30 - ICE AND RAIN PROTECTION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ANTI ICE ENG 1(2) VALVE CLSD

Ident.: ME-30-00008068.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 30-21-01 Engine Anti-Ice
Valve

ECAM Alert: ANTI ICE ENG 1(2) VALVE OPEN

Ident.: ME-30-00008070.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 30-21-01 Engine Anti-Ice
Valve

ECAM Alert: ANTI ICE F/O+STBY PITOT

Ident.: ME-30-00008071.0002001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ANTI ICE ICE DETECTED

Ident.: ME-30-00008073.0002001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: ANTI ICE L(R) WINDOW

Ident.: ME-30-00008089.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

If the Window Heat Computer is affected Refer to Item 30-42-01 Window Heat
Computer
............................................................................................................. ................................................................................
Continued on the following page

LAN COLOMBIA FLEET ME-30 P 3/6

MEL J to N 27 FEB 15
 MEL ENTRIES
30 - ICE AND RAIN PROTECTION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

AIRCRAFT STATUS CONDITION OF DISPATCH
NIL Refer to Item 30-42-02 Fixed Lateral
Window and Sliding Window Heating

ECAM Alert: ANTI ICE L(R) WINDSHIELD

Ident.: ME-30-00008096.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

If the Window Heat Computer is affected Refer to Item 30-42-01 Window Heat
Computer
............................................................................................................. ................................................................................
NIL Refer to Item 30-42-03 Windshield
Heating

ECAM Alert: ANTI ICE L+R WINDSHIELD

Ident.: ME-30-00008075.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: SEVERE ICE DETECTED

Ident.: ME-30-00008097.0002001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

LAN COLOMBIA FLEET ME-30 P 4/6

MEL N to Q 27 FEB 15
 MEL ENTRIES
30 - ICE AND RAIN PROTECTION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: WING ANTI ICE L(R) HI PR

Ident.: ME-30-00008098.0001001 / 17 SEP 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 30-11-01B Wing Anti-Ice
Control Valve

ECAM Alert: WING ANTI ICE L(R) VALVE OPEN

Ident.: ME-30-00008099.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 30-11-01 Wing Anti-Ice
Control Valve

ECAM Alert: WING ANTI ICE OPEN ON GND

Ident.: ME-30-00008100.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 30-11-01 Wing Anti-Ice
Control Valve

ECAM Alert: WING ANTI ICE SYS FAULT

Ident.: ME-30-00008101.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 30-11-01 Wing Anti-Ice
Control Valve

LAN COLOMBIA FLEET ME-30 P 5/6

MEL R to U 27 FEB 15
 MEL ENTRIES
30 - ICE AND RAIN PROTECTION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET ME-30 P 6/6

MEL 27 FEB 15
 MEL ENTRIES
31 - INDICATING/RECORDING SYSTEMS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: EIS DMC 1 FAULT

Ident.: ME-31-00008102.0002001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 31-62-01 DMC 1

ECAM Alert: EIS DMC 2 FAULT

Ident.: ME-31-00008103.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 31-62-02 DMC 2

ECAM Alert: EIS DMC 3 FAULT

Ident.: ME-31-00008104.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 31-62-03 DMC 3

ECAM Alert: EIS DMC/FWC COM FAULT

Ident.: ME-31-00014303.0001001 / 27 FEB 15
1 Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: FWS FWC 1 FAULT

Ident.: ME-31-00008105.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-31 P 1/4

MEL A to E 27 FEB 15
 MEL ENTRIES
31 - INDICATING/RECORDING SYSTEMS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: FWS FWC 2 FAULT

Ident.: ME-31-00008106.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 31-53-01 Flight Warning
Computer (FWC)

ECAM Alert: FWS FWC 1+2 FAULT

Ident.: ME-31-00008107.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: FWS OEB/FWC DISCREPANCY

Ident.: ME-31-00008108.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: FWS SDAC 1 FAULT

Ident.: ME-31-00008109.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: FWS SDAC 2 FAULT

Ident.: ME-31-00008110.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 31-55-01 System Data
Acquisition Concentrator (SDAC)

LAN COLOMBIA FLEET ME-31 P 2/4

MEL F to J 27 FEB 15
 MEL ENTRIES
31 - INDICATING/RECORDING SYSTEMS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: FWS SDAC 1+2 FAULT

Ident.: ME-31-00008111.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: RECORDER DFDR FAULT

Ident.: ME-31-00008112.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 31-30-03 Digital Flight Data
Recorder (DFDR)

ECAM Alert: RECORDER SYS FAULT

Ident.: ME-31-00008113.0002001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 31-30-05 Flight Data
Interface (FDIU or FDIMU Flight Data
Interface function)

LAN COLOMBIA FLEET ME-31 P 3/4

MEL K to M 27 FEB 15
 MEL ENTRIES
31 - INDICATING/RECORDING SYSTEMS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET ME-31 P 4/4

MEL 27 FEB 15
 MEL ENTRIES
32 - LANDING GEAR
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: BRAKES ALTN BRK FAULT

Ident.: ME-32-00008135.0002001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: BRAKES ALTN L(R) RELEASED

Ident.: ME-32-00008138.0002001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: BRAKES A/SKID N/WS FAULT

Ident.: ME-32-00008129.0002001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: BRAKES A/SKID N/WS OFF

Ident.: ME-32-00008131.0002001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: BRAKES AUTO BRK FAULT

Ident.: ME-32-00008132.0002001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 32-42-05 AUTO/BRK
Function

LAN COLOMBIA FLEET ME-32 P 1/8

MEL A to E 27 FEB 15
 MEL ENTRIES
32 - LANDING GEAR
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: BRAKES BRK Y ACCU LO PR

Ident.: ME-32-00008134.0002001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 32-44-02 ACCU PRESS
Indicator

ECAM Alert: BRAKES SYS 1 FAULT

Ident.: ME-32-00008139.0002001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 32-42-03 Braking/Steering
Control Unit (BSCU) Channel 1 / System
1

ECAM Alert: BRAKES SYS 2 FAULT

Ident.: ME-32-00008140.0002001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 32-42-04 Braking/Steering
Control Unit (BSCU) Channel 2 / System
2

ECAM Alert: BRAKES HOT

Ident.: ME-32-00008141.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 32-07-01 Brakes
Temperature Indication on the WHEEL
SD page

LAN COLOMBIA FLEET ME-32 P 2/8

MEL F to I 27 FEB 15
 MEL ENTRIES
32 - LANDING GEAR
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: BRAKES NORM BRK FAULT

Ident.: ME-32-00008136.0002001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: BRAKES NORM+ALT FAULT

Ident.: ME-32-00008137.0002001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: BRAKES PARK BRK FAULT

Ident.: ME-32-00013833.0002001 / 27 FEB 15
1 Applicable to: MSN 4892-4943, 5229, 5263-5364

AIRCRAFT STATUS CONDITION OF DISPATCH

If associated with the BRK PRESS STILL ON subtitle NO DISPATCH
............................................................................................................. ................................................................................
If there is no subtitle Apply ECAM procedure

ECAM Alert: BRAKES PARK BRK FAULT

Ident.: ME-32-00013833.0003001 / 27 FEB 15
2 Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

If associated with the BRK PRESS STILL APPLIED NO DISPATCH
subtitle
............................................................................................................. ................................................................................
If there is no subtitle Apply ECAM procedure

LAN COLOMBIA FLEET ME-32 P 3/8

MEL J to L 27 FEB 15
 MEL ENTRIES
32 - LANDING GEAR
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: BRAKES PARK BRK LO PR

Ident.: ME-32-00013832.0003001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: BRAKES PARK BRK ON

Ident.: ME-32-00008142.0002001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: BRAKES RELEASED

Ident.: ME-32-00008133.0002001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

If green brake supply affected Refer to Item 32-42-02 Green System
Brake
............................................................................................................. ................................................................................
If a tachometer is affected Refer to Item 32-42-06 Tachometer

ECAM Alert: BRAKES-N/WS MINOR FAULT

Ident.: ME-32-00008143.0002001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 32-09-01 WHEEL
BRAKES-N/WS MINOR FAULT Alert

LAN COLOMBIA FLEET ME-32 P 4/8

MEL M to P 27 FEB 15
 MEL ENTRIES
32 - LANDING GEAR
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: CONFIG PARK BRK ON

Ident.: ME-32-00008127.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: L/G DOORS NOT CLOSED

Ident.: ME-32-00008115.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: L/G GEAR NOT DOWN

Ident.: ME-32-00008116.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: L/G GEAR NOT DOWNLOCKED

Ident.: ME-32-00008117.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: L/G GEAR NOT UPLOCKED

Ident.: ME-32-00008118.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

LAN COLOMBIA FLEET ME-32 P 5/8

MEL Q to U 27 FEB 15
 MEL ENTRIES
32 - LANDING GEAR
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: L/G GEAR UPLOCK FAULT

Ident.: ME-32-00008119.0001001 / 17 SEP 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 32-31-02 Landing Gear
Retracting System

ECAM Alert: L/G LGCIU 1 FAULT

Ident.: ME-32-00008120.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: L/G LGCIU 2 FAULT

Ident.: ME-32-00008121.0003001 / 17 SEP 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

If the LGCIU 2 is inoperative Refer to Item 32-31-01 Landing Gear
Control and Interface Unit (LGCIU)
............................................................................................................. ................................................................................
If a RH L/G proximity detector associated with the Refer to Item 32-32-02 LGCIU 2 RH L/G
LGCIU 2 is inoperative: apply the relevant item. Shock Absorber Proximity Detector
or
Refer to Item 32-32-05 LGCIU 2 RH L/G
Down Lock Proximity Detector
or
Refer to Item 32-32-08 LGCIU 2 RH L/G
Up Lock Proximity Detector
or
Refer to Item 32-32-11 LGCIU 2 RH L/G
Doors Open Proximity Detector
or
Refer to Item 32-32-14 LGCIU 2 RH L/G
Doors Closed Proximity Detector
............................................................................................................. ................................................................................
Continued on the following page

LAN COLOMBIA FLEET ME-32 P 6/8

MEL V to X 27 FEB 15
 MEL ENTRIES
32 - LANDING GEAR
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

AIRCRAFT STATUS CONDITION OF DISPATCH
If a LH L/G proximity detector associated with the LGCIU Refer to Item 32-32-03 LGCIU 2 LH L/G
2 is inoperative: apply the relevant item. Shock Absorber Proximity Detector
or
Refer to Item 32-32-06 LGCIU 2 LH L/G
Down Lock Proximity Detector
or
Refer to Item 32-32-09 LGCIU 2 LH L/G
Up Lock Proximity Detector
or
Refer to Item 32-32-12 LGCIU 2 LH L/G
Doors Open Proximity Detector
or
Refer to Item 32-32-15 LGCIU 2 LH L/G
Doors Closed Proximity Detector
............................................................................................................. ................................................................................
If a Nose L/G proximity detector associated with the Refer to Item 32-32-04 LGCIU 2 Nose
LGCIU 2 is inoperative: apply the relevant item. L/G Shock Absorber Proximity Detector
or
Refer to Item 32-32-07 LGCIU 2 Nose
L/G Down Lock Proximity Detector
or
Refer to Item 32-32-10 LGCIU 2 Nose
L/G Up Lock Proximity Detector
or
Refer to Item 32-32-13 LGCIU 2 Nose
L/G Doors Open Proximity Detector
or
Refer to Item 32-32-16 LGCIU 2 Nose
L/G Doors Closed Proximity Detector

ECAM Alert: L/G LGCIU 1+2 FAULT

Ident.: ME-32-00014276.0001001 / 27 FEB 15
3 Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-32 P 7/8

MEL X to Y 27 FEB 15
 MEL ENTRIES
32 - LANDING GEAR
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: L/G SHOCK ABSORBER FAULT

Ident.: ME-32-00008122.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: L/G SYS DISAGREE

Ident.: ME-32-00008123.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: WHEEL HYD SEL FAULT

Ident.: ME-32-00008124.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: WHEEL N/W STRG FAULT

Ident.: ME-32-00008125.0002001 / 18 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 32-51-01 Nose Wheel
Steering Control System

LAN COLOMBIA FLEET ME-32 P 8/8

MEL Z to AC 27 FEB 15
 MEL ENTRIES
34 - NAVIGATION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: NAV ADR 1 FAULT

Ident.: ME-34-00008145.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-10-01 ADR 1

ECAM Alert: NAV ADR 2 FAULT

Ident.: ME-34-00008146.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-10-02 ADR 2

ECAM Alert: NAV ADR 3 FAULT

Ident.: ME-34-00008147.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-10-03 ADR 3

ECAM Alert: NAV ADR(1+2)(1+3)(2+3) FAULT

Ident.: ME-34-00008148.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: NAV ADR 1+2+3 FAULT

Ident.: ME-34-00008149.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-34 P 1/8

MEL A to E 27 FEB 15
 MEL ENTRIES
34 - NAVIGATION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: NAV ALTI DISCREPANCY

Ident.: ME-34-00008150.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-10-01 ADR 1
or
Refer to Item 34-10-02 ADR 2
or
Refer to Item 34-10-03 ADR 3

ECAM Alert: NAV ATC/XPDR 1(2)(1+2) FAULT

Ident.: ME-34-00013848.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-50-01 ATC

ECAM Alert: NAV ATC/XPDR STBY

Ident.: ME-34-00013846.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: NAV ADR DISAGREE

Ident.: ME-34-00008144.0002001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-34 P 2/8

MEL F to I 27 FEB 15
 MEL ENTRIES
34 - NAVIGATION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: NAV ATT DISCREPANCY

Ident.: ME-34-00008151.0001001 / 25 MAY 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-10-04 IR 1
or
Refer to Item 34-10-05 IR 2
or
Refer to Item 34-10-06 IR 3

ECAM Alert: NAV BARO REF DISCREPANCY

Ident.: ME-34-00008152.0001001 / 27 FEB 15
1 Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: NAV CAPT(F/O)(STBY) AOA FAULT

Ident.: ME-34-00010323.0003001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-11-01 Angle of Attack
(AOA) Sensor

ECAM Alert: NAV FM/GPS POS DISAGREE

Ident.: ME-34-00008153.0001001 / 18 MAY 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

LAN COLOMBIA FLEET ME-34 P 3/8

MEL J to M 27 FEB 15
 MEL ENTRIES
34 - NAVIGATION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: NAV GPS 1(2) FAULT

Ident.: ME-34-00008158.0001001 / 18 MAY 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-50-09 Global
Positioning System (GPS)

ECAM Alert: NAV GPWS FAULT

Ident.: ME-34-00008159.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-40-01 Ground Proximity
Warning System (GPWS)/Terrain
Awareness and Warning System
(TAWS)

ECAM Alert: NAV GPWS TERR DET FAULT

Ident.: ME-34-00008160.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-40-01 Ground Proximity
Warning System (GPWS)/Terrain
Awareness and Warning System
(TAWS)

LAN COLOMBIA FLEET ME-34 P 4/8

MEL N to P 27 FEB 15
 MEL ENTRIES
34 - NAVIGATION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: NAV HDG DISCREPANCY

Ident.: ME-34-00008161.0001001 / 25 MAY 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-10-04 IR 1
or
Refer to Item 34-10-05 IR 2
or
Refer to Item 34-10-06 IR 3

ECAM Alert: NAV IAS DISCREPANCY

Ident.: ME-34-00008165.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-10-01 ADR 1
or
Refer to Item 34-10-02 ADR 2
or
Refer to Item 34-10-03 ADR 3

ECAM Alert: NAV ILS 1(2)(1+2) FAULT

Ident.: ME-34-00008166.0004001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-30-04 Instrument
Landing System (ILS)

ECAM Alert: NAV IR DISAGREE

Ident.: ME-34-00008167.0002001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-34 P 5/8

MEL Q to T 27 FEB 15
 MEL ENTRIES
34 - NAVIGATION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: NAV IR NOT ALIGNED

Ident.: ME-34-00008172.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-10-04 IR 1
or
Refer to Item 34-10-05 IR 2
or
Refer to Item 34-10-06 IR 3

ECAM Alert: NAV IR 1 FAULT

Ident.: ME-34-00008168.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-10-04 IR 1

ECAM Alert: NAV IR 2 FAULT

Ident.: ME-34-00008169.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-10-05 IR 2

ECAM Alert: NAV IR 3 FAULT

Ident.: ME-34-00008170.0001001 / 25 MAY 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-10-06 IR 3

LAN COLOMBIA FLEET ME-34 P 6/8

MEL U to X 27 FEB 15
 MEL ENTRIES
34 - NAVIGATION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: NAV IR 1+2(1+3)(2+3) FAULT

Ident.: ME-34-00008171.0001001 / 31 MAY 12
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: NAV LS TUNING DISAGREE

Ident.: ME-34-00008155.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: NAV PRED W/S DET FAULT

Ident.: ME-34-00008157.0001001 / 18 MAY 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-40-06 Predictive
Windshear Detection Function

ECAM Alert: NAV RA DEGRADED

Ident.: ME-34-00010321.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

During the previous flight, both RA s disagreed. If the Refer to Item 34-40-03 Radio Altimeter
RA 1(2) is confirmed faulty by troubleshooting, the radio System
altimeter 1(2) must be considered inoperative.

LAN COLOMBIA FLEET ME-34 P 7/8

MEL Y to AB 27 FEB 15
 MEL ENTRIES
34 - NAVIGATION
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: NAV RA 1(2) FAULT

Ident.: ME-34-00008174.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-40-03 Radio Altimeter
System

ECAM Alert: NAV TCAS FAULT

Ident.: ME-34-00008175.0001001 / 18 MAY 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 34-40-04 Traffic Collision
Avoidance System (TCAS)

ECAM Alert: NAV TCAS STANDBY

Ident.: ME-34-00010322.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: OVERSPEED

Ident.: ME-34-00008176.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

LAN COLOMBIA FLEET ME-34 P 8/8

MEL AC to AF 27 FEB 15
 MEL ENTRIES
36 - PNEUMATIC
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: AIR APU BLEED FAULT

Ident.: ME-36-00008236.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 36-12-02 APU Bleed Valve

ECAM Alert: AIR APU BLEED LEAK

Ident.: ME-36-00008238.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: AIR BLEED 1(2) OFF

Ident.: ME-36-00008244.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 36-11-01 Engine Bleed Air
Supply System

ECAM Alert: AIR ENG HP VALVE FAULT

Ident.: ME-36-00008251.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 36-11-07 Engine Bleed HP
Valve

LAN COLOMBIA FLEET ME-36 P 1/4

MEL A to D 27 FEB 15
 MEL ENTRIES
36 - PNEUMATIC
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: AIR ENG 1(2) BLEED ABNORM PR

Ident.: ME-36-00008246.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 36-11-01 Engine Bleed Air
Supply System

ECAM Alert: AIR ENG 1(2) BLEED FAULT

Ident.: ME-36-00008247.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 36-11-01 Engine Bleed Air
Supply System

ECAM Alert: AIR ENG 1(2) BLEED HI TEMP

Ident.: ME-36-00014305.0001001 / 27 FEB 15
1 Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Apply ECAM procedure.

ECAM Alert: AIR ENG 1(2) BLEED LEAK

Ident.: ME-36-00008248.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 36-22-01 Pylon Leak
Detection System

LAN COLOMBIA FLEET ME-36 P 2/4

MEL E to H 27 FEB 15
 MEL ENTRIES
36 - PNEUMATIC
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: AIR ENG 1(2)(1+2) BLEED LO TEMP

Ident.: ME-36-00008245.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 36-11-04 Engine Bleed
Fan Air Valve

ECAM Alert: AIR ENG 1(2) BLEED NOT CLSD

Ident.: ME-36-00008249.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 36-11-02 Engine Bleed
Valve (PRV)

ECAM Alert: AIR ENG 1(2) LEAK DET FAULT

Ident.: ME-36-00008250.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 36-22-01 Pylon Leak
Detection System

ECAM Alert: AIR L(R) WING LEAK

Ident.: ME-36-00008252.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-36 P 3/4

MEL I to L 27 FEB 15
 MEL ENTRIES
36 - PNEUMATIC
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: AIR L(R) WING LEAK DET FAULT

Ident.: ME-36-00008253.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: AIR X BLEED FAULT

Ident.: ME-36-00008254.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

2 If the automatic control of the crossbleed valve is Refer to Item 36-12-04 Automatic
affected Control of the X Bleed Valve
............................................................................................................. ................................................................................
3 If the manual control of the crossbleed valve is affected Refer to Item 36-12-05 Manual Control of
the X Bleed Valve

ECAM Alert: BLEED MONITORING FAULT

Ident.: ME-36-00008255.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: BLEED MONIT SYS 1(2) FAULT

Ident.: ME-36-00008256.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 36-11-08 Bleed Monitoring
Computer (BMC)

LAN COLOMBIA FLEET ME-36 P 4/4

MEL M to P 27 FEB 15
 MEL ENTRIES
46 - INFORMATION SYSTEMS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: DATA LINK ATC FAULT

Ident.: ME-46-00008259.0005001 / 18 MAY 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 46-21-01 Air Traffic Service
Unit (ATSU)

ECAM Alert: DATA LINK ATSU FAULT

Ident.: ME-46-00008257.0005001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 46-21-01 Air Traffic Service
Unit (ATSU)

ECAM Alert: DATA LINK COMPANY FAULT

Ident.: ME-46-00008258.0005001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 46-21-01 Air Traffic Service
Unit (ATSU)

LAN COLOMBIA FLEET ME-46 P 1/2

MEL A to C 05 NOV 13
 MEL ENTRIES
46 - INFORMATION SYSTEMS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET ME-46 P 2/2

MEL 05 NOV 13
 MEL ENTRIES
47 - INERT GAS SYSTEM
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: FUEL INERTING SYS FAULT

Ident.: ME-47-00014410.0002001 / 27 FEB 15
1 Applicable to: MSN 5178, 5234, 5443-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 47-10-01 Fuel Tank
Inerting System

LAN COLOMBIA FLEET ME-47 P 1/2

MEL A 27 FEB 15
 MEL ENTRIES
47 - INERT GAS SYSTEM
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET ME-47 P 2/2

MEL 27 FEB 15
 MEL ENTRIES
49 - AIRBORNE AUXILIARY POWER
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: APU AUTO(EMER) SHUT DOWN

Ident.: ME-49-00008260.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 49-10-01 Power Plant
(APU)

LAN COLOMBIA FLEET ME-49 P 1/2

MEL A 05 NOV 13
 MEL ENTRIES
49 - AIRBORNE AUXILIARY POWER
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET ME-49 P 2/2

MEL 05 NOV 13
 MEL ENTRIES
52 - DOORS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: DOOR AFT(BULK)(FWD) CARGO

Ident.: ME-52-00008261.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 52-07-05 Cargo Door
Indication on the DOOR/OXY SD page

ECAM Alert: DOOR L(R) AFT AVIONICS

Ident.: ME-52-00008262.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 52-07-06 Avionics
Compartment Access Door Indication on
the DOOR/OXY SD page

ECAM Alert: DOOR L(R) AFT CABIN

Ident.: ME-52-00008264.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 52-07-01 Passenger
Door/Emergency Exit Permanently
Indicated Open on the DOOR/OXY SD
page

ECAM Alert: DOOR L(R) AFT EMER EXIT

Ident.: ME-52-00008266.0002001 / 10 OCT 14
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
Continued on the following page

LAN COLOMBIA FLEET ME-52 P 1/2

MEL A to D 10 OCT 14
 MEL ENTRIES
52 - DOORS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

AIRCRAFT STATUS CONDITION OF DISPATCH
False alert Refer to Item 52-07-03 Overwing
Emergency Exit Permanently Indicated
Open on the DOOR/OXY SD page

ECAM Alert: DOOR L(R) FWD AVIONICS

Ident.: ME-52-00008263.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 52-07-06 Avionics
Compartment Access Door Indication on
the DOOR/OXY SD page

ECAM Alert: DOOR L(R) FWD CABIN

Ident.: ME-52-00008265.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 52-07-01 Passenger
Door/Emergency Exit Permanently
Indicated Open on the DOOR/OXY SD
page

ECAM Alert: DOOR L(R) FWD EMER EXIT

Ident.: ME-52-00008267.0001001 / 10 OCT 14
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 52-07-03 Overwing
Emergency Exit Permanently Indicated
Open on the DOOR/OXY SD page

LAN COLOMBIA FLEET ME-52 P 2/2

MEL D to G 10 OCT 14
 MEL ENTRIES
70 - ENGINE
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ENG COMPRESSOR VANE

Ident.: ME-70-00008404.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG DUAL FAILURE

Ident.: ME-70-00008406.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: ENG THR LEVERS NOT SET

Ident.: ME-70-00008408.0004001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 73-20-01 Flex Takeoff
Mode

ECAM Alert: ENG REV SET

Ident.: ME-70-00008409.0003001 / 23 MAR 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: ENG SAT ABOVE FLEX TEMP

Ident.: ME-70-00014248.0003001 / 27 FEB 15
1 Applicable to: MSN 5178, 5234, 5443-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Apply ECAM procedure

LAN COLOMBIA FLEET ME-70 P 1/14

MEL A to E 27 FEB 15
 MEL ENTRIES
70 - ENGINE
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ENG THRUST LOCKED

Ident.: ME-70-00008411.0001001 / 18 MAY 11
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: ENG TYPE DISAGREE

Ident.: ME-70-00008415.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG VIB SYS FAULT

Ident.: ME-70-00008416.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 77-07-02-05 N1 Vibration
Indication on the ENGINE SD page
or
Refer to Item 77-07-02-06 N2 Vibration
Indication on the ENGINE SD page

ECAM Alert: ENG 1(2) A/C FADEC SUPPLY

Ident.: ME-70-00008284.0001001 / 27 FEB 15
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 73-20-06 EEC ACFT 28V
Power Supply

LAN COLOMBIA FLEET ME-70 P 2/14

MEL F to I 27 FEB 15
 MEL ENTRIES
70 - ENGINE
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ENG 1(2) AIR EXCHANGR FAULT

AIR VALVE CLOSED
Ident.: ME-70-00008285.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) AIR EXCHANGR FAULT

AIR VALVE OPEN
Ident.: ME-70-00008289.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 79-20-01 Air Cooled Oil
Cooler (ACOC) Modulating Valve

ECAM Alert: ENG 1(2) BEARING 4 OIL SYS

HI PRESS
Ident.: ME-70-00008299.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) BEARING 4 OIL SYS

SCAVENGE VALVE FAULT
Ident.: ME-70-00008292.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 79-09-03 ENG 1(2)
BEARING 4 OIL SYS Alert

LAN COLOMBIA FLEET ME-70 P 3/14

MEL J to M 27 FEB 15
 MEL ENTRIES
70 - ENGINE
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ENG 1(2) BLEED STATUS FAULT

Ident.: ME-70-00008302.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

If this alert is displayed on the EWD before the first Apply ECAM procedure.
engine start, check that no amber cross is displayed
on the ENG SD page for OIL TEMP indication of
the affected engine. If an amber cross is displayed,
the associated EIU may be the cause of the failure
(associated engine start not possible).

ECAM Alert: ENG 1(2) COMPRESSOR VANE

Ident.: ME-70-00008303.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) CTL VALVE FAULT

Ident.: ME-70-00008305.0003001 / 27 FEB 15
Applicable to: MSN 4758-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) EGT(FF)(N1)(N2) DISCREPANCY

Ident.: ME-70-00008311.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-70 P 4/14

MEL N to Q 27 FEB 15
 MEL ENTRIES
70 - ENGINE
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ENG 1(2) EGT(EPR)(FF)(N1)(N2) DISCREPANCY

Ident.: ME-70-00008311.0002001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) EGT EXCEEDED DURING AIR START

Ident.: ME-70-00008306.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) EIU FAULT

Ident.: ME-70-00008308.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) EPR MODE FAULT

Ident.: ME-70-00008310.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 73-20-04 EPR Control
Mode

ECAM Alert: ENG 1(2) FADEC A(B) FAULT

Ident.: ME-70-00008313.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-70 P 5/14

MEL R to V 27 FEB 15
 MEL ENTRIES
70 - ENGINE
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ENG 1(2) FADEC ALTERNATOR

Ident.: ME-70-00008315.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) FADEC FAULT

Ident.: ME-70-00008317.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) FADEC HI TEMP

Ident.: ME-70-00008319.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) FADEC OVHT

Ident.: ME-70-00008319.0003001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) FADEC PLUG FAULT

Ident.: ME-70-00008320.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-70 P 6/14

MEL W to AA 27 FEB 15
 MEL ENTRIES
70 - ENGINE
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ENG 1(2) FAIL

Ident.: ME-70-00008321.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: ENG 1(2) FUEL CTL FAULT

Ident.: ME-70-00008323.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) FUEL FILTER CLOG

Ident.: ME-70-00008325.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 73-09-01 ENG 1(2) FUEL
FILTER CLOG Alert

ECAM Alert: ENG 1(2) FUEL HEAT SYS

Ident.: ME-70-00008327.0002001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-70 P 7/14

MEL AB to AE 27 FEB 15
 MEL ENTRIES
70 - ENGINE
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ENG 1(2) FUEL RETURN VALVE

Ident.: ME-70-00008329.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 73-10-01 Fuel Return
Valve

ECAM Alert: ENG 1(2) FUEL VALVE FAULT

Ident.: ME-70-00008331.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) HOT FUEL

Ident.: ME-70-00008333.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) HP FUEL VALVE

Ident.: ME-70-00008335.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) IGN A(B) FAULT

Ident.: ME-70-00008337.0001001 / 05 APR 12
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert Refer to Item 74-31-01 Ignition System A
or
Refer to Item 74-31-02 Ignition System B
............................................................................................................. ................................................................................
Continued on the following page

LAN COLOMBIA FLEET ME-70 P 8/14

MEL AF to AJ 27 FEB 15
 MEL ENTRIES
70 - ENGINE
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

AIRCRAFT STATUS CONDITION OF DISPATCH
False alert Refer to Item 74-09-01 ENG 1(2) IGN
A(B)(A+B) FAULT Alert

ECAM Alert: ENG 1(2) IGN A+B FAULT

Ident.: ME-70-00008339.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 74-09-01 ENG 1(2) IGN
A(B)(A+B) FAULT Alert

ECAM Alert: ENG 1(2) LOW N1

Ident.: ME-70-00008342.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) N1(N2)(EGT) OVER LIMIT

Ident.: ME-70-00008343.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: ENG 1(2) OIL FILTER CLOG

Ident.: ME-70-00008346.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
Continued on the following page

LAN COLOMBIA FLEET ME-70 P 9/14

MEL AJ to AN 27 FEB 15
 MEL ENTRIES
70 - ENGINE
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

AIRCRAFT STATUS CONDITION OF DISPATCH
False alert Refer to Item 79-09-02 ENG 1(2) OIL
FILTER CLOG Alert

ECAM Alert: ENG 1(2) OIL FILTER CLOG

Ident.: ME-70-00008346.0002001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) OIL HI TEMP

Ident.: ME-70-00008348.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) OIL LO PR

Ident.: ME-70-00008350.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

Actual alert NO DISPATCH
............................................................................................................. ................................................................................
False alert Refer to Item 79-09-01 ENG 1(2) OIL LO
PR Alert

ECAM Alert: ENG 1(2) OIL LO TEMP

Ident.: ME-70-00008352.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Apply ECAM procedure.

LAN COLOMBIA FLEET ME-70 P 10/14

MEL AN to AQ 27 FEB 15
 MEL ENTRIES
70 - ENGINE
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ENG 1(2) ONE TLA FAULT

Ident.: ME-70-00008353.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 76-11-01 Thrust lever
Position Sensor

ECAM Alert: ENG 1(2) OVSPD PROT FAULT

Ident.: ME-70-00008355.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) PROBES FAULT

Ident.: ME-70-00008358.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) REV INHIBITED

Ident.: ME-70-00008360.0001001 / 27 FEB 15
2 Applicable to: MSN 5178, 5234, 5443-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 78-30-01 Thrust Reverser

ECAM Alert: ENG 1(2) REV ISOL FAULT

Ident.: ME-70-00008361.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 78-30-03 Thrust Reverser
Shutoff Valve

LAN COLOMBIA FLEET ME-70 P 11/14

MEL AR to AV 27 FEB 15
 MEL ENTRIES
70 - ENGINE
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ENG 1(2) REV PRESSURIZED

Ident.: ME-70-00008367.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) REV SWITCH FAULT

Ident.: ME-70-00008369.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 78-30-02 Thrust Reverser
Inhibition Relay sw

ECAM Alert: ENG 1(2) REVERSE UNLOCKED

Ident.: ME-70-00008370.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) REVERSER FAULT

Ident.: ME-70-00008372.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 78-30-01 Thrust Reverser

ECAM Alert: ENG 1(2) SENSOR FAULT

Ident.: ME-70-00008374.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-70 P 12/14

MEL AW to BA 27 FEB 15
 MEL ENTRIES
70 - ENGINE
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ENG 1(2) SHUT DOWN

Ident.: ME-70-00008376.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: ENG 1(2) STALL

Ident.: ME-70-00008378.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: ENG 1(2) START FAULT

Ident.: ME-70-00008379.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

AIRCRAFT STATUS CONDITION OF DISPATCH

If the associated THR LEVER NOT AT IDLE subtitle is Apply ECAM procedure.
displayed
............................................................................................................. ................................................................................
NIL Refer to FCOM/PRO-SUP-70 Manual
Engine Start

ECAM Alert: ENG 1(2) START FAULT

Ident.: ME-70-00008379.0003001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

If the associated THR LEVER NOT AT IDLE subtitle is Apply ECAM procedure.
displayed
............................................................................................................. ................................................................................
Dispatch is permitted if MAN start is successful, all Refer to FCOM/PRO-SUP-70 Manual
engine parameters are normal and at least one auto Engine Start
start attempt is performed each day. This auto start
attempt must show successful engine light-off (EGT
rise).

LAN COLOMBIA FLEET ME-70 P 13/14

MEL BB to BD 27 FEB 15
 MEL ENTRIES
70 - ENGINE
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM Alert: ENG 1(2) START VALVE FAULT

Ident.: ME-70-00008381.0001001 / 27 FEB 15
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Refer to Item 80-11-01 Start Valve

ECAM Alert: ENG 1(2) SYSTEM FAULT

Ident.: ME-70-00008383.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) THR LEVER ABV IDLE

Ident.: ME-70-00008387.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL Not related to MEL

ECAM Alert: ENG 1(2) THR LEVER DISAGREE

Ident.: ME-70-00008389.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

ECAM Alert: ENG 1(2) THR LEVER FAULT

Ident.: ME-70-00008391.0001001 / 11 MAR 10
Applicable to: ALL

AIRCRAFT STATUS CONDITION OF DISPATCH

NIL NO DISPATCH

LAN COLOMBIA FLEET ME-70 P 14/14

MEL BE to BI 27 FEB 15
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LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

MI-00 Preamble
MI-00-01 Approval Reference
MMEL Approval Reference..................................................................................................................................... A

MI-00-02 Introduction to the MMEL/MEL

Introduction to the MMEL .......................................................................................................................................A
Introduction to the MEL ..........................................................................................................................................B

MI-00-03 Criteria for Dispatch

Criteria for Dispatch.................................................................................................................................................A

MI-00-04 Maintenance Action

Maintenance Action................................................................................................................................................. A

MI-00-05 Repair Interval

Repair Interval..........................................................................................................................................................A

MI-00-06 Repair Interval Extension

Repair Interval Extension........................................................................................................................................ A

MI-00-07 Definitions
Definitions.................................................................................................................................................................A

MI-00-08 ECAM and MAINTENANCE STATUS

ECAM and MAINTENANCE STATUS ................................................................................................................... A

MI-21 Air Conditioning

MI-21-00 MAINTENANCE Messages on the STATUS SD page
21-00-04 TEMP CTL 1(2) MAINTENANCE Message.............................................................................................A

MI-21-01 Overhead Panels

MI-21-01-01 AIR COND Overhead Panel
21-01-01-01 PACK pb-sw FAULT light ..................................................................................................................A
21-01-01-02 PACK pb-sw OFF light ...................................................................................................................... B
21-01-01-03 HOT AIR pb-sw FAULT light .............................................................................................................C
21-01-01-04 HOT AIR pb-sw OFF light .................................................................................................................D

MI-21-01-02 CABIN PRESS Overhead Panel

21-01-02-01 CABIN PRESS MODE SEL pb-sw FAULT light ................................................................................A

MI-21-01-03 CARGO VENT Overhead Panel

21-01-03-02 AFT ISOL VALVE pb-sw FAULT light ...............................................................................................A
Continued on the following page

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Continued from the previous page

MI-21-01-04 VENTILATION Overhead Panel
21-01-04-01 CAB FANS pb-sw OFF light ..............................................................................................................A
21-01-04-02 BLOWER pb-sw FAULT light ............................................................................................................ B
21-01-04-03 EXTRACT pb-sw FAULT light ...........................................................................................................C

MI-21-07 Indications on SD pages

MI-21-07-01 Indications on the BLEED SD page
21-07-01-01 Pack Outlet Temperature Indication on the BLEED SD page ........................................................... A
21-07-01-02 Pack Turbine Bypass Valve Position Indication on the BLEED SD page ..........................................B
21-07-01-03 Pack Compressor Outlet Temperature Indication on the BLEED SD page .......................................C
21-07-01-04 Pack Flow Indication on the BLEED SD page ..................................................................................D
21-07-01-05 Pack Flow Control Valve Position Indication on the BLEED SD page .............................................. E
21-07-01-06 Emergency Ram Air Inlet Indication on the BLEED SD page ........................................................... F

MI-21-07-02 Indications on the CAB PRESS SD page

21-07-02-01 INLET and EXTRACT Indications on the CAB PRESS SD page ......................................................A
21-07-02-02 Pressure Safety Valves Position Indication on the CAB PRESS SD page ........................................B
21-07-02-03 Pack 1 and 2 Indications on the CAB PRESS SD page ...................................................................C

MI-21-07-03 Indications on the COND SD page

21-07-03-01 Indications on the COND SD page ................................................................................................... A

MI-21-07-04 Indications on the CRUISE SD page

21-07-04-01 Indications on the CRUISE SD page ................................................................................................ A

MI-21-09 ECAM Alerts

21-09-01 VENT BLOWER FAULT Alert .................................................................................................................A
21-09-02 VENT EXTRACT FAULT Alert ............................................................................................................... B
21-09-03 CAB PR SAFETY VALVE OPEN Alert....................................................................................................C

MI-21-21 Air Distribution and Recirculation

21-21-01 Cabin Fan.................................................................................................................................................A

MI-21-23 Lavatory and Galley Ventilation

21-23-01 Lavatory and Galley Extraction Fan........................................................................................................ A
Continued on the following page

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Continued from the previous page

MI-21-26 Avionics Equipment Ventilation
21-26-01 Avionics Blower Fan................................................................................................................................ A
21-26-02 Avionics Extract Fan................................................................................................................................ B
21-26-03 Avionics Skin Exchanger Inlet Bypass Valve.......................................................................................... C
21-26-04 Avionics Skin Air Outlet Valve.................................................................................................................D
21-26-05 Avionics Skin Air Inlet Valve....................................................................................................................E
21-26-06 Avionics Skin Exchanger Isolation Valve................................................................................................. F
21-26-07 Avionics Skin Exchanger Outlet Bypass Valve....................................................................................... G
21-26-08 Avionics Air Conditioning Inlet Valve.......................................................................................................H
21-26-09 Avionics Ventilation Filter.......................................................................................................................... I
21-26-10 Avionics Equipment Ventilation Computer ( AEVC ) ...............................................................................J

MI-21-28 Cargo Compartment Ventilation

21-28-03 AFT Cargo Extraction Fan....................................................................................................................... A
21-28-04 AFT Cargo Isolation Valve.......................................................................................................................B

MI-21-31 Pressure Control and Monitoring

21-31-01 Automatic Cabin Pressure Control System ( CPC , Outflow Valve AUTO Channel) .............................. A
21-31-02 Manual Cabin Pressure Control System (MAN V/S CTL selector, Outflow Valve MAN Channel)............B
21-31-03 Pressure Safety Valve............................................................................................................................. C
21-31-04 Landing Elevation Selection AUTO Function ......................................................................................... D
21-31-05 Landing Elevation Selection MAN Function ........................................................................................... E

MI-21-51 Pack Flow Control

21-51-02 Pack Flow Selection.................................................................................................................................A
21-51-03 Pack Flow Sensor.................................................................................................................................... B

MI-21-52 Air Cooling System

21-52-01 Air Conditioning Pack...............................................................................................................................A
21-52-02 Air Conditioning Pack Ram Air Inlet Flap................................................................................................ B

MI-21-55 Emergency Ram Air Inlet

21-55-01 Emergency Ram Air Inlet.........................................................................................................................A

MI-21-61 Pack Temperature Control

21-61-01 Pack Turbine Bypass Valve.....................................................................................................................A

MI-21-63 Cockpit and Cabin Temperature Control

21-63-02 Cockpit and Cabin Trim Air Valve........................................................................................................... A
21-63-03 Hot Air Pressure Regulating Valve.......................................................................................................... B
21-63-04 Air Conditioning System Controller Channel (COND CTL 1(2)-A(B))......................................................C
Continued on the following page

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COLOMBIA
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MINIMUM EQUIPMENT LIST

Continued from the previous page

MI-22 Auto Flight
MI-22-01 FLT CTL Overhead Panel
22-01-01 FAC pb-sw FAULT light ..........................................................................................................................A
22-01-02 FAC pb-sw OFF light ..............................................................................................................................B

MI-22-05 FMA Indications on the PFD

22-05-01 AP Related Indications on the FMA ....................................................................................................... A
22-05-02 A/THR Related Indications on the FMA ................................................................................................. B
22-05-03 Approach and Landing Capabilities on the FMA ....................................................................................C
22-05-04 Special Messages on the FMA .............................................................................................................. D

MI-22-10 Autopilot/Flight Director (AP/FD)

22-10-01 Autopilot ( AP ) ....................................................................................................................................... A
22-10-02 Flight Director ( FD ) .............................................................................................................................. B
22-10-03 Take-over pb Priority Function................................................................................................................ C
22-10-04 Take-over pb AP Disconnection Function .............................................................................................. D
22-10-05 AUTO LAND light ................................................................................................................................... E
22-10-06 AP Disengagement Warning ...................................................................................................................F
22-10-07 Sticks and Rudder Pedals Locking Solenoid in AP Mode ..................................................................... G

MI-22-30 Autothrust
22-30-01 Autothrust ( A/THR ) ...............................................................................................................................A
22-30-02 Autothrust Instinctive Disconnect pb ...................................................................................................... B
22-30-03 Autothrust Disengagement Warning........................................................................................................ C

MI-22-60 Flight Augmentation (FAC)

22-60-01 FAC 1 ......................................................................................................................................................A
22-60-02 FAC 2 ......................................................................................................................................................B
22-60-03 Reactive Windshear Detection Function..................................................................................................C
22-60-04 Yaw Damper System............................................................................................................................... D

MI-22-70 Flight Management System (FMS)

22-70-01 Flight Management System ( FMS ) ...................................................................................................... A
22-70-02 Navigation Database................................................................................................................................ B
22-70-03 Performance Information ........................................................................................................................ C
22-70-04 Fuel/Time Prediction................................................................................................................................ D
Continued on the following page

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MEL 27 FEB 15
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COLOMBIA
LAN COLOMBIA AIRLINES
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Continued from the previous page

MI-22-81 Flight Control Unit (FCU)
MI-22-81-01 Auto Flight Control Panel (FCU)
22-81-01-01 AP Engagement pb ........................................................................................................................... A
22-81-01-02 A/THR Arming pb .............................................................................................................................. B
22-81-01-03 Mode Engagement pb (LOC, EXPED, APPR)................................................................................... C
22-81-01-04 Selection knob (ALT, HDG-TRK, SPD-MACH).................................................................................. D
22-81-01-05 V/S-FPA Selection knob .................................................................................................................... E
22-81-01-06 HDG-V/S/TRK-FPA Change Over pb ................................................................................................ F
22-81-01-07 SPD/MACH Change Over pb ............................................................................................................G
22-81-01-09 Selection Window (SPD-MACH, HDG-TRK, ALT, V/S-FPA)..............................................................H
22-81-01-10 AP1, AP2 and A/THR pb light Bars..................................................................................................... I
22-81-01-11 Mode Engagement (LOC, EXPED, APPR) pb light Bars....................................................................J

MI-22-81-02 EFIS Control Panel (FCU)

22-81-02-01 Baro Reference Display Window........................................................................................................ A
22-81-02-02 Baro Reference selector Outer Ring (in Hg/hPa)............................................................................... B
22-81-02-03 Baro Reference selector Inner knob ................................................................................................. C
22-81-02-04 FD pb .................................................................................................................................................D
22-81-02-05 LS pb ................................................................................................................................................. E
22-81-02-06 Optional Data (ARPT, NDB, VOR.D, WPT, CSTR) Display pb.......................................................... F
22-81-02-07 ND Range selector ............................................................................................................................G
22-81-02-08 ND Mode selector ............................................................................................................................. H
22-81-02-09 ADF/VOR sw .......................................................................................................................................I
22-81-02-10 LS and FD pb light Bars..................................................................................................................... J
22-81-02-11 Optional Data (ARPT, NDB, VOR.D, WPT, CSTR) Display pb light Bars.......................................... K

MI-22-81-03 FCU Channel

22-81-03-01 FCU Channel...................................................................................................................................... A

MI-22-82 Multipurpose Control and Display Unit (MCDU)

22-82-01 MCDU 1................................................................................................................................................... A
22-82-02 MCDU 2................................................................................................................................................... B
22-82-04 MCDU Annunciator light.......................................................................................................................... C

MI-22-83 Flight Management and Guidance Computer (FMGC)

22-83-01 Flight Management and Guidance Computer ( FMGC ) ........................................................................ A

MI-23 Communications
MI-23-00 MAINTENANCE Message on the STATUS SD page
23-00-01 CIDS 1(2) MAINTENANCE Message...................................................................................................... A
Continued on the following page

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Continued from the previous page

MI-23-01 Overhead Panels
MI-23-01-01 RCDR Overhead Panel
23-01-01-01 RCDR GND CTL pb-sw ON light ...................................................................................................... A
23-01-01-31 RCDR GND CTL pb-sw .....................................................................................................................B
23-01-01-32 CVR ERASE pb ................................................................................................................................ C
23-01-01-33 CVR TEST pb ................................................................................................................................... D

MI-23-01-02 CALLS Overhead Panel

23-01-02-31 CALLS ALL pb ...................................................................................................................................A
23-01-02-32 CALLS EMER pb, CALLS FWD pb, CALLS EXIT pb, CALLS AFT pb ............................................. B

MI-23-01-03 AUDIO SWITCHING Overhead Panel

23-01-03-31 AUDIO SWITCHING selector ............................................................................................................ A

MI-23-09 ECAM Alerts

23-09-01 COMHF 1(2) EMITTING Alert ................................................................................................................ A
23-09-02 COM VHF 1(2)(3) EMITTING Alert ........................................................................................................ B

MI-23-10 Speech Communication

23-10-01 HF System............................................................................................................................................... A
23-10-02 VHF System............................................................................................................................................. B

MI-23-13 Radio Management

23-13-01 Radio Management Panel (RMP)............................................................................................................A
23-13-02 RMP Selection Key.................................................................................................................................. B

MI-23-20 Data Transmission and Automatic Calling

23-20-01 Aircraft Communications Addressing Reporting System (ACARS)..........................................................A

MI-23-31 Passenger Address System

23-31-01 Passenger Address System.....................................................................................................................A
23-31-02 PA IN USE light ......................................................................................................................................B

MI-23-40 Interphone
23-40-01 Ground External Horn.............................................................................................................................. A
23-40-02 Flight Crew Interphone System............................................................................................................... B
23-40-03 Flight Crew to Ground Communication System...................................................................................... C
23-40-04 Service Interphone Jack.......................................................................................................................... D
Continued on the following page

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Continued from the previous page

MI-23-51 Audio Management
23-51-01 SELCAL Function.....................................................................................................................................A
23-51-02 Boomset................................................................................................................................................... B
23-51-03 Hand Microphone.....................................................................................................................................C
23-51-04 Cockpit Loudspeaker............................................................................................................................... D
23-51-05 Cockpit Loudspeaker Volume Control..................................................................................................... E
23-51-06 Sidestick PTT sw .................................................................................................................................... F

MI-23-52 Audio Control Panel (ACP)

23-52-01 CAPT and F/O ACP ............................................................................................................................... A
23-52-02 ACP 3.......................................................................................................................................................B
23-52-05 ACP Transmission Key............................................................................................................................C
23-52-06 ACP Reception knob............................................................................................................................... D
23-52-07 ACP Reception knob light ...................................................................................................................... E

MI-23-71 Cockpit Voice Recorder (CVR)

23-71-01 Cockpit Voice Recorder (CVR)................................................................................................................ A

MI-23-73 Cabin Intercommunication Data System

MI-23-73-01 Cabin Intercommunication Data System (CIDS)
23-73-01-01 Cabin Intercommunication Data System ( CIDS ) Function .............................................................. A

MI-23-73-02 DEU A
23-73-02-01 Cabin DEU A...................................................................................................................................... A

MI-23-73-03 DEU B
23-73-03-01 Cabin DEU B ..................................................................................................................................... A

MI-23-73-04 Cabin Individual Call

23-73-04-01 Passenger Call....................................................................................................................................A

MI-23-73-05 Cabin Loudspeaker

23-73-05-01 Cabin Loudspeaker............................................................................................................................. A
23-73-05-02 Lavatory Loudspeaker.........................................................................................................................B

MI-23-73-06 Handset
23-73-06-01 Cockpit Handset..................................................................................................................................A
23-73-06-02 Cabin Handset.................................................................................................................................... B
23-73-06-03 Cabin Handset Key.............................................................................................................................C

MI-23-73-08 Cabin Assignment Module (CAM)

23-73-08-01 Cabin Assignment Module (CAM)...................................................................................................... A
Continued on the following page

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Continued from the previous page

MI-23-73-10 Smoke Detection Function
23-73-10-01 Smoke Detection Function ( CIDS - SDF ) ....................................................................................... A

MI-23-74 Cabin Crew Panel

23-74-01 FAP Display Unit .................................................................................................................................... A
23-74-02 EMER pb on Hardkey FAP Sub-panel.................................................................................................... B
23-74-03 Other Controls on Hardkey FAP Sub-panel............................................................................................ C
23-74-06 Door Bottle Pressure Monitoring on the FAP .........................................................................................D
23-74-08 Slide Pressure Monitoring on the FAP ................................................................................................... E
23-74-09 Area Call Panel........................................................................................................................................ F
23-74-10 Attendant Indication Panel (AIP)............................................................................................................. G
23-74-11 Additional Attendant Panel (AAP)............................................................................................................H

MI-24 Electrical Power

MI-24-00 MAINTENANCE Messages on the STATUS SD page
24-00-01 DC BUS TIE MAINTENANCE Message..................................................................................................A
24-00-03 AC GEN MAINTENANCE Message........................................................................................................ B

MI-24-01 Overhead Panels

MI-24-01-01 ELEC Overhead Panel
24-01-01-01 BAT 1(2) pb-sw FAULT light ............................................................................................................. A
24-01-01-02 BAT 1(2) pb-sw OFF light ................................................................................................................. B
24-01-01-03 GEN pb-sw FAULT light and APU GEN pb-sw FAULT light .............................................................C
24-01-01-04 GEN pb-sw OFF light and APU GEN pb-sw OFF light .....................................................................D
24-01-01-05 AC ESS FEED pb-sw FAULT light ....................................................................................................E
24-01-01-06 AC ESS FEED pb-sw ALTN light ...................................................................................................... F
24-01-01-07 EXT PWR pb-sw AVAIL light ............................................................................................................G
24-01-01-08 EXT PWR pb-sw ON light .................................................................................................................H
24-01-01-09 GALY & CAB pb-sw FAULT light ....................................................................................................... I
24-01-01-10 GALY & CAB pb-sw OFF light ...........................................................................................................J
24-01-01-11 COMMERCIAL pb-sw OFF light ........................................................................................................K
24-01-01-12 BUS TIE pb-sw OFF light .................................................................................................................. L
24-01-01-13 IDG pb-sw FAULT light .....................................................................................................................M

MI-24-01-02 EMER ELEC PWR Overhead Panel

24-01-02-01 RAT & EMER GEN FAULT light ....................................................................................................... A

MI-24-07 Indications on the ELEC SD page

24-07-01 AC Generation Indications on the ELEC SD page .................................................................................A
24-07-02 DC Generation Indications on the ELEC SD page .................................................................................B
24-07-03 AC ESS BUS SHED Indication on the ELEC SD page ......................................................................... C
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MI-24-09 ECAM Alerts
24-09-01 ELEC AC ESS BUS SHED Alert ............................................................................................................A
24-09-02 C/B TRIPPED Alert.................................................................................................................................. B

MI-24-22 AC Main Generation

24-22-01 AC Main Generation ( IDG , GCU , Line Contactor) .............................................................................. A
24-22-02 AC Bus Tie Control Function...................................................................................................................B

MI-24-23 AC Auxiliary Generation

24-23-01 AC Auxiliary Generation (APU Generator, GCU or GAPCU Auxiliary Power Control function, Line
Contactor).................................................................................................................................................................A

MI-24-24 AC Emergency Generation

24-24-01 Emergency Generator.............................................................................................................................. A
24-24-02 RAT Extension Automatic Control........................................................................................................... B
24-24-03 RAT Extension Manual Control............................................................................................................... C

MI-24-25 AC Essential Generation Switching

24-25-01 Manual Transfer to the AC BUS 2 (ALTN Function) .............................................................................. A
24-25-02 Automatic Transfer to the AC BUS 2 ..................................................................................................... B

MI-24-26 Galley and Commercial Supply System

24-26-01 GALY & CAB Automatic Load Shed System...........................................................................................A
24-26-02 GALY & CAB Manual Load Shed System ( GALY & CAB pb-sw ) ........................................................ B
24-26-03 Commercial Supply System.....................................................................................................................C

MI-24-28 Static Inverter AC Generation

24-28-01 Static Inverter AC Generation..................................................................................................................A

MI-24-32 DC Main Generation (TR 1, TR 2)

24-32-01 DC Main Generation ( TR 1, TR 2) ........................................................................................................A

MI-24-34 DC Emergency Generation (ESS TR)

24-34-01 DC Emergency Generation (ESS TR)..................................................................................................... A

MI-24-35 DC Essential and Normal Generation Switching

24-35-01 DC TIE Contactor 1PC1 (DC BUS 1-DC BAT BUS), 4PC (DC ESS BUS-DC BAT BUS)....................... A
24-35-02 DC TIE Contactor 1PC2 (DC BUS 2-DC BAT BUS)............................................................................... B

MI-24-38 DC Battery Generation

24-38-01 BAT 1(2) Channel.................................................................................................................................... A
24-38-02 Battery Charger Limiter ( BCL ) ............................................................................................................. B
24-38-03 Battery Voltmeter..................................................................................................................................... C
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MI-24-41 AC External Power Control
24-41-01 Ground Power Control (GPCU or GAPCU Ground Power Control function)........................................... A
24-41-02 External Power Receptacle......................................................................................................................B

MI-25 Equipment/Furnishings
MI-25-07 Indications on the DOOR/OXY SD page
25-07-01 Passenger Door Slide Permanently Indicated Armed............................................................................. A
25-07-02 Passenger Door Slide Permanently Indicated Not Armed.......................................................................B
25-07-03 Emergency Exit Slide Permanently Indicated Armed.............................................................................. C
25-07-04 Overwing Emergency Exit Slide Permanently Indicated Not Armed....................................................... D

MI-25-11 Pilot Seats

25-11-01 Pilot Seat Manual Horizontal Adjustment................................................................................................ A
25-11-02 Pilot Seat Manual Vertical Adjustment.....................................................................................................B
25-11-03 Pilot Seat Recline Adjustment................................................................................................................. C
25-11-04 Pilot Seat Other Manual Adjustments..................................................................................................... D
25-11-05 Pilot Seat Electrical Adjustment...............................................................................................................E
25-11-06 Pilot Seat Shoulder Harness....................................................................................................................F
25-11-07 Pilot Seat Fifth Strap............................................................................................................................... G
25-11-08 Pilot Sidestick Armrest Height Adjustment.............................................................................................. H
25-11-09 Pilot Sidestick Armrest Pitch Adjustment.................................................................................................. I
25-11-10 Pilot Sidestick Armrest Memory Position Display.....................................................................................J
25-11-11 Pilot Inboard Armrest Vertical Adjustment............................................................................................... K
25-11-12 Pilot Seat Headrest.................................................................................................................................. L

MI-25-12 Third and Fourth Occupant Seats

25-12-01 Third Occupant Seat................................................................................................................................ A
25-12-02 Third Occupant Seat Shoulder Harness..................................................................................................B
25-12-03 Third Occupant Seat Abdominal Belt...................................................................................................... C
25-12-04 Third Occupant Seat Fifth Strap..............................................................................................................D
25-12-05 Fourth Occupant Seat..............................................................................................................................E
25-12-06 Fourth Occupant Seat Shoulder Harness................................................................................................ F
25-12-07 Fourth Occupant Seat Abdominal Belt....................................................................................................G
25-12-08 Fourth Occupant Seat Fifth Strap............................................................................................................H

MI-25-13 Lining and Furnishings

25-13-01 Pilot Sliding Table.................................................................................................................................... A
25-13-02 Pilot Retractable Footrest........................................................................................................................ B
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MI-25-20 Cabin Seats
MI-25-20-01 Passenger Seat
25-20-01-01 Passenger Seat...................................................................................................................................A
25-20-01-02 Recline Mechanism.............................................................................................................................B
25-20-01-03 Underseat Baggage Restraining Bars................................................................................................ C
25-20-01-04 Economy Class Armrests................................................................................................................... D
25-20-01-05 Premium Economy Convertible Seats Armrest ................................................................................. E
25-20-01-06 Back Table Seats...............................................................................................................................F
25-20-01-07 AMSAFE Seat Belt Airbag System.................................................................................................... G

MI-25-20-03 Cabin Attendant Seat

25-20-03 Cabin Attendant Seat...............................................................................................................................A

MI-25-35 Galley Equipment

25-35-01 Galley Waste Compartment Flapper Door...............................................................................................A

MI-25-40 Lavatories
25-40-01 Toilet Waste Compartment Flapper Door................................................................................................ A
25-40-02 Exterior Lavatory Ashtray.........................................................................................................................B
25-40-03 Interior Lavatory Ashtray..........................................................................................................................C
25-40-90 Lavatory Compartment.............................................................................................................................D

MI-25-50 Cargo Compartments

25-50-02 Decompression Panels in the Cargo Compartments...............................................................................A
25-50-03 Sidewall Linings and Ceiling Panels in the Cargo Compartments...........................................................B
25-50-04 Cargo Compartment Restraint Components (Nets, Attach Points, Stanchions)...................................... C
25-50-05 Protection Panels of Decompression Panels at the FWD Partition Wall of FWD Cargo Compartment. ... D

MI-25-62 Cabin Escape Facilities

25-62-01 Cabin Passenger Door Slide or Slide Raft.............................................................................................. A
25-62-02 Overwing Emergency Exit Slide or Slide Raft......................................................................................... B
25-62-04 SLIDE ARMED light ............................................................................................................................... C
25-62-06 Passenger Door CHECK SLIDE PRESSURE Message on Flight Attendant Panel (FAP) .............D
25-62-07 Overwing Emergency Exit CHECK SLIDE PRESSURE Message on Flight Attendant Panel (FAP)....... E
25-62-08 Overwing Escape Life Line...................................................................................................................... F

MI-25-63 Evacuation Signaling Equipment

25-63-01 Emergency Evacuation Signaling System (COMMAND pb-sw, HORN SHUT OFF pb, CAPT&PURS and
CAPT sw).................................................................................................................................................................A
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MI-25-64 First Aid Equipment
25-64-01 First Aid Kit.............................................................................................................................................. A
25-64-02 Emergency Medical Kit............................................................................................................................ B
25-64-03 Automated External Defibrillator (AED)................................................................................................... C
25-64-90 Universal Precaution Kit (KPU)............................................................................................................... D

MI-25-65 Emergency Equipment

25-65-01 Cockpit Flashlight.....................................................................................................................................A
25-65-02 Cabin Flashlight........................................................................................................................................B
25-65-03 Crash Axe/Crowbar..................................................................................................................................C
25-65-04 Emergency Locator Transmitter (ELT).................................................................................................... D
25-65-05 Fireproof Gloves.......................................................................................................................................E
25-65-06 Megaphone...............................................................................................................................................F

MI-25-66 Floatation and Survival Equipment

25-66-01 Life Vest................................................................................................................................................... A

MI-26 Fire Protection

MI-26-00 MAINTENANCE Message on the STATUS SD page
26-00-01 SMOKE MAINTENANCE Message......................................................................................................... A

MI-26-01 Overhead Panels

MI-26-01-01 FIRE Overhead Panel
26-01-01-01 Bulb/LED in the ENG FIRE-PUSH pb-sw ......................................................................................... A
26-01-01-02 ENG AGENT pb DISCH light ............................................................................................................ B
26-01-01-03 ENG AGENT pb SQUIB light ............................................................................................................C
26-01-01-04 Bulb/ LED in the APU FIRE-PUSH pb-sw ........................................................................................ D
26-01-01-05 APU AGENT pb DISCH light .............................................................................................................E
26-01-01-06 APU AGENT pb SQUIB light .............................................................................................................F
26-01-01-31 ENG FIRE TEST pb ..........................................................................................................................G
26-01-01-32 APU FIRE TEST pb .......................................................................................................................... H
26-01-01-33 APU FIRE PUSH pb-sw ..................................................................................................................... I
26-01-01-34 APU AGENT pb ................................................................................................................................. J

MI-26-01-02 CARGO SMOKE Overhead Panel

26-01-02-01 CARGO SMOKE DISCH light ........................................................................................................... A
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MI-26-12 Engine Fire and Overheat Detection
26-12-01 Engine Fire Detection Loop A on the Engine 1.......................................................................................A
26-12-02 Engine Fire Detection Loop A on the Engine 2.......................................................................................B
26-12-03 Engine Fire Detection Loop B on the Engine 1.......................................................................................C
26-12-04 Engine Fire Detection Loop B on the Engine 2.......................................................................................D
26-12-05 FIRE light on the ENG MASTER Panel.................................................................................................. E

MI-26-13 APU Fire and Overheat Detection

26-13-01 APU Fire Detection Loop ........................................................................................................................A

MI-26-15 Avionics Compartment Smoke Detection

26-15-01 Avionics Smoke Detection System.......................................................................................................... A

MI-26-16 Cargo Compartment Smoke Detection

26-16-01 Smoke Detector in the FWD Cargo Compartment ................................................................................. A
26-16-02 Smoke Detector in the AFT and the BULK Cargo Compartments.......................................................... B

MI-26-17 Lavatory Smoke Detection

26-17-01 Lavatory Smoke Detection System..........................................................................................................A

MI-26-22 APU Fire Extinguishing

26-22-01 APU Automatic Fire Extinguishing Control on Ground ...........................................................................A
26-22-02 APU Fire Extinguisher Overpressure Indication (Red Disc) ................................................................... B
26-22-03 Squib of the APU Fire Extinguisher Bottle ............................................................................................. C
26-22-04 APU Fire Extinguisher Bottle ..................................................................................................................D
26-22-05 APU AUTO EXTING TEST pb-sw on the Maintenance Panel ............................................................... E
26-22-06 APU FIRE light on the External Power Panel ........................................................................................ F
26-22-07 APU SHUT OFF pb on the External Power Panel .................................................................................G

MI-26-23 Cargo Compartment Fire Extinguishing

26-23-01 Cargo Agent Bottle...................................................................................................................................A
26-23-02 Squib of the Cargo Bottle 1.....................................................................................................................B

MI-26-24 Portable Fire Extinguisher

26-24-01 Portable Fire Extinguisher........................................................................................................................A

MI-26-25 Lavatory Fire Extinguishing

26-25-01 Lavatory Waste Bin Fire Extinguishing System.......................................................................................A

MI-27 Flight Controls

MI-27-00 MAINTENANCE Messages on the STATUS SD page
27-00-01 F/CTL MAINTENANCE Message............................................................................................................ A
27-00-02 SFCS MAINTENANCE Message.............................................................................................................B
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MI-27-01 Overhead Panels
MI-27-01-01 FLT CTL Overhead Panel
27-01-01-01 ELAC pb-sw FAULT light .................................................................................................................. A
27-01-01-02 ELAC pb-sw OFF light ...................................................................................................................... B
27-01-01-03 SEC pb-sw FAULT light .................................................................................................................... C
27-01-01-04 SEC pb-sw OFF light ........................................................................................................................ D

MI-27-07 Indications on SD pages

27-07-01 Aileron Actuator Indication on the F/CTL SD page ................................................................................ A
27-07-02 Aileron Position Indication on the F/CTL SD page .................................................................................B
27-07-03 Elevator Actuator Indication on the F/CTL SD page .............................................................................. C
27-07-04 Elevator Position Indication on the F/CTL SD page ...............................................................................D
27-07-05 Pitch Trim Position Indication on the F/CTL SD page ............................................................................E
27-07-06 Rudder Position Indication on the F/CTL SD page ................................................................................ F
27-07-07 Rudder Trim Position Indication on the F/CTL SD page ........................................................................G
27-07-08 Rudder Travel Limiter Position Indication on the F/CTL SD page ......................................................... H
27-07-09 ELAC Indication on the F/CTL SD page ..................................................................................................I
27-07-10 SEC Indication on the F/CTL SD page ...................................................................................................J
27-07-11 Spoilers/Speedbrakes Indication on the F/CTL SD page ....................................................................... K
27-07-12 Spoilers/Speedbrakes Indication on the WHEEL SD page .....................................................................L

MI-27-08 Indications on the EWD

27-08-01 Flap Position Indication on the EWD ......................................................................................................A
27-08-02 Slat Position Indication on the EWD ...................................................................................................... B

MI-27-14 Aileron and Hydraulic Actuation

27-14-01 Left Aileron Blue Servo-Control (Controlled by ELAC 1) ........................................................................A
27-14-02 Left Aileron Green Servo-Control (Controlled by ELAC 2)...................................................................... B
27-14-03 Right Aileron Green Servo-Control (Controlled by ELAC 1) ...................................................................C
27-14-04 Right Aileron Blue Servo-Control (Controlled by ELAC 2)...................................................................... D

MI-27-21 Rudder Mechanical Control

27-21-01 Rudder Pedal Adjustment System...........................................................................................................A

MI-27-22 Rudder Trim Actuation

27-22-01 Rudder Trim System................................................................................................................................ A
27-22-02 Manual Rudder Trim Reset Function.......................................................................................................B
27-22-03 Rudder Trim Position Indication on the Center Pedestal........................................................................ C

MI-27-23 Artificial feel and rudder travel limiting actuation

27-23-01 Rudder Travel Limiter System(Including Rudder and Pedals Travel Limiter Units)................................. A
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MI-27-34 Elevator and Hydraulic Actuation
27-34-01 Elevator Servo-Control............................................................................................................................. A
27-34-02 Elevator Servo-Control Position Transducer............................................................................................B

MI-27-40 Trimmable Horizontal Stabilizer (THS)

27-40-01 Stabilizer Mechanical Control...................................................................................................................A
27-40-02 Stabilizer Actuator Electric Motor.............................................................................................................B

MI-27-51 Flaps Electrical Control and Monitoring

27-51-01 SFCC Flap Channel ............................................................................................................................... A
27-51-02 SFCC Slat Channel ................................................................................................................................ B
27-51-03 Flap Wing Tip Brakes Solenoid............................................................................................................... C

MI-27-54 Flaps Hydraulic Actuation and Power Transmission

27-54-01 Flap Hydraulic Motor................................................................................................................................A
27-54-02 Flap PCU Valve Block ............................................................................................................................ B
27-54-03 Flap Pressure-Off Brake.......................................................................................................................... C

MI-27-64 Spoiler Hydraulic Actuation

27-64-01 Spoiler 5................................................................................................................................................... A
27-64-02 Spoiler 1 or 3........................................................................................................................................... B
27-64-03 Spoiler 2 or 4...........................................................................................................................................C
27-64-04 Spoilers 1 and 2...................................................................................................................................... D
27-64-05 Spoilers 3 and 4.......................................................................................................................................E

MI-27-81 Slats Electrical Control and Monitoring

27-81-01 Slat Wing Tip Brakes Solenoids.............................................................................................................. A

MI-27-84 Slats Hydraulic Actuation and Power Transmission

27-84-01 Slats Hydraulic Motor...............................................................................................................................A
27-84-02 Slat PCU Valve Block .............................................................................................................................B
27-84-03 Slat Pressure-Off Brake...........................................................................................................................C

MI-27-92 Electrical Flight Control System (EFCS) Control Inputs and Power Supply
27-92-01 Speedbrake Control System.................................................................................................................... A
27-92-02 Ground Spoiler Control System............................................................................................................... B
27-92-03 SIDESTICK PRIORITY light ................................................................................................................... C
27-92-04 Sidestick Dual Input Visual Warnings......................................................................................................D
27-92-05 Sidestick Dual Input Aural Warning......................................................................................................... E
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MI-27-93 ELAC System (Elevator Aileron Computer)
27-93-01 ELAC 1 ................................................................................................................................................... A
27-93-02 ELAC 2.....................................................................................................................................................B
27-93-03 Pitch Normal Law.....................................................................................................................................C

MI-27-94 SEC System (Spoiler and Elevator Computer)

27-94-01 SEC 1 ..................................................................................................................................................... A
27-94-02 SEC 2 ..................................................................................................................................................... B
27-94-03 SEC 3 ..................................................................................................................................................... C

MI-27-95 FCDC System (Flight Control Data Concentrator)

27-95-01 FCDC 1.................................................................................................................................................... A
27-95-02 FCDC 2 ...................................................................................................................................................B

MI-28 Fuel
MI-28-00 MAINTENANCE Message on the STATUS SD page
28-00-01 FUEL MAINTENANCE Message............................................................................................................. A

MI-28-01 Overhead Panels

MI-28-01-01 FUEL Overhead Panel
28-01-01-01 Wing TK PUMP pb-sw FAULT light .................................................................................................. A
28-01-01-02 Wing TK PUMP pb-sw OFF light ...................................................................................................... B
28-01-01-03 X FEED pb-sw ON light .................................................................................................................... C
28-01-01-04 X FEED pb-sw OPEN light ............................................................................................................... D
28-01-01-05 CTR TK PUMP pb-sw FAULT light ................................................................................................... E
28-01-01-06 CTR TK PUMP pb-sw OFF light ....................................................................................................... F
28-01-01-07 FUEL MODE SEL pb-sw FAULT light .............................................................................................. G

MI-28-07 Indications on the FUEL SD page

MI-28-07-01 Fuel Quantity Indications on the FUEL SD page
28-07-01-01 Fuel On Board (FOB) Indication on the FUEL SD page ................................................................... A
28-07-01-02 Fuel Quantity Indication (FQI) in Degraded Mode on the FUEL SD page .........................................B
28-07-01-03 Outer Tank Fuel Quantity Indication on the FUEL SD page ............................................................. C
28-07-01-04 Inner Tank Fuel Quantity Indication on the FUEL SD page ..............................................................D
28-07-01-05 Center Tank Fuel Quantity Indication on the FUEL SD page ........................................................... E

MI-28-07-02 Fuel Temperature Indications on the FUEL SD page

28-07-02-01 Fuel Temperature Indication on the FUEL SD page ......................................................................... A

MI-28-07-03 Tank Pump Indications on the FUEL SD page

28-07-03-01 Wing Tank Pump Indication on the FUEL SD page ..........................................................................A
28-07-03-02 Center Tank Pump Indication on the FUEL SD page ....................................................................... B
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MI-28-07-04 Valve Indications on the FUEL SD page
28-07-04-01 Engine LP Fuel Valve Indication on the FUEL SD page ...................................................................A
28-07-04-02 APU LP Fuel Valve Indication on the FUEL SD page ...................................................................... B
28-07-04-03 Crossfeed Valve Indication on the FUEL SD page ...........................................................................C
28-07-04-04 Wing Transfer Valve Indication on the FUEL SD page .....................................................................D

MI-28-07-05 Fuel Flow Indication on the FUEL SD page

28-07-05-01 Fuel Flow 1+2 Indication on the FUEL SD page ...............................................................................A

MI-28-07-06 Fuel Used Indication on the FUEL SD page

28-07-06-01 Fuel Used Indication on the FUEL SD page .....................................................................................A
28-07-06-02 Fuel Used 1+2 Indication on the FUEL SD page ..............................................................................B

MI-28-09 ECAM Alerts

28-09-01 FUEL L(R) INNER(OUTER) TK HI TEMP Alert ..................................................................................... A
28-09-02 FUEL L(R) INNER(OUTER) TK LO TEMP Alert .................................................................................... B

MI-28-12 Tank Venting System

28-12-01 Overpressure Protector between the Inner and the Outer Tank............................................................. A
28-12-02 Overpressure Protector in the Vent Surge Tank..................................................................................... B
28-12-03 Overpressure Protector in the Inner Tank...............................................................................................C
28-12-04 Overpressure Protector between the Center and the Inner Tank........................................................... D

MI-28-15 Intercell Transfer System

28-15-01 LH Wing Transfer Valve ......................................................................................................................... A
28-15-02 RH Wing Transfer Valve .........................................................................................................................B

MI-28-20 Distribution
28-20-01 Automatic Fuel Feed System...................................................................................................................A

MI-28-21 Main Fuel Pump System

28-21-01 Wing Tank Pump..................................................................................................................................... A
28-21-02 Center Tank Pump...................................................................................................................................B
28-21-03 Wing Tank Pump Sequence Valve..........................................................................................................C

MI-28-22 APU Fuel Pump System

28-22-01 APU Fuel Pump ......................................................................................................................................A

MI-28-23 Crossfeed System

28-23-01 Crossfeed Valve.......................................................................................................................................A

MI-28-24 Engine LP Fuel Shutoff

28-24-01 Engine LP Fuel Valve Electrical Motor.................................................................................................... A
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MI-28-25 Refuel/Defuel System
28-25-01 Fuel Quantity Preselector........................................................................................................................ A
28-25-02 Fuel Quantity on the Refuel/Defuel Control Panel...................................................................................B
28-25-03 Refuel Valve.............................................................................................................................................C
28-25-04 Transfer Defuel Valve.............................................................................................................................. D
28-25-05 Exterior Refuel/Defuel Control Panel....................................................................................................... E

MI-28-29 APU LP Fuel Shutoff

28-29-01 APU LP Fuel Valve ................................................................................................................................ A

MI-28-43 Manual Magnetic Indicators

28-43-01 Manual Magnetic Indicators..................................................................................................................... A

MI-28-46 Tank Level Sensing

28-46-01 High Level Detection System in the Inner Tank...................................................................................... A
28-46-02 High Level Detection System in the Center Tank................................................................................... B
28-46-04 Low Level Detection System in the Inner Tank.......................................................................................C

MI-28-50 Fuel Management

28-50-01 Fuel Quantity Indicating Computer ( FQIC ) Channel ............................................................................ A

MI-29 Hydraulic Power

MI-29-01 Overhead Panels
MI-29-01-01 HYD Overhead Panel
29-01-01-01 B(Y) ELEC PUMP pb-sw FAULT light ...............................................................................................A
29-01-01-02 B ELEC PUMP pb-sw OFF light ....................................................................................................... B
29-01-01-03 Y ELEC PUMP pb-sw ON light .........................................................................................................C
29-01-01-04 G(Y) ENG 1(2) PUMP pb-sw FAULT light ........................................................................................ D
29-01-01-05 G(Y) ENG 1(2) PUMP pb-sw OFF light ............................................................................................ E
29-01-01-06 PTU pb-sw FAULT light .....................................................................................................................F
29-01-01-07 PTU pb-sw OFF light ........................................................................................................................ G

MI-29-01-02 Maintenance HYD Overhead Panel

29-01-02-01 G(B)(Y) LEAK MEASUREMENT VALVES pb-sw OFF light ..............................................................A
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MI-29-07 Indications on the HYD SD page
29-07-01 Yellow ELEC Pump Indication on the HYD SD page .............................................................................A
29-07-02 Pump Indication on the HYD SD page ...................................................................................................B
29-07-03 Fire Valve Indication on the HYD SD page ........................................................................................... C
29-07-04 PTU Indication on the HYD SD page .................................................................................................... D
29-07-05 Reservoir Quantity Indication on the HYD SD page .............................................................................. E
29-07-06 RAT Indication on the HYD SD page .....................................................................................................F
29-07-07 System Label Indication on the HYD SD page ......................................................................................G
29-07-08 System Pressure Indication on the HYD SD page .................................................................................H

MI-29-09 ECAM Alerts

29-09-01 HYD B(Y) ELEC PUMP LO PR Alert...................................................................................................... A
29-09-02 HYD B(Y) ELEC PUMP OVHT Alert....................................................................................................... B
29-09-03 HYD G(Y) ENG 1(2) PUMP LO PR Alert ...............................................................................................C
29-09-04 HYD G(B)(Y) RSVR LO AIR PR Alert.....................................................................................................D
29-09-05 HYD G(B)(Y) RSVR LO LVL Alert ......................................................................................................... E
29-09-06 HYD G(B)(Y) RSVR OVHT Alert............................................................................................................. F
29-09-07 HYD PTU FAULT Alert .......................................................................................................................... G
29-09-08 HYD RAT FAULT Alert............................................................................................................................H
29-09-09 HYD G(B)(Y)(B+G)(G+Y)(B+Y) SYS LO PR Alert ...................................................................................I

MI-29-10 Main Hydraulic Power

29-10-01 Engine Driven Pump................................................................................................................................ A
29-10-02 Engine Driven Pump Depressurization Function..................................................................................... B
29-10-03 Blue System Electric Pump..................................................................................................................... C
29-10-04 Hydraulic System Accumulator................................................................................................................ D
29-10-05 Yellow Brake Accumulator....................................................................................................................... E
29-10-07 Engine Pump Fire Valve.......................................................................................................................... F
29-10-08 Hydraulic System Filter............................................................................................................................G
29-10-09 Hydraulic Case Drain Filter......................................................................................................................H

MI-29-22 Blue Auxiliary Hydraulic Power

29-22-01 Ram Air Turbine.......................................................................................................................................A

MI-29-23 Power Transfer

29-23-01 Power Transfer Unit ( PTU ) .................................................................................................................. A

MI-29-24 Yellow Auxiliary Hydraulic Power

29-24-01 Yellow System Electric Pump.................................................................................................................. A
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MI-30 Ice and Rain Protection
MI-30-00 MAINTENANCE Message on the STATUS SD page
30-00-01 ICE DETECT MAINTENANCE Message.................................................................................................A

MI-30-01 Overhead Panels

MI-30-01-01 ANTI ICE Overhead Panel
30-01-01-01 ANTI ICE ENG 1(2) pb-sw FAULT light ............................................................................................A
30-01-01-02 ANTI ICE ENG 1(2) pb-sw ON light ..................................................................................................B
30-01-01-03 ANTI ICE WING pb-sw FAULT light ................................................................................................. C
30-01-01-04 ANTI ICE WING pb-sw ON light ....................................................................................................... D

MI-30-01-02 WIPER Overhead Panel

30-01-02-01 Wiper High Speed Function (FAST Position)..................................................................................... A
30-01-02-02 Wiper Low Speed Function (SLOW Position).....................................................................................B

MI-30-07 Indications on the BLEED SD page

30-07-01 ANTI ICE Indication on the BLEED SD page .........................................................................................A
30-07-02 Arrow Indication on the BLEED SD page .............................................................................................. B

MI-30-11 Wing Ice Protection

30-11-01 Wing Anti-Ice Control Valve.....................................................................................................................A

MI-30-21 Engine Air Intake Ice Protection

30-21-01 Engine Anti-Ice Valve...............................................................................................................................A

MI-30-31 Probe Ice Protection

30-31-01 Probe Heat Computer ( PHC ) ............................................................................................................... A
30-31-02 Pitot Heater.............................................................................................................................................. B
30-31-03 Static Ports Heater...................................................................................................................................C
30-31-04 Angle of Attack ( AOA ) Probes Heating ................................................................................................D
30-31-05 TAT Probes Heating................................................................................................................................ E

MI-30-42 Windshield Anti-Icing and Defogging

30-42-01 Window Heat Computer...........................................................................................................................A
30-42-02 Fixed Lateral Window and Sliding Window Heating................................................................................ B
30-42-03 Windshield Heating.................................................................................................................................. C
30-42-04 PROBES/WINDOW HEAT pb-sw AUTO Control.................................................................................... D
30-42-05 PROBES/WINDOW HEAT pb-sw ON light .............................................................................................E

MI-30-45 Windshield Rain Protection

30-45-01 Windshield Wiper..................................................................................................................................... A
30-45-02 Windshield Wiper PARK Function........................................................................................................... B
30-45-03 Rain Repellent System............................................................................................................................ C
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MI-30-71 Waste Water Ice Protection
30-71-01 Waste Water Drain Mast Heating System............................................................................................... A

MI-30-81 Ice Detection

30-81-01 Ice Detection System............................................................................................................................... A
30-81-02 External Visual Icing Indicator................................................................................................................. B
30-81-03 Lighting of External Visual Icing Indicator............................................................................................... C

MI-31 Indicating/Recording Systems

MI-31-00 MAINTENANCE Message on the STATUS SD page
31-00-02 ACMS MAINTENANCE Message............................................................................................................ A
31-00-04 CFDIU MAINTENANCE Message........................................................................................................... B
31-00-05 DMC 1/3 MAINTENANCE Message........................................................................................................C
31-00-06 DMC 2/3 MAINTENANCE Message........................................................................................................D

MI-31-05 Indications on the Primary Flight Display (PFD)

31-05-01 AP Related Indications on the FMA ....................................................................................................... A
31-05-02 A/THR Related Indications on the FMA ................................................................................................. B
31-05-03 Approach and Landing Capabilities on the FMA ....................................................................................C
31-05-04 Special Messages on the FMA .............................................................................................................. D
31-05-05 Actual Airspeed Reference Line and Scale Indications on the PFD .......................................................E
31-05-06 Mach Number Indication on the PFD ..................................................................................................... F
31-05-07 VMO / MMO Characteristic Speed Indication on the PFD .....................................................................G
31-05-08 Altitude Indication on the PFD ............................................................................................................... H
31-05-09 Vertical Speed Indication on the PFD ......................................................................................................I
31-05-10 Other Air Data Related Indications on the PFD ......................................................................................J
31-05-11 Attitude Indication on the PFD ............................................................................................................... K
31-05-12 Heading Indication on the PFD ...............................................................................................................L
31-05-30 Lateral Deviation Scale (L/DEV)............................................................................................................. M
31-05-31 Vertical Deviation Scale (V/DEV)............................................................................................................ N

MI-31-06 Indications on the Navigation Display (ND)

31-06-01 Ground Speed Indication on the ND ...................................................................................................... A
31-06-02 True Air Speed Indication on the ND ..................................................................................................... B
31-06-03 Wind Indication on the ND ..................................................................................................................... C
31-06-04 Heading Indication on the ND ................................................................................................................ D
31-06-05 Position (Aircraft Symbol) Indication on the ND ..................................................................................... E
31-06-06 Navigation Station Information on the ND .............................................................................................. F
31-06-07 Chrono Indication on the ND ................................................................................................................. G
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MI-31-07 Indications on the System Display (SD)
31-07-01 Indications on the System Display pages................................................................................................A
31-07-02 Permanent Data ( TAT , SAT , ISA , GLOAD - ALT SEL, UTC , GW ) Indications on the SD ................ B

MI-31-08 Indications on the Engine Warning Display (EWD)

31-08-01 Engine Parameter Indications on the EWD ............................................................................................A
31-08-02 Fuel On Board ( FOB ) Indication on the EWD ......................................................................................B
31-08-03 MEMO Messages on the EWD .............................................................................................................. C
31-08-04 Slats/Flaps Position Indications on the EWD ......................................................................................... D

MI-31-20 Independent Instruments

31-20-01 Electrical Clock Indicator..........................................................................................................................A

MI-31-30 Centralized Fault Display System (CFDS) and Data Recording System
31-30-01 Centralized Fault Display System (CFDS)...............................................................................................A
31-30-03 Digital Flight Data Recorder ( DFDR ) ................................................................................................... B
31-30-04 Data Management (DMU or FDIMU Data Management function)...........................................................C
31-30-05 Flight Data Interface (FDIU or FDIMU Flight Data Interface function).....................................................D
31-30-07 Printer....................................................................................................................................................... E

MI-31-38 Up and Down Data Loading System Acquisition/Interface and Equipment

31-38-01 DATA LOADING selector ....................................................................................................................... A
31-38-02 Data Loading Routing Box (DLRB)..........................................................................................................B
31-38-03 Multipurpose Disk Drive Unit (MDDU).....................................................................................................C

MI-31-53 Flight Warning Computer (FWC)

31-53-01 Flight Warning Computer ( FWC ) ......................................................................................................... A
31-53-02 MASTER CAUT Cancel Function............................................................................................................ B
31-53-03 MASTER WARN Cancel Function...........................................................................................................C
31-53-04 MASTER CAUT light .............................................................................................................................. D
31-53-05 MASTER WARN light ............................................................................................................................. E
31-53-06 Altitude Alert............................................................................................................................................. F

MI-31-55 System Data Acquisition Concentrator (SDAC)

31-55-01 System Data Acquisition Concentrator (SDAC).......................................................................................A
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MI-31-56 ECAM Control Panel (ECP)
31-56-01 System Page Manual Call pb on the ECP ............................................................................................. A
31-56-02 ALL pb on the ECP ................................................................................................................................ B
31-56-03 CLR pb on the ECP ............................................................................................................................... C
31-56-04 EMER CANC pb on the ECP .................................................................................................................D
31-56-05 RCL pb on the ECP ............................................................................................................................... E
31-56-06 STS pb on the ECP................................................................................................................................. F
31-56-07 T.O CONFIG pb on the ECP ................................................................................................................. G

MI-31-62 Display Management Computer (DMC)

31-62-01 DMC 1 .....................................................................................................................................................A
31-62-02 DMC 2 .....................................................................................................................................................B
31-62-03 DMC 3 .................................................................................................................................................... C

MI-31-63 Display Unit (DU)

31-63-01 PFDU 1.................................................................................................................................................... A
31-63-02 PFDU 2 ................................................................................................................................................... B
31-63-03 NDU 1 .....................................................................................................................................................C
31-63-04 NDU 2 .....................................................................................................................................................D
31-63-05 SDU .........................................................................................................................................................E
31-63-06 EWDU ..................................................................................................................................................... F

MI-31-68 Switching Panel

31-68-01 AIR DATA SWITCHING selector on the Center Pedestal....................................................................... A
31-68-02 ATT HDG SWITCHING selector on the Center Pedestal........................................................................B
31-68-03 ECAM/ND XFR SWITCHING selector on the Center Pedestal...............................................................C
31-68-04 EIS DMC SWITCHING selector on the Center Pedestal........................................................................ D
31-68-05 PFD/ND XFR pb on the Lateral Instrument Panel ................................................................................. E

MI-32 Landing Gear

MI-32-07 Indications on the WHEEL SD page
32-07-01 Brakes Temperature Indication on the WHEEL SD page ...................................................................... A
32-07-02 L/G Position Indication on the WHEEL SD page ................................................................................... B
32-07-03 L/G Doors Position Indication on the WHEEL SD page .........................................................................C
32-07-04 L/G CTL Indication on the WHEEL SD page .........................................................................................D
32-07-05 UP LOCK Indication on the WHEEL SD page ....................................................................................... E
32-07-06 [Y] N/W STEERING Indication on the WHEEL SD page ....................................................................... F
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32-07-08 ANTI SKID, [1], [2] Indication on the WHEEL SD page .........................................................................G
32-07-09 AUTO BRK Indication on the WHEEL SD page .................................................................................... H
32-07-10 [G] NORM BRK Indication on the WHEEL SD page ............................................................................... I
32-07-11 Release Brake Indication on the WHEEL SD page ................................................................................ J
32-07-12 ACCU PRESS/ACCU ONLY Indication on the WHEEL SD page .......................................................... K
32-07-13 [Y] ALTN BRK Indication on the WHEEL SD page ................................................................................ L

MI-32-09 ECAM Alerts

32-09-01 BRAKES-N/WS MINOR FAULT Alert .....................................................................................................A

MI-32-11 Main Gear

32-11-01 Main Gear Torque Link Damper.............................................................................................................. A

MI-32-12 Main Gear Doors

32-12-01 Main Gear Door Ground Opening Cable.................................................................................................A

MI-32-31 Normal Extension and Retraction

32-31-01 Landing Gear Control and Interface Unit ( LGCIU ) ...............................................................................A
32-31-02 Landing Gear Retracting System.............................................................................................................B

MI-32-32 Proximity Detector System

32-32-01 LGCIU 1 Proximity Detector.................................................................................................................... A
32-32-02 LGCIU 2 RH L/G Shock Absorber Proximity Detector ........................................................................... B
32-32-03 LGCIU 2 LH L/G Shock Absorber Proximity Detector ............................................................................C
32-32-04 LGCIU 2 Nose L/G Shock Absorber Proximity Detector ........................................................................ D
32-32-05 LGCIU 2 RH L/G Down Lock Proximity Detector ...................................................................................E
32-32-06 LGCIU 2 LH L/G Down Lock Proximity Detector ....................................................................................F
32-32-07 LGCIU 2 Nose L/G Down Lock Proximity Detector ............................................................................... G
32-32-08 LGCIU 2 RH L/G Up Lock Proximity Detector ....................................................................................... H
32-32-09 LGCIU 2 LH L/G Up Lock Proximity Detector ......................................................................................... I
32-32-10 LGCIU 2 Nose L/G Up Lock Proximity Detector .....................................................................................J
32-32-11 LGCIU 2 RH L/G Doors Open Proximity Detector ................................................................................. K
32-32-12 LGCIU 2 LH L/G Doors Open Proximity Detector .................................................................................. L
32-32-13 LGCIU 2 Nose L/G Doors Open Proximity Detector ..............................................................................M
32-32-14 LGCIU 2 RH L/G Doors Closed Proximity Detector ...............................................................................N
32-32-15 LGCIU 2 LH L/G Doors Closed Proximity Detector ............................................................................... O
32-32-16 LGCIU 2 Nose L/G Doors Closed Proximity Detector ............................................................................P

MI-32-33 Free Fall Extension

32-33-01 Landing Gear Gravity Extension System.................................................................................................A
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MI-32-41 Wheels
32-41-01 Nose Wheel Tie Bolt................................................................................................................................A
32-41-02 Main Wheel Tie Bolt................................................................................................................................ B

MI-32-42 Normal Braking

32-42-01 Main Wheel Brake....................................................................................................................................A
32-42-02 Green System Brake................................................................................................................................B
32-42-03 Braking/Steering Control Unit ( BSCU ) System 1 ................................................................................. C
32-42-04 Braking/Steering Control Unit (BSCU) System 2.....................................................................................D
32-42-05 AUTO/BRK Function................................................................................................................................ E
32-42-06 Tachometer...............................................................................................................................................F
32-42-08 AUTO/BRK (LO, MED, MAX) pb-sw DECEL light ................................................................................. G
32-42-09 AUTO/BRK (LO, MED, MAX) pb-sw ON light ........................................................................................ H

MI-32-44 Alternate Braking

32-44-01 Yellow System Brake............................................................................................................................... A
32-44-02 ACCU PRESS Indicator...........................................................................................................................B
32-44-03 BRAKES Pressure Indicator.................................................................................................................... C
32-44-04 Alternate Braking Control Unit (ABCU)....................................................................................................D

MI-32-45 Parking/Ultimate Emergency Braking

32-45-01 Parking Brake Control Valve Electrical Motor..........................................................................................A

MI-32-47 Brake Temperature System

32-47-01 Brake Temperature Monitoring Unit ( BTMU ) ....................................................................................... A

MI-32-48 Brake Cooling

32-48-01 Brake Fan System................................................................................................................................... A
32-48-02 BRK FAN pb-sw HOT light ................................................................................................................... B
32-48-03 BRK FAN pb-sw ON light .......................................................................................................................C

MI-32-51 Steering
32-51-01 Nose Wheel Steering Control System..................................................................................................... A
32-51-02 Rudder PEDALS DISC pb ......................................................................................................................B
32-51-03 NWS Electrical Deactivation Box ........................................................................................................... C
32-51-04 PARKING BRAKE light on the NWS Electrical Deactivation Box .......................................................... D

MI-32-61 Landing Gear Panel on the Center Instrument Panel

32-61-01 LDG GEAR Indicator Panel..................................................................................................................... A
32-61-02 DOWN Red Arrow light on the Landing Gear lever ............................................................................... B
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MI-33 Lights
MI-33-01 Overhead Panels
MI-33-01-01 ANN LT Overhead Panel
33-01-01-01 TEST Function of ANN LT sw ...........................................................................................................A
33-01-01-02 DIM Function of ANN LT sw ............................................................................................................. B
33-01-01-03 BRT Function of ANN LT sw ............................................................................................................ C

MI-33-01-02 SIGNS Overhead Panel

33-01-02-01 EMER EXIT LT OFF light ..................................................................................................................A
33-01-02-02 AUTO Function of SEAT BELT SIGNS sw ....................................................................................... B
33-01-02-03 AUTO Function of NO SMOKING SIGNS sw ................................................................................... C

MI-33-10 Cockpit General Illumination

33-10-01 Cockpit General Illumination (Center & Main Instrument Lighting, Console and Floor Lighting, Dome lights
and Lighting Strips, Instrument and Panel Integral Lighting, Map Holder Lighting, Center Pedestal Lighting)........ A

MI-33-20 Cabin General Illumination

33-20-01 Cabin General Illumination.......................................................................................................................A
33-20-02 Cabin Signs (No Smoking/No Electronic Devices/Fasten Seat Belt/Return to Seat)............................... B
33-20-03 Lavatory Sign (Return to seat)................................................................................................................ C

MI-33-30 Cargo and Service Compartment Lighting

33-30-01 Cargo and Service Compartment Lighting System..................................................................................A

MI-33-40 Exterior Lighting

33-40-01 Navigation light System 1........................................................................................................................ A
33-40-02 Navigation light System 2........................................................................................................................ B
33-40-03 Landing light.............................................................................................................................................C
33-40-04 Landing light Extension/Retraction System............................................................................................. D
33-40-05 Runway Turnoff light................................................................................................................................ E
33-40-06 Taxi and Takeoff light.............................................................................................................................. F
33-40-07 Logo light................................................................................................................................................. G
33-40-08 Beacon light............................................................................................................................................. H
33-40-09 Wing Scan light......................................................................................................................................... I
33-40-10 Strobe light................................................................................................................................................J
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MI-33-51 Cabin Emergency Lighting
33-51-01 Exit Marking Sign..................................................................................................................................... A
33-51-02 Exit Location Sign in the Main Aisle........................................................................................................B
33-51-03 Overhead Emergency Lighting System in the Main Aisle....................................................................... C
33-51-04 Overhead Emergency Lighting System in the Door Vicinity....................................................................D
33-51-05 Floor Proximity Emergency Escape Path Marking System in the Main Aisle.......................................... E
33-51-07 Floor Proximity Emergency Escape Path Marking System Exit Marker...................................................F
33-51-08 Overwing Emergency light.......................................................................................................................G
33-51-09 Overwing Exit Handle light...................................................................................................................... H
33-51-10 Escape Slide Lighting................................................................................................................................I
33-51-11 Lavatory Auxiliary light..............................................................................................................................J

MI-34 Navigation
MI-34-00 MAINTENANCE Messages on the STATUS SD page
34-00-01 ADR MAINTENANCE Message...............................................................................................................A
34-00-02 IR MAINTENANCE Message...................................................................................................................B

MI-34-01 Overhead Panels

MI-34-01-01 ADIRS Overhead Panel
34-01-01-01 ADR pb-sw FAULT light .................................................................................................................... A
34-01-01-02 ADR pb-sw OFF light ........................................................................................................................ B
34-01-01-03 IR pb-sw FAULT light ........................................................................................................................C
34-01-01-04 IR pb-sw OFF light ............................................................................................................................ D
34-01-01-05 ON BAT light ..................................................................................................................................... E
34-01-01-31 ADR pb-sw .........................................................................................................................................F
34-01-01-32 IR pb-sw ............................................................................................................................................ G
34-01-01-33 IR Mode selector ............................................................................................................................... H

MI-34-01-02 GPWS Overhead Panel

34-01-02-01 GPWS SYS FAULT light ................................................................................................................... A

MI-34-05 Indications on the Primary Flight Display (PFD)

34-05-01 Actual Airspeed Reference Line and Scale Indication on the PFD ........................................................ A
34-05-02 Mach Number Indication on the PFD ..................................................................................................... B
34-05-03 VMO/MMO Characteristic Speed Indication on the PFD ....................................................................... C
34-05-04 Altitude Indication on the PFD ............................................................................................................... D
34-05-05 Baro Reference Indication on the PFD .................................................................................................. E
34-05-06 Vertical Speed in Inertial Mode Indication on the PFD ...........................................................................F
34-05-07 Other Air Data Related Indications on the PFD .....................................................................................G
34-05-08 Attitude Indication on the PFD ............................................................................................................... H
34-05-09 Heading Indication on the PFD ................................................................................................................I
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MI-34-06 Indications on the Navigation Display (ND)
34-06-01 Ground Speed Indication on the ND ...................................................................................................... A
34-06-02 True Air Speed Indication on the ND ..................................................................................................... B
34-06-03 Wind Indication on the ND ..................................................................................................................... C
34-06-04 Heading Indication on the ND ................................................................................................................ D
34-06-05 Position (Aircraft Symbol) Indication on the ND ..................................................................................... E
34-06-06 Radio Navaids Indications on the ND .....................................................................................................F
34-06-07 Chrono Indication on the ND ................................................................................................................. G

MI-34-10 Air Data/Inertial Reference System (ADIRS)

34-10-01 ADR 1.......................................................................................................................................................A
34-10-02 ADR 2 ..................................................................................................................................................... B
34-10-03 ADR 3 ..................................................................................................................................................... C
34-10-04 IR 1 ......................................................................................................................................................... D
34-10-05 IR 2 ........................................................................................................................................................E
34-10-06 IR 3 ......................................................................................................................................................... F

MI-34-11 Sensors
34-11-01 Angle of Attack ( AOA ) Sensor ............................................................................................................. A
34-11-02 CAPT Total Air Temperature ( TAT ) Sensor Element Connected to the ADR 1 ................................... B
34-11-03 CAPT Total Air Temperature ( TAT ) Sensor Element Connected to the ADR 3 ................................... C
34-11-04 F/O Total Air Temperature ( TAT ) Sensor Element Connected to the ADR 2 .......................................D

MI-34-22 Attitude and Heading Standby Data

34-22-01 Standby Compass Indicator.....................................................................................................................A
34-22-02 Standby Compass Lighting...................................................................................................................... B

MI-34-23 Integrated Standby Instrument System (ISIS)

34-23-01 ISIS Altitude Indication.............................................................................................................................A
34-23-02 ISIS Airspeed Indication...........................................................................................................................B
34-23-03 ISIS Bugs Indication................................................................................................................................ C
34-23-04 ISIS Attitude Indication............................................................................................................................ D
34-23-05 ISIS ILS Indication................................................................................................................................... E
34-23-06 ISIS Mach Number Indication.................................................................................................................. F

MI-34-30 Landing and Taxiing Aid

34-30-04 Instrument Landing System ( ILS ) ........................................................................................................ A
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MI-34-40 GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar
34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness and Warning System (TAWS)............. A
34-40-02 Radio Altimeter Automatic Callout........................................................................................................... B
34-40-03 Radio Altimeter System........................................................................................................................... C
34-40-04 Traffic Collision Avoidance System (TCAS)............................................................................................ D
34-40-05 Weather Radar System............................................................................................................................E
34-40-06 Predictive Windshear Detection Function................................................................................................ F
34-40-07 PULL UP-GPWS pb-sw ..........................................................................................................................G

MI-34-50 ATC and Radio / GPS Navigation Systems

34-50-01 ATC ......................................................................................................................................................... A
34-50-03 ADF ......................................................................................................................................................... B
34-50-04 DME ........................................................................................................................................................ C
34-50-05 VOR ........................................................................................................................................................ D
34-50-06 MARKER.................................................................................................................................................. E
34-50-09 Global Positioning System (GPS)............................................................................................................ F

MI-35 Oxygen
MI-35-01 Overhead Panels
MI-35-01-01 OXYGEN Overhead Panel
35-01-01-01 CREW SUPPLY pb-sw OFF light ......................................................................................................A
35-01-01-02 PASSENGER SYS ON light ..............................................................................................................B
35-01-01-03 HI ALT LANDING pb-sw ON light ..................................................................................................... C
35-01-01-31 MANUAL Control of the MASK MAN ON pb .................................................................................... D
35-01-01-32 AUTO Control of the MASK MAN ON pb ..........................................................................................E
35-01-01-33 HI ALT LANDING pb-sw ....................................................................................................................F

MI-35-07 Indications on the DOOR/OXY SD page

35-07-01 Crew OXY High Pressure Indication on the DOOR/OXY SD page ........................................................A
35-07-02 Crew Oxygen REGUL LO PR Indication on the DOOR/OXY SD page ..................................................B

MI-35-10 Crew Oxygen

35-10-01 Crew Oxygen Mask..................................................................................................................................A
35-10-02 Crew Oxygen Mask Microphone..............................................................................................................B
35-10-03 Exterior Crew Oxygen Overpressure Indicator Disc (Green Disc)...........................................................C
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MI-35-20 Passenger Oxygen
35-20-01 Passenger Oxygen Unit........................................................................................................................... A
35-20-02 Cabin Attendant Oxygen Unit.................................................................................................................. B
35-20-03 Lavatory Oxygen Unit.............................................................................................................................. C
35-20-04 Galley Oxygen Unit..................................................................................................................................D
35-20-05 Manual Release Tool............................................................................................................................... E
1
MI-35-30 Portable Oxygen
35-30-01 Flight Crew Portable Device.................................................................................................................... A
35-30-02 Cabin Attendant Portable Device.............................................................................................................B
35-30-03 Cabin Attendant Portable Device............................................................................................................ C

MI-36 Pneumatic
2
MI-36-00 MAINTENANCE Message on the STATUS SD Page
36-00-01 AIR BLEED MAINTENANCE Message................................................................................................... A

MI-36-01 AIR COND Overhead Panel

36-01-01 ENG BLEED pb-sw FAULT light ............................................................................................................ A
36-01-02 ENG BLEED pb-sw OFF light ................................................................................................................ B
36-01-03 APU BLEED pb-sw FAULT light ............................................................................................................ C
36-01-04 APU BLEED pb-sw ON light .................................................................................................................. D

MI-36-07 Indications on the BLEED SD page

36-07-01 APU Bleed Valve Indication on the BLEED SD page ............................................................................ A
36-07-02 Engine Bleed Valve Indication on the BLEED SD page .........................................................................B
36-07-03 Engine Bleed HP Valve Indication on the BLEED SD page .................................................................. C
36-07-04 Engine Bleed Precooler Inlet Pressure Indication on the BLEED SD page ........................................... D
36-07-05 Engine Bleed Precooler Outlet Temperature Indication on the BLEED SD page ...................................E
36-07-06 X Bleed Valve Indication on the BLEED SD page ................................................................................. F

MI-36-11 Engine Bleed Air Supply System

36-11-01 Engine Bleed Air Supply System.............................................................................................................A
36-11-02 Engine Bleed Valve ( PRV ) ...................................................................................................................B
36-11-03 Engine Bleed Overpressure Valve...........................................................................................................C
36-11-04 Engine Bleed Fan Air Valve.................................................................................................................... D
36-11-05 Engine Bleed Air Precooler......................................................................................................................E
36-11-06 Engine Bleed IP Check Valve ................................................................................................................ F
36-11-07 Engine Bleed HP Valve ..........................................................................................................................G
36-11-08 Bleed Monitoring Computer ( BMC ) ......................................................................................................H
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MI-36-12 APU Bleed Air Supply and Crossbleed Systems
36-12-01 APU Bleed Air Supply System.................................................................................................................A
36-12-02 APU Bleed Valve .................................................................................................................................... B
36-12-03 APU Bleed Check Valve ........................................................................................................................ C
36-12-04 Automatic Control of the X Bleed Valve..................................................................................................D
36-12-05 Manual Control of the X Bleed Valve...................................................................................................... E

MI-36-22 Leak Detection Loop

36-22-01 Pylon Leak Detection System..................................................................................................................A
36-22-02 Wing Leak Detection System...................................................................................................................B
36-22-03 APU Leak Detection Loop....................................................................................................................... C

MI-46 Information Systems

MI-46-21 Air Traffic and Information Management System
46-21-01 Air Traffic Service Unit (ATSU)................................................................................................................A

MI-47 Inert Gas System

MI-47-00 MAINTENANCE Message on the STATUS SD Page
47-00-01 FUEL INERT MAINTENANCE Message................................................................................................. A

MI-47-10 Generation/Storage
47-10-01 Fuel Tank Inerting System.......................................................................................................................A

MI-49 Airborne Auxiliary Power

MI-49-00 MAINTENANCE Message on the STATUS SD page
49-00-01 APU MAINTENANCE Message............................................................................................................... A

MI-49-01 APU Overhead Panel

49-01-01 APU MASTER SW pb-sw FAULT light .................................................................................................. A
49-01-02 APU MASTER SW pb-sw ON light ........................................................................................................ B
49-01-03 APU START pb-sw AVAIL light ............................................................................................................. C
49-01-04 APU START pb-sw ON light .................................................................................................................. D

MI-49-07 Indications on the APU SD page

49-07-01 Indications on the APU SD page ........................................................................................................... A

MI-49-10 Power Plant

49-10-01 Power Plant ( APU ) ...............................................................................................................................A
49-10-02 APU Air Intake Flap................................................................................................................................. B
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MI-52 Doors
MI-52-01 Overhead Panels
MI-52-01-01 CKPT DOOR CONT Normal Overhead Panel
52-01-01-01 CHAN (1, 2) LEDs on the CKPT DOOR CONT Overhead Panel...................................................... A
52-01-01-02 STRIKE (TOP, MID, BOT) LEDs on the CKPT DOOR CONT Overhead Panel.................................B
52-01-01-03 Pressure Rate Sensor on the CKPT DOOR CONT Overhead Panel................................................ C

MI-52-07 Indications on the DOOR/OXY SD page

52-07-01 Passenger Door Permanently Indicated Open on the DOOR/OXY SD page ......................................... A
52-07-02 Passenger Door Permanently Indicated Closed on the DOOR/OXY SD page .......................................B
52-07-03 Overwing Emergency Exit Permanently Indicated Open on the DOOR/OXY SD page ..........................C
52-07-04 Overwing Emergency Exit Permanently Indicated Closed on the DOOR/OXY SD page ........................D
52-07-05 Cargo Door Indication on the DOOR/OXY SD page ..............................................................................E
52-07-06 Avionics Compartment Access Door Indication on the DOOR/OXY SD page ........................................F

MI-52-10 Passenger/Crew Door

52-10-01 Cabin Passenger Door.............................................................................................................................A
52-10-02 Overwing Emergency Exit........................................................................................................................B
52-10-03 Passenger Exit Stop Fitting..................................................................................................................... C
52-10-04 Door Damper Function............................................................................................................................ D
52-10-05 Door Emergency Opening Function.........................................................................................................E
52-10-06 CHECK DOOR PRESSURE Message on the Flight Attendant Panel (FAP)...........................................F
52-10-07 Passenger Door Stay Mechanism...........................................................................................................G
52-10-08 CABIN PRESSURE light (on Doors)....................................................................................................... H

MI-52-30 Cargo Door

52-30-01 Cargo Door (FWD, AFT and BULK)........................................................................................................ A
52-30-02 Cargo Door Actuator................................................................................................................................ B
52-30-03 Cargo Door Electrical Control..................................................................................................................C
52-30-04 Cargo Door Locking Hooks and Spools (Rollers)....................................................................................D
52-30-05 Cargo Door Hand Pump.......................................................................................................................... E
52-30-06 Cargo Door Drift Pin................................................................................................................................ F
52-30-07 Cargo Doors Open/Locked Indicator light .............................................................................................. G

MI-52-33 Bulk Cargo Compartment Door

52-33-01 Cargo Door Balance Mechanism.............................................................................................................A
Continued on the following page

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Continued from the previous page

MI-52-51 Reinforced Cockpit Door (CDLS)
52-51-01 CDLS Normal System (Normal Control Unit, Toggle Switch and Lights on Cockpit Door Panel, Buzzer,
Keypad, Door Strike Release). .............................................................................................................................. A
52-51-03 CDLS Buzzer........................................................................................................................................... B
52-51-04 CDLS Keypad .........................................................................................................................................C
52-51-05 CDLS Keypad LED .................................................................................................................................D
52-51-06 CDLS Door Release Strike (Catch, Spring, Solenoid, Bolt).................................................................... E
52-51-07 CDLS Deadbolt........................................................................................................................................ F

MI-52-53 COCKPIT DOOR Panel on the Center Pedestal

52-53-01 COCKPIT DOOR FAULT light ................................................................................................................A
52-53-02 COCKPIT DOOR OPEN light .................................................................................................................B
52-53-03 LOCK Function of the COCKPIT DOOR sw .......................................................................................... C
52-53-04 UNLOCK Function of the COCKPIT DOOR sw ..................................................................................... D

MI-56 Windows
MI-56-10 Cockpit
56-10-01 Front Windshield...................................................................................................................................... A
56-10-02 Lateral Fixed/Sliding Window...................................................................................................................B
56-10-03 Sliding Window Opening/Closing Mechanism......................................................................................... C

MI-56-20 Cabin
56-20-01 Cabin Window.......................................................................................................................................... A

MI-70 Engine
MI-70-00 MAINTENANCE Messages on the STATUS SD page
70-00-01 ENG FADEC MAINTENANCE Message................................................................................................. A
70-00-02 ENG EIU MAINTENANCE Message....................................................................................................... B
70-00-03 ENG EVMU MAINTENANCE Message...................................................................................................C

MI-73 Engine Fuel and Control

MI-73-07 Indications on the ENGINE SD page
73-07-01 Fuel Used Indication on the ENGINE SD page ..................................................................................... A
73-07-02 Fuel Filter Clog Indication on the ENGINE SD page ............................................................................. B

MI-73-08 Indications on the EWD

73-08-01 Fuel Flow Indication on the EWD............................................................................................................A

MI-73-09 ECAM Alert

73-09-01 ENG 1(2) FUEL FILTER CLOG Alert...................................................................................................... A
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MI-73-10 Distribution
73-10-01 Fuel Return Valve.................................................................................................................................... A
73-10-03 Fuel Metering Valve................................................................................................................................. B
73-10-04 Engine HP Fuel Valve............................................................................................................................. C

MI-73-20 Controlling
73-20-01 Flex Takeoff Mode................................................................................................................................... A
73-20-04 EPR Control Mode ..................................................................................................................................B
73-20-05 Minimum Idle on Ground......................................................................................................................... C
73-20-06 EEC ACFT 28V Power Supply................................................................................................................ D

MI-74 Ignition
MI-74-07 Indications on the ENGINE SD page
74-07-01 Selected Igniter Indication on the ENGINE SD page ............................................................................. A

MI-74-09 ECAM Alert

74-09-01 ENG 1(2) IGN A(B)(A+B) FAULT Alert....................................................................................................A

MI-74-31 Ignition Starting and Continuous Relight

74-31-01 Ignition System A..................................................................................................................................... A
74-31-02 Ignition System B..................................................................................................................................... B

MI-76 Engine Controls

MI-76-11 Throttle Control
76-11-01 Thrust lever Position Sensor....................................................................................................................A

MI-77 Engine Indicating

MI-77-07 Indications on SD pages
MI-77-07-01 Indications on the CRUISE SD page
77-07-01-01 N1 Vibration Indication on the CRUISE SD page ............................................................................. A
77-07-01-02 N2 Vibration Indication on the CRUISE SD page ............................................................................. B
77-07-01-03 F. USED (Fuel Used) Indication on the CRUISE SD page ...............................................................C
77-07-01-04 OIL QT (Oil Quantity) Indication on the CRUISE SD page ...............................................................D

MI-77-07-02 Indications on the ENGINE SD page

77-07-02-01 Engine Bleed Pressure Indication on the ENGINE SD page ............................................................ A
77-07-02-02 Fuel Filter Clog Indication on the ENGINE SD page ........................................................................ B
77-07-02-03 Fuel Used Indication on the ENGINE SD page ................................................................................ C
77-07-02-04 Nacelle Temperature Indication on the ENGINE SD page ............................................................... D
77-07-02-05 N1 Vibration Indication on the ENGINE SD page ............................................................................. E
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77-07-02-06 N2 Vibration Indication on the ENGINE SD page ............................................................................. F
77-07-02-07 Oil Filter Clog Indication on the ENGINE SD page ...........................................................................G
77-07-02-08 Oil Pressure Indication on the ENGINE SD page .............................................................................H
77-07-02-09 Oil Quantity Indication on the ENGINE SD page ............................................................................... I
77-07-02-10 Oil Temperature Indication on the ENGINE SD page ........................................................................J
77-07-02-11 Selected Igniter Indication on the ENGINE SD page ........................................................................ K
77-07-02-12 Start Valve Position Indication on the ENGINE SD page .................................................................. L

MI-77-08 Indications on the EWD

77-08-01 EGT Indication on the EWD ................................................................................................................... A
77-08-02 EPR Indication on the EWD ................................................................................................................... B
77-08-03 Fuel Flow Indication on the EWD .......................................................................................................... C
77-08-04 N1 Indication on the EWD ......................................................................................................................D
77-08-05 N2 Indication on the EWD ......................................................................................................................E

MI-78 Exhaust
MI-78-08 Indications on the EWD
78-08-01 REV Indication on the EWD ................................................................................................................... A

MI-78-30 Thrust Reversers

78-30-01 Thrust Reverser........................................................................................................................................A
78-30-02 Thrust Reverser Inhibition Relay sw .......................................................................................................B
78-30-03 Thrust Reverser Shutoff Valve................................................................................................................ C

MI-79 Oil
MI-79-07 Indications on the ENGINE SD page
79-07-01 CLOG Indication on the ENGINE SD page ............................................................................................A
79-07-02 Oil Pressure Indication and Advisory on the ENGINE SD page ........................................................... B
79-07-03 Oil Quantity Indication on the ENGINE SD page ...................................................................................C
79-07-04 Oil Temperature Indication on the ENGINE SD page ............................................................................D

MI-79-09 ECAM Alerts

79-09-01 ENG 1(2) OIL LO PR Alert .....................................................................................................................A
79-09-02 ENG 1(2) OIL FILTER CLOG Alert......................................................................................................... B
79-09-03 ENG 1(2) BEARING 4 OIL SYS Alert..................................................................................................... C

MI-79-20 Distribution
79-20-01 Air Cooled Oil Cooler ( ACOC ) Modulating Valve .................................................................................A
79-20-02 EMCD Visual Pop-Out Indicator.............................................................................................................. B

MI-79-40 IDG Oil Cooling System

79-40-01 Fuel Return Valve.................................................................................................................................... A
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MI-80 Starting
MI-80-01 ENG MAN START Overhead Panel
80-01-31 ENG MAN START pb-sw ....................................................................................................................... A

MI-80-07 Indication on the ENGINE SD page

80-07-01 Start Valve Position Indication on the ENGINE SD page .......................................................................A

MI-80-11 Pneumatic Starter and Valve System

80-11-01 Start Valve................................................................................................................................................A

MI-80-12 ENG MASTER Panel on the Center Pedestal

80-12-01 FAULT light on the ENG MASTER Panel............................................................................................... A

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Localization Toc ID Reason

Title Index
MI-PLP-TOC 1 Documentation update: Deletion of the "20800295.9001002 Cabin
Portable Oxygen Attendant Portable Device" documentary unit.
MI-PLP-TOC 2 Documentation update: Deletion of the "00008776 AIR BLEED
MAINTENANCE Message on the MAINTENANCE Message" table of content entry.
STATUS SD Page Documentation update: Deletion of the "00008776.0014001 AIR
BLEED MAINTENANCE Message" documentary unit.
MI-23-10 B 1 Clarification of note 2 to reflect that note applies when 2 VHFs are
23-10-02 VHF System needed.
MI-35-30 C 1 Documentation update: Addition of "Cabin Attendant Portable
35-30-03 Cabin Attendant Portable Device" documentary unit
Device
MI-00-08 A 1 Effectivity update: The information no longer applies to MSN 4972.
ECAM and MAINTENANCE STATUS
MI-00-08 A 2 Effectivity update: The information now also applies to MSN 4972.
ECAM and MAINTENANCE STATUS
MI-31-00 C 1 Effectivity update: The information no longer applies to MSN 4516,
31-00-05 DMC 1/3 MAINTENANCE 4767, 4972, 5178, 5234.
Message
MI-31-00 C 2 Effectivity update: The information now also applies to MSN 4516,
31-00-05 DMC 1/3 MAINTENANCE 4767, 4972, 5178, 5234.
Message
MI-47-00 A 1 Effectivity update: The information no longer applies to MSN 5178,
47-00-01 FUEL INERT 5234.
MAINTENANCE Message
MI-47-10 A 1 Effectivity update: The information now also applies to MSN 5178,
47-10-01 Fuel Tank Inerting System 5234.

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MMEL APPROVAL REFERENCE

Ident.: MI-00-01-00010655.0001001 / 27 FEB 15
Applicable to: ALL

LAN COLOMBIA AIRLINES

REVISION
MINIMUM EQUIPMENT LIST
31 October 2014

APPROVAL REFERENCE
APPROVED BY: EASA
Approval date: 31 OCT 14
Approval reference: 0010002556-001
Approved by: David SOLAR EASA - Large Transport Aeroplanes Section Manager

This Master Minimum Equipment List (MMEL) is approved by the European Aviation Safety Agency
(EASA) at the above revision date under the Type Certificate (EASA TC No. A.064 as part of the
Operational Suitability Data (OSD) as per Regulation (EU) 748/2012 as amended by Regulation (EU)
No. 69/2014.
The applicability date of this MMEL starts at the issue date + 30 calendar days.
Note: The issue date is different from the EASA approval date. The issue date corresponds to the
date of initiation of the publication of the Operator's MMEL by Airbus. The issue date may vary from
Operator to Operator. The issue date appears in the Transmittal Letter (for the PDF format) and in the
LIBRARY panel of the OPS LIBRARY Browser (for the electronic consultation).
The EASA approval date appears in the MMEL Approval Reference of the MMEL Preamble.
The 90 days limit as referred to in PART ORO.MLR.105(c) is recommended to start from the
applicability date.

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INTRODUCTION TO THE MMEL

Ident.: MI-00-02-00012615.0001001 / 14 SEP 10
Applicable to: ALL

The MMEL is developed to improve the aircraft utilization and thereby to provide more convenient
and economic air transportation for the public.
The MMEL is a document that lists the system, function, or equipment which may be temporarily
inoperative, subject to certain conditions, while maintaining an acceptable level of safety. It does not
contain obviously required items such as wings, flaps, and rudders.
ALL ITEMS RELATED TO THE AIRWORTHINESS OF THE AIRCRAFT AND NOT INCLUDED IN
THE MMEL ARE AUTOMATICALLY REQUIRED TO BE OPERATIVE FOR DISPATCH.
Non-safety related equipment such as galley equipment and passenger convenience items need not
be listed.
The MMEL is the basis for the development of individual Operator's MEL which take into
consideration the Operator's particular aircraft equipment configuration and operational conditions. In
order to maintain an acceptable level of safety and reliability, the MMEL establishes limitations on the
duration of and conditions for operation with inoperative item.

INTRODUCTION TO THE MEL

Ident.: MI-00-02-00012616.0001001 / 14 SEP 10
Applicable to: ALL

The Minimum Equipment List (MEL) is based on the Master Minimum Equipment List (MMEL).
An Operator's MEL may differ in format from the MMEL, but cannot be less restrictive than the
MMEL.
The MEL shall not deviate from any applicable Airworthiness Directive or any other Mandatory
Requirement.
The MEL is intended to permit operation with inoperative items of system, function, or equipment for
a period of time until repairs can be accomplished. It is important that repairs be accomplished at the
earliest opportunity.
Suitable conditions and limitations in the form of placards, maintenance procedures, crew operational
procedures, and other restrictions are necessary in the MEL to ensure that an acceptable level of
safety is maintained.
The MEL takes into consideration the Operator's particular aircraft equipment, configuration and
operational conditions, routes being flown, and requirements set by the appropriate Authority.
When an item is discovered to be inoperative, it is reported by making an entry in the technical
logbook. The item is then either rectified or may be deferred per the MEL before further operation.
MEL conditions and limitations do not relieve the operator from determining that the aircraft is in a fit
condition for safe operation with items inoperative.
The provisions of the MEL are applicable until the aircraft commences the flight. Any decision
to continue a flight following a failure or unserviceability which becomes apparent after the

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commencement of a flight must be subject to pilot judgment and good airmanship. The Commander
may continue to make reference to and use the MEL as appropriate.
By approval of the MEL, the Authority permits dispatch of the aircraft for revenue, ferry, or training
flights with certain items inoperative provided an acceptable level of safety is maintained by use of
appropriate operational or maintenance procedures, by transfer of the function to another operating
system, or by reference to other instruments or system providing the required information.
Operators are to establish a controlled and sound repair programme including the parts, personnel,
facilities, procedures, and schedules to ensure timely repair. This programme should identify the
actions required for Maintenance discrepancy messages.

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CRITERIA FOR DISPATCH

Ident.: MI-00-03-00012617.0001001 / 14 SEP 10
Applicable to: ALL

The decision of the Commander of the flight to have inoperative items corrected before the flight
will take precedence over the provisions contained in the MEL. The Commander may request
requirements above the minimum listed, whenever in his judgment such added equipment is
essential to the safety of a particular flight under the special condition prevailing at the time.
The MEL cannot take into account all multiple unserviceabilities. Therefore, before dispatching an
aircraft with multiple MEL items inoperative, it must be assured that any interface or inter-relationship
between inoperative items will not result in a degradation in the level of safety and/or an undue
increase in crew workload. It is particularly in this area of multiple discrepancies and especially
discrepancies in related systems, that good judgment, based on the circumstances of the case,
including climatic and en-route conditions, must be used.

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MAINTENANCE ACTION
Ident.: MI-00-04-00012619.0001001 / 14 SEP 10
Applicable to: ALL

Every effort shall be made by the maintenance to correct all technical defects as early as practicable
and that the aircraft be released from a maintenance station in fully operational condition. The
Commander must be informed by the maintenance as soon as practicable, should it be impossible to
rectify the inoperative item before the dispatch.
Whenever an aircraft is released by the maintenance for dispatch with items inoperative, the
following is required:
The technical logbook aboard the aircraft must contain a detailed description of the inoperative
item(s), special advice to the flight crew, if necessary, and information about corrective action
taken.
When they are accessible to the crew in flight, the control(s), and/or indicator(s) related to
inoperative system(s), function(s) or component(s) must be clearly placarded.
Note: 1. To the extent practical, placards should be located adjacent to the control or indicator
for the item affected. However, unless otherwise specified, placard wording and location
should be determined by the operator.
2. If inadvertent operation could produce a hazard, such equipment must be rendered
inoperative (physically) as given in the appropriate Maintenance Procedure.
3. The relevant Operational Procedures are contained in the MEL.
4. The relevant Maintenance Procedures are contained in the Aircraft Maintenance Manual.

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REPAIR INTERVAL
Ident.: MI-00-05-00012620.0001001 / 12 SEP 11
Applicable to: ALL

Inoperative items, deferred in accordance with the MEL, must be rectified at or before the expiration
of the repair interval that is established by the following letter designators given in the "Repair
Interval" column.
Repair Interval A : No standard interval is specified, however, items in this category shall
be rectified in accordance with the dispatch conditions stated in the
MEL.
Where a time period is specified in calendar days, it shall start at 00:01
on the calendar day following the day of discovery.
Where a time period is specified in number of flights or flight hours, it
shall start at the beginning of the first flight following the discovery of
the failure.
Repair Interval B : Items in this category shall be rectified within three (3) consecutive
calendar days, excluding the day of discovery.
For example, if it were recorded at 13:00 on January 26th, the 3-day
interval begins at 00:01 on January 27th and ends at 23:59 on January
29th.
Repair Interval C : Items in this category shall be rectified within ten (10) consecutive
calendar days, excluding the day of discovery.
For example, if it were recorded at 13:00 on January 26th, the 10-day
interval begins at 00:01 on January 27th and ends at 23:59 on February
5th.
Repair Interval D : Items in this category shall be rectified within one hundred and twenty
(120) consecutive calendar days, excluding the day of discovery.
Repair Interval (-) : Items with dash in the rectification interval mean that its rectification
interval is subject to the referenced item usually by the phrase Refer to.

LAN COLOMBIA FLEET MI-00-05 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
00 - PREAMBLE
00-05 - Repair Interval
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-00-05 P 2/2

MEL 05 NOV 13
 MEL ITEMS
00 - PREAMBLE
00-06 - Repair Interval Extension
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

REPAIR INTERVAL EXTENSION

Ident.: MI-00-06-00012621.0001001 / 14 SEP 10
Applicable to: ALL

Subject to the approval of the Authority, the operator may use a procedure for the extension of the
applicable Repair Interval B, C, and D, for the same duration as specified in the MEL, provided that:
A description of specific duties and responsibilities for controlling extensions is established by the
operator and accepted by the Authority, and
The operator only grants a one-time extension of the applicable Repair Interval, and
The Authority is notified of any extension granted within a timescale acceptable to the Authority,
and
Repair is accomplished at the earliest opportunity.

LAN COLOMBIA FLEET MI-00-06 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
00 - PREAMBLE
00-06 - Repair Interval Extension
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-00-06 P 2/2

MEL 05 NOV 13
 MEL ITEMS
00 - PREAMBLE
00-07 - Definitions
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

DEFINITIONS
Ident.: MI-00-07-00012622.0001001 / 10 OCT 14
Applicable to: ALL

As required by : The listed item must comply with applicable Operational regulations.
regulations
Calendar day : A 24 hour period from 00:01 to 23:59 based on local time.
Centralized Fault Display : It identifies the faulty system for maintenance purpose and is not
System (CFDS) required for dispatch of the aircraft.
Considered inoperative : The listed item of equipment must be treated as inoperative.
For example, MEL item 36-11-05 Bleed Air Precooler indicates that
associated bleed air supply system is considered inoperative and
therefore MEL item 36-11-01 Bleed Air Supply System must be applied.
Therefore, the considered inoperative MEL item must also be entered
and the associated dispatch conditions must be applied, including the
respective (o) and (m) procedures if any.
The shorter rectification interval between the initial inoperative item and
the considered inoperative item shall be applied.
Daylight operations : Period between the beginning of the morning civil twilight and the end
of the evening civil twilight relevant to the local aeronautical airspace; or
such other period, as may be prescribed by the appropriate Authority.
Flammable or : Material which is capable of catching fire and burning.
combustible material Where loading of flammable or combustible material is prohibited, no
material may be loaded except the following: cargo handling equipment
(Unloaded, empty or with ballast), fly away kits (excluding e.g. cans
of hydraulic fluid, cleaning solvents, batteries, capacitors, chemical
generators, etc.), and in-flight service material (Return catering - only
closed catering trolleys/boxes, no newspapers, no alcohol or duty free
goods).
Note: If serviceable tires are included, they should only be inflated to
a minimum pressure that preserves their serviceability.

Flight : For the purpose of an MEL, one flight is defined as the period of time
that begins the moment at which an aircraft begins to move by its own
means in preparation for takeoff, continues during takeoff and the
applicable flight phases, and ends when the aircraft lands and comes to
a complete stop in its parking area.
Icing Conditions : Refer to AFM/ ---.

LAN COLOMBIA FLEET MI-00-07 P 1/2

MEL A 10 OCT 14
 MEL ITEMS
00 - PREAMBLE
00-07 - Definitions
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Inoperative : The listed item of equipment is unserviceable or malfunctioning to

the extent that it does not accomplish its intended purpose, or is
not consistently functioning within its designed operating limits or
tolerances.
Some systems have been designed to be fault tolerant and are
monitored by digital computers which transmit fault messages to the
CFDS. The presence of this category of fault messages does not mean
that the system is inoperative.
... provided that system : The system X must not be reported to be inoperative in the logbook.
X is operative
... provided that system : The system X must be checked and confirmed operative via either an
X is checked operative (o) and/or an (m) procedure.
Required cabin attendant: A seat in the aeroplane cabin which meets the following conditions:
seat Where the certification of the cabin requires this seat to be occupied
by a qualified cabin crew member as specified in the Operations
Manual, and
This seat is a part of the station to which a qualified cabin crew
member is to be assigned for the flight, and
The qualified cabin crew member assigned to the station is a
member of the minimum cabin crew designated for the flight.
VMC (Visual : Under IFR or VFR the crew must maintain Visual Meteorological
Meteorological Conditions.
Conditions)
** Double Asterisk : Shows items affected for CAT II/III operations.
Note: This list is not exhaustive and the Operator should include in their MEL any definition which
is considered to be relevant.

LAN COLOMBIA FLEET MI-00-07 P 2/2

MEL A 10 OCT 14
 MEL ITEMS
00 - PREAMBLE
00-08 - ECAM and MAINTENANCE STATUS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM AND MAINTENANCE STATUS

Ident.: MI-00-08-00012623.0002001 / 27 FEB 15
Applicable to: MSN 5229, 5263-5364

ECAM
The A320 Family aircraft is equipped with the Electronic Centralized Aircraft Monitoring ( ECAM )
which provides different levels of aircraft systems monitoring messages:
ECAM warning
ECAM advisory
ECAM caution
ECAM memo
ECAM warning and ECAM caution messages are listed in the " MMEL Entries" section.
ECAM advisory and ECAM memo messages are not listed in the " MMEL Entries" section.
HANDLING OF MAINTENANCE MESSAGES ON THE STATUS SD page
At the beginning of each ATA chapter of the " MMEL Item" section, the related MAINTENANCE
messages which may be displayed on the STATUS SD page are listed in the Sub-Chapter "00"
with the associated dispatch status.
A MAINTENANCE message indicates the presence of a category of failure which can only be
identified by interrogation of the CFDS .
Operator must implement procedures to manage the MAINTENANCE messages and associated
CFDS messages, to handle fault recording and repair within the repair interval C (10 days).
All MAINTENANCE messages have a repair interval C except the following messages: DAR ,
DMU or ACMS , QAR and ICE DETECT which have a repair interval D.
Dispatch with MAINTENANCE messages displayed on the STATUS SD page is permitted without
condition except for the following messages:
AIR BLEED: Refer to Item 36-00-01 AIR BLEED MAINTENANCE Message
DMC 1/3: Refer to Item 31-00-05 DMC 1/3 MAINTENANCE Message
DMC 2/3: Refer to Item 31-00-06 DMC 2/3 MAINTENANCE Message
It is left to Operator to define the role devoted to flight crew and/or maintenance personnel in these
procedures.

LAN COLOMBIA FLEET MI-00-08 P 1/4

MEL A 27 FEB 15
 MEL ITEMS
00 - PREAMBLE
00-08 - ECAM and MAINTENANCE STATUS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM AND MAINTENANCE STATUS

Ident.: MI-00-08-00012623.0011001 / 27 FEB 15
1 Applicable to: MSN 4892-4943

ECAM
The A320 Family aircraft is equipped with the Electronic Centralized Aircraft Monitoring ( ECAM )
which provides different levels of aircraft systems monitoring messages:
ECAM warning
ECAM advisory
ECAM caution
ECAM memo
ECAM warning and ECAM caution messages are listed in the " MMEL Entries" section.
ECAM advisory and ECAM memo messages are not listed in the " MMEL Entries" section.
HANDLING OF MAINTENANCE MESSAGES ON THE STATUS SD page
At the beginning of each ATA chapter of the " MMEL Item" section, the related MAINTENANCE
messages which may be displayed on the STATUS SD page are listed in the Sub-Chapter "00"
with the associated dispatch status.
A MAINTENANCE message indicates the presence of a category of failure which can only be
identified by interrogation of the CFDS .
Operator must implement procedures to manage the MAINTENANCE messages and associated
CFDS messages, to handle fault recording and repair within the repair interval C (10 days).
All MAINTENANCE messages have a repair interval C except the following messages: DAR ,
DMU or ACMS , QAR and ICE DETECT which have a repair interval D.
Dispatch with MAINTENANCE messages displayed on the STATUS SD page is permitted without
condition except for the following messages:
AIR BLEED: Refer to Item 36-00-01 AIR BLEED MAINTENANCE Message
DMC 1/3: Refer to Item 31-00-05 DMC 1/3 MAINTENANCE Message
DMC 2/3: Refer to Item 31-00-06 DMC 2/3 MAINTENANCE Message
ENG FADEC : Refer to Item 70-00-01 ENG FADEC MAINTEANCE Message (for engines
affected by CFM VSB 73-0241)
It is left to Operator to define the role devoted to flight crew and/or maintenance personnel in these
procedures.

LAN COLOMBIA FLEET MI-00-08 P 2/4

MEL A 27 FEB 15
 MEL ITEMS
00 - PREAMBLE
00-08 - ECAM and MAINTENANCE STATUS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM AND MAINTENANCE STATUS

Ident.: MI-00-08-00012623.0017001 / 27 FEB 15
Applicable to: MSN 4516-4546, 5178, 5234, 5443-5453

ECAM
The A320 Family aircraft is equipped with the Electronic Centralized Aircraft Monitoring ( ECAM )
which provides different levels of aircraft systems monitoring messages:
ECAM warning
ECAM advisory
ECAM caution
ECAM memo.
ECAM warning and ECAM caution messages are listed in the " MMEL Entries" section.
ECAM advisory and ECAM memo messages are not listed in the " MMEL Entries" section.
HANDLING OF MAINTENANCE MESSAGES ON THE STATUS SD page
At the beginning of each ATA chapter of the " MMEL Item" section, the related MAINTENANCE
messages which may be displayed on the STATUS SD page are listed in the Sub-Chapter "00"
with the associated dispatch status.
A MAINTENANCE message indicates the presence of a category of failure which can only be
identified by interrogation of the CFDS .
Operator must implement procedures to manage the MAINTENANCE messages and associated
CFDS messages, to handle fault recording and repair within the repair interval C (10 days).
All MAINTENANCE messages have a repair interval C except the following messages: DAR ,
DMU or ACMS , QAR and ICE DETECT which have a repair interval D.
Dispatch with MAINTENANCE messages displayed on the STATUS SD page is permitted without
condition except for the following message:
AIR BLEED: Refer to Item 36-00-01 AIR BLEED MAINTENANCE Message .
It is left to Operator to define the role devoted to flight crew and/or maintenance personnel in these
procedures.

ECAM AND MAINTENANCE STATUS

Ident.: MI-00-08-00012623.0026001 / 27 FEB 15
2 Applicable to: MSN 4758-4767, 4972

ECAM
The A320 Family aircraft is equipped with the Electronic Centralized Aircraft Monitoring ( ECAM )
which provides different levels of aircraft systems monitoring messages:

LAN COLOMBIA FLEET MI-00-08 P 3/4

MEL A 27 FEB 15
 MEL ITEMS
00 - PREAMBLE
00-08 - ECAM and MAINTENANCE STATUS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ECAM warning
ECAM advisory
ECAM caution
ECAM memo.
ECAM warning and ECAM caution messages are listed in the " MMEL Entries" section.
ECAM advisory and ECAM memo messages are not listed in the " MMEL Entries" section.
HANDLING OF MAINTENANCE MESSAGES ON THE STATUS SD page
At the beginning of each ATA chapter of the " MMEL Item" section, the related MAINTENANCE
messages which may be displayed on the STATUS SD page are listed in the Sub-Chapter "00"
with the associated dispatch status.
A MAINTENANCE message indicates the presence of a category of failure which can only be
identified by interrogation of the CFDS .
Operator must implement procedures to manage the MAINTENANCE messages and associated
CFDS messages, to handle fault recording and repair within the repair interval C (10 days).
All MAINTENANCE messages have a repair interval C except the following messages: DAR ,
DMU or ACMS , QAR and ICE DETECT which have a repair interval D.
Dispatch with MAINTENANCE messages displayed on the STATUS SD page is permitted without
condition except for the following messages:
AIR BLEED: Refer to Item 36-00-01 AIR BLEED MAINTENANCE Message
ENG FADEC : Refer to Item 70-00-01 ENG FADEC MAINTEANCE Message (for engines
affected by CFM VSB 73-0241).
It is left to Operator to define the role devoted to flight crew and/or maintenance personnel in these
procedures.

LAN COLOMBIA FLEET MI-00-08 P 4/4

MEL A 27 FEB 15
 MEL ITEMS
21 - AIR CONDITIONING
21-00 - MAINTENANCE Messages on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-00-04 TEMP CTL 1(2) MAINTENANCE Message

Ident.: MI-21-00-00007461.0001001 / 27 FEB 15
Applicable to: ALL

21-00-04A
Repair interval Nbr installed Nbr required Placard
C No
TEMP CTL 1(2) MAINTENANCE message may be displayed on the STATUS SD page.

LAN COLOMBIA FLEET MI-21-00 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
21 - AIR CONDITIONING
21-00 - MAINTENANCE Messages on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-00 P 2/2

MEL 27 FEB 15
 MEL ITEMS
21 - AIR CONDITIONING
21-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 21-01-01 - AIR COND Overhead Panel
MINIMUM EQUIPMENT LIST

21-01-01-01 PACK pb-sw FAULT light

Ident.: MI-21-01-01-00007462.0001001 / 21 MAR 10
Applicable to: ALL

21-01-01-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

21-01-01-02 PACK pb-sw OFF light

Ident.: MI-21-01-01-00007463.0001001 / 21 MAR 10
Applicable to: ALL

21-01-01-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

21-01-01-03 HOT AIR pb-sw FAULT light

Ident.: MI-21-01-01-00007464.0001001 / 21 MAR 10
Applicable to: ALL

21-01-01-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that all zone duct temperature indications are operative on the
COND SD page.

LAN COLOMBIA FLEET MI-21-01-01 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 21-01-01 - AIR COND Overhead Panel
MINIMUM EQUIPMENT LIST

21-01-01-04 HOT AIR pb-sw OFF light

Ident.: MI-21-01-01-00007465.0001001 / 21 MAR 10
Applicable to: ALL

21-01-01-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-21-01-01 P 2/2

MEL D 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 21-01-02 - CABIN PRESS Overhead Panel
MINIMUM EQUIPMENT LIST

21-01-02-01 CABIN PRESS MODE SEL pb-sw FAULT light

Ident.: MI-21-01-02-00007466.0001001 / 21 MAR 10
Applicable to: ALL

21-01-02-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-21-01-02 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 21-01-02 - CABIN PRESS Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-01-02 P 2/2

MEL 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 21-01-03 - CARGO VENT Overhead Panel
MINIMUM EQUIPMENT LIST

21-01-03-02 AFT ISOL VALVE pb-sw FAULT light

Ident.: MI-21-01-03-00007468.0001001 / 27 FEB 15
Applicable to: ALL

21-01-03-02A
Repair interval Nbr installed Nbr required Placard
D 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-21-01-03 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
21 - AIR CONDITIONING
21-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 21-01-03 - CARGO VENT Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-01-03 P 2/2

MEL 27 FEB 15
 MEL ITEMS
21 - AIR CONDITIONING
21-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 21-01-04 - VENTILATION Overhead Panel
MINIMUM EQUIPMENT LIST

21-01-04-01 CAB FANS pb-sw OFF light

Ident.: MI-21-01-04-00007469.0001001 / 21 MAR 10
Applicable to: ALL

21-01-04-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

21-01-04-02 BLOWER pb-sw FAULT light

Ident.: MI-21-01-04-00007470.0001001 / 21 MAR 10
Applicable to: ALL

21-01-04-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

21-01-04-03 EXTRACT pb-sw FAULT light

Ident.: MI-21-01-04-00007471.0001001 / 21 MAR 10
Applicable to: ALL

21-01-04-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-21-01-04 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 21-01-04 - VENTILATION Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-01-04 P 2/2

MEL 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES 21-07-01 - Indications on the BLEED SD page
MINIMUM EQUIPMENT LIST

21-07-01-01 Pack Outlet Temperature Indication on the BLEED SD page

Ident.: MI-21-07-01-00007512.0001001 / 21 MAR 10
Applicable to: ALL

21-07-01-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

21-07-01-02 Pack Turbine Bypass Valve Position Indication on the BLEED SD page
Ident.: MI-21-07-01-00007513.0001001 / 21 MAR 10
Applicable to: ALL

21-07-01-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

21-07-01-03 Pack Compressor Outlet Temperature

Indication on the BLEED SD page
Ident.: MI-21-07-01-00007514.0001001 / 21 MAR 10
Applicable to: ALL

21-07-01-03A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

LAN COLOMBIA FLEET MI-21-07-01 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES 21-07-01 - Indications on the BLEED SD page
MINIMUM EQUIPMENT LIST

21-07-01-04 Pack Flow Indication on the BLEED SD page

Ident.: MI-21-07-01-00007515.0001001 / 21 MAR 10
Applicable to: ALL

21-07-01-04A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

21-07-01-05 Pack Flow Control Valve Position Indication on the BLEED SD page
Ident.: MI-21-07-01-00007516.0001001 / 21 MAR 10
Applicable to: ALL

21-07-01-05A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

21-07-01-06 Emergency Ram Air Inlet Indication on the BLEED SD page

Ident.: MI-21-07-01-00007517.0001001 / 21 MAR 10
Applicable to: ALL

21-07-01-06A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-21-07-01 P 2/2

MEL D to F 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES 21-07-02 - Indications on the CAB PRESS SD page
MINIMUM EQUIPMENT LIST

21-07-02-01 INLET and EXTRACT Indications on the CAB PRESS SD page

Ident.: MI-21-07-02-00007518.0001001 / 21 MAR 10
Applicable to: ALL

21-07-02-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.
Note: During ground operations, correct avionics ventilation should be provided.

21-07-02-02 Pressure Safety Valves Position Indication on the CAB PRESS SD page
Ident.: MI-21-07-02-00007519.0001001 / 21 MAR 10
Applicable to: ALL

21-07-02-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(m) Pressure safety valves may be indicated open provided that both valves are visually
checked closed.
Reference(s)
(m) Refer to AMM 21-31-00-040-004

21-07-02-03 Pack 1 and 2 Indications on the CAB PRESS SD page

Ident.: MI-21-07-02-00007520.0001001 / 21 MAR 10
Applicable to: ALL

21-07-02-03A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

LAN COLOMBIA FLEET MI-21-07-02 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES 21-07-02 - Indications on the CAB PRESS SD page
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-07-02 P 2/2

MEL 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES 21-07-03 - Indications on the COND SD page
MINIMUM EQUIPMENT LIST

21-07-03-01 Indications on the COND SD page

Ident.: MI-21-07-03-00007521.0001001 / 23 MAR 11
Applicable to: ALL

21-07-03-01A
Repair interval Nbr installed Nbr required Placard
C 11 0 No
One or more indications may be inoperative.

LAN COLOMBIA FLEET MI-21-07-03 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES 21-07-03 - Indications on the COND SD page
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-07-03 P 2/2

MEL 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES 21-07-04 - Indications on the CRUISE SD page
MINIMUM EQUIPMENT LIST

21-07-04-01 Indications on the CRUISE SD page

Ident.: MI-21-07-04-00007522.0001001 / 23 MAR 11
Applicable to: ALL

21-07-04-01A
Repair interval Nbr installed Nbr required Placard
C 7 4 No
Cabin and cockpit zone indications may be inoperative.

LAN COLOMBIA FLEET MI-21-07-04 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES 21-07-04 - Indications on the CRUISE SD page
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-07-04 P 2/2

MEL 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-09-01 VENT BLOWER FAULT Alert

Ident.: MI-21-09-00007523.0001001 / 12 SEP 11
Applicable to: ALL

Note: During ground operations, correct avionics ventilation should be provided.

21-09-01A Blower fan operative

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be displayed provided that:
1) The blower fan is checked operative before each flight, and
2) The VENT AVNCS SYS FAULT alert is checked operative before each flight.
Reference(s)
(o) Refer to OpsProc 21-09-01A VENT BLOWER FAULT Alert
(m) Refer to AMM 21-26-00-040-010

21-09-01B Blower fan inoperative

Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be displayed provided that the avionics blower fan is considered inoperative.
Refer to Item 21-26-01 Avionics Blower Fan

21-09-02 VENT EXTRACT FAULT Alert

Ident.: MI-21-09-00007524.0001001 / 12 SEP 11
Applicable to: ALL

Note: During ground operations, correct avionics ventilation should be provided.

Continued on the following page

LAN COLOMBIA FLEET MI-21-09 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

21-09-02A Extract fan operative
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be displayed provided that:
1) The extract fan is checked operative before each flight, and
2) The VENT AVNCS SYS FAULT alert is checked operative before each flight.
Reference(s)
(o) Refer to OpsProc 21-09-02A VENT EXTRACT FAULT Alert
(m) Refer to AMM 21-26-00-040-011

21-09-02B Extract fan inoperative

Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be displayed provided that the avionics extract fan is considered inoperative.
Refer to Item 21-26-02 Avionics Extract Fan

21-09-03 CAB PR SAFETY VALVE OPEN Alert

Ident.: MI-21-09-00007525.0001001 / 21 MAR 10
Applicable to: ALL

21-09-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(m) May be displayed provided that both safety valves are visually checked closed.
Reference(s)
(m) Refer to AMM 21-31-00-040-005

LAN COLOMBIA FLEET MI-21-09 P 2/2

MEL B to C 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-21 - Air Distribution and Recirculation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-21-01 Cabin Fan

Ident.: MI-21-21-00007472.0001001 / 21 MAR 10
Applicable to: ALL

21-21-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative.

LAN COLOMBIA FLEET MI-21-21 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-21 - Air Distribution and Recirculation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-21 P 2/2

MEL 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-23 - Lavatory and Galley Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-23-01 Lavatory and Galley Extraction Fan

Ident.: MI-21-23-00007473.0002001 / 21 MAR 10
Applicable to: ALL

21-23-01B
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative provided that all duct temperatures indications for the cabin are
operative on the COND SD page .
Reference(s)
(o) Refer to OpsProc 21-23-01B Lavatory and Galley Extraction Fan

LAN COLOMBIA FLEET MI-21-23 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-23 - Lavatory and Galley Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-23 P 2/2

MEL 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-26-01 Avionics Blower Fan

Ident.: MI-21-26-00007474.0001001 / 12 SEP 11
Applicable to: ALL

Note: During ground operation, correct avionics ventilation should be provided.

21-26-01A VENT AVNCS SYS FAULT not displayed

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that:
1) The BLOWER pb-sw is set to OVRD, and
2) Both air conditioning packs are operative, and
3) The VENT AVNCS SYS FAULT alert is not displayed.
Reference(s)
(o) Refer to OpsProc 21-26-01A Avionics Blower Fan (VENT AVNCS SYS FAULT Alert not
displayed)

21-26-01B Air conditioning inlet valve checked open

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) (m) May be inoperative provided that:
1) The BLOWER pb-sw is set to OVRD, and
2) Both air conditioning packs are operative, and
3) The air conditioning inlet valve is checked open before each flight.
Reference(s)
(o) Refer to OpsProc 21-26-01B Avionics Blower Fan (Air conditioning inlet valve checked open
before each flight)
(m) Refer to AMM 21-26-00-040-006
Continued on the following page

LAN COLOMBIA FLEET MI-21-26 P 1/10

MEL A 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

21-26-01C Avionics ventilation system checked
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) (m) May be inoperative provided that:
1) The BLOWER pb-sw is set to OVRD, and
2) Both air conditioning packs are operative, and
3) The air conditioning inlet valve is secured in the open position, and
4) The avionics ventilation system is checked before each flight.
Reference(s)
(o) Refer to OpsProc 21-26-01C Avionics Blower Fan (Avionics ventilation system checked
before each flight)
(m) Refer to AMM 21-26-00-040-013

21-26-02 Avionics Extract Fan

Ident.: MI-21-26-00007475.0001001 / 12 SEP 11
Applicable to: ALL

Note: During ground operation, correct avionics ventilation should be provided.

21-26-02A VENT AVNCS SYS FAULT not displayed

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that:
1) The blower fan is operative, and
2) The EXTRACT pb-sw is set to OVRD, and
3) Both air conditioning packs are operative, and
4) The VENT AVNCS SYS FAULT alert is not displayed.
Reference(s)
(o) Refer to OpsProc 21-26-02A Avionics Extract Fan (VENT AVNCS SYS FAULT Alert not
displayed)
Continued on the following page

LAN COLOMBIA FLEET MI-21-26 P 2/10

MEL A to B 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

21-26-02B Air conditioning inlet valve checked open
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) (m) May be inoperative provided that:
1) The blower fan is operative, and
2) The EXTRACT pb-sw is set to OVRD, and
3) Both air conditioning packs are operative, and
4) The air conditioning inlet valve is checked open before each flight.
Reference(s)
(o) Refer to OpsProc 21-26-02B Avionics Extract Fan (Air conditioning inlet valve checked open
before each flight)
(m) Refer to AMM 21-26-00-040-007

21-26-02C Avionics ventilation system checked

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) (m) May be inoperative provided that:
1) The blower fan is operative, and
2) The EXTRACT pb-sw is set to OVRD, and
3) Both air conditioning packs are operative, and
4) The air conditioning inlet valve is secured in the open position, and
5) The avionics ventilation system is checked before each flight.
Reference(s)
(o) Refer to OpsProc 21-26-02C Avionics Extract Fan (Avionics ventilation system checked
before each flight)
(m) Refer to AMM 21-26-00-040-015

LAN COLOMBIA FLEET MI-21-26 P 3/10

MEL B 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-26-03 Avionics Skin Exchanger Inlet Bypass Valve

Ident.: MI-21-26-00007476.0001001 / 21 MAR 10
Applicable to: ALL

21-26-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that:
1) The avionics skin exchanger inlet bypass valve is manually secured in the closed
position, and
2) The avionics ventilation system is checked before each flight.
Note: During ground operations, correct avionics ventilation should be provided.
Reference(s)
(o) Refer to OpsProc 21-26-03A Avionics Skin Exchanger Inlet Bypass Valve
(m) Refer to AMM 21-26-00-040-001

21-26-04 Avionics Skin Air Outlet Valve

Ident.: MI-21-26-00007477.0001001 / 21 MAR 10
Applicable to: ALL

21-26-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that:
1) The internal flap is manually secured in the open position, and
2) The skin air outlet valve is displayed in a partially open position amber or green on the
CAB PRESS SD page , and
3) Both air conditioning packs are operative, and
4) The skin exchanger isolation valve is secured in the open position, and
5) The avionics ventilation system is checked before each flight.
Note: During ground operations, correct avionics ventilation should be provided.
Continued on the following page

LAN COLOMBIA FLEET MI-21-26 P 4/10

MEL C to D 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 21-26-04A Avionics Skin Air Outlet Valve
(m) Refer to AMM 21-26-00-040-002

21-26-05 Avionics Skin Air Inlet Valve

Ident.: MI-21-26-00007478.0001001 / 12 SEP 11
Applicable to: ALL

Note: During ground operations, correct avionics ventilation should be provided.

21-26-05A Air Conditioning Inlet Valve open on ground

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that:
1) The avionics skin air inlet valve is manually secured in the closed position, and
2) The air conditioning inlet valve is open on ground, and
3) The avionics ventilation system is checked before each flight.
Reference(s)
(o) Refer to OpsProc 21-26-05A Avionics Skin Air Inlet Valve (Air conditioning inlet valve open
on the ground)
(m) Refer to AMM 21-26-00-040-004

21-26-05B Air Conditioning Inlet Valve Secured Open

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that:
1) The avionics skin air inlet valve is manually secured in the closed position, and
2) The air conditioning inlet valve is secured in the open position, and
3) The avionics ventilation system is checked before each flight.
Continued on the following page

LAN COLOMBIA FLEET MI-21-26 P 5/10

MEL D to E 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 21-26-05B Avionics Skin Air Inlet Valve (Air conditioning inlet valve
secured in the open position)
(m) Refer to AMM 21-26-00-040-014

21-26-06 Avionics Skin Exchanger Isolation Valve

Ident.: MI-21-26-00007479.0001001 / 12 SEP 11
Applicable to: ALL

Note: During ground operations, correct avionics ventilation should be provided.

21-26-06A Valve inoperative in the open position

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative in the open position provided that the avionics ventilation system is
checked before each flight.
Reference(s)
(o) Refer to OpsProc 21-26-06A Avionics Skin Exchanger Isolation Valve
(m) Refer to AMM 21-26-00-040-008

21-26-06B Valve secured open

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that:
1) The avionics skin exchanger isolation valve is secured in the open position, and
Note: If the valve cannot be secured in the open position, it can be interchanged with
the skin exchanger outlet bypass valve.
2) The avionics ventilation system is checked before each flight.
Continued on the following page

LAN COLOMBIA FLEET MI-21-26 P 6/10

MEL E to F 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 21-26-06B Avionics Skin Exchanger Isolation Valve
(m) Refer to AMM 21-26-00-040-016

21-26-07 Avionics Skin Exchanger Outlet Bypass Valve

Ident.: MI-21-26-00007480.0001001 / 21 MAR 10
Applicable to: ALL

21-26-07A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.
Note: During ground operations, correct avionics ventilation should be provided.

21-26-08 Avionics Air Conditioning Inlet Valve

Ident.: MI-21-26-00007481.0001001 / 21 MAR 10
Applicable to: ALL

21-26-08A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that:
1) The avionics air conditioning inlet valve is manually secured in the open position, and
2) Both air conditioning packs are operative, and
3) The avionics ventilation is checked before each flight.
Note: During ground operations, correct avionics ventilation should be provided.
Reference(s)
(o) Refer to OpsProc 21-26-08A Avionics Air Conditioning Inlet Valve
(m) Refer to AMM 21-26-00-040-003

LAN COLOMBIA FLEET MI-21-26 P 7/10

MEL F to H 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-26-09 Avionics Ventilation Filter

Ident.: MI-21-26-00007483.0001001 / 12 SEP 11
Applicable to: ALL

Note: During ground operations, correct avionics ventilation should be provided.

21-26-09A VENT AVNCS SYS FAULT not displayed

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative (clogged) provided that:
1) The blower and extract fans are operative, and
2) The EXTRACT pb-sw is set to OVRD, and
3) Both air conditioning packs are operative, and
4) The VENT AVNCS SYS FAULT alert is not displayed.
Reference(s)
(o) Refer to OpsProc 21-26-09A Avionics Ventilation Filter (VENT AVNCS SYS FAULT Alert
not displayed)

21-26-09B Valve checked open

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative (clogged) provided that:
1) The blower and extract fans are operative, and
2) The EXTRACT pb-sw is set to OVRD, and
3) Both air conditioning packs are operative, and
4) The air conditioning inlet valve is checked open before each flight.
Reference(s)
(o) Refer to OpsProc 21-26-09B Avionics Ventilation Filter (Air conditioning inlet valve checked
open before each flight)
(m) Refer to AMM 21-26-00-040-009
Continued on the following page

LAN COLOMBIA FLEET MI-21-26 P 8/10

MEL I 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

21-26-09C Valve secured open
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative (clogged) provided that:
1) The blower and extract fans are operative, and
2) The EXTRACT pb-sw is set to OVRD, and
3) Both air conditioning packs are operative, and
4) The air conditioning inlet valve is secured in the open position, and
5) The avionics ventilation system is checked before each flight.
Reference(s)
(o) Refer to OpsProc 21-26-09C Avionics Ventilation Filter (Avionics ventilation system checked
before each flight)
(m) Refer to AMM 21-26-00-040-017

21-26-10 Avionics Equipment Ventilation Computer ( AEVC )

Ident.: MI-21-26-00007484.0001001 / 21 MAR 10
Applicable to: ALL

21-26-10A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that:
1) Both air conditioning packs are operative, and
2) The BLOWER pb-sw and the EXTRACT pb-sw are set to OVRD, and
3) The air conditioning inlet valve and the skin air outlet valve are checked in the correct
position before each flight, and
4) The extract fan is checked operative before each flight, and
5) The skin air inlet valve is secured in the closed position.
Note: During ground operations, correct avionics ventilation should be provided.
Reference(s)
(o) Refer to OpsProc 21-26-10A Avionics Equipment Ventilation Computer (AEVC)
(m) Refer to AMM 21-26-00-040-005

LAN COLOMBIA FLEET MI-21-26 P 9/10

MEL I to J 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-26 P 10/10

MEL 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-28 - Cargo Compartment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-28-03 AFT Cargo Extraction Fan

Ident.: MI-21-28-00007488.0001001 / 27 FEB 15
Applicable to: ALL

21-28-03A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 21-28-03A AFT Cargo Extraction Fan

21-28-04 AFT Cargo Isolation Valve

Ident.: MI-21-28-00007489.0001001 / 10 OCT 14
Applicable to: ALL

21-28-04A AFT ISOL VALVE pb-sw FAULT light operative

Repair interval Nbr installed Nbr required Placard
D 2 0 No
(o) One or both may be inoperative provided that:
1) Both valves are checked closed, and
2) AFT ISOL VALVE pb-sw FAULT light is checked operative.
Reference(s)
(o) Refer to OpsProc 21-28-04A AFT Cargo Isolation Valve (Valves ckecked closed)

21-28-04B Both valves secured closed

Repair interval Nbr installed Nbr required Placard
D 2 0 No
(o) (m) One or both may be inoperative provided that both valves are secured in the closed
position.
Reference(s)
(o) Refer to OpsProc 21-28-04B AFT Cargo Isolation Valve (Valves secured closed)
(m) Refer to AMM 21-28-00-040-002

LAN COLOMBIA FLEET MI-21-28 P 1/2

MEL A to B 27 FEB 15
 MEL ITEMS
21 - AIR CONDITIONING
21-28 - Cargo Compartment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-28 P 2/2

MEL 27 FEB 15
 MEL ITEMS
21 - AIR CONDITIONING
21-31 - Pressure Control and Monitoring
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-31-01 Automatic Cabin Pressure Control System

( CPC , Outflow Valve AUTO Channel)
Ident.: MI-21-31-00007492.0001001 / 12 SEP 11
Applicable to: ALL

21-31-01A Automatic CPC 1 inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) Automatic cabin pressure control system 1 may be inoperative provided that:
1) ETOPS is not conducted, and
2) It is deactivated, and
3) The cabin pressure indications on the CAB PRESS SD page are checked operative in
manual mode, and
4) The LDG ELEV selector MAN function is operative.
Reference(s)
(o) Refer to OpsProc 21-31-01A Automatic Cabin Pressure Control System (CPC, Outflow
Valve AUTO Channel)

21-31-01B Automatic CPC 2 inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) Automatic cabin pressure control system 2 may be inoperative provided that:
1) It is deactivated, and
2) The cabin pressure indications on the CAB PRESS SD page are checked operative in
manual mode, and
3) The LDG ELEV selector MAN function is operative.
Reference(s)
(o) Refer to OpsProc 21-31-01B Automatic Cabin Pressure Control System (CPC, Outflow
Valve AUTO Channel)
Continued on the following page

LAN COLOMBIA FLEET MI-21-31 P 1/4

MEL A 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-31 - Pressure Control and Monitoring
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

21-31-01C Both automatic CPC s inoperative
Repair interval Nbr installed Nbr required Placard
C 2 0 No
Both may be inoperative provided that:
1) The manual cabin pressure control system is operative, and
2) The flight is not pressurized.
Refer to FCOM/PRO-SPO-20 Flight Without Cabin Pressurization

21-31-02 Manual Cabin Pressure Control System (MAN

V/S CTL selector, Outflow Valve MAN Channel)
Ident.: MI-21-31-00007493.0001001 / 21 MAR 10
Applicable to: ALL

21-31-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(m) May be inoperative provided that:
1) The LDG ELEV selector MAN function is operative, and
2) Both automatic cabin pressure control systems are checked operative before each flight.
Reference(s)
(m) Refer to AMM 21-31-00-040-002

21-31-03 Pressure Safety Valve

Ident.: MI-21-31-00007494.0001001 / 21 MAR 10
Applicable to: ALL

21-31-03A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(m) One may be inoperative in the closed position provided that:
1) Both automatic cabin pressure control systems are operative, and
2) The three outflow valve motors are checked operative.
Continued on the following page

LAN COLOMBIA FLEET MI-21-31 P 2/4

MEL A to C 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-31 - Pressure Control and Monitoring
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(m) Refer to AMM 21-31-00-040-001

21-31-04 Landing Elevation Selection AUTO Function

Ident.: MI-21-31-00007495.0001001 / 21 MAR 10
Applicable to: ALL

21-31-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 21-31-04A Landing Elevation Selection AUTO Function

21-31-05 Landing Elevation Selection MAN Function

Ident.: MI-21-31-00007496.0001001 / 21 MAR 10
Applicable to: ALL

21-31-05A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that:
1) The landing elevation selection AUTO function is operative, and
2) Both FMGC s are operative.
Reference(s)
(o) Refer to OpsProc 21-31-05A Landing Elevation Selection MAN Function

LAN COLOMBIA FLEET MI-21-31 P 3/4

MEL C to E 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-31 - Pressure Control and Monitoring
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-31 P 4/4

MEL 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-51 - Pack Flow Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-51-02 Pack Flow Selection

Ident.: MI-21-51-00007500.0001001 / 21 MAR 10
Applicable to: ALL

21-51-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

21-51-03 Pack Flow Sensor

Ident.: MI-21-51-00007501.0001001 / 27 FEB 15
Applicable to: ALL

21-51-03A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) One may be inoperative.
Reference(s)
(o) Refer to OpsProc 21-51-03A Pack Flow Sensor

LAN COLOMBIA FLEET MI-21-51 P 1/2

MEL A to B 27 FEB 15
 MEL ITEMS
21 - AIR CONDITIONING
21-51 - Pack Flow Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-51 P 2/2

MEL 27 FEB 15
 MEL ITEMS
21 - AIR CONDITIONING
21-52 - Air Cooling System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-52-01 Air Conditioning Pack

Ident.: MI-21-52-00007502.0010001 / 27 FEB 15
Applicable to: ALL

21-52-01D With speedbrakes available for 'C' repair interval

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(o) (m) One may be inoperative provided that:
1) ETOPS is not conducted, and
2) The following alerts:
AIR PACK 1(2) REGUL FAULT
AIR COND CTL 1(2)-A FAULT
AIR COND CTL 1(2)-B FAULT
associated with the operative pack are not displayed on the EWD , and
3) The affected PACK 1(2) pb-sw is set to OFF, and
4) The speedbrakes are operative, and
5) The associated pack flow control valve is secured in the closed position, and
Reference(s)
(o) Refer to OpsProc 21-52-01D Air Conditioning Pack (One Air Conditioning Pack Inoperative
for C Repair Interval)
(m) Refer to AMM 21-51-00-040-002

21-52-01E Limitation to 31 500 ft for 'C' repair interval

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(o) (m) One may be inoperative provided that:
1) ETOPS is not conducted, and
2) The flight altitude is limited to 31 500 ft ( 9 600 m ), and
3) The following alerts:
AIR PACK 1(2) REGUL FAULT
AIR COND CTL 1(2)-A FAULT
AIR COND CTL 1(2)-B FAULT
associated with the operative pack are not displayed on the EWD , and
4) The affected PACK 1(2) pb-sw is set to OFF, and
5) The associated pack flow control valve is secured in the closed position, and
Continued on the following page

LAN COLOMBIA FLEET MI-21-52 P 1/4

MEL A 27 FEB 15
 MEL ITEMS
21 - AIR CONDITIONING
21-52 - Air Cooling System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 21-52-01E Air Conditioning Pack (One Air Conditioning Pack Inoperative
for C Repair Interval)
(m) Refer to AMM 21-51-00-040-002

21-52-01G Air cycle machine failed

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) One may be operated on heat exchanger cooling only (air cycle machine failure) provided
that:
1) The following alerts:
AIR COND CTL 1(2)-A FAULT
AIR COND CTL 1(2)-B FAULT
associated with the operative pack are not displayed on the EWD , and
2) The affected pack outlet temperature indication is operative on the BLEED SD page .
Reference(s)
(o) Refer to OpsProc 21-52-01G Air Conditioning Pack (One Air Conditioning Pack in Heat
Exchanger Cooling Mode Only)

21-52-01H Non pressurized flight

Repair interval Nbr installed Nbr required Placard
C 2 0 No
Both may be inoperative provided that the flight is not pressurized.
Refer to FCOM/PRO-SPO-20 Flight Without Cabin Pressurization

LAN COLOMBIA FLEET MI-21-52 P 2/4

MEL A 27 FEB 15
 MEL ITEMS
21 - AIR CONDITIONING
21-52 - Air Cooling System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-52-02 Air Conditioning Pack Ram Air Inlet Flap

Ident.: MI-21-52-00007503.0002001 / 12 SEP 11
Applicable to: ALL

21-52-02A Flap deactivated

Repair interval Nbr installed Nbr required Placard
C 2 0 No
(m) One or both may be inoperative provided that the affected flap is deactivated in the open
position.
Reference(s)
(m) Refer to AMM 21-61-00-040-002

21-52-02B Only one inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative in the closed position provided that the associated air conditioning
pack is considered inoperative.
Refer to Item 21-52-01 Air Conditioning Pack

21-52-02C Non pressurized flight

Repair interval Nbr installed Nbr required Placard
C 2 0 No
Both may be inoperative in the closed position provided that the flight is not pressurized.
Refer to FCOM/PRO-SPO-20 Flight Without Cabin Pressurization

LAN COLOMBIA FLEET MI-21-52 P 3/4

MEL B 27 FEB 15
 MEL ITEMS
21 - AIR CONDITIONING
21-52 - Air Cooling System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-52 P 4/4

MEL 27 FEB 15
 MEL ITEMS
21 - AIR CONDITIONING
21-55 - Emergency Ram Air Inlet
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-55-01 Emergency Ram Air Inlet

Ident.: MI-21-55-00007505.0001001 / 12 SEP 11
Applicable to: ALL

21-55-01A Ram air inlet deactivated

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(m) May be inoperative provided that:
1) The emergency ram air inlet is deactivated in the closed position, and
2) Both air conditioning packs are checked operative.
Reference(s)
(m) Refer to AMM 21-55-00-040-002

21-55-01B Non pressurized flight

Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative in the open position provided that:
1) ETOPS and extended overwater flight is not conducted, and
2) The flight is not pressurized.
Refer to FCOM/PRO-SPO-20 Flight Without Cabin Pressurization

LAN COLOMBIA FLEET MI-21-55 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-55 - Emergency Ram Air Inlet
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-55 P 2/2

MEL 05 NOV 13
 MEL ITEMS
21 - AIR CONDITIONING
21-61 - Pack Temperature Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-61-01 Pack Turbine Bypass Valve

Ident.: MI-21-61-00007506.0001001 / 21 MAR 10
Applicable to: ALL

21-61-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative.

LAN COLOMBIA FLEET MI-21-61 P 1/2

MEL A 10 OCT 14
 MEL ITEMS
21 - AIR CONDITIONING
21-61 - Pack Temperature Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-61 P 2/2

MEL 10 OCT 14
 MEL ITEMS
21 - AIR CONDITIONING
21-63 - Cockpit and Cabin Temperature Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-63-02 Cockpit and Cabin Trim Air Valve

Ident.: MI-21-63-00007509.0002001 / 27 FEB 15
Applicable to: ALL

21-63-02A Affected valve checked closed

Repair interval Nbr installed Nbr required Placard
C 3 0 No
(o) One or more may be inoperative provided that the affected valve is checked closed on the
COND SD page .
Reference(s)
(o) Refer to OpsProc 21-63-02A Cockpit and Cabin Trim Air Valve (Affected valve
secured/checked in the closed position)

21-63-02B Hot air pressure valve checked operative

Repair interval Nbr installed Nbr required Placard
C 3 0 No
(o) One or more may be inoperative provided that the hot air pressure regulating valve is
checked operative on the COND SD page .
Reference(s)
(o) Refer to OpsProc 21-63-02B Cockpit and Cabin Trim Air Valve (Hot air pressure regulating
valve checked closed/operative)

21-63-02E Hot air pressure valve considered inoperative

Repair interval Nbr installed Nbr required Placard
C 3 0 No
One or more may be inoperative provided that the hot air pressure regulating valve is
considered inoperative.
Refer to Item 21-63-03 Hot Air Pressure Regulating Valve

LAN COLOMBIA FLEET MI-21-63 P 1/4

MEL A 27 FEB 15
 MEL ITEMS
21 - AIR CONDITIONING
21-63 - Cockpit and Cabin Temperature Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-63-03 Hot Air Pressure Regulating Valve

Ident.: MI-21-63-00007510.0002001 / 27 FEB 15
Applicable to: ALL

Note: 1. Unequal passengers distribution may cause high temperature in the rear cabin when
more than one trim air valves are inoperative or when the hot air pressure regulating
valve is closed.
2. The temperature in the cockpit may be low when the hot air pressure regulating valve is
closed combined with single pack operation.

21-63-03A Hot air pressure valve checked closed

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative in the closed position provided that:
1) HOT AIR pb-sw is set to OFF, and
2) Hot Air Pressure Regulating Valve is checked closed on the COND SD page .
Reference(s)
(o) Refer to OpsProc 21-63-03A Hot Air Pressure Regulating Valve (Hot air pressure valve
checked closed)

21-63-03B All trim valve checked closed

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative in the open position provided that:
1) HOT AIR pb-sw is set to OFF, and
2) All Trim Air Valves are checked closed on the COND SD page .
Reference(s)
(o) Refer to OpsProc 21-63-03B Hot Air Pressure Regulating Valve (Trim air valve checked
closed)
Continued on the following page

LAN COLOMBIA FLEET MI-21-63 P 2/4

MEL B 27 FEB 15
 MEL ITEMS
21 - AIR CONDITIONING
21-63 - Cockpit and Cabin Temperature Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

21-63-03C Hot air pressure valve secured closed
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) (m) May be inoperative provided that the hot air pressure regulating valve is secured in the
closed position.
Reference(s)
(o) Refer to OpsProc 21-63-03C Hot Air Pressure Regulating Valve (Affected valve secured in
the closed position)
(m) Refer to AMM 21-63-00-040-002

21-63-04 Air Conditioning System Controller Channel (COND CTL 1(2)-A(B))

Ident.: MI-21-63-00007511.0001001 / 27 FEB 15
Applicable to: ALL

21-63-04A Non ETOPS flight

Repair interval Nbr installed Nbr required Placard
C 4 2 No
One may be inoperative on each side provided that ETOPS is not conducted.

LAN COLOMBIA FLEET MI-21-63 P 3/4

MEL B to C 27 FEB 15
 MEL ITEMS
21 - AIR CONDITIONING
21-63 - Cockpit and Cabin Temperature Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-21-63 P 4/4

MEL 27 FEB 15
 MEL ITEMS
22 - AUTO FLIGHT
22-01 - FLT CTL Overhead Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-01-01 FAC pb-sw FAULT light

Ident.: MI-22-01-00007527.0001001 / 21 MAR 10
Applicable to: ALL

22-01-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
One may be inoperative.

22-01-02 FAC pb-sw OFF light

Ident.: MI-22-01-00007528.0001001 / 21 MAR 10
Applicable to: ALL

22-01-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

LAN COLOMBIA FLEET MI-22-01 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
22 - AUTO FLIGHT
22-01 - FLT CTL Overhead Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-22-01 P 2/2

MEL 05 NOV 13
 MEL ITEMS
22 - AUTO FLIGHT
22-05 - FMA Indications on the PFD
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-05-01 AP Related Indications on the FMA

Ident.: MI-22-05-00007577.0001001 / 12 SEP 11
Applicable to: ALL

22-05-01A Inoperative on one FMA

Repair interval Nbr installed Nbr required Placard
C 54 27 No
**
One or more indications may be inoperative on one FMA .

22-05-01B Inoperative on both FMA s

Repair interval Nbr installed Nbr required Placard
C 54 0 No
(o) One or more indications may be inoperative on both FMA s provided that:
1) ETOPS is not conducted, and
2) The AP is not used.
Reference(s)
(o) Refer to OpsProc 22-05-01B AP/FD Related Indications on the FMA

22-05-02 A/THR Related Indications on the FMA

Ident.: MI-22-05-00007578.0001001 / 12 SEP 11
Applicable to: ALL

22-05-02A Inoperative on one FMA

Repair interval Nbr installed Nbr required Placard
C 34 17 No
**
One or more indications may be inoperative on one FMA .
Continued on the following page

LAN COLOMBIA FLEET MI-22-05 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
22 - AUTO FLIGHT
22-05 - FMA Indications on the PFD
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

22-05-02B Inoperative on both FMA s
Repair interval Nbr installed Nbr required Placard
C 34 0 No
One or more indications may be inoperative on both FMA s provided that the autothrust (
A/THR ) is considered inoperative.
Refer to Item 22-30-01 Autothrust (A/THR)

22-05-03 Approach and Landing Capabilities on the FMA

Ident.: MI-22-05-00007579.0001001 / 23 MAR 11
Applicable to: ALL

22-05-03A
Repair interval Nbr installed Nbr required Placard
C 14 0 No
(o) **
One or more may be inoperative on one or both FMA s.
Reference(s)
(o) Refer to OpsProc 22-05-03A Approach and Landing Capabilities on the FMA

22-05-04 Special Messages on the FMA

Ident.: MI-22-05-00007580.0001001 / 23 MAR 11
Applicable to: ALL

22-05-04A
Repair interval Nbr installed Nbr required Placard
C 16 1 No
MAN PITCH TRIM ONLY is required on one side.

LAN COLOMBIA FLEET MI-22-05 P 2/2

MEL B to D 05 NOV 13
 MEL ITEMS
22 - AUTO FLIGHT
22-10 - Autopilot/Flight Director (AP/FD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-10-01 Autopilot ( AP )
Ident.: MI-22-10-00007529.0001001 / 27 NOV 12
Applicable to: ALL

Note: RVSM Item

Note: RNP Item

22-10-01A One inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(o) **One may be inoperative.
Note: For RVSM operation, one automatic altitude control system must be operative.
Reference(s)
(o) Refer to OpsProc 22-10-01A Autopilot (AP)

22-10-01B Both inoperative

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(o) ** Both may be inoperative provided:
1) ETOPS , RNAV ( RNP ) and RVSM operations are not conducted, and
2) Revenue flight is not dispatched.
Reference(s)
(o) Refer to OpsProc 22-10-01B Autopilot (AP)

22-10-01C
Repair interval Nbr installed Nbr required Placard
2 2 No
Both AP must be operative if RNP < 0.3 for departure or < 1NM in Go-Around is required.

LAN COLOMBIA FLEET MI-22-10 P 1/4

MEL A 18 JUL 14
 MEL ITEMS
22 - AUTO FLIGHT
22-10 - Autopilot/Flight Director (AP/FD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-10-02 Flight Director ( FD )

Ident.: MI-22-10-00007530.0001001 / 14 FEB 13
Applicable to: ALL

Note: RNP item.

Note: RNAV item.

22-10-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(o) Except for RNAV ( RNP ) and RNAV ( GNSS ) both may be inoperative.
Reference(s)
(o) Refer to OpsProc 22-10-02A Flight Director (FD)

22-10-02B
Repair interval Nbr installed Nbr required Placard
2 2 No
Both FD must be operative for RNAV ( RNP ) and RNAV ( GNSS ) operations.

22-10-03 Take-over pb Priority Function

Ident.: MI-22-10-00007531.0001001 / 23 MAR 11
Applicable to: ALL

22-10-03A
Repair interval Nbr installed Nbr required Placard
2 2 No
**
Both must be operative.

LAN COLOMBIA FLEET MI-22-10 P 2/4

MEL B to C 18 JUL 14
 MEL ITEMS
22 - AUTO FLIGHT
22-10 - Autopilot/Flight Director (AP/FD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-10-04 Take-over pb AP Disconnection Function

Ident.: MI-22-10-00007532.0001001 / 12 SEP 11
Applicable to: ALL

22-10-04A One inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) One may be inoperative.
Reference(s)
(o) Refer to OpsProc 22-10-04A Take-over pb AP Disconnection Function (One inoperative)

22-10-04B Both inoperative

Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) Both may be inoperative provided that the AP is not used for approach.
Reference(s)
(o) Refer to OpsProc 22-10-04B Take-over pb AP Disconnection Function (Both inoperative)

22-10-05 AUTO LAND light

Ident.: MI-22-10-00007533.0001001 / 23 MAR 11
Applicable to: ALL

22-10-05A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(o) **
One or both may be inoperative.
Reference(s)
(o) Refer to OpsProc 22-10-05A AUTO LAND light

LAN COLOMBIA FLEET MI-22-10 P 3/4

MEL D to E 18 JUL 14
 MEL ITEMS
22 - AUTO FLIGHT
22-10 - Autopilot/Flight Director (AP/FD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-10-06 AP Disengagement Warning

Ident.: MI-22-10-00007534.0001001 / 23 MAR 11
Applicable to: ALL

22-10-06A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) **
May be inoperative provided that:
1) ETOPS is not conducted, and
2) The AP is not engaged.
Reference(s)
(o) Refer to OpsProc 22-10-06A AP Disengagement Warning

22-10-07 Sticks and Rudder Pedals Locking Solenoid in AP Mode

Ident.: MI-22-10-00007535.0001001 / 23 MAR 11
Applicable to: ALL

22-10-07A
Repair interval Nbr installed Nbr required Placard
C 3 1 No
(o) **
One or two may be inoperative unlocked provided that no autoland is performed.
Reference(s)
(o) Refer to OpsProc 22-10-07A Sticks and Rudder Pedals Locking Solenoid in AP Mode

LAN COLOMBIA FLEET MI-22-10 P 4/4

MEL F to G 18 JUL 14
 MEL ITEMS
22 - AUTO FLIGHT
22-30 - Autothrust
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-30-01 Autothrust ( A/THR )

Ident.: MI-22-30-00007536.0001001 / 23 MAR 11
Applicable to: ALL

22-30-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) **
May be inoperative provided that the autothrust ( A/THR ) is disconnected before each
flight.
Reference(s)
(o) Refer to OpsProc 22-30-01A Autothrust (A/THR)

22-30-02 Autothrust Instinctive Disconnect pb

Ident.: MI-22-30-00007537.0001001 / 21 MAR 10
Applicable to: ALL

22-30-02A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) One may be inoperative provided that the ability to disconnect the autothrust ( A/THR ) via
the remaining Instinctive Disconnect pb and by the FCU A/THR pb is checked before each
flight.
Reference(s)
(o) Refer to OpsProc 22-30-02A Autothrust Instinctive Disconnect pb

LAN COLOMBIA FLEET MI-22-30 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
22 - AUTO FLIGHT
22-30 - Autothrust
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-30-03 Autothrust Disengagement Warning

Ident.: MI-22-30-00007538.0001001 / 12 SEP 11
Applicable to: ALL

22-30-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
** May be inoperative provided that the autothrust ( A/THR ) is considered inoperative.
Refer to Item 22-30-01 Autothrust (A/THR)

LAN COLOMBIA FLEET MI-22-30 P 2/2

MEL C 05 NOV 13
 MEL ITEMS
22 - AUTO FLIGHT
22-60 - Flight Augmentation (FAC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-60-01 FAC 1
Ident.: MI-22-60-00007539.0001001 / 05 NOV 13
Applicable to: ALL

Note: RNP Item

22-60-01A
Repair interval Nbr installed Nbr required Placard
1 1 No
(m) ** Must be operative.
Note: The AUTO FLT FAC 1 FAULT alert may be displayed with the associated AUTO
FLT/FAC1/28VDC C/B tripped.
This may be due to a short circuit within either rudder trim actuator channel 1 or
rudder travel actuator channel 1.
In this case, the FAC 1 may be recovered provided that the affected part of the
faulty actuator is deactivated using the associated maintenance procedure.
Refer to AMM 27-22-00-040-001, or
Refer to AMM 27-23-00-040-001.
Refer to Item 27-22-01 Rudder Trim System , or
Refer to Item 27-23-01 Rudder Travel Limiter System (Including Rudder and
Pedals Travel Limiter Units)
Reference(s)
(m) Refer to AMM

22-60-02 FAC 2
Ident.: MI-22-60-00007540.0001001 / 05 NOV 13
Applicable to: ALL

Note: RNP Item

Continued on the following page

LAN COLOMBIA FLEET MI-22-60 P 1/4

MEL A to B 05 NOV 13
 MEL ITEMS
22 - AUTO FLIGHT
22-60 - Flight Augmentation (FAC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

22-60-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) ** May be inoperative provided that:
1) RNAV ( RNP ) operations are not conducted, and
2) All ADIRS s, ELAC s, SEC s, SFCC s, LGCIU s and RA s are operative, and
3) The Rudder Travel Limiter System 2 is considered inoperative.
Refer to Item 22-60-04 Yaw Damper System , and
Refer to Item 27-22-01 Rudder Trim System , and
Refer to Item 27-23-01 Rudder Travel Limiter System (Including Rudder and Pedals
Travel Limiter Units)
Reference(s)
(o) Refer to OpsProc 22-60-02A FAC 2

22-60-03 Reactive Windshear Detection Function

Ident.: MI-22-60-00007542.0001001 / 05 APR 12
Applicable to: ALL

22-60-03A
Repair interval Nbr installed Nbr required Placard
B 1 0 No
May be inoperative provided Windshear Detection System Predictive is operative.

22-60-04 Yaw Damper System

Ident.: MI-22-60-00007543.0001001 / 23 MAR 11
Applicable to: ALL

22-60-04A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) **
One may be inoperative.
Continued on the following page

LAN COLOMBIA FLEET MI-22-60 P 2/4

MEL B to D 05 NOV 13
 MEL ITEMS
22 - AUTO FLIGHT
22-60 - Flight Augmentation (FAC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 22-60-04A Yaw Damper System

LAN COLOMBIA FLEET MI-22-60 P 3/4

MEL D 05 NOV 13
 MEL ITEMS
22 - AUTO FLIGHT
22-60 - Flight Augmentation (FAC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-22-60 P 4/4

MEL 05 NOV 13
 MEL ITEMS
22 - AUTO FLIGHT
22-70 - Flight Management System (FMS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-70-01 Flight Management System ( FMS )

Ident.: MI-22-70-00007544.0002001 / 27 FEB 15
Applicable to: ALL

Note: Except for RNAV ( RNP ), RNAV ( GNSS ) and RNAV -10, FMS 1 may be inoperative
provided:
Note: RNP item.

22-70-01A FMS 1 inoperative with IR 1 ( NAV mode) or GPS 1 operative

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(o) Except for RNAV ( RNP ), RNAV ( GNSS ) and RNAV -10,
FMS 1 may be inoperative provided that:
1) ETOPS is not conducted, and
2) Two MCDU s are operative, and
3) The IR 1 NAV mode or GPS 1 is operative.
Reference(s)
(o) Refer to OpsProc 22-70-01A Flight Management System (FMS)

22-70-01B FMS 2 inoperative with IR 1 ( NAV mode) or GPS 1 operative

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(o) Except for RNAV ( RNP ), RNAV ( GNSS ) and RNAV -10,
FMS 2 may be inoperative provided that the IR 1 N AV mode or GPS 1 is operative.
Reference(s)
(o) Refer to OpsProc 22-70-01B Flight Management System (FMS)
Continued on the following page

LAN COLOMBIA FLEET MI-22-70 P 1/4

MEL A 27 FEB 15
 MEL ITEMS
22 - AUTO FLIGHT
22-70 - Flight Management System (FMS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

22-70-01C FMS 1 inoperative
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
Except for RNAV ( RNP ), RNAV ( GNSS ) and RNAV -10,
FMS 1 may be inoperative provided that:
1) ETOPS is not conducted, and
2) The flight remains within radio navaids coverage.

22-70-01D FMS 2 inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
Except for RNAV ( RNP ), RNAV ( GNSS ) and RNAV -10, FMS 2 may be inoperative
provided flight remains within radio navaids coverage.

22-70-02 Navigation Database

Ident.: MI-22-70-00007545.0001001 / 05 APR 12
Applicable to: ALL

Note: RNP item.

Note: RNAV item.

22-70-02A
Repair interval Nbr installed Nbr required Placard
C 2 2 No
Only for RNAV-5 and RNAV-10 operations may be expired provided pilot charts are used as
a primary navigation information source.

LAN COLOMBIA FLEET MI-22-70 P 2/4

MEL A to B 27 FEB 15
 MEL ITEMS
22 - AUTO FLIGHT
22-70 - Flight Management System (FMS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-70-03 Performance Information

Ident.: MI-22-70-00007546.0001001 / 27 NOV 12
Applicable to: ALL

Note: RNP item.

Note: RNAV item.

22-70-03A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
Except for RNAV ( RNP )and RNAV ( GNSS ), one or both may be inoperative.

22-70-04 Fuel/Time Prediction

Ident.: MI-22-70-00007547.0001001 / 21 MAR 10
Applicable to: ALL

22-70-04A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

LAN COLOMBIA FLEET MI-22-70 P 3/4

MEL C to D 27 FEB 15
 MEL ITEMS
22 - AUTO FLIGHT
22-70 - Flight Management System (FMS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-22-70 P 4/4

MEL 27 FEB 15
 MEL ITEMS
22 - AUTO FLIGHT
22-81 - Flight Control Unit (FCU)
COLOMBIA
LAN COLOMBIA AIRLINES 22-81-01 - Auto Flight Control Panel (FCU)
MINIMUM EQUIPMENT LIST

22-81-01-01 AP Engagement pb
Ident.: MI-22-81-01-00007549.0001001 / 21 MAR 10
Applicable to: ALL

22-81-01-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative provided that the associated autopilot ( AP ) is considered
inoperative.
Refer to Item 22-10-01 Autopilot (AP)

22-81-01-02 A/THR Arming pb

Ident.: MI-22-81-01-00007550.0001001 / 21 MAR 10
Applicable to: ALL

22-81-01-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that the autothrust ( A/THR ) is considered inoperative.
Refer to Item 22-30-01 Autothrust (A/THR)

22-81-01-03 Mode Engagement pb (LOC, EXPED, APPR)

Ident.: MI-22-81-01-00007551.0001001 / 27 FEB 15
Applicable to: ALL

22-81-01-03A
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
**
One or more may be inoperative.

LAN COLOMBIA FLEET MI-22-81-01 P 1/4

MEL A to C 27 FEB 15
 MEL ITEMS
22 - AUTO FLIGHT
22-81 - Flight Control Unit (FCU)
COLOMBIA
LAN COLOMBIA AIRLINES 22-81-01 - Auto Flight Control Panel (FCU)
MINIMUM EQUIPMENT LIST

22-81-01-04 Selection knob (ALT, HDG-TRK, SPD-MACH)

Ident.: MI-22-81-01-00007552.0001001 / 21 MAR 10
Applicable to: ALL

22-81-01-04A
Repair interval Nbr installed Nbr required Placard
3 3 No
Must be operative.

22-81-01-05 V/S-FPA Selection knob

Ident.: MI-22-81-01-00007553.0001001 / 21 MAR 10
Applicable to: ALL

22-81-01-05A
Repair interval Nbr installed Nbr required Placard
B 1 0 Yes
May be inoperative provided that operations do not required its use.

22-81-01-06 HDG-V/S/TRK-FPA Change Over pb

Ident.: MI-22-81-01-00007554.0001001 / 21 MAR 10
Applicable to: ALL

22-81-01-06A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that the HDG-V/S selection is operative.

LAN COLOMBIA FLEET MI-22-81-01 P 2/4

MEL D to F 27 FEB 15
 MEL ITEMS
22 - AUTO FLIGHT
22-81 - Flight Control Unit (FCU)
COLOMBIA
LAN COLOMBIA AIRLINES 22-81-01 - Auto Flight Control Panel (FCU)
MINIMUM EQUIPMENT LIST

22-81-01-07 SPD/MACH Change Over pb

Ident.: MI-22-81-01-00007555.0001001 / 21 MAR 10
Applicable to: ALL

22-81-01-07A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that the SPD selection is operative.

22-81-01-09 Selection Window (SPD-MACH, HDG-TRK, ALT, V/S-FPA)

Ident.: MI-22-81-01-00007557.0002001 / 21 MAR 10
Applicable to: ALL

22-81-01-09B
Repair interval Nbr installed Nbr required Placard
C 4 0 Yes
One or more may be inoperative provided that the associated indications are operative on
both PFDs and both NDs.

22-81-01-10 AP1, AP2 and A/THR pb light Bars

Ident.: MI-22-81-01-00007558.0001001 / 23 MAR 11
Applicable to: ALL

22-81-01-10A
Repair interval Nbr installed Nbr required Placard
C 3 0 No
One or more may be inoperative provided that the associated indication is operative on both
PFDs.

LAN COLOMBIA FLEET MI-22-81-01 P 3/4

MEL G to I 27 FEB 15
 MEL ITEMS
22 - AUTO FLIGHT
22-81 - Flight Control Unit (FCU)
COLOMBIA
LAN COLOMBIA AIRLINES 22-81-01 - Auto Flight Control Panel (FCU)
MINIMUM EQUIPMENT LIST

22-81-01-11 Mode Engagement (LOC, EXPED, APPR) pb light Bars

Ident.: MI-22-81-01-00007559.0001001 / 27 FEB 15
Applicable to: ALL

22-81-01-11A
Repair interval Nbr installed Nbr required Placard
C 3 0 No
One or more may be inoperative.

LAN COLOMBIA FLEET MI-22-81-01 P 4/4

MEL J 27 FEB 15
 MEL ITEMS
22 - AUTO FLIGHT
22-81 - Flight Control Unit (FCU)
COLOMBIA
LAN COLOMBIA AIRLINES 22-81-02 - EFIS Control Panel (FCU)
MINIMUM EQUIPMENT LIST

22-81-02-01 Baro Reference Display Window

Ident.: MI-22-81-02-00007560.0001001 / 21 MAR 10
Applicable to: ALL

22-81-02-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

22-81-02-02 Baro Reference selector Outer Ring (in Hg/hPa)

Ident.: MI-22-81-02-00007561.0001001 / 21 MAR 10
Applicable to: ALL

22-81-02-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative provided that the unit required for the intended flight is
operative on both EFIS control panels.

22-81-02-03 Baro Reference selector Inner knob

Ident.: MI-22-81-02-00007562.0001001 / 21 MAR 10
Applicable to: ALL

22-81-02-03A
Repair interval Nbr installed Nbr required Placard
2 2 No
Both must be operative.

LAN COLOMBIA FLEET MI-22-81-02 P 1/4

MEL A to C 05 NOV 13
 MEL ITEMS
22 - AUTO FLIGHT
22-81 - Flight Control Unit (FCU)
COLOMBIA
LAN COLOMBIA AIRLINES 22-81-02 - EFIS Control Panel (FCU)
MINIMUM EQUIPMENT LIST

22-81-02-04 FD pb
Ident.: MI-22-81-02-00007563.0001001 / 21 MAR 10
Applicable to: ALL

22-81-02-04A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative provided that the associated FD is considered inoperative.
Refer to Item 22-10-02 Flight Director (FD)

22-81-02-05 LS pb
Ident.: MI-22-81-02-00007564.0002001 / 18 MAY 11
Applicable to: ALL

22-81-02-05A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
**
One may be inoperative provided that the associated ILS is considered inoperative.
Refer to Item 34-30-04 Instrument Landing System (ILS)

22-81-02-06 Optional Data (ARPT, NDB, VOR.D, WPT, CSTR) Display pb

Ident.: MI-22-81-02-00007565.0001001 / 21 MAR 10
Applicable to: ALL

22-81-02-06A
Repair interval Nbr installed Nbr required Placard
C 10 0 Yes
One or more may be inoperative.

LAN COLOMBIA FLEET MI-22-81-02 P 2/4

MEL D to F 05 NOV 13
 MEL ITEMS
22 - AUTO FLIGHT
22-81 - Flight Control Unit (FCU)
COLOMBIA
LAN COLOMBIA AIRLINES 22-81-02 - EFIS Control Panel (FCU)
MINIMUM EQUIPMENT LIST

22-81-02-07 ND Range selector

Ident.: MI-22-81-02-00007566.0001001 / 21 MAR 10
Applicable to: ALL

22-81-02-07A
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
One may be inoperative provided that the ND unit associated with the operative ND range
selector is operative.

22-81-02-08 ND Mode selector

Ident.: MI-22-81-02-00007567.0001001 / 21 MAR 10
Applicable to: ALL

22-81-02-08A
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
One may be inoperative provided that the ND unit associated with the operative ND mode
selector is operative.

22-81-02-09 ADF/VOR sw
Ident.: MI-22-81-02-00007568.0001001 / 14 SEP 10
Applicable to: ALL

22-81-02-09A
Repair interval Nbr installed Nbr required Placard
C 4 0 No
One or more may be inoperative provided that the associated ADF / VOR indication on ND
is considered inoperative.
Refer to Item 34-06-06 Radio Navaids Indications on the ND

LAN COLOMBIA FLEET MI-22-81-02 P 3/4

MEL G to I 05 NOV 13
 MEL ITEMS
22 - AUTO FLIGHT
22-81 - Flight Control Unit (FCU)
COLOMBIA
LAN COLOMBIA AIRLINES 22-81-02 - EFIS Control Panel (FCU)
MINIMUM EQUIPMENT LIST

22-81-02-10 LS and FD pb light Bars

Ident.: MI-22-81-02-00007569.0002001 / 23 MAR 11
Applicable to: ALL

22-81-02-10A
Repair interval Nbr installed Nbr required Placard
C 4 0 No
One or more may be inoperative provided that the associated indication is operative on both
PFDs.

22-81-02-11 Optional Data (ARPT, NDB, VOR.D, WPT, CSTR) Display pb light Bars
Ident.: MI-22-81-02-00007570.0001001 / 23 MAR 11
Applicable to: ALL

22-81-02-11A
Repair interval Nbr installed Nbr required Placard
C 10 0 No
One or more may be inoperative.

LAN COLOMBIA FLEET MI-22-81-02 P 4/4

MEL J to K 05 NOV 13
 MEL ITEMS
22 - AUTO FLIGHT
22-81 - Flight Control Unit (FCU)
COLOMBIA
LAN COLOMBIA AIRLINES 22-81-03 - FCU Channel
MINIMUM EQUIPMENT LIST

22-81-03-01 FCU Channel

Ident.: MI-22-81-03-00007571.0002001 / 27 FEB 15
Applicable to: ALL

Note: RVSM item.

Note: RNP item.
Note: RNAV item.

22-81-03-01A Non ETOPS flight

Repair interval Nbr installed Nbr required Placard
C 2 1 No
One channel may be inoperative provided that:
1) ETOPS, RNAV ( RNP ) and RNAV ( GNSS ) are not conducted, and
2) Two RMPs, all DUs, both RAs, both LGCIUs, both FACs, both Automatic Cabin
Pressure Control Systems, all ADIRUs and the ISIS altitude indication are operative.

22-81-03-01C
Repair interval Nbr installed Nbr required Placard
2 2 No
BothFCUchannels must be operative for RNAV ( RNP ) and RNAV ( GNSS ) operations.

LAN COLOMBIA FLEET MI-22-81-03 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
22 - AUTO FLIGHT
22-81 - Flight Control Unit (FCU)
COLOMBIA
LAN COLOMBIA AIRLINES 22-81-03 - FCU Channel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-22-81-03 P 2/2

MEL 27 FEB 15
 MEL ITEMS
22 - AUTO FLIGHT
22-82 - Multipurpose Control and Display Unit (MCDU)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-82-01 MCDU 1
Ident.: MI-22-82-00007572.0001001 / 05 NOV 13
Applicable to: ALL

Note: RNAV item.

Note: RNP item.

22-82-01B Flight within navaids coverage

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that:
1) ETOPS, RNAV ( RNP ),and RNAV-10 are not conducted, and
2) The MCDU 2 is operative, and
3) The flight remains within radio navaids coverage.

22-82-02 MCDU 2
Ident.: MI-22-82-00007573.0001001 / 05 NOV 13
Applicable to: ALL

Note: RNAV item.

Note: RNP item.

22-82-02B Flight within navaids coverage

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that:
1) ETOPS, RNAV ( RNP ),and RNAV-10 are not conducted, and
2) The MCDU 1 is operative, and
3) The flight remains within radio navaids coverage.

LAN COLOMBIA FLEET MI-22-82 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
22 - AUTO FLIGHT
22-82 - Multipurpose Control and Display Unit (MCDU)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-82-04 MCDU Annunciator light

Ident.: MI-22-82-00007575.0001001 / 27 NOV 12
Applicable to: ALL

Note: RNAV item.

Note: RNP item.

22-82-04A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or more may be inoperative.

LAN COLOMBIA FLEET MI-22-82 P 2/2

MEL C 05 NOV 13
 MEL ITEMS
22 - AUTO FLIGHT
22-83 - Flight Management and Guidance Computer (FMGC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-83-01 Flight Management and Guidance Computer ( FMGC )

Ident.: MI-22-83-00007576.0001001 / 27 FEB 15
Applicable to: ALL

Note: RNAV item.

Note: RNP item.

22-83-01A FMGC 1 inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(o) ** FMGC 1 may be inoperative provided that:
1) ETOPS is not conducted, and
2) FMGC 1 is deactivated, and
3) FMS 1 is considered inoperative, and
Refer to Item 22-70-01 Flight Management System (FMS)
4) AP 1 is considered inoperative.
Refer to Item 22-10-01 Autopilot (AP)
Reference(s)
(o) Refer to OpsProc 22-83-01A Flight Management and Guidance Computer (FMGC)

22-83-01B FMGC 2 inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(o) ** FMGC 2 may be inoperative provided that:
1) FMGC 2 is deactivated, and
2) FMS 2 is considered inoperative.
Refer to Item 22-70-01 Flight Management System (FMS)
3) AP 2 is considered inoperative.
Refer to Item 22-10-01 Autopilot (AP)
Reference(s)
(o) Refer to OpsProc 22-83-01B Flight Management and Guidance Computer (FMGC)

LAN COLOMBIA FLEET MI-22-83 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
22 - AUTO FLIGHT
22-83 - Flight Management and Guidance Computer (FMGC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-22-83 P 2/2

MEL 27 FEB 15
 MEL ITEMS
23 - COMMUNICATIONS
23-00 - MAINTENANCE Message on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-00-01 CIDS 1(2) MAINTENANCE Message

Ident.: MI-23-00-00007581.0001001 / 21 MAR 10
Applicable to: ALL

23-00-01A
Repair interval Nbr installed Nbr required Placard
C No
CIDS 1(2) MAINTENANCE message may be displayed on the STATUS SD page.

LAN COLOMBIA FLEET MI-23-00 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-00 - MAINTENANCE Message on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-00 P 2/2

MEL 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 23-01-01 - RCDR Overhead Panel
MINIMUM EQUIPMENT LIST

23-01-01-01 RCDR GND CTL pb-sw ON light

Ident.: MI-23-01-01-00007582.0001001 / 21 MAR 10
Applicable to: ALL

23-01-01-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

23-01-01-31 RCDR GND CTL pb-sw

Ident.: MI-23-01-01-00007583.0001001 / 12 SEP 11
Applicable to: ALL

23-01-01-31A AUTO position

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative in the AUTO position.
Reference(s)
(o) Refer to OpsProc 23-01-01-31A RCDR GND CTL pb-sw (Inoperative in the AUTO position)

23-01-01-31B ON position
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative in the ON position.
Reference(s)
(o) Refer to OpsProc 23-01-01-31B RCDR GND CTL pb-sw (Inoperative in the ON position)
Continued on the following page

LAN COLOMBIA FLEET MI-23-01-01 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 23-01-01 - RCDR Overhead Panel
MINIMUM EQUIPMENT LIST

Continued from the previous page

23-01-01-31C CVR considered inoperative
Repair interval Nbr installed Nbr required Placard
1 0 Yes
May be inoperative provided that the CVR is considered inoperative.
Refer to Item 23-71-01 Cockpit Voice Recorder (CVR)

23-01-01-32 CVR ERASE pb

Ident.: MI-23-01-01-00007584.0001001 / 21 MAR 10
Applicable to: ALL

23-01-01-32A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

23-01-01-33 CVR TEST pb

Ident.: MI-23-01-01-00007585.0001001 / 21 MAR 10
Applicable to: ALL

23-01-01-33A
Repair interval Nbr installed Nbr required Placard
1 0 Yes
May be inoperative provided that the Cockpit Voice Recorder ( CVR ) is considered
inoperative.
Refer to Item 23-71-01 Cockpit Voice Recorder (CVR)

LAN COLOMBIA FLEET MI-23-01-01 P 2/2

MEL B to D 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 23-01-02 - CALLS Overhead Panel
MINIMUM EQUIPMENT LIST

23-01-02-31 CALLS ALL pb

Ident.: MI-23-01-02-00007586.0001001 / 18 MAY 11
Applicable to: ALL

23-01-02-31A
Repair interval Nbr installed Nbr required Placard
D 1 0 Yes
May be inoperative.

23-01-02-32 CALLS EMER pb, CALLS FWD pb, CALLS EXIT pb, CALLS AFT pb
Ident.: MI-23-01-02-00007587.0001001 / 12 SEP 12
Applicable to: ALL

23-01-02-32A Use of passenger address system

Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative provided that the passenger address system is used for
communication between the cockpit and the cabin.

23-01-02-32B Use of cockpit handset interphone

Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative provided that the cockpit handset interphone is used for
communication between the cockpit and the cabin.

LAN COLOMBIA FLEET MI-23-01-02 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 23-01-02 - CALLS Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-01-02 P 2/2

MEL 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 23-01-03 - AUDIO SWITCHING Overhead Panel
MINIMUM EQUIPMENT LIST

23-01-03-31 AUDIO SWITCHING selector

Ident.: MI-23-01-03-00007616.0001001 / 28 NOV 11
Applicable to: ALL

23-01-03-31A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-23-01-03 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 23-01-03 - AUDIO SWITCHING Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-01-03 P 2/2

MEL 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-09-01 COMHF 1(2) EMITTING Alert

Ident.: MI-23-09-00007665.0001001 / 18 MAY 11
Applicable to: ALL

23-09-01A
Repair interval Nbr installed Nbr required Placard
2 No
(o) One or both may be displayed provided that :
1) The alert is confirmed to be false by troubleshooting, and
2) The affected HF is deactivated and considered inoperative.
Refer to Item 23-10-01 HF System
Reference(s)
(o) Refer to OpsProc 23-09-01A COM HF 1(2) EMITTING Alert

23-09-02 COM VHF 1(2)(3) EMITTING Alert

Ident.: MI-23-09-00007666.0001001 / 21 MAR 10
Applicable to: ALL

23-09-02A
Repair interval Nbr installed Nbr required Placard
3 No
(o) One or more may be displayed provided that :
1) The alert is confirmed to be false by troubleshooting, and
2) The affected VHF is deactivated and considered inoperative.
Refer to Item 23-10-02 VHF System
Reference(s)
(o) Refer to OpsProc 23-09-02A COM VHF 1(2)(3) EMITTING Alert

LAN COLOMBIA FLEET MI-23-09 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-09 P 2/2

MEL 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-10 - Speech Communication
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-10-01 HF System
Ident.: MI-23-10-00007588.0001001 / 27 NOV 12
Applicable to: ALL

23-10-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided :
1) Continuous VHF coverage is assured, and
2) Flight is not conducted for overwater flight for more than 30 minutes, or 100 nautical
miles away from the coast, and
3) Two VHF Systems must be operative.
4) Do not dispatch IFR Operations South of SCTE TMA below FL 245.
Note: For ETOPS, if HF is required, HF 1 voice mode must be operative.

23-10-02 VHF System

Ident.: MI-23-10-00007589.0002001 / 27 FEB 15
Applicable to: ALL

1
23-10-02B
Repair interval Nbr installed Nbr required Placard
C 3 1 Yes
Number 2 and Number 3 may be inoperative provided HF is operative.
Note: 1. For ETOPS, the VHF 1 must be operative.
2. The VHF 3 may be used as one of the VHFs required by regulations (in addition
to VFH 1), provided that the VHF 3 is set to VOICE mode before each flight.

LAN COLOMBIA FLEET MI-23-10 P 1/2

MEL A to B 27 FEB 15
 MEL ITEMS
23 - COMMUNICATIONS
23-10 - Speech Communication
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-10 P 2/2

MEL 27 FEB 15
 MEL ITEMS
23 - COMMUNICATIONS
23-13 - Radio Management
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-13-01 Radio Management Panel (RMP)

Ident.: MI-23-13-00007591.0002001 / 21 MAR 10
Applicable to: ALL

23-13-01B
Repair interval Nbr installed Nbr required Placard
C 3 2 Yes
RMP 2 or RMP 3 may be inoperative.

23-13-02 RMP Selection Key

Ident.: MI-23-13-00007592.0001001 / 23 MAR 11
Applicable to: ALL

23-13-02A
Repair interval Nbr installed Nbr required Placard
C 30 Yes
One may be inoperative on each RMP provided that :
1) VHF 1 selection key is operative on RMP 1, and
2) If HF is required, HF 1 selection key is operative on RMP 1.

LAN COLOMBIA FLEET MI-23-13 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-13 - Radio Management
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-13 P 2/2

MEL 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-20 - Data Transmission and Automatic Calling
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-20-01 Aircraft Communications Addressing Reporting System (ACARS)

Ident.: MI-23-20-00007593.0001001 / 18 MAY 11
Applicable to: ALL

23-20-01A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative

LAN COLOMBIA FLEET MI-23-20 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-20 - Data Transmission and Automatic Calling
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-20 P 2/2

MEL 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-31 - Passenger Address System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-31-01 Passenger Address System

Ident.: MI-23-31-00007595.0001001 / 21 MAR 10
Applicable to: ALL

23-31-01A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.
Note: 1. In the case of partial failure of the passenger address system, refer to the
item(s) of the affected system(s).
2. Total failure of the passenger address system (indicated by the COM CIDS 1+2
FAULT alert displayed on the EWD) is not permitted.

23-31-02 PA IN USE light

Ident.: MI-23-31-00007596.0001001 / 10 OCT 14
Applicable to: MSN 4758-5453

23-31-02A
Repair interval Nbr installed Nbr required Placard
D 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-23-31 P 1/2

MEL A to B 10 OCT 14
 MEL ITEMS
23 - COMMUNICATIONS
23-31 - Passenger Address System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-31 P 2/2

MEL 10 OCT 14
 MEL ITEMS
23 - COMMUNICATIONS
23-40 - Interphone
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-40-01 Ground External Horn

Ident.: MI-23-40-00007597.0001001 / 02 NOV 11
Applicable to: ALL

23-40-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 23-40-01A Ground External Horn

23-40-02 Flight Crew Interphone System

Ident.: MI-23-40-00007598.0001001 / 18 MAY 11
Applicable to: ALL

23-40-02A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative for each person on cockpit duty.

23-40-03 Flight Crew to Ground Communication System

Ident.: MI-23-40-00007599.0001001 / 21 MAR 10
Applicable to: ALL

23-40-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 23-40-03A Flight Crew to Ground Communication System

LAN COLOMBIA FLEET MI-23-40 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-40 - Interphone
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-40-04 Service Interphone Jack

Ident.: MI-23-40-00007600.0001001 / 21 MAR 10
Applicable to: ALL

23-40-04A
Repair interval Nbr installed Nbr required Placard
D 8 0 No
(o) One or more may be inoperative.
Reference(s)
(o) Refer to OpsProc 23-40-04A Service Interphone Jack

LAN COLOMBIA FLEET MI-23-40 P 2/2

MEL D 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-51 - Audio Management
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-51-01 SELCAL Function

Ident.: MI-23-51-00007601.0001001 / 23 MAR 11
Applicable to: ALL

23-51-01A
Repair interval Nbr installed Nbr required Placard
C 3 0 No
May be inoperative.

23-51-02 Boomset
Ident.: MI-23-51-00007602.0001001 / 05 NOV 13
Applicable to: ALL

23-51-02A Earphone Function

Repair interval Nbr installed Nbr required Placard
C 3 2 No
Captain and First Officer earphone must be operative.

23-51-02B Mike Function

Repair interval Nbr installed Nbr required Placard
C 3 2 No
One may be inoperative provided Captain and First Officer boom mic operate normally.

23-51-03 Hand Microphone

Ident.: MI-23-51-00007603.0001001 / 12 SEP 11
Applicable to: ALL

23-51-03A
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative, or missing, or removed provided Captain and First Officer
boom mike operates normally.

LAN COLOMBIA FLEET MI-23-51 P 1/4

MEL A to C 10 OCT 14
 MEL ITEMS
23 - COMMUNICATIONS
23-51 - Audio Management
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-51-04 Cockpit Loudspeaker

Ident.: MI-23-51-00007604.0001001 / 10 OCT 14
Applicable to: ALL

23-51-04A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
Only F/O loudspeaker may be inoperative provided that at least one crewmember on
cockpit duty wears a boomset for the entire flight.

23-51-05 Cockpit Loudspeaker Volume Control

Ident.: MI-23-51-00007605.0001001 / 10 OCT 14
Applicable to: ALL

23-51-05A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) One may be inoperative provided that the affected crewmember on cockpit duty wears a
boomset for the entire flight.
Reference(s)
(o) Refer to OpsProc 23-51-05A Cockpit Loudspeaker Volume Control

23-51-06 Sidestick PTT sw

Ident.: MI-23-51-00007606.0001001 / 12 SEP 11
Applicable to: ALL

23-51-06B
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(m) One or both may be inoperative in the open position (non transmitting position) provided
that the INT/RAD sw on CAPT ACP, on F/O ACP and on ACP 3 are operative.
Note: Apply the maintenance procedure only when the inoperative sidestick PTT sw is
failed in the closed position (transmitting position).
Continued on the following page

LAN COLOMBIA FLEET MI-23-51 P 2/4

MEL D to F 10 OCT 14
 MEL ITEMS
23 - COMMUNICATIONS
23-51 - Audio Management
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(m) Refer to AMM 23-51-00-040-001

LAN COLOMBIA FLEET MI-23-51 P 3/4

MEL F 10 OCT 14
 MEL ITEMS
23 - COMMUNICATIONS
23-51 - Audio Management
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-51 P 4/4

MEL 10 OCT 14
 MEL ITEMS
23 - COMMUNICATIONS
23-52 - Audio Control Panel (ACP)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-52-01 CAPT and F/O ACP

Ident.: MI-23-52-00007609.0001001 / 21 MAR 10
Applicable to: ALL

23-52-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(o) One may be inoperative provided that :
1) ACP 3 is operative, and
2) The AUDIO SWITCHING selector is operative.
Reference(s)
(o) Refer to OpsProc 23-52-01A CAPT and F/O ACP

23-52-02 ACP 3
Ident.: MI-23-52-00007610.0001001 / 21 MAR 10
Applicable to: ALL

23-52-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

23-52-05 ACP Transmission Key

Ident.: MI-23-52-00007613.0001001 / 23 MAR 11
Applicable to: ALL

23-52-05A
Repair interval Nbr installed Nbr required Placard
C 7 6 Yes
One may be inoperative on each ACP provided that :
1) VHF 1 transmission key is operative either on CAPT ACP or on F/O ACP, and
2) If HF is required, HF 1 transmission key is operative either on CAPT ACP or on F/O
ACP.

LAN COLOMBIA FLEET MI-23-52 P 1/2

MEL A to C 20 JUN 14
 MEL ITEMS
23 - COMMUNICATIONS
23-52 - Audio Control Panel (ACP)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-52-06 ACP Reception knob

Ident.: MI-23-52-00007614.0001001 / 23 MAR 11
Applicable to: ALL

23-52-06A
Repair interval Nbr installed Nbr required Placard
C 7 6 Yes
One may be inoperative on each ACP provided that :
1) VHF 1 reception knob is operative either on CAPT ACP or on F/O ACP, and
2) If HF is required, HF 1 reception knob is operative either on CAPT ACP or on F/O ACP,
and
3) If ILS is required for approach, one ILS reception knob is operative either on CAPT ACP
or on F/O ACP.

23-52-07 ACP Reception knob light

Ident.: MI-23-52-00007615.0001001 / 23 MAR 11
Applicable to: ALL

23-52-07A
Repair interval Nbr installed Nbr required Placard
D 7 0 No
One or more may be inoperative.

LAN COLOMBIA FLEET MI-23-52 P 2/2

MEL D to E 20 JUN 14
 MEL ITEMS
23 - COMMUNICATIONS
23-71 - Cockpit Voice Recorder (CVR)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-71-01 Cockpit Voice Recorder (CVR)

Ident.: MI-23-71-00007617.0001001 / 23 MAR 11
Applicable to: ALL

23-71-01A
Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative for three flight days maximum provided Digital Flight Data Recorder is
operative.

LAN COLOMBIA FLEET MI-23-71 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-71 - Cockpit Voice Recorder (CVR)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-71 P 2/2

MEL 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-01 - Cabin Intercommunication Data System (CIDS)
MINIMUM EQUIPMENT LIST

23-73-01-01 Cabin Intercommunication Data System ( CIDS ) Function

Ident.: MI-23-73-01-00007619.0002001 / 27 FEB 15
Applicable to: ALL

23-73-01-01A
Repair interval Nbr installed Nbr required Placard
1 1 No
The CIDS function must be operative.
Note: 1. Failure of a single CIDS director is indicated by a MAINTENANCE message on
the STATUS SD page .
Refer to Item 23-00-01 CIDS 1(2) MAINTENANCE Message
2. In the case of disturbance of the CIDS function, the deactivation of the affected
CIDS director may recover normal operation of the CIDS function.
Refer to AMM TASK 23-73-00-040-001

LAN COLOMBIA FLEET MI-23-73-01 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-01 - Cabin Intercommunication Data System (CIDS)
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-73-01 P 2/2

MEL 27 FEB 15
 MEL ITEMS
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-02 - DEU A
MINIMUM EQUIPMENT LIST

23-73-02-01 Cabin DEU A

Ident.: MI-23-73-02-00007620.9001003 / 10 OCT 14
Applicable to: ALL

23-73-02-01A Affected seat occupied

Repair interval Nbr installed Nbr required Placard
C 12 0 No
(o) One or more may be inoperative and affected passenger seat may be occupied provided
that :
1) The passenger announcement can be heard throughout the cabin during the flight, and
2) The passenger address system is used to alert the passengers when "Return to Seat /
Fasten Seat Belt / No Smoking" signs are requested.
Reference(s)
(o) Refer to OpsProc 23-73-02-01A Cabin DEU A

23-73-02-01B Affected seat not occupied

Repair interval Nbr installed Nbr required Placard
C 12 0 No
One or more may be inoperative provided that the affected seats are blocked and placarded
inoperative.

LAN COLOMBIA FLEET MI-23-73-02 P 1/2

MEL A 10 OCT 14
 MEL ITEMS
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-02 - DEU A
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-73-02 P 2/2

MEL 10 OCT 14
 MEL ITEMS
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-03 - DEU B
MINIMUM EQUIPMENT LIST

23-73-03-01 Cabin DEU B

Ident.: MI-23-73-03-00007622.0004001 / 27 FEB 15
Applicable to: ALL

23-73-03-01B
Repair interval Nbr installed Nbr required Placard
C 8 2 No
(o) One or more may be inoperative provided that:
1) One DEU B and the associated handset are operative at each pair of floor level exit
doors, and
2) The slide bottle pressure and door bottle pressure associated with each affected DEU
B are checked on the associated direct reading pressure gauge before the first flight of
each day, and
3) The associated lavatory fire extinguisher system is checked operative, and
4) The absence of smoke in the affected lavatory is periodically checked.
Refer to Item 52-10-06 DOOR PRESS LOW/CHECK DOOR PRESSURE Message on
the PTP/FAP , and
Refer to Item 26-17-01 Lavatory Smoke Detection System .
Reference(s)
(o) Refer to OpsProc 23-73-03-01B Cabin DEU B

LAN COLOMBIA FLEET MI-23-73-03 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-03 - DEU B
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-73-03 P 2/2

MEL 27 FEB 15
 MEL ITEMS
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-04 - Cabin Individual Call
MINIMUM EQUIPMENT LIST

23-73-04-01 Passenger Call

Ident.: MI-23-73-04-00007623.0001001 / 23 MAR 11
Applicable to: ALL

23-73-04-01A
Repair interval Nbr installed Nbr required Placard
C 55 0 No
One or more may be inoperative.

LAN COLOMBIA FLEET MI-23-73-04 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-04 - Cabin Individual Call
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-73-04 P 2/2

MEL 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-05 - Cabin Loudspeaker
MINIMUM EQUIPMENT LIST

23-73-05-01 Cabin Loudspeaker

Ident.: MI-23-73-05-00007624.0001001 / 23 MAR 11
Applicable to: ALL

23-73-05-01A
Repair interval Nbr installed Nbr required Placard
C 36 No
One or more may be inoperative provided that no seat is occupied from which a passenger
cannot hear a passenger announcement.

23-73-05-02 Lavatory Loudspeaker

Ident.: MI-23-73-05-00007625.0001001 / 23 MAR 11
Applicable to: ALL

23-73-05-02A
Repair interval Nbr installed Nbr required Placard
C 3 0 No
(o) One or more may be inoperative.
Reference(s)
(o) Refer to OpsProc 23-73-05-02A Lavatory Loudspeaker

LAN COLOMBIA FLEET MI-23-73-05 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-05 - Cabin Loudspeaker
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-73-05 P 2/2

MEL 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-06 - Handset
MINIMUM EQUIPMENT LIST

23-73-06-01 Cockpit Handset

Ident.: MI-23-73-06-00007626.0001001 / 21 MAR 10
Applicable to: ALL

23-73-06-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the cockpit audio control panel (ACP) is used for the
communication between the cockpit and the cabin.

23-73-06-02 Cabin Handset

Ident.: MI-23-73-06-00007627.0001001 / 18 MAY 11
Applicable to: ALL

23-73-06-02A
Repair interval Nbr installed Nbr required Placard
C 3 2 Yes
(o) One may be inoperative provided that one handset is operative at each pair of floor level
exit doors.
Reference(s)
(o) Refer to OpsProc 23-73-06-02A Cabin Handset

23-73-06-03 Cabin Handset Key

Ident.: MI-23-73-06-00007628.0001001 / 12 SEP 11
Applicable to: ALL

23-73-06-03A Passenger address and Cabin to cockpit interphone operative

Repair interval Nbr installed Nbr required Placard
C 12 3 Yes
One or more may be inoperative provided that:
1) Passenger address from the affected handset is operative, and
2) Cabin to cockpit interphone from affected handset is operative.
Continued on the following page

LAN COLOMBIA FLEET MI-23-73-06 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-06 - Handset
MINIMUM EQUIPMENT LIST

Continued from the previous page

23-73-06-03B Affected handset considered inoperative
Repair interval Nbr installed Nbr required Placard
C 12 0 Yes
One or more may be inoperative provided that the affected handset is considered
inoperative.
Refer to Item 23-73-06-02 Cabin Handset

LAN COLOMBIA FLEET MI-23-73-06 P 2/2

MEL C 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-08 - Cabin Assignment Module (CAM)
MINIMUM EQUIPMENT LIST

23-73-08-01 Cabin Assignment Module (CAM)

Ident.: MI-23-73-08-00007630.0001001 / 21 MAR 10
Applicable to: ALL

23-73-08-01A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative or missing.

LAN COLOMBIA FLEET MI-23-73-08 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-08 - Cabin Assignment Module (CAM)
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-73-08 P 2/2

MEL 05 NOV 13
 MEL ITEMS
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-10 - Smoke Detection Function
MINIMUM EQUIPMENT LIST

23-73-10-01 Smoke Detection Function ( CIDS - SDF )

Ident.: MI-23-73-10-00007632.0005001 / 27 FEB 15
Applicable to: ALL

23-73-10-01B
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that the restrictions concerning lavatory smoke detection
system and cargo smoke detection system are applied.
Refer to Item 26-17-01 Lavatory Smoke Detection System , and
Refer to Item 26-16-01 Smoke Detector in the FWD Cargo Compartment (if FWD cargo
compartment smoke detection system installed) and
Refer to Item 26-16-02 Smoke Detector in the AFT and the BULK Cargo Compartments (if
AFT cargo compartment smoke detection system installed).
Note: Failure of a single CIDS - SDF channel is indicated by a MAINTENANCE message
on the STATUS SD page .
Refer to Item 26-00-01 SDCU/SMOKE MAINTENANCE Message

LAN COLOMBIA FLEET MI-23-73-10 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-10 - Smoke Detection Function
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-73-10 P 2/2

MEL 27 FEB 15
 MEL ITEMS
23 - COMMUNICATIONS
23-74 - Cabin Crew Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-74-01 FAP Display Unit

Ident.: MI-23-74-00007634.0004001 / 10 OCT 14
Applicable to: ALL

23-74-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that the safety related messages on the FAP are considered
inoperative.
Refer to Item 52-10-06 DOOR PRESS LOW/CHECK DOOR PRESSURE Message on the
PTP/FAP , and
Refer to Item 25-62-07 Overwing Emergency Exit Slide Pressure Message on the PTP/FAP
Reference(s)
(o) Refer to OpsProc 23-74-01A FAP Display Unit

23-74-02 EMER pb on Hardkey FAP Sub-panel

Ident.: MI-23-74-00007648.0001001 / 21 MAR 10
Applicable to: ALL

23-74-02A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

23-74-03 Other Controls on Hardkey FAP Sub-panel

Ident.: MI-23-74-00007649.0001001 / 21 MAR 10
Applicable to: ALL

23-74-03A
Repair interval Nbr installed Nbr required Placard
D 0 No
One or more may be inoperative.

LAN COLOMBIA FLEET MI-23-74 P 1/4

MEL A to C 27 FEB 15
 MEL ITEMS
23 - COMMUNICATIONS
23-74 - Cabin Crew Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-74-06 Door Bottle Pressure Monitoring on the FAP

Ident.: MI-23-74-00007653.0004001 / 27 FEB 15
Applicable to: ALL

23-74-06A
Repair interval Nbr installed Nbr required Placard

Refer to Item 52-10-06 DOOR PRESS LOW/CHECK DOOR PRESSURE Message on the
PTP/FAP

23-74-08 Slide Pressure Monitoring on the FAP

Ident.: MI-23-74-00007656.0004001 / 10 OCT 14
Applicable to: ALL

23-74-08A
Repair interval Nbr installed Nbr required Placard

Refer to Item 25-62-07 Overwing Emergency Exit Slide Pressure Message on the PTP/FAP
Note: Apply MEL Item.

23-74-09 Area Call Panel

Ident.: MI-23-74-00007660.0001001 / 23 MAR 11
Applicable to: ALL

23-74-09A
Repair interval Nbr installed Nbr required Placard
D 4 0 Yes
One or more may be inoperative.

LAN COLOMBIA FLEET MI-23-74 P 2/4

MEL D to F 27 FEB 15
 MEL ITEMS
23 - COMMUNICATIONS
23-74 - Cabin Crew Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-74-10 Attendant Indication Panel (AIP)

Ident.: MI-23-74-00007661.0001001 / 01 AUG 13
Applicable to: ALL

23-74-10A
Repair interval Nbr installed Nbr required Placard
D 3 0 Yes
One or more may be inoperative.

23-74-11 Additional Attendant Panel (AAP)

Ident.: MI-23-74-00007663.0001001 / 18 MAY 11
Applicable to: ALL

23-74-11A
Repair interval Nbr installed Nbr required Placard
D 1 0 Yes
One or more may be inoperative.

LAN COLOMBIA FLEET MI-23-74 P 3/4

MEL G to H 27 FEB 15
 MEL ITEMS
23 - COMMUNICATIONS
23-74 - Cabin Crew Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-23-74 P 4/4

MEL 27 FEB 15
 MEL ITEMS
24 - ELECTRICAL POWER
24-00 - MAINTENANCE Messages on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-00-01 DC BUS TIE MAINTENANCE Message

Ident.: MI-24-00-00008421.0001001 / 21 MAR 10
Applicable to: ALL

24-00-01A
Repair interval Nbr installed Nbr required Placard
C No
DC BUS TIE MAINTENANCE message may be displayed on the STATUS SD page.

24-00-03 AC GEN MAINTENANCE Message

Ident.: MI-24-00-00008423.0001001 / 21 MAR 10
Applicable to: ALL

24-00-03A
Repair interval Nbr installed Nbr required Placard
C No
AC GEN MAINTENANCE message may be displayed on the STATUS SD page.

LAN COLOMBIA FLEET MI-24-00 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-00 - MAINTENANCE Messages on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-24-00 P 2/2

MEL 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 24-01-01 - ELEC Overhead Panel
MINIMUM EQUIPMENT LIST

24-01-01-01 BAT 1(2) pb-sw FAULT light

Ident.: MI-24-01-01-00008424.0001001 / 21 MAR 10
Applicable to: ALL

24-01-01-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

24-01-01-02 BAT 1(2) pb-sw OFF light

Ident.: MI-24-01-01-00008425.0001001 / 21 MAR 10
Applicable to: ALL

24-01-01-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

24-01-01-03 GEN pb-sw FAULT light and APU GEN pb-sw FAULT light
Ident.: MI-24-01-01-00008426.0001001 / 21 MAR 10
Applicable to: ALL

24-01-01-03A
Repair interval Nbr installed Nbr required Placard
C 3 1 Yes
One GEN pb-sw FAULT light and/or the APU GEN pb-sw FAULT light may be inoperative
provided that the associated generator indications are operative on the ELEC SD page.

LAN COLOMBIA FLEET MI-24-01-01 P 1/6

MEL A to C 27 FEB 15
 MEL ITEMS
24 - ELECTRICAL POWER
24-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 24-01-01 - ELEC Overhead Panel
MINIMUM EQUIPMENT LIST

24-01-01-04 GEN pb-sw OFF light and APU GEN pb-sw OFF light
Ident.: MI-24-01-01-00008427.0001001 / 21 MAR 10
Applicable to: ALL

24-01-01-04A
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative.

24-01-01-05 AC ESS FEED pb-sw FAULT light

Ident.: MI-24-01-01-00008428.0001001 / 21 MAR 10
Applicable to: ALL

24-01-01-05A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the AC ESS bus indication is operative on the ELEC SD
page.

24-01-01-06 AC ESS FEED pb-sw ALTN light

Ident.: MI-24-01-01-00008429.0001001 / 21 MAR 10
Applicable to: ALL

24-01-01-06A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the AC ESS bus indication is operative on the ELEC SD
page.

LAN COLOMBIA FLEET MI-24-01-01 P 2/6

MEL D to F 27 FEB 15
 MEL ITEMS
24 - ELECTRICAL POWER
24-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 24-01-01 - ELEC Overhead Panel
MINIMUM EQUIPMENT LIST

24-01-01-07 EXT PWR pb-sw AVAIL light

Ident.: MI-24-01-01-00008430.0001001 / 21 MAR 10
Applicable to: ALL

24-01-01-07A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 24-01-01-07A EXT PWR pb-sw AVAIL light

24-01-01-08 EXT PWR pb-sw ON light

Ident.: MI-24-01-01-00008431.0001001 / 21 MAR 10
Applicable to: ALL

24-01-01-08A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

24-01-01-09 GALY & CAB pb-sw FAULT light

Ident.: MI-24-01-01-00008432.0002001 / 02 NOV 11
Applicable to: ALL

24-01-01-09A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that:
1) For each generator, the AC load indication is operative on the ELEC SD page , and
2) The GALY & CAB automatic load shed system is checked operative.
Reference(s)
(o) Refer to OpsProc 24-01-01-09A GALLEY/GALY and CAB pb-sw FAULT light

LAN COLOMBIA FLEET MI-24-01-01 P 3/6

MEL G to I 27 FEB 15
 MEL ITEMS
24 - ELECTRICAL POWER
24-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 24-01-01 - ELEC Overhead Panel
MINIMUM EQUIPMENT LIST

24-01-01-10 GALY & CAB pb-sw OFF light

Ident.: MI-24-01-01-00008433.0002001 / 21 MAR 10
Applicable to: ALL

24-01-01-10A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

24-01-01-11 COMMERCIAL pb-sw OFF light

Ident.: MI-24-01-01-00008434.0004001 / 27 FEB 15
Applicable to: ALL

24-01-01-11A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

24-01-01-12 BUS TIE pb-sw OFF light

Ident.: MI-24-01-01-00008435.0001001 / 21 MAR 10
Applicable to: ALL

24-01-01-12A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-24-01-01 P 4/6

MEL J to L 27 FEB 15
 MEL ITEMS
24 - ELECTRICAL POWER
24-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 24-01-01 - ELEC Overhead Panel
MINIMUM EQUIPMENT LIST

24-01-01-13 IDG pb-sw FAULT light

Ident.: MI-24-01-01-00008436.0001001 / 21 MAR 10
Applicable to: ALL

24-01-01-13A
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
One may be inoperative provided that the frequency and the temperature indications of the
affected generator are operative on the ELEC SD page.

LAN COLOMBIA FLEET MI-24-01-01 P 5/6

MEL M 27 FEB 15
 MEL ITEMS
24 - ELECTRICAL POWER
24-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 24-01-01 - ELEC Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-24-01-01 P 6/6

MEL 27 FEB 15
 MEL ITEMS
24 - ELECTRICAL POWER
24-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 24-01-02 - EMER ELEC PWR Overhead Panel
MINIMUM EQUIPMENT LIST

24-01-02-01 RAT & EMER GEN FAULT light

Ident.: MI-24-01-02-00008437.0001001 / 21 MAR 10
Applicable to: ALL

24-01-02-01A
Repair interval Nbr installed Nbr required Placard
B 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-24-01-02 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 24-01-02 - EMER ELEC PWR Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-24-01-02 P 2/2

MEL 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-07 - Indications on the ELEC SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-07-01 AC Generation Indications on the ELEC SD page

Ident.: MI-24-07-00008472.0001001 / 02 NOV 11
Applicable to: ALL

24-07-01A
Repair interval Nbr installed Nbr required Placard
C 16 3 No
(o) One or more indications related to the AC generation may be inoperative provided that:
1) The load, voltage, and frequency indications are operative on one engine driven
generator , and
2) The associated ELEC GEN 1(2) FAULT alert is operative, and
3) The galley automatic load shed system is checked operative.
Reference(s)
(o) Refer to OpsProc 24-07-01A AC Generation Indications on the ELEC SD page

24-07-02 DC Generation Indications on the ELEC SD page

Ident.: MI-24-07-00008474.0001001 / 23 MAR 11
Applicable to: ALL

24-07-02A
Repair interval Nbr installed Nbr required Placard
C 12 0 No
One or more indications related to the DC generation may be inoperative.

24-07-03 AC ESS BUS SHED Indication on the ELEC SD page

Ident.: MI-24-07-00008475.0001001 / 21 MAR 10
Applicable to: ALL

24-07-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be displayed.

LAN COLOMBIA FLEET MI-24-07 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-07 - Indications on the ELEC SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-24-07 P 2/2

MEL 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-09-01 ELEC AC ESS BUS SHED Alert

Ident.: MI-24-09-00008477.0002001 / 02 NOV 11
Applicable to: ALL

24-09-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be displayed provided that:
1) The alert is confirmed to be false by troubleshooting, and
2) The AC ESS BUS SHED is checked operative before each flight, and
3) HF 1 is deactivated.
Refer to Item 23-10-01 HF System
Reference(s)
(o) Refer to OpsProc 24-09-01A ELEC AC ESS BUS SHED Alert

24-09-02 C/B TRIPPED Alert

Ident.: MI-24-09-00008479.0001001 / 21 MAR 10
Applicable to: ALL

24-09-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(m) May be displayed provided that the alert is confirmed to be false by troubleshooting.
Reference(s)
(m) Refer to AMM 24-50-00-040-001

LAN COLOMBIA FLEET MI-24-09 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-24-09 P 2/2

MEL 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-22 - AC Main Generation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-22-01 AC Main Generation ( IDG , GCU , Line Contactor)

Ident.: MI-24-22-00008438.0002001 / 27 FEB 15
Applicable to: MSN 4758-5453

24-22-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(o) (m) ** One may be inoperative provided that:
1) ETOPS is not conducted, and
2) The flight altitude is limited to 33 500 ft , and
3) The APU and AC auxiliary generation are operative and used throughout the flight, and
4) The APU fuel pump is operative, and
5) The APU oil consumption is checked adequate for the intended flight, and
6) All busses have power, and
7) The indications and alerts for the remaining AC main generation and the AC auxiliary
generation are operative, and
8) The galley automatic load shed system is checked operative.
Reference(s)
(o) Refer to OpsProc 24-22-01A AC Main Generation (IDG, GCU, Line Contactor)
(m) Refer to AMM 24-20-00-040-001

LAN COLOMBIA FLEET MI-24-22 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
24 - ELECTRICAL POWER
24-22 - AC Main Generation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-22-01 AC Main Generation ( IDG , GCU , Line Contactor)

Ident.: MI-24-22-00008438.0005001 / 10 OCT 14
Applicable to: MSN 4516-4546

24-22-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(o) (m) ** One may be inoperative provided that:
1) ETOPS is not conducted, and
2) The flight altitude is limited to 33 500 ft , and
3) The APU and AC auxiliary generation are operative and used throughout the flight, and
4) The APU fuel pump is operative, and
5) The APU oil consumption is checked adequate for the intended flight, and
6) The fuel recirculation system associated with the operative IDG is checked operative
before each flight, and
7) All busses have power, and
8) The indications and alerts for the remaining AC main generation and the AC auxiliary
generation are operative, and
9) The galley automatic load shed system is checked operative.
Reference(s)
(o) Refer to OpsProc 24-22-01A AC Main Generation (IDG, GCU, Line Contactor)
(m) Refer to AMM 24-20-00-040-001

24-22-02 AC Bus Tie Control Function

Ident.: MI-24-22-00008439.0001001 / 21 MAR 10
Applicable to: ALL

24-22-02A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

LAN COLOMBIA FLEET MI-24-22 P 2/2

MEL A to B 27 FEB 15
 MEL ITEMS
24 - ELECTRICAL POWER
24-23 - AC Auxiliary Generation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-23-01 AC Auxiliary Generation (APU Generator, GCU or GAPCU

Auxiliary Power Control function, Line Contactor)
Ident.: MI-24-23-00008440.0002001 / 10 OCT 14
Applicable to: ALL

Note: When the GPCU/GAPCU Auxiliary Power Control function and the APU Generator are both
inoperative, the engines cannot be started.

24-23-01A Non ETOPS flight and APU GEN pb-sw set to OFF
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that:
1) ETOPS is not conducted, and
2) The APU GEN pb-sw is set to OFF.

24-23-01B ETOPS 120 min flight and APU GEN pb-sw set to OFF
Repair interval Nbr installed Nbr required Placard
A 1 0 Yes
May be inoperative for four flights provided that:
1) ETOPS beyond 120 min is not conducted, and
2) The APU GEN pb-sw is set to OFF.

24-23-01C Non ETOPS flight and AC auxiliary generation deactivated or removed

Repair interval Nbr installed Nbr required Placard
D 1 0 Yes
(m) May be inoperative provided that:
1) ETOPS is not conducted, and
2) The AC auxiliary generation is deactivated or removed.
Reference(s)
(m) Refer to AMM

LAN COLOMBIA FLEET MI-24-23 P 1/2

MEL A 10 OCT 14
 MEL ITEMS
24 - ELECTRICAL POWER
24-23 - AC Auxiliary Generation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-24-23 P 2/2

MEL 10 OCT 14
 MEL ITEMS
24 - ELECTRICAL POWER
24-24 - AC Emergency Generation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-24-01 Emergency Generator

Ident.: MI-24-24-00008441.0001001 / 21 MAR 10
Applicable to: ALL

24-24-01A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

24-24-02 RAT Extension Automatic Control

Ident.: MI-24-24-00008442.0001001 / 21 MAR 10
Applicable to: ALL

24-24-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(m) May be inoperative provided that:
1) ETOPS is not conducted, and
2) The RAT extension manual control is checked operative every day.
Reference(s)
(m) Refer to AMM 24-20-00-040-002

24-24-03 RAT Extension Manual Control

Ident.: MI-24-24-00008443.0001001 / 21 MAR 10
Applicable to: ALL

24-24-03A
Repair interval Nbr installed Nbr required Placard
B 1 0 Yes
May be inoperative provided that ETOPS is not conducted.

LAN COLOMBIA FLEET MI-24-24 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-24 - AC Emergency Generation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-24-24 P 2/2

MEL 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-25 - AC Essential Generation Switching
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-25-01 Manual Transfer to the AC BUS 2 (ALTN Function)

Ident.: MI-24-25-00008444.0001001 / 21 MAR 10
Applicable to: ALL

24-25-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that:
1) The AC ESS FEED pb-sw is set to NORM, and
2) It is checked on the ELEC SD page that the AC BUS 1 supplies the AC ESS BUS, and
3) The TR 2 is operative.
Reference(s)
(o) Refer to OpsProc 24-25-01A Manual Transfer to the AC BUS 2 (ALTN Function)

24-25-02 Automatic Transfer to the AC BUS 2

Ident.: MI-24-25-00008445.0001001 / 01 AUG 13
Applicable to: ALL

24-25-02A
Repair interval Nbr installed Nbr required Placard
D 1 0 Yes
(o) May be inoperative provided that:
1) The AC ESS FEED pb-sw is set to NORM, and
2) It is checked on the ELEC SD page that the AC BUS 1 supplies the AC ESS BUS, and
3) The TR 2 is operative.
Reference(s)
(o) Refer to OpsProc 24-25-02A Automatic Transfer to the AC BUS 2

LAN COLOMBIA FLEET MI-24-25 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-25 - AC Essential Generation Switching
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-24-25 P 2/2

MEL 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-26 - Galley and Commercial Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-26-01 GALY & CAB Automatic Load Shed System

Ident.: MI-24-26-00008446.0002001 / 12 SEP 11
Applicable to: ALL

24-26-01A Manual load shed system operative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the manual load shed system and the GALY & CAB pb-sw
FAULT light are operative.

24-26-01B All GALY & CAB loads disconnected

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that all GALY & CAB loads are disconnected.
Reference(s)
(m) Refer to AMM 24-56-00-040-001

24-26-02 GALY & CAB Manual Load Shed System ( GALY & CAB pb-sw )
Ident.: MI-24-26-00008448.0004001 / 27 FEB 15
Applicable to: ALL

24-26-02A All GALY & CAB loads disconnected

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that all GALY & CAB loads are disconnected.
Reference(s)
(m) Refer to AMM 24-56-00-040-002

24-26-02B COMMERCIAL supply system operative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) (m) May be inoperative provided that the COMMERCIAL supply system is checked operative.
Continued on the following page

LAN COLOMBIA FLEET MI-24-26 P 1/2

MEL A to B 27 FEB 15
 MEL ITEMS
24 - ELECTRICAL POWER
24-26 - Galley and Commercial Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 24-26-02B Galley Manual Load Shed System (GALLEY/GALY &amp;
CAB pb-sw)
(m) Refer to AMM 24-51-00-040-001

24-26-03 Commercial Supply System

Ident.: MI-24-26-00008449.0001001 / 27 FEB 15
Applicable to: ALL

24-26-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 24-26-03A Commercial Supply System

LAN COLOMBIA FLEET MI-24-26 P 2/2

MEL B to C 27 FEB 15
 MEL ITEMS
24 - ELECTRICAL POWER
24-28 - Static Inverter AC Generation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-28-01 Static Inverter AC Generation

Ident.: MI-24-28-00008457.0001001 / 21 MAR 10
Applicable to: ALL

24-28-01A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

LAN COLOMBIA FLEET MI-24-28 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-28 - Static Inverter AC Generation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-24-28 P 2/2

MEL 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-32 - DC Main Generation (TR 1, TR 2)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-32-01 DC Main Generation ( TR 1, TR 2)

Ident.: MI-24-32-00008458.0002001 / 27 FEB 15
Applicable to: ALL

24-32-01A TR 1 inoperative
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) TR 1 may be inoperative provided that ETOPS is not conducted.
Reference(s)
(o) Refer to OpsProc 24-32-01A DC Main Generation (TR 1 inoperative)

24-32-01B TR 2 inoperative
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) (m) TR 2 may be inoperative provided that:
1) ETOPS is not conducted, and
2) The AC ESS FEED control is checked operative every day, and
3) The ISIS airspeed indication is operative, and
4) The ISIS altitude indication is operative, and
5) The ISIS attitude indication is operative, and
6) The standby compass is operative.
Reference(s)
(o) Refer to OpsProc 24-32-01B DC Main Generation (TR 2 inoperative)
(m) Refer to AMM 24-30-00-040-002

LAN COLOMBIA FLEET MI-24-32 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
24 - ELECTRICAL POWER
24-32 - DC Main Generation (TR 1, TR 2)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-24-32 P 2/2

MEL 27 FEB 15
 MEL ITEMS
24 - ELECTRICAL POWER
24-34 - DC Emergency Generation (ESS TR)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-34-01 DC Emergency Generation (ESS TR)

Ident.: MI-24-34-00008460.0001001 / 21 MAR 10
Applicable to: ALL

24-34-01A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

LAN COLOMBIA FLEET MI-24-34 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-34 - DC Emergency Generation (ESS TR)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-24-34 P 2/2

MEL 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-35 - DC Essential and Normal Generation Switching
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-35-01 DC TIE Contactor 1PC1 (DC BUS 1-DC BAT

BUS), 4PC (DC ESS BUS-DC BAT BUS)
Ident.: MI-24-35-00008462.0001001 / 21 MAR 10
Applicable to: ALL

24-35-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative in the open position.

24-35-02 DC TIE Contactor 1PC2 (DC BUS 2-DC BAT BUS)

Ident.: MI-24-35-00008463.0001001 / 21 MAR 10
Applicable to: ALL

24-35-02A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

LAN COLOMBIA FLEET MI-24-35 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-35 - DC Essential and Normal Generation Switching
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-24-35 P 2/2

MEL 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-38 - DC Battery Generation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-38-01 BAT 1(2) Channel

Ident.: MI-24-38-00008464.0001001 / 21 MAR 10
Applicable to: ALL

24-38-01A
Repair interval Nbr installed Nbr required Placard
2 2 No
Must be operative.

24-38-02 Battery Charger Limiter ( BCL )

Ident.: MI-24-38-00008465.0001001 / 21 MAR 10
Applicable to: ALL

24-38-02A
Repair interval Nbr installed Nbr required Placard
A 2 1 No
(o) (m) One may be inoperative for 10 flights provided that:
1) ETOPS is not conducted, and
2) No APU start is attempted neither on ground nor in flight, and
3) Both AC main generations are operative, and
4) The refueling is made with an external power unit connected, and
5) The battery associated with the inoperative BCL is charged before each flight.
Reference(s)
(o) Refer to OpsProc 24-38-02A Battery Charger Limiter (BCL)
(m) Refer to AMM 24-30-00-040-001

LAN COLOMBIA FLEET MI-24-38 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-38 - DC Battery Generation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-38-03 Battery Voltmeter

Ident.: MI-24-38-00008466.0001001 / 21 MAR 10
Applicable to: ALL

24-38-03A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative provided that the associated voltage indication is operative
on the ELEC SD page.

LAN COLOMBIA FLEET MI-24-38 P 2/2

MEL C 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-41 - AC External Power Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-41-01 Ground Power Control (GPCU or

GAPCU Ground Power Control function)
Ident.: MI-24-41-00008468.0001001 / 12 SEP 12
Applicable to: ALL

24-41-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.
Note: When the GPCU/GAPCU Ground Power Control function and the APU Generator
are both inoperative, the engines cannot be started.

24-41-02 External Power Receptacle

Ident.: MI-24-41-00008471.0001001 / 12 SEP 12
Applicable to: ALL

24-41-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that the receptacle is placarded inoperative and not used.
Note: When the GPCU/GAPCU Ground Power Control function and the APU Generator
are both inoperative, the engines cannot be started.
Reference(s)
(m) Refer to AMM 24-41-00-040-001

LAN COLOMBIA FLEET MI-24-41 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
24 - ELECTRICAL POWER
24-41 - AC External Power Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-24-41 P 2/2

MEL 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-07-01 Passenger Door Slide Permanently Indicated Armed

Ident.: MI-25-07-00008583.0001001 / 10 OCT 14
Applicable to: ALL

Note: The correct indication may be recovered by performing the AMM task 52-70-00-040-07.

25-07-01A
Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) One or more may be permanently indicated in the armed position provided that the
associated slide is visually checked to be armed before each flight.
Reference(s)
(o) Refer to OpsProc 25-07-01A Passenger Door/Cabin Passenger Door - Emergency Exit
Slide Permanently Indicated Armed on the DOOR/OXY SD page

25-07-02 Passenger Door Slide Permanently Indicated Not Armed

Ident.: MI-25-07-00008584.0001001 / 10 OCT 14
Applicable to: ALL

Note: The correct indication may be recovered by performing the AMM task 52-70-00-040-07.

25-07-02A Associated door considered operative

Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) One or more may be permanently indicated in the not armed position provided that:
1) The aircraft is not operated at night, and
2) The associated slide is visually checked to be armed before each flight.
Reference(s)
(o) Refer to OpsProc 25-07-02A Passenger Door/Cabin Passenger Door - Emergency Exit
Slide Permanently Indicated Not Armed on the DOOR/OXY SD page
Continued on the following page

LAN COLOMBIA FLEET MI-25-07 P 1/4

MEL A to B 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

25-07-02B Associated door considered inoperative
Repair interval Nbr installed Nbr required Placard
B 4 3 No
One may be permanently indicated in the not armed position provided that the associated
door is considered inoperative.
Refer to Item 52-10-01 Cabin Passenger Door

25-07-03 Emergency Exit Slide Permanently Indicated Armed

Ident.: MI-25-07-00008585.0001001 / 10 OCT 14
Applicable to: ALL

Note: The correct indication may be recovered by performing the AMM task 52-70-00-040-07.

25-07-03A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(m) One or both may be permanently indicated in the armed position provided that the
associated slide is visually checked to be armed before the first flight of the day.
Reference(s)
(m) Refer to AMM 52-70-00-040-008

25-07-04 Overwing Emergency Exit Slide Permanently Indicated Not Armed

Ident.: MI-25-07-00008586.0001001 / 10 OCT 14
Applicable to: ALL

Note: The correct indication may be recovered by performing the AMM task 52-70-00-040-007.

Continued on the following page

LAN COLOMBIA FLEET MI-25-07 P 2/4

MEL B to D 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

25-07-04A Overwing emergency exits considered operative
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(m) One or both may be permanently indicated in the not armed position provided that:
1) The aircraft is not operated at night, and
2) The associated slide is visually checked to be armed before the first flight of the day.
Reference(s)
(m) Refer to AMM 52-70-00-040-009

25-07-04B Overwing Emergency exits considered inoperative

Repair interval Nbr installed Nbr required Placard
B 2 1 No
One may be permanently indicated in the not armed position provided that both overwing
emergency exits on the same side are considered inoperative.
Refer to Item 52-10-02 Overwing Emergency Exit

LAN COLOMBIA FLEET MI-25-07 P 3/4

MEL D 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-25-07 P 4/4

MEL 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-11 - Pilot Seats
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-11-01 Pilot Seat Manual Horizontal Adjustment

Ident.: MI-25-11-00008481.0001001 / 21 MAR 10
Applicable to: ALL

25-11-01A
Repair interval Nbr installed Nbr required Placard
2 2 No
Both must be operative.

25-11-02 Pilot Seat Manual Vertical Adjustment

Ident.: MI-25-11-00008483.0001001 / 12 SEP 11
Applicable to: ALL

25-11-02A Associated electrical control operative

Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative provided that the associated electrical control is operative.

25-11-02B Associated electrical control inoperative

Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative provided that the seating position is acceptable to the
affected crewmember.

25-11-03 Pilot Seat Recline Adjustment

Ident.: MI-25-11-00008487.0001001 / 21 MAR 10
Applicable to: ALL

25-11-03A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(m) One or both may be inoperative provided that the seat is secured in an upright position
acceptable to the affected crewmember.
Continued on the following page

LAN COLOMBIA FLEET MI-25-11 P 1/6

MEL A to C 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-11 - Pilot Seats
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(m) Refer to AMM 25-11-00-040-001

25-11-04 Pilot Seat Other Manual Adjustments

Ident.: MI-25-11-00008507.0001001 / 23 MAR 11
Applicable to: ALL

25-11-04A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or more may be inoperative provided that the seating position is acceptable to the
affected crewmember.

25-11-05 Pilot Seat Electrical Adjustment

Ident.: MI-25-11-00008508.0001001 / 21 MAR 10
Applicable to: ALL

25-11-05A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(m) One or both may be inoperative provided that the electrical adjustment of the associated
seat is deactivated.
Reference(s)
(m) Refer to AMM 25-11-00-040-002

LAN COLOMBIA FLEET MI-25-11 P 2/6

MEL C to E 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-11 - Pilot Seats
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-11-06 Pilot Seat Shoulder Harness

Ident.: MI-25-11-00008514.0001001 / 18 MAY 11
Applicable to: ALL

25-11-06A
Repair interval Nbr installed Nbr required Placard
2 2 No
Must be operative.

25-11-07 Pilot Seat Fifth Strap

Ident.: MI-25-11-00008515.0001001 / 21 MAR 10
Applicable to: ALL

25-11-07A
Repair interval Nbr installed Nbr required Placard
D 2 0 No
(o) One or both may be inoperative.
Reference(s)
(o) Refer to OpsProc 25-11-07A Pilot Seat Fifth Strap

25-11-08 Pilot Sidestick Armrest Height Adjustment

Ident.: MI-25-11-00008517.0001001 / 21 MAR 10
Applicable to: ALL

25-11-08A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative provided that the associated armrest position is acceptable
to the affected crewmember.

LAN COLOMBIA FLEET MI-25-11 P 3/6

MEL F to H 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-11 - Pilot Seats
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-11-09 Pilot Sidestick Armrest Pitch Adjustment

Ident.: MI-25-11-00008518.0001001 / 21 MAR 10
Applicable to: ALL

25-11-09A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative provided that the associated armrest position is acceptable
to the affected crewmember.

25-11-10 Pilot Sidestick Armrest Memory Position Display

Ident.: MI-25-11-00008519.0001001 / 21 MAR 10
Applicable to: ALL

25-11-10A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

25-11-11 Pilot Inboard Armrest Vertical Adjustment

Ident.: MI-25-11-00008520.0001001 / 21 MAR 10
Applicable to: ALL

25-11-11A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

LAN COLOMBIA FLEET MI-25-11 P 4/6

MEL I to K 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-11 - Pilot Seats
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-11-12 Pilot Seat Headrest

Ident.: MI-25-11-00008522.0001001 / 18 MAY 11
Applicable to: ALL

25-11-12A
Repair interval Nbr installed Nbr required Placard
D 2 0 No
One or both may be inoperative.

LAN COLOMBIA FLEET MI-25-11 P 5/6

MEL L 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-11 - Pilot Seats
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-25-11 P 6/6

MEL 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-12 - Third and Fourth Occupant Seats
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-12-01 Third Occupant Seat

Ident.: MI-25-12-00008524.0001001 / 12 SEP 11
Applicable to: ALL

25-12-01A Seat stowed

Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that the seat is in its stowed position.

25-12-01B Seat removed

Repair interval Nbr installed Nbr required Placard
D 1 0 No
(m) May be removed.
Reference(s)
(m) Refer to AMM 25-11-00-040-003

25-12-02 Third Occupant Seat Shoulder Harness

Ident.: MI-25-12-00008525.0001001 / 21 MAR 10
Applicable to: ALL

25-12-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that the seat is not occupied during takeoff and landing.

LAN COLOMBIA FLEET MI-25-12 P 1/4

MEL A to B 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-12 - Third and Fourth Occupant Seats
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-12-03 Third Occupant Seat Abdominal Belt

Ident.: MI-25-12-00008527.0001001 / 21 MAR 10
Applicable to: ALL

25-12-03A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative provided that:
1) The seat is placarded inoperative, and
2) The seat is not occupied.

25-12-04 Third Occupant Seat Fifth Strap

Ident.: MI-25-12-00008528.0001001 / 21 MAR 10
Applicable to: ALL

25-12-04A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 25-12-04A Third Occupant Seat Fifth Strap

25-12-05 Fourth Occupant Seat

Ident.: MI-25-12-00008529.0001001 / 12 SEP 11
Applicable to: ALL

25-12-05A Seat stowed

Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative provided that the seat is in its stowed position.
Continued on the following page

LAN COLOMBIA FLEET MI-25-12 P 2/4

MEL C to E 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-12 - Third and Fourth Occupant Seats
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

25-12-05B Seat removed
Repair interval Nbr installed Nbr required Placard
D 1 0 No
(m) May be removed.
Reference(s)
(m) Refer to AMM 25-11-00-040-004

25-12-06 Fourth Occupant Seat Shoulder Harness

Ident.: MI-25-12-00008531.0001001 / 21 MAR 10
Applicable to: ALL

25-12-06A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative provided that the seat is not occupied during takeoff and landing.

25-12-07 Fourth Occupant Seat Abdominal Belt

Ident.: MI-25-12-00008532.0001001 / 21 MAR 10
Applicable to: ALL

25-12-07A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative provided that:
1) The seat is placarded inoperative, and
2) The seat is not occupied.

LAN COLOMBIA FLEET MI-25-12 P 3/4

MEL E to G 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-12 - Third and Fourth Occupant Seats
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-12-08 Fourth Occupant Seat Fifth Strap

Ident.: MI-25-12-00008533.0002001 / 21 MAR 10
Applicable to: ALL

25-12-08A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 25-12-08A Fourth Occupant Seat Fifth Strap

LAN COLOMBIA FLEET MI-25-12 P 4/4

MEL H 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-13 - Lining and Furnishings
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-13-01 Pilot Sliding Table

Ident.: MI-25-13-00008535.0001001 / 12 SEP 11
Applicable to: ALL

25-13-01A Table stowed

Repair interval Nbr installed Nbr required Placard
D 2 0 No
One or both may be inoperative in its stowed position.

25-13-01B Table removed

Repair interval Nbr installed Nbr required Placard
D 2 0 No
(m) One or both may be removed.
Reference(s)
(m) Refer to AMM 25-13-00-040-001

25-13-02 Pilot Retractable Footrest

Ident.: MI-25-13-00008536.0001001 / 12 SEP 11
Applicable to: ALL

25-13-02A Footrest stowed

Repair interval Nbr installed Nbr required Placard
D 4 0 No
One or more may be inoperative in its stowed position.

25-13-02B Footrest removed

Repair interval Nbr installed Nbr required Placard
D 4 0 No
(m) One or more may be removed.
Reference(s)
(m) Refer to AMM 25-13-00-040-002

LAN COLOMBIA FLEET MI-25-13 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-13 - Lining and Furnishings
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-25-13 P 2/2

MEL 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-20 - Cabin Seats
COLOMBIA
LAN COLOMBIA AIRLINES 25-20-01 - Passenger Seat
MINIMUM EQUIPMENT LIST

25-20-01-01 Passenger Seat

Ident.: MI-25-20-01-20800499.9001004 / 10 OCT 14
Applicable to: MSN 4758-5453

25-20-01-01A Passanger seat

Repair interval Nbr installed Nbr required Placard
D 174 0 Yes
One or more may be inoperative or considered inoperative provided :
1) Seat(s) does (do) not block an emergency exit, and
2) Seat(s) does (do) not restrict to any passenger access to main aircraft aisle, and
3) The effected seat(s) is (are) blocked and placarded Do not occupy and No Ocupar
Note: A seat with an inoperative seat belt is considered inoperative.
Note: Inoperative seats do not affect the required number of flight attendants.

25-20-01-01 Passenger Seat

Ident.: MI-25-20-01-20800499.9001001 / 10 OCT 14
Applicable to: MSN 4516-4546

25-20-01-01A Passanger seat

Repair interval Nbr installed Nbr required Placard
D 168 0 Yes
One or more may be inoperative or considered inoperative provided :
1) Seat(s) does (do) not block an emergency exit, and
2) Seat(s) does (do) not restrict to any passenger access to main aircraft aisle, and
3) The effected seat(s) is (are) blocked and placarded Do not occupy and No Ocupar
Note: A seat with an inoperative seat belt is considered inoperative.
Note: Inoperative seats do not affect the required number of flight attendants.

LAN COLOMBIA FLEET MI-25-20-01 P 1/6

MEL A 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-20 - Cabin Seats
COLOMBIA
LAN COLOMBIA AIRLINES 25-20-01 - Passenger Seat
MINIMUM EQUIPMENT LIST

25-20-01-02 Recline Mechanism

Ident.: MI-25-20-01-20800500.9001004 / 10 OCT 14
Applicable to: MSN 4758-5453

25-20-01-02B Recline Mechanism

Repair interval Nbr installed Nbr required Placard
D 162 0 No
1) May be inoperative and seat occupied provided seat is secured in full upright position.
OR,
2) May be inoperative and seat occupied provided seat is immovable in full upright position.

25-20-01-02 Recline Mechanism

Ident.: MI-25-20-01-20800500.9001001 / 10 OCT 14
Applicable to: MSN 4516-4546

25-20-01-02B Recline Mechanism

Repair interval Nbr installed Nbr required Placard
D 168 0 No
1) May be inoperative and seat occupied provided seat is secured in full upright position.
OR,
2) May be inoperative and seat occupied provided seat is immovable in full upright position.

LAN COLOMBIA FLEET MI-25-20-01 P 2/6

MEL B 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-20 - Cabin Seats
COLOMBIA
LAN COLOMBIA AIRLINES 25-20-01 - Passenger Seat
MINIMUM EQUIPMENT LIST

25-20-01-03 Underseat Baggage Restraining Bars

Ident.: MI-25-20-01-20800501.9001004 / 10 OCT 14
Applicable to: MSN 4758-5453

25-20-01-03C Underseat Baggage Restraining Bars

Repair interval Nbr installed Nbr required Placard
C 58 0 Yes
May be inoperative provided :
1) Baggage is not stowed under seat with inoperative restraining bar, and
2) Associated seat is placarded: DO NOT STOW BAGGAGE UNDER THIS SEAT/NO
COLOCAR EQUIPAJE BAJO ESTE ASIENTO, and
3) Ensure cabin crew is notified of the inoperative restraining bar and that baggage is not to
be placed under the associated seat.

25-20-01-03 Underseat Baggage Restraining Bars

Ident.: MI-25-20-01-20800501.9001001 / 10 OCT 14
Applicable to: MSN 4516-4546

25-20-01-03C Underseat Baggage Restraining Bars

Repair interval Nbr installed Nbr required Placard
C 56 0 Yes
May be inoperative provided :
1) Baggage is not stowed under seat with inoperative restraining bar, and
2) Associated seat is placarded: DO NOT STOW BAGGAGE UNDER THIS SEAT/NO
COLOCAR EQUIPAJE BAJO ESTE ASIENTO, and
3) Ensure cabin crew is notified of the inoperative restraining bar and that baggage is not to
be placed under the associated seat.

LAN COLOMBIA FLEET MI-25-20-01 P 3/6

MEL C 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-20 - Cabin Seats
COLOMBIA
LAN COLOMBIA AIRLINES 25-20-01 - Passenger Seat
MINIMUM EQUIPMENT LIST

25-20-01-04 Economy Class Armrests

Ident.: MI-25-20-01-20800502.9001004 / 10 OCT 14
Applicable to: MSN 4758-5453

25-20-01-04A Economy Class Armrests

Repair interval Nbr installed Nbr required Placard
D 220 0 No
May be inoperative or missing and seat occupied provided:
1) Arm rest does not block an Emergency Exit, and
2) Armrest does not restrict any passenger from access to main aircraft aisle, and
3) If armrest is missing, seat is secured in upright position.

25-20-01-04 Economy Class Armrests

Ident.: MI-25-20-01-20800502.9001001 / 10 OCT 14
Applicable to: MSN 4516-4546

25-20-01-04A Economy Class Armrests

Repair interval Nbr installed Nbr required Placard
D 212 0 No
May be inoperative or missing and seat occupied provided:
1) Arm rest does not block an Emergency Exit, and
2) Armrest does not restrict any passenger from access to main aircraft aisle, and
3) If armrest is missing, seat is secured in upright position.

LAN COLOMBIA FLEET MI-25-20-01 P 4/6

MEL D 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-20 - Cabin Seats
COLOMBIA
LAN COLOMBIA AIRLINES 25-20-01 - Passenger Seat
MINIMUM EQUIPMENT LIST

25-20-01-05 Premium Economy Convertible Seats Armrest

Ident.: MI-25-20-01-20800503.9001001 / 10 OCT 14
Applicable to: MSN 4516-4546

25-20-01-05A Premium Economy Convertible Seats Armrest

Repair interval Nbr installed Nbr required Placard
D 12 0 No
May be inoperative or missing and seat occupied provided:
1) Affected seat is not used as Premium Economy, and
2) Arm rest does not block an Emergency Exit, and
3) Armrest does not restrict any passenger from access to main aircraft aisle, and
4) If armrest is missing, seat is secured in upright position.

25-20-01-06 Back Table Seats

Ident.: MI-25-20-01-20800504.9001004 / 10 OCT 14
Applicable to: MSN 4758-5453

25-20-01-06C Back Table Seats

Repair interval Nbr installed Nbr required Placard
D 174 0 No
May be inoperative provided:
1) It is secured in the retracted position, and
2) Affected table is placarded DO NOT USE/NO USAR.

25-20-01-06 Back Table Seats

Ident.: MI-25-20-01-20800504.9001001 / 10 OCT 14
Applicable to: MSN 4516-4546

25-20-01-06C Back Table Seats

Repair interval Nbr installed Nbr required Placard
D 168 0 No
May be inoperative provided:
1) It is secured in the retracted position, and
2) Affected table is placarded DO NOT USE/NO USAR.

LAN COLOMBIA FLEET MI-25-20-01 P 5/6

MEL E to F 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-20 - Cabin Seats
COLOMBIA
LAN COLOMBIA AIRLINES 25-20-01 - Passenger Seat
MINIMUM EQUIPMENT LIST

25-20-01-07 AMSAFE Seat Belt Airbag System.

Ident.: MI-25-20-01-20800914.9001002 / 10 OCT 14
Applicable to: MSN 4758-5453

25-20-01-07A
Repair interval Nbr installed Nbr required Placard
C 6 0 Yes
Any part of the Seat Belt Airbag system may be damaged, inoperative or missing provided:
1) Affected seat (s) is (are) not required by flight attendant, and
2) Affected seat(s) is (are) blocked and placarded "DO NOT OCCUPY/ NO OCUPAR".
Refer to Item 25-20-01-01 Passenger Seat

LAN COLOMBIA FLEET MI-25-20-01 P 6/6

MEL G 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-20 - Cabin Seats
COLOMBIA
LAN COLOMBIA AIRLINES 25-20-03 - Cabin Attendant Seat
MINIMUM EQUIPMENT LIST

25-20-03 Cabin Attendant Seat

Ident.: MI-25-20-03-20800505.9001003 / 10 OCT 14
Applicable to: ALL

Note: A cabin attendant seat with an inoperative or missing seat belt or harness should be
considered inoperative.

25-20-03A Non required cabin attendant seat

Repair interval Nbr installed Nbr required Placard
D 5 4 No
(o) (m) One non-required cabin attendant seats may be inoperative or not usable provided that the
affected seat is secured in its stowed position or removed.
Reference(s)
(o) Refer to OpsProc 25-20-03A Cabin Attendant Seat
(m) Refer to AMM 25-22-00-040-001

25-20-03B Required cabin attendant seat

Repair interval Nbr installed Nbr required Placard
C 5 4 No
(o) (m) One required cabin attendant seats may be inoperative or not usable provided that:
1) The cabin attendant assigned to affected seat occupies a passenger seat as close to or
closer than nearest seated passenger to the associated exit, and
2) The passenger seat to be used by cabin attendant is correctly placarded, and
3) The cabin attendant can reach assigned exit and emergency equipment in nearly the
same time as from normally assigned seat, and
4) The direct view of passenger cabin by flight attendants is not impaired, and
5) The alternate procedures are established for displaced flight attendant according to
national regulations, and
6) The affected seat is secured in its stowed position or removed.
Note: For flights with 4 cabin attendants, 2 attendant seat in FWD Cabin and 2 in AFT
Cabin are considered as Required Cabin Attendant Seats.
Note: For flights with 5 cabin attendants, 2 attendant seat in FWD Cabin and 3 in AFT
Cabin are considered as Required Cabin Attendant Seats.
Continued on the following page

LAN COLOMBIA FLEET MI-25-20-03 P 1/2

MEL A 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-20 - Cabin Seats
COLOMBIA
LAN COLOMBIA AIRLINES 25-20-03 - Cabin Attendant Seat
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 25-20-03B Cabin Attendant Seat
(m) Refer to AMM 25-22-00-040-001

LAN COLOMBIA FLEET MI-25-20-03 P 2/2

MEL A 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-35 - Galley Equipment
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-35-01 Galley Waste Compartment Flapper Door

Ident.: MI-25-35-00008543.0001001 / 04 AUG 11
Applicable to: ALL

25-35-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) (m) One or more may be inoperative or missing provided that:
1) The galley waste compartment is empty, and
2) The associated access is secured in the closed position to prevent waste introduction.
Note: Non-safety related galley equipment is not listed in this MEL .
Reference(s)
(o) Refer to OpsProc 25-35-01A Galley Waste Compartment Flapper Door
(m) Refer to AMM 25-35-00-040-001

LAN COLOMBIA FLEET MI-25-35 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-35 - Galley Equipment
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-25-35 P 2/2

MEL 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-40 - Lavatories
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-40-01 Toilet Waste Compartment Flapper Door

Ident.: MI-25-40-00008544.0001001 / 10 OCT 14
Applicable to: ALL

25-40-01A Lavatory Locked closed.

Repair interval Nbr installed Nbr required Placard
C 3 1 Yes
(o) (m) One or two may be inoperative or missing provided that:
1) The toilet waste compartment is empty, and
2) The associated access is secured in the closed position to prevent waste introduction,
and
3) The associated lavatory(ies) is(are) locked closed and placarded inoperative.
Note: If forward lavatory is locked closed, it can be used only by pilots on duty when
flight time is more than 1:30 hour.
Note: Non-safety related toilet equipment is not listed in this MEL .
Reference(s)
(o) Refer to OpsProc 25-40-01A Toilet Waste Compartment Flapper Door
(m) Refer to AMM 25-40-00-040-001

25-40-01B Lavatory Locked closed.

Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
(o) (m) All may be inoperative or missing provided that:
1) The toilet waste compartment is empty, and
2) The associated access is secured in the closed position to prevent waste introduction,
and
3) The lavatories are locked closed and placarded inoperative, and
4) Lavatory(ies) is(are) only used by crew members,and
5) Only non revenue flight is permitted.
Reference(s)
(o) Refer to OpsProc 25-40-01B Toilet Waste Compartment Flapper Door
(m) Refer to AMM 25-40-00-040-001

LAN COLOMBIA FLEET MI-25-40 P 1/4

MEL A 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-40 - Lavatories
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-40-02 Exterior Lavatory Ashtray

Ident.: MI-25-40-00012606.0001001 / 10 OCT 14
Applicable to: ALL

25-40-02A
Repair interval Nbr installed Nbr required Placard
D 3 0 Yes
One or more may be damaged or missing provided that the flight is non-smoking.

25-40-03 Interior Lavatory Ashtray

Ident.: MI-25-40-00012607.0001001 / 10 OCT 14
Applicable to: ALL

25-40-03A Lavatory fire extinguishing system operative

Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be damaged or missing provided that the associated lavatory fire
extinguishing system is operative.

25-40-03B Lavatory Locked closed.

Repair interval Nbr installed Nbr required Placard
C 3 1 Yes
One or two may be inoperative or missing provided that:
1) The associated lavatory(ies) is(are) locked closed and placarded inoperative.
Note: If forward lavatory is locked closed, it can be used only by pilots on duty when
flight time is more than 1:30 hour.
Continued on the following page

LAN COLOMBIA FLEET MI-25-40 P 2/4

MEL B to C 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-40 - Lavatories
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

25-40-03C Lavatory Locked closed.
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
All may be inoperative or missing provided that:
1) The lavatories are locked closed and placarded inoperative, and
2) Lavatory(ies) is(are) only used by crew members,and
3) Only non revenue flight is permitted.

25-40-90 Lavatory Compartment

Ident.: MI-25-40-20801235.9001001 / 10 OCT 14
Applicable to: ALL

25-40-90A Lavatory Compartment Locked closed.

Repair interval Nbr installed Nbr required Placard
C 3 1 Yes
Associated lavatory compartment may be inoperative provided:
1) The associated lavatory door is placarded INOPERATIVE DO NOT USE
INOPERATIVO NO USAR and locked closed.
Note: If forward lavatory is locked closed, it can be used only by pilots on duty when
flight time is more than 1:30 hour.

25-40-90B Lavatory Compartment Locked closed.

Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
All lavatory compartments may be inoperative provided:
1) The associated lavatory door is placarded INOPERATIVE DO NOT USE
INOPERATIVO NO USAR and locked closed, and
2) Lavatory(ies) is(are) only used by crew members,and
3) Only non revenue flight is permitted.

LAN COLOMBIA FLEET MI-25-40 P 3/4

MEL C to D 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-40 - Lavatories
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-25-40 P 4/4

MEL 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-50 - Cargo Compartments
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-50-02 Decompression Panels in the Cargo Compartments

Ident.: MI-25-50-00008548.0001001 / 14 FEB 13
Applicable to: ALL

25-50-02A
Repair interval Nbr installed Nbr required Placard
C 31 0 No
One or more may be damaged or missing provided that the associated cargo compartment
is empty or does not contain flammable or combustible materials.

25-50-03 Sidewall Linings and Ceiling Panels in the Cargo Compartments

Ident.: MI-25-50-00008550.0001001 / 12 SEP 11
Applicable to: ALL

25-50-03A Damaged panel

Repair interval Nbr installed Nbr required Placard
C 40 0 No
One or more may be damaged provided that the associated cargo compartment is empty or
does not contain flammable or combustible materials.

25-50-03B Missing panel

Repair interval Nbr installed Nbr required Placard
C 40 0 No
One or more may be missing provided that the associated cargo compartment is empty.

LAN COLOMBIA FLEET MI-25-50 P 1/2

MEL A to B 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-50 - Cargo Compartments
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-50-04 Cargo Compartment Restraint Components

(Nets, Attach Points, Stanchions)
Ident.: MI-25-50-00008551.0001001 / 12 SEP 11
Applicable to: ALL

25-50-04A
Repair interval Nbr installed Nbr required Placard
C 10 0 No
Refer to Weight and Balance Manual.

25-50-05 Protection Panels of Decompression Panels at the

FWD Partition Wall of FWD Cargo Compartment.
Ident.: MI-25-50-00014516.0001001 / 10 OCT 14
Applicable to: ALL

25-50-05A
Repair interval Nbr installed Nbr required Placard
C 6 0 No
(m) One or more may be damaged provided that:
1) The affected protection panel is removed if the damage prevents correct operation of the
decompression panel, and
2) Bulk loading is not permitted in the section between the affected protection panel and the
closest divider net.
Reference(s)
(m) Refer to AMM Task 25-54-00-040-801

LAN COLOMBIA FLEET MI-25-50 P 2/2

MEL C to D 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-62 - Cabin Escape Facilities
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-62-01 Cabin Passenger Door Slide or Slide Raft

Ident.: MI-25-62-00008553.0001001 / 12 SEP 11
Applicable to: ALL

25-62-01A Slide inoperative

Repair interval Nbr installed Nbr required Placard
B 4 3 No
One may be inoperative provided that the associated door is considered inoperative.
Refer to Item 52-10-01 Cabin Passenger Door

25-62-01B Slide removed

Repair interval Nbr installed Nbr required Placard
B 4 3 No
(m) One may be removed provided that the associated door is considered inoperative.
Refer to Item 52-10-01 Cabin Passenger Door
Reference(s)
(m) Refer to AMM 52-10-00-040-001

25-62-02 Overwing Emergency Exit Slide or Slide Raft

Ident.: MI-25-62-00008555.0001001 / 10 OCT 14
Applicable to: ALL

25-62-02A Slide inoperative

Repair interval Nbr installed Nbr required Placard
B 2 1 No
One may be inoperative provided that the associated overwing emergency exit is
considered inoperative.
Refer to Item 52-10-02 Overwing Emergency Exit
Note: When an overwing escape slide is inoperative, both overwing emergency exits on
the same side are considered inoperative.
Note: Weight and balance manifest must be revised.
Continued on the following page

LAN COLOMBIA FLEET MI-25-62 P 1/4

MEL A to B 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-62 - Cabin Escape Facilities
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

25-62-02B Slide removed
Repair interval Nbr installed Nbr required Placard
B 2 1 No
(m) One may be removed provided that the associated overwing emergency exit is considered
inoperative.
Refer to Item 52-10-02 Overwing Emergency Exit
Note: When an overwing escape slide is inoperative, both overwing emergency exits on
the same side are considered inoperative.
Note: Weight and balance manifest must be revised.
Reference(s)
(m) Refer to AMM 25-62-00-040-006

25-62-04 SLIDE ARMED light

Ident.: MI-25-62-00008557.0001001 / 10 OCT 14
Applicable to: ALL

25-62-04A
Repair interval Nbr installed Nbr required Placard
C 6 0 Yes
One or more may be inoperative.

25-62-06 Passenger Door CHECK SLIDE PRESSURE

Message on Flight Attendant Panel (FAP)
Ident.: MI-25-62-00008563.0002001 / 10 OCT 14
Applicable to: ALL

25-62-06A
Repair interval Nbr installed Nbr required Placard
D 4 0 No
(m) One or more messages may be displayed provided that the slide bottle pressure is
checked before the first MMEL dispatch and then every 600 flight hours or every 4 months,
whichever occurs first.
Continued on the following page

LAN COLOMBIA FLEET MI-25-62 P 2/4

MEL B to D 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-62 - Cabin Escape Facilities
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(m) Refer to AMM 25-62-00-040-009

25-62-07 Overwing Emergency Exit CHECK SLIDE PRESSURE

Message on Flight Attendant Panel (FAP)
Ident.: MI-25-62-00008565.0005001 / 10 OCT 14
Applicable to: ALL

25-62-07A Check of the slide bottle pressure

Repair interval Nbr installed Nbr required Placard
D 2 0 No
(m) One or both messages may be displayed provided that the associated slide bottle pressure
is checked before the first flight of each day.
Reference(s)
(m) Refer to AMM 25-62-00-040-005

25-62-07B Overwing emergency exits considered inoperative

Repair interval Nbr installed Nbr required Placard
B 2 1 No
One message may be displayed provided that both overwing emergency exits on the same
side are considered inoperative.
Refer to Item 52-10-02 Overwing Emergency Exit

LAN COLOMBIA FLEET MI-25-62 P 3/4

MEL D to E 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-62 - Cabin Escape Facilities
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-62-08 Overwing Escape Life Line

Ident.: MI-25-62-00008567.0001001 / 10 OCT 14
Applicable to: ALL

25-62-08A Associated overwing emergency exit considered inoperative

Repair interval Nbr installed Nbr required Placard
B 4 3 No
One may be inoperative or missing provided that the associated overwing emergency exit is
considered inoperative.
Refer to Item 52-10-02 Overwing Emergency Exit

25-62-08B Non extended overwater flight

Repair interval Nbr installed Nbr required Placard
D 4 0 No
One or more may be inoperative or missing provided that extended overwater flight is not
conducted.

LAN COLOMBIA FLEET MI-25-62 P 4/4

MEL F 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-63 - Evacuation Signaling Equipment
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-63-01 Emergency Evacuation Signaling System (COMMAND

pb-sw, HORN SHUT OFF pb, CAPT&PURS and CAPT sw)
Ident.: MI-25-63-00008568.0001001 / 18 MAY 11
Applicable to: ALL

25-63-01A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 25-63-01A Emergency Evacuation Signaling System (COMMAND pb-sw,
HORN SHUT OFF pb, CAPT&amp;PURS and CAPT sw)

LAN COLOMBIA FLEET MI-25-63 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-63 - Evacuation Signaling Equipment
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-25-63 P 2/2

MEL 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-64 - First Aid Equipment
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-64-01 First Aid Kit

Ident.: MI-25-64-00008569.9001002 / 10 OCT 14
Applicable to: ALL

25-64-01A
Repair interval Nbr installed Nbr required Placard
C 3 2 No
One may be inoperative or missing.

25-64-02 Emergency Medical Kit

Ident.: MI-25-64-00008570.0001001 / 01 AUG 13
Applicable to: ALL

25-64-02A
Repair interval Nbr installed Nbr required Placard
A 1 0 No
Emergency Medical Kit may be inoperative or missing only provided:
1) Flights with flight time up to 2 hours are permitted, and
2) Repair is made within 3 flight days.

25-64-02B Elements of the Emergency Medical Kit

Repair interval Nbr installed Nbr required Placard
A 1 1 No
Any in excess of those minimum required, according with the Lista de Elementos Mnimos
Operativos placed in the kit, may be missing or inoperative provided:
1) Emergency Medical Kit is resealed in a manner that will identify it is a unit that was used,
and
2) Repair is made within 3 flight days.

LAN COLOMBIA FLEET MI-25-64 P 1/2

MEL A to B 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-64 - First Aid Equipment
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-64-03 Automated External Defibrillator (AED)

Ident.: MI-25-64-00008571.0001001 / 05 NOV 13
Applicable to: ALL

25-64-03A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

25-64-03B Accessories of the Automated External Defibrillator (AED)

Repair interval Nbr installed Nbr required Placard
A 1 1 No
Accessories of the Automated External Defibrillator (AED) may be inoperative or missing
provided:
1) One pair of patches must be operative.
2) Repair is made within 3 flight days.

25-64-90 Universal Precaution Kit (KPU)

Ident.: MI-25-64-20801281.9001001 / 05 NOV 13
Applicable to: ALL

25-64-90A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative or missing.

LAN COLOMBIA FLEET MI-25-64 P 2/2

MEL C to D 10 OCT 14
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-65 - Emergency Equipment
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-65-01 Cockpit Flashlight

Ident.: MI-25-65-00008574.0001001 / 23 MAR 11
Applicable to: ALL

25-65-01A
Repair interval Nbr installed Nbr required Placard
2 2 No
Must be operative

25-65-02 Cabin Flashlight

Ident.: MI-25-65-00008576.0001001 / 23 MAR 11
Applicable to: ALL

25-65-02A
Repair interval Nbr installed Nbr required Placard
C 6 0 No
One or more flash light and/or holder(s) may be inoperative, however, an operable flashlight
must be readily available for each required cabin attendant.

25-65-03 Crash Axe/Crowbar

Ident.: MI-25-65-00008577.0001001 / 01 SEP 11
Applicable to: ALL

25-65-03A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

LAN COLOMBIA FLEET MI-25-65 P 1/4

MEL A to C 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-65 - Emergency Equipment
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-65-04 Emergency Locator Transmitter (ELT)

Ident.: MI-25-65-00008578.0001001 / 05 APR 12
Applicable to: ALL

25-65-04A Survival ELT

Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative or removal except for overwater flight for more than 30 minutes, or 100
nautical miles away from the coast.

25-65-04B Automatic (Impact). Control Panel

Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative or removed provided Automatic (Impact).Locator Transmitter is
operative.

25-65-04C Automatic (Impact).Locator Transmitter

Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

25-65-05 Fireproof Gloves

Ident.: MI-25-65-00008579.0001001 / 12 SEP 11
Applicable to: ALL

25-65-05A All damaged or missing

Repair interval Nbr installed Nbr required Placard
C 3 0 No
One or more may be damaged or missing.
Continued on the following page

LAN COLOMBIA FLEET MI-25-65 P 2/4

MEL D to E 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-65 - Emergency Equipment
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

25-65-05B One available
Repair interval Nbr installed Nbr required Placard
D 3 1 No
One must be available.

25-65-06 Megaphone
Ident.: MI-25-65-00008580.0001001 / 23 MAR 11
Applicable to: ALL

25-65-06A
Repair interval Nbr installed Nbr required Placard
2 2 No
Both Must be operative

LAN COLOMBIA FLEET MI-25-65 P 3/4

MEL E to F 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-65 - Emergency Equipment
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-25-65 P 4/4

MEL 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-66 - Floatation and Survival Equipment
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-66-01 Life Vest

Ident.: MI-25-66-00008581.0001001 / 02 NOV 11
Applicable to: ALL

25-66-01A
Repair interval Nbr installed Nbr required Placard
C No
One lifejacket for each person on board is required to overwater routes that contains a point
further than 50 nm from the coast. Any in excess of one lifejacket for each person on board
may be missing.

LAN COLOMBIA FLEET MI-25-66 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
25 - EQUIPMENT/FURNISHINGS
25-66 - Floatation and Survival Equipment
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-25-66 P 2/2

MEL 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-00 - MAINTENANCE Message on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-00-01 SMOKE MAINTENANCE Message

Ident.: MI-26-00-00008419.0004001 / 27 FEB 15
Applicable to: ALL

26-00-01A
Repair interval Nbr installed Nbr required Placard
C No
SMOKE MAINTENANCE message may be displayed on the STATUS SD page.

LAN COLOMBIA FLEET MI-26-00 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
26 - FIRE PROTECTION
26-00 - MAINTENANCE Message on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-26-00 P 2/2

MEL 27 FEB 15
 MEL ITEMS
26 - FIRE PROTECTION
26-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 26-01-01 - FIRE Overhead Panel
MINIMUM EQUIPMENT LIST

26-01-01-01 Bulb/LED in the ENG FIRE-PUSH pb-sw

Ident.: MI-26-01-01-00008447.0001001 / 21 MAR 10
Applicable to: ALL

26-01-01-01A
Repair interval Nbr installed Nbr required Placard
C 16 8 No
A maximum of four bulbs or LEDs may be inoperative in each ENG FIRE-PUSH pb-sw.

26-01-01-02 ENG AGENT pb DISCH light

Ident.: MI-26-01-01-00008450.0001001 / 05 APR 12
Applicable to: ALL

26-01-01-02A One inoperative on each engine

Repair interval Nbr installed Nbr required Placard
C 4 2 Yes
(m) One may be inoperative on each engine provided that the associated fire extinguisher bottle
is checked before the first flight of each day.
Reference(s)
(m) Refer to AMM 26-21-00-040-001

26-01-01-02B Both inoperative on one engine

Repair interval Nbr installed Nbr required Placard
A 4 2 Yes
(m) Both may be inoperative on one engine for four flights or 15 flight hours, whichever occurs
first, provided that the associated fire extinguisher bottles are checked before each flight.
Reference(s)
(m) Refer to AMM 26-21-00-040-001

LAN COLOMBIA FLEET MI-26-01-01 P 1/6

MEL A to B 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 26-01-01 - FIRE Overhead Panel
MINIMUM EQUIPMENT LIST

26-01-01-03 ENG AGENT pb SQUIB light

Ident.: MI-26-01-01-00008451.0001001 / 21 MAR 10
Applicable to: ALL

26-01-01-03A
Repair interval Nbr installed Nbr required Placard
C 4 0 Yes
(m) One or more may be inoperative provided that the engine extinguishing system firing circuit
is checked operative before the first flight of each day.
Reference(s)
(m) Refer to AMM 26-21-00-040-003

26-01-01-04 Bulb/ LED in the APU FIRE-PUSH pb-sw

Ident.: MI-26-01-01-00008452.0001001 / 12 SEP 11
Applicable to: ALL

26-01-01-04A A maximum of four bulbs or LED s inoperative

Repair interval Nbr installed Nbr required Placard
C 8 4 No
A maximum of four bulbs or LED s may be inoperative.

26-01-01-04B Five or more bulbs or LED s inoperative

Repair interval Nbr installed Nbr required Placard
C 8 0 No
Five or more bulbs or LED s may be inoperative provided that:
1) ETOPS is not conducted, and
2) The APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)

LAN COLOMBIA FLEET MI-26-01-01 P 2/6

MEL C to D 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 26-01-01 - FIRE Overhead Panel
MINIMUM EQUIPMENT LIST

26-01-01-05 APU AGENT pb DISCH light

Ident.: MI-26-01-01-00008453.0001001 / 12 SEP 11
Applicable to: ALL

26-01-01-05A Check of bottle pressure

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that the APU fire extinguisher bottle is checked before the first
flight of each day.
Reference(s)
(m) Refer to AMM 26-22-00-040-004

26-01-01-05B APU deactivated

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)

26-01-01-06 APU AGENT pb SQUIB light

Ident.: MI-26-01-01-00008454.0001001 / 12 SEP 11
Applicable to: ALL

26-01-01-06A Check of APU extinguishing system firing circuit

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that the APU extinguishing system firing circuit is checked
operative before the first flight of each day.
Reference(s)
(m) Refer to AMM 26-22-00-040-005
Continued on the following page

LAN COLOMBIA FLEET MI-26-01-01 P 3/6

MEL E to F 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 26-01-01 - FIRE Overhead Panel
MINIMUM EQUIPMENT LIST

Continued from the previous page

26-01-01-06B APU deactivated
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)

26-01-01-31 ENG FIRE TEST pb

Ident.: MI-26-01-01-00008455.0001001 / 21 MAR 10
Applicable to: ALL

26-01-01-31A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(m) One may be inoperative provided that the associated engine fire extinguishing and detection
systems are checked operative before the first flight of each day.
Reference(s)
(m) Refer to AMM 26-21-00-040-002

26-01-01-32 APU FIRE TEST pb

Ident.: MI-26-01-01-00008456.0001001 / 12 SEP 11
Applicable to: ALL

26-01-01-32A Daily check

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that the APU extinguishing system firing circuit and the bottle
low pressure detection system are checked operative before the first flight of each day.
Reference(s)
(m) Refer to AMM 26-22-00-040-012
Continued on the following page

LAN COLOMBIA FLEET MI-26-01-01 P 4/6

MEL F to H 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 26-01-01 - FIRE Overhead Panel
MINIMUM EQUIPMENT LIST

Continued from the previous page

26-01-01-32B APU deactivated
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)

26-01-01-33 APU FIRE PUSH pb-sw

Ident.: MI-26-01-01-00008459.0001001 / 21 MAR 10
Applicable to: ALL

26-01-01-33A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)

26-01-01-34 APU AGENT pb

Ident.: MI-26-01-01-00008461.0001001 / 21 MAR 10
Applicable to: ALL

26-01-01-34A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)

LAN COLOMBIA FLEET MI-26-01-01 P 5/6

MEL H to J 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 26-01-01 - FIRE Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-26-01-01 P 6/6

MEL 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 26-01-02 - CARGO SMOKE Overhead Panel
MINIMUM EQUIPMENT LIST

26-01-02-01 CARGO SMOKE DISCH light

Ident.: MI-26-01-02-00008467.0001001 / 12 SEP 11
Applicable to: ALL

26-01-02-01A Check of bottle weight

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(m) May be inoperative provided that the associated bottle weight is checked before the first
flight of each day.
Reference(s)
(m) Refer to AMM 26-23-00-040-001

26-01-02-01B Associated bottle considered inoperative

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
May be inoperative provided that the associated bottle is considered inoperative.
Refer to Item 26-23-01 Cargo Agent Bottle

LAN COLOMBIA FLEET MI-26-01-02 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 26-01-02 - CARGO SMOKE Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-26-01-02 P 2/2

MEL 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-12 - Engine Fire and Overheat Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-12-01 Engine Fire Detection Loop A on the Engine 1

Ident.: MI-26-12-00008470.0001001 / 10 OCT 14
Applicable to: ALL

26-12-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that:
1) ETOPS beyond 120 min is not conducted, and
2) The associated detection loop B is operative, and
3) The engine fire test is made before each flight.
Reference(s)
(o) Refer to OpsProc 26-12-01A Engine Fire Detection Loop

26-12-02 Engine Fire Detection Loop A on the Engine 2

Ident.: MI-26-12-00008473.0001001 / 10 OCT 14
Applicable to: ALL

26-12-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that:
1) The associated detection loop B is operative, and
2) The engine fire test is made before each flight.
Reference(s)
(o) Refer to OpsProc 26-12-02A Engine Fire Detection Loop

LAN COLOMBIA FLEET MI-26-12 P 1/2

MEL A to B 10 OCT 14
 MEL ITEMS
26 - FIRE PROTECTION
26-12 - Engine Fire and Overheat Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-12-03 Engine Fire Detection Loop B on the Engine 1

Ident.: MI-26-12-00008476.0001001 / 10 OCT 14
Applicable to: ALL

26-12-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that the engine fire test is made before each flight.
Reference(s)
(o) Refer to OpsProc 26-12-03A Engine Fire Detection Loop

26-12-04 Engine Fire Detection Loop B on the Engine 2

Ident.: MI-26-12-00008478.0001001 / 10 OCT 14
Applicable to: ALL

26-12-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that:
1) ETOPS beyond 120 min is not conducted, and
2) The engine fire test is made before each flight.
Reference(s)
(o) Refer to OpsProc 26-12-04A Engine Fire Detection Loop

26-12-05 FIRE light on the ENG MASTER Panel

Ident.: MI-26-12-00008480.0001001 / 21 MAR 10
Applicable to: ALL

26-12-05A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

LAN COLOMBIA FLEET MI-26-12 P 2/2

MEL C to E 10 OCT 14
 MEL ITEMS
26 - FIRE PROTECTION
26-13 - APU Fire and Overheat Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-13-01 APU Fire Detection Loop

Ident.: MI-26-13-00008482.0001001 / 27 FEB 15
Applicable to: ALL

26-13-01A Loop A inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) APU fire detection loop A may be inoperative provided that:
1) ETOPS beyond 120 min is not conducted, and
2) The APU fire test is made before each APU start, and
3) During APU operations on ground, APU condition is continuously monitored in the
cockpit.
Reference(s)
(o) Refer to OpsProc 26-13-01A APU Fire Detection Loop

26-13-01B Loop B inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) APU fire detection loop B may be inoperative provided that:
1) ETOPS beyond 120 min is not conducted, and
2) The APU fire test is made before each APU start.
Reference(s)
(o) Refer to OpsProc 26-13-01B APU Fire Detection Loop

26-13-01C Both loops inoperative

Repair interval Nbr installed Nbr required Placard
C 2 0 No
Both loops may be inoperative provided that:
1) ETOPS is not conducted, and
2) The APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)

LAN COLOMBIA FLEET MI-26-13 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
26 - FIRE PROTECTION
26-13 - APU Fire and Overheat Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-26-13 P 2/2

MEL 27 FEB 15
 MEL ITEMS
26 - FIRE PROTECTION
26-15 - Avionics Compartment Smoke Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-15-01 Avionics Smoke Detection System

Ident.: MI-26-15-00008485.0001001 / 21 MAR 10
Applicable to: ALL

26-15-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative provided that ETOPS is not conducted.
Reference(s)
(o) Refer to OpsProc 26-15-01A Avionics Smoke Detection System

LAN COLOMBIA FLEET MI-26-15 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-15 - Avionics Compartment Smoke Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-26-15 P 2/2

MEL 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-16 - Cargo Compartment Smoke Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-16-01 Smoke Detector in the FWD Cargo Compartment

Ident.: MI-26-16-00008486.0009001 / 10 OCT 14
Applicable to: ALL

Note: 1. The cargo smoke detection function is part of the CIDS Smoke Detection Function (
CIDS - SDF ).
Refer to Item 23-73-10-01 Smoke Detection Function (CIDS-SDF)
2. Failure of a single detector in the cavity is indicated by a MAINTENANCE message on
the STATUS SD page .
Refer to Item 26-00-01 SDCU/SMOKE MAINTENANCE Message

26-16-01A Empty FWD cargo compartment

Repair interval Nbr installed Nbr required Placard
D 2 0 No
Both detectors in the cavity may be inoperative provided that the FWD cargo compartment
is empty.

26-16-01B Non ETOPS flight

Repair interval Nbr installed Nbr required Placard
C 2 0 No
Both detectors in the cavity may be inoperative provided that ETOPS is not conducted.

26-16-01D Check of liner integrity

Repair interval Nbr installed Nbr required Placard
C 2 0 No
(m) Both detectors in the cavity may be inoperative provided that the liner integrity in the FWD
cargo compartment is checked before each flight.
Reference(s)
(m) Refer to AMM Task 25-50-00-200-002

LAN COLOMBIA FLEET MI-26-16 P 1/4

MEL A 27 FEB 15
 MEL ITEMS
26 - FIRE PROTECTION
26-16 - Cargo Compartment Smoke Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-16-02 Smoke Detector in the AFT and the BULK Cargo Compartments
Ident.: MI-26-16-00008488.0016001 / 27 FEB 15
Applicable to: ALL

Note: 1. The cargo smoke detection function is part of the CIDS Smoke Detection Function (
CIDS - SDF ).
Refer to Item 23-73-10-01 Smoke Detection Function (CIDS-SDF)
2. Failure of a single detector in the cavity is indicated by a MAINTENANCE message on
the STATUS SD page .
Refer to Item 26-00-01 SDCU/SMOKE MAINTENANCE Message
3. Depending on applicable regulation, smoke detection system may be required for
dispatch.

26-16-02A No flammable or combustible materials

Repair interval Nbr installed Nbr required Placard
D 4 0 No
Both detectors in one or both cavities may be inoperative provided that the AFT and the
BULK cargo compartments are empty or do not contain flammable or combustible materials.

26-16-02C Non ETOPS flight

Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) Both detectors in one or both cavities may be inoperative provided that:
1) ETOPS is not conducted, and
2) The AFT cargo ventilation is closed.
Reference(s)
(o) Refer to OpsProc 26-16-02C Smoke Detector in the AFT and the BULK Cargo
Compartments
Continued on the following page

LAN COLOMBIA FLEET MI-26-16 P 2/4

MEL B 27 FEB 15
 MEL ITEMS
26 - FIRE PROTECTION
26-16 - Cargo Compartment Smoke Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

26-16-02E Check of liner integrity
Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) (m) Both detectors in one or both cavities may be inoperative provided that:
1) The liner integrity in the AFT and the BULK cargo compartments is checked before each
flight, and
2) The AFT cargo ventilation is closed.
Reference(s)
(o) Refer to OpsProc 26-16-02E Smoke Detector in the AFT and the BULK Cargo
Compartments
(m) Refer to AMM Task 25-50-00-200-002

LAN COLOMBIA FLEET MI-26-16 P 3/4

MEL B 27 FEB 15
 MEL ITEMS
26 - FIRE PROTECTION
26-16 - Cargo Compartment Smoke Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-26-16 P 4/4

MEL 27 FEB 15
 MEL ITEMS
26 - FIRE PROTECTION
26-17 - Lavatory Smoke Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-17-01 Lavatory Smoke Detection System

Ident.: MI-26-17-00008489.0002001 / 27 FEB 15
Applicable to: ALL

Note: The lavatory smoke detection function is part of CIDS Smoke Detection Function ( CIDS -
SDF ).
Refer to Item 23-73-10-01 Smoke Detection Function (CIDS-SDF)

26-17-01A Associated lavatory fire extinguishing system operative

Repair interval Nbr installed Nbr required Placard
C 0 No
(o) One or more may be inoperative provided that:
1) The associated lavatory fire extinguishing system is operative, and
2) A procedure is used to periodically check absence of smoke in the associated lavatory.
Reference(s)
(o) Refer to OpsProc 26-17-01A Lavatory Smoke Detection System

26-17-01B Associated lavatory not used

Repair interval Nbr installed Nbr required Placard
C No
(o) One or more may be inoperative provided that:
1) The associated lavatory waste receptacle is empty, and
2) The associated lavatory door is locked closed and placarded inoperative, and
3) The lavatory is not used for storage or for any other purpose, and
4) A procedure is used to periodically check the absence of smoke in the associated
lavatory.
Reference(s)
(o) Refer to OpsProc 26-17-01B Lavatory Smoke Detection System

LAN COLOMBIA FLEET MI-26-17 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
26 - FIRE PROTECTION
26-17 - Lavatory Smoke Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-26-17 P 2/2

MEL 27 FEB 15
 MEL ITEMS
26 - FIRE PROTECTION
26-22 - APU Fire Extinguishing
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-22-01 APU Automatic Fire Extinguishing Control on Ground

Ident.: MI-26-22-00008491.0001001 / 26 JUN 11
Applicable to: ALL

26-22-01A APU operations on ground monitored

Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that the APU condition is continuously monitored in the cockpit
during APU operations on ground .

26-22-01B APU deactivated

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)

26-22-02 APU Fire Extinguisher Overpressure Indication (Red Disc)

Ident.: MI-26-22-00008492.0001001 / 12 SEP 11
Applicable to: ALL

26-22-02A APU Fire extinguisher bottle pressure switch operative

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(m) May be damaged or missing provided that the APU fire extinguisher bottle pressure switch
is checked operative before the fist flight of each day.
Reference(s)
(m) Refer to AMM 26-22-00-040-007
Continued on the following page

LAN COLOMBIA FLEET MI-26-22 P 1/4

MEL A to B 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-22 - APU Fire Extinguishing
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

26-22-02B APU deactivated
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)

26-22-03 Squib of the APU Fire Extinguisher Bottle

Ident.: MI-26-22-00008493.0001001 / 12 SEP 11
Applicable to: ALL

26-22-03A One inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(m) One may be inoperative provided that the remaining squib is checked operative before the
fist flight of each day.
Reference(s)
(m) Refer to AMM 26-22-00-040-008

26-22-03B Both inoperative

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
Both may be inoperative provided that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)

LAN COLOMBIA FLEET MI-26-22 P 2/4

MEL B to C 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-22 - APU Fire Extinguishing
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-22-04 APU Fire Extinguisher Bottle

Ident.: MI-26-22-00008494.0001001 / 21 MAR 10
Applicable to: ALL

26-22-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the APU is deactivated.
Refer to Item 49-10-01C Power Plant (APU)

26-22-05 APU AUTO EXTING TEST pb-sw on the Maintenance Panel

Ident.: MI-26-22-00008495.0001001 / 21 MAR 10
Applicable to: ALL

26-22-05A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that the APU automatic fire extinguishing control on ground is
considered inoperative.
Refer to Item 26-22-01 APU Automatic Fire Extinguishing Control on Ground

26-22-06 APU FIRE light on the External Power Panel

Ident.: MI-26-22-00008496.0001001 / 12 SEP 11
Applicable to: ALL

26-22-06A APU Automatic fire extinguishing control on ground operative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that the APU automatic fire extinguishing control on ground is
checked operative.
Reference(s)
(m) Refer to AMM 26-22-00-040-010
Continued on the following page

LAN COLOMBIA FLEET MI-26-22 P 3/4

MEL D to F 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-22 - APU Fire Extinguishing
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

26-22-06B APU Automatic fire extinguishing control on ground considered inoperative
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the APU automatic fire extinguishing control on ground is
considered inoperative.
Refer to Item 26-22-01 APU Automatic Fire Extinguishing Control on Ground

26-22-07 APU SHUT OFF pb on the External Power Panel

Ident.: MI-26-22-00008497.0001001 / 12 SEP 11
Applicable to: ALL

26-22-07A APU Automatic fire extinguishing control on ground operative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that the APU automatic fire extinguishing control on ground is
checked operative.
Reference(s)
(m) Refer to AMM 26-22-00-040-011

26-22-07B APU Automatic fire extinguishing control on ground considered inoperative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the APU automatic fire extinguishing control on ground is
considered inoperative.
Refer to Item 26-22-01 APU Automatic Fire Extinguishing Control on Ground

LAN COLOMBIA FLEET MI-26-22 P 4/4

MEL F to G 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-23 - Cargo Compartment Fire Extinguishing
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-23-01 Cargo Agent Bottle

Ident.: MI-26-23-00008498.0013001 / 10 OCT 14
Applicable to: ALL

Note: The cargo smoke detection function is part of CIDS Smoke Detection Function ( CIDS -
SDF ).
Refer to Item 23-73-10-01 Smoke Detection Function (CIDS-SDF)

26-23-01A No flammable or combustible materials

Repair interval Nbr installed Nbr required Placard
D 1 0 Yes
May be inoperative provided that the cargo compartments are empty or do not contain
flammable or combustible materials.

26-23-01B Non ETOPS flight

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that ETOPS is not conducted.

26-23-01D Check of liner integrity

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that the liner integrity in the cargo compartments is checked
before each flight.
Reference(s)
(m) Refer to AMM Task 25-50-00-200-002

LAN COLOMBIA FLEET MI-26-23 P 1/2

MEL A 10 OCT 14
 MEL ITEMS
26 - FIRE PROTECTION
26-23 - Cargo Compartment Fire Extinguishing
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-23-02 Squib of the Cargo Bottle 1

Ident.: MI-26-23-00008499.0006001 / 10 OCT 14
Applicable to: ALL

26-23-02A No flammable or combustible materials

Repair interval Nbr installed Nbr required Placard
D 2 0 Yes
One or both may be inoperative provided that the associated cargo compartment is empty
or does not contain flammable or combustible materials.

26-23-02B Non ETOPS flight

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative provided that ETOPS is not conducted.

26-23-02C Check of liner integrity

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(m) One or both may be inoperative provided that the liner integrity in the associated cargo
compartment is checked before each flight.
Reference(s)
(m) Refer to AMM Task 25-50-00-200-002

LAN COLOMBIA FLEET MI-26-23 P 2/2

MEL B 10 OCT 14
 MEL ITEMS
26 - FIRE PROTECTION
26-24 - Portable Fire Extinguisher
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-24-01 Portable Fire Extinguisher

Ident.: MI-26-24-00008501.0001001 / 23 MAR 11
Applicable to: ALL

26-24-01A
Repair interval Nbr installed Nbr required Placard
4 4 No
Must be operative.

LAN COLOMBIA FLEET MI-26-24 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-24 - Portable Fire Extinguisher
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-26-24 P 2/2

MEL 05 NOV 13
 MEL ITEMS
26 - FIRE PROTECTION
26-25 - Lavatory Fire Extinguishing
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-25-01 Lavatory Waste Bin Fire Extinguishing System

Ident.: MI-26-25-00008502.0001001 / 10 OCT 14
Applicable to: ALL

26-25-01A Lavatory Smoke Detection system operative

Repair interval Nbr installed Nbr required Placard
C 3 0 No
One or more may be inoperative provided associated lavatory smoke detection system
operates normally.

26-25-01B Lavatory Locked closed

Repair interval Nbr installed Nbr required Placard
C 3 1 No
(o) One or two may be inoperative provided:
1) The associated lavatory waste receptacle is empty, and
2) The associated lavatory doors are placarded INOPERATIVE DO NOT USE
INOPERATIVO NO USAR and locked closed,
3) The lavatory is not used for storage or any other purpose,
4) A procedure is used to check periodically absence of smoke in affected lavatory.
Note: If forward lavatory is locked closed, it can be used only by pilots on duty when
flight time is more than 1:30 hour.
Reference(s)
(o) Refer to OpsProc 26-25-01B Lavatory Smoke Detection System

26-25-01C Lavatory Locked closed

Repair interval Nbr installed Nbr required Placard
C 3 0 No
(o) One or more may be inoperative provided:
1) The associated lavatory waste receptacle is empty, and
2) The associated lavatory doors are placarded INOPERATIVE DO NOT USE
INOPERATIVO NO USAR and locked closed,
3) A procedure is used to check periodically absence of smoke in affected lavatory, and
4) Lavatory(ies) is(are) only used by crew members,and
5) Only non revenue flight is permitted.
Continued on the following page

LAN COLOMBIA FLEET MI-26-25 P 1/2

MEL A 10 OCT 14
 MEL ITEMS
26 - FIRE PROTECTION
26-25 - Lavatory Fire Extinguishing
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 26-25-01C Lavatory Smoke Detection System

LAN COLOMBIA FLEET MI-26-25 P 2/2

MEL A 10 OCT 14
 MEL ITEMS
27 - FLIGHT CONTROLS
27-00 - MAINTENANCE Messages on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-00-01 F/CTL MAINTENANCE Message

Ident.: MI-27-00-00008295.0001001 / 21 MAR 10
Applicable to: ALL

27-00-01A
Repair interval Nbr installed Nbr required Placard
C No
F/CTL MAINTENANCE message may be displayed on the STATUS SD page.

27-00-02 SFCS MAINTENANCE Message

Ident.: MI-27-00-00008296.0001001 / 21 MAR 10
Applicable to: ALL

27-00-02A
Repair interval Nbr installed Nbr required Placard
C No
SFCS MAINTENANCE message may be displayed on the STATUS SD page.

LAN COLOMBIA FLEET MI-27-00 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-00 - MAINTENANCE Messages on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-27-00 P 2/2

MEL 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 27-01-01 - FLT CTL Overhead Panel
MINIMUM EQUIPMENT LIST

27-01-01-01 ELAC pb-sw FAULT light

Ident.: MI-27-01-01-00008297.0001001 / 21 MAR 10
Applicable to: ALL

27-01-01-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
One may be inoperative.

27-01-01-02 ELAC pb-sw OFF light

Ident.: MI-27-01-01-00008298.0001001 / 21 MAR 10
Applicable to: ALL

27-01-01-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

27-01-01-03 SEC pb-sw FAULT light

Ident.: MI-27-01-01-00008300.0001001 / 21 MAR 10
Applicable to: ALL

27-01-01-03A
Repair interval Nbr installed Nbr required Placard
C 3 2 Yes
One may be inoperative.

LAN COLOMBIA FLEET MI-27-01-01 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 27-01-01 - FLT CTL Overhead Panel
MINIMUM EQUIPMENT LIST

27-01-01-04 SEC pb-sw OFF light

Ident.: MI-27-01-01-00008301.0001001 / 21 MAR 10
Applicable to: ALL

27-01-01-04A
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative.

LAN COLOMBIA FLEET MI-27-01-01 P 2/2

MEL D 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-07-01 Aileron Actuator Indication on the F/CTL SD page

Ident.: MI-27-07-00008397.0001001 / 21 MAR 10
Applicable to: ALL

27-07-01A
Repair interval Nbr installed Nbr required Placard
C 4 0 No
One or more may be inoperative.

27-07-02 Aileron Position Indication on the F/CTL SD page

Ident.: MI-27-07-00008398.0001001 / 21 MAR 10
Applicable to: ALL

27-07-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) One or more may be inoperative provided that the deflection of the affected aileron through
each servo-control is visually checked before each flight.
Reference(s)
(o) Refer to OpsProc 27-07-02A Aileron Position Indication on the F/CTL SD page

27-07-03 Elevator Actuator Indication on the F/CTL SD page

Ident.: MI-27-07-00008399.0001001 / 21 MAR 10
Applicable to: ALL

27-07-03A
Repair interval Nbr installed Nbr required Placard
C 4 0 No
One or more may be inoperative.

LAN COLOMBIA FLEET MI-27-07 P 1/6

MEL A to C 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-07-04 Elevator Position Indication on the F/CTL SD page

Ident.: MI-27-07-00008400.0001001 / 21 MAR 10
Applicable to: ALL

27-07-04A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) One or both may be inoperative provided that the deflection of the affected elevator is
visually checked before each flight.
Reference(s)
(o) Refer to OpsProc 27-07-04A Elevator Position Indication on the F/CTL SD page

27-07-05 Pitch Trim Position Indication on the F/CTL SD page

Ident.: MI-27-07-00008401.0001001 / 21 MAR 10
Applicable to: ALL

27-07-05A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative provided that the pitch trim handwheel and the stabilizer are visually
checked to synchronously operate before each flight.
Reference(s)
(o) Refer to OpsProc 27-07-05A Pitch Trim Position Indication on the F/CTL SD page

27-07-06 Rudder Position Indication on the F/CTL SD page

Ident.: MI-27-07-00008402.0001001 / 21 MAR 10
Applicable to: ALL

27-07-06A
Repair interval Nbr installed Nbr required Placard
B 1 0 No
(o) May be inoperative provided that the deflection of the rudder is visually checked before
each flight.
Continued on the following page

LAN COLOMBIA FLEET MI-27-07 P 2/6

MEL D to F 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 27-07-06A Rudder Position Indication on the F/CTL SD page

27-07-07 Rudder Trim Position Indication on the F/CTL SD page

Ident.: MI-27-07-00008403.0001001 / 12 SEP 11
Applicable to: ALL

27-07-07A Rudder trim position indication operative on the center pedestal

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the rudder trim position indication is operative on the
center pedestal .

27-07-07B Rudder position checked at zero

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the rudder position is checked at zero on the F/CTL SD
page before takeoff.

27-07-08 Rudder Travel Limiter Position Indication on the F/CTL SD page

Ident.: MI-27-07-00008405.0003001 / 27 FEB 15
Applicable to: ALL

27-07-08A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-27-07 P 3/6

MEL F to H 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-07-09 ELAC Indication on the F/CTL SD page

Ident.: MI-27-07-00008407.0001001 / 21 MAR 10
Applicable to: ALL

27-07-09A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

27-07-10 SEC Indication on the F/CTL SD page

Ident.: MI-27-07-00008410.0001001 / 21 MAR 10
Applicable to: ALL

27-07-10A
Repair interval Nbr installed Nbr required Placard
C 3 0 No
One or more may be inoperative.

27-07-11 Spoilers/Speedbrakes Indication on the F/CTL SD page

Ident.: MI-27-07-00008412.0001001 / 21 MAR 10
Applicable to: ALL

27-07-11A
Repair interval Nbr installed Nbr required Placard
C 10 0 No
(o) One or more may be inoperative provided that the deflection of the affected surface is
visually checked before each flight.
Reference(s)
(o) Refer to OpsProc 27-07-11A Spoilers/Speedbrakes Indication on the F/CTL SD page

LAN COLOMBIA FLEET MI-27-07 P 4/6

MEL I to K 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-07-12 Spoilers/Speedbrakes Indication on the WHEEL SD page

Ident.: MI-27-07-00008414.0001001 / 21 MAR 10
Applicable to: ALL

27-07-12A
Repair interval Nbr installed Nbr required Placard
C 10 0 No
(o) One or more may be inoperative provided that the deflection of the affected surface is
visually checked before each flight.
Reference(s)
(o) Refer to OpsProc 27-07-12A Spoilers/Speedbrakes Indication on the WHEEL SD page

LAN COLOMBIA FLEET MI-27-07 P 5/6

MEL L 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-27-07 P 6/6

MEL 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-08 - Indications on the EWD
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-08-01 Flap Position Indication on the EWD

Ident.: MI-27-08-00008417.0001001 / 21 MAR 10
Applicable to: ALL

27-08-01A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

27-08-02 Slat Position Indication on the EWD

Ident.: MI-27-08-00008418.0001001 / 21 MAR 10
Applicable to: ALL

27-08-02A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

LAN COLOMBIA FLEET MI-27-08 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-08 - Indications on the EWD
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-27-08 P 2/2

MEL 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-14 - Aileron and Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-14-01 Left Aileron Blue Servo-Control (Controlled by ELAC 1)

Ident.: MI-27-14-00008312.0002001 / 21 MAR 10
Applicable to: ALL

27-14-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that:
1) It is electrically disconnected, and
2) It remains mechanically connected and hydraulically supplied (damping function is not
affected), and
3) The left aileron green servo-control (controlled by ELAC 2) is operative, and
4) The right aileron blue servo-control (controlled by ELAC 2) is operative, and
5) All roll spoilers are operative, and
6) The TR 1 and TR 2 are operative, and
7) The DC TIE contactor 1PC1 is checked closed.
Reference(s)
(o) Refer to OpsProc 27-14-01A Left Aileron Blue Servo-Control (Controlled by ELAC 1)
(m) Refer to AMM 27-14-00-040-001

27-14-02 Left Aileron Green Servo-Control (Controlled by ELAC 2)

Ident.: MI-27-14-00008314.0002001 / 21 MAR 10
Applicable to: ALL

27-14-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(m) May be inoperative provided that:
1) It is electrically disconnected, and
2) It remains mechanically connected and hydraulically supplied (damping function is not
affected), and
3) All roll spoilers are operative.
Reference(s)
(m) Refer to AMM 27-14-00-040-001

LAN COLOMBIA FLEET MI-27-14 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-14 - Aileron and Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-14-03 Right Aileron Green Servo-Control (Controlled by ELAC 1)

Ident.: MI-27-14-00008316.0002001 / 21 MAR 10
Applicable to: ALL

27-14-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that:
1) It is electrically disconnected, and
2) It remains mechanically connected and hydraulically supplied (damping function is not
affected), and
3) The right aileron blue servo-control (controlled by ELAC 2) is operative, and
4) The left aileron green servo-control (controlled by ELAC 2) is operative, and
5) All roll spoilers are operative, and
6) The TR 1 and TR 2 are operative, and
7) The DC TIE contactor 1PC1 is checked closed.
Reference(s)
(o) Refer to OpsProc 27-14-03A Right Aileron Green Servo-Control (Controlled by ELAC 1)
(m) Refer to AMM 27-14-00-040-001

27-14-04 Right Aileron Blue Servo-Control (Controlled by ELAC 2)

Ident.: MI-27-14-00008318.0002001 / 21 MAR 10
Applicable to: ALL

27-14-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(m) May be inoperative provided that:
1) It is electrically disconnected, and
2) It remains mechanically connected and hydraulically supplied (damping function is not
affected), and
3) All roll spoilers are operative.
Reference(s)
(m) Refer to AMM 27-14-00-040-001

LAN COLOMBIA FLEET MI-27-14 P 2/2

MEL C to D 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-21 - Rudder Mechanical Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-21-01 Rudder Pedal Adjustment System

Ident.: MI-27-21-00008322.0001001 / 21 MAR 10
Applicable to: ALL

27-21-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) One or both may be inoperative provided that:
1) The rudder pedals can be secured in a position which meets individual pilot
requirements, and
2) The full and unrestricted movement of the rudder pedals and brake pedals deflection is
possible at both pilot stations.
Reference(s)
(o) Refer to OpsProc 27-21-01A Rudder Pedal Adjustment System

LAN COLOMBIA FLEET MI-27-21 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-21 - Rudder Mechanical Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-27-21 P 2/2

MEL 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-22 - Rudder Trim Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-22-01 Rudder Trim System

Ident.: MI-27-22-00008324.0001001 / 12 SEP 12
Applicable to: ALL

27-22-01A Rudder trim system 1 inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) ** Rudder Trim System 1 may be inoperative provided that ETOPS is not conducted.
Reference(s)
(o) Refer to OpsProc 27-22-01A Rudder Trim System

27-22-01B Rudder trim system 2 inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) ** Rudder Trim System 2 may be inoperative.
Reference(s)
(o) Refer to OpsProc 27-22-01B Rudder Trim System

27-22-02 Manual Rudder Trim Reset Function

Ident.: MI-27-22-00008326.0001001 / 21 MAR 10
Applicable to: ALL

27-22-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that one rudder trim position indication is operative.

LAN COLOMBIA FLEET MI-27-22 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-22 - Rudder Trim Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-22-03 Rudder Trim Position Indication on the Center Pedestal

Ident.: MI-27-22-00008328.0001001 / 21 MAR 10
Applicable to: ALL

27-22-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-27-22 P 2/2

MEL C 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-23 - Artificial feel and rudder travel limiting actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-23-01 Rudder Travel Limiter System(Including

Rudder and Pedals Travel Limiter Units)
Ident.: MI-27-23-00008330.0001001 / 12 SEP 12
Applicable to: ALL

27-23-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
** One may be inoperative.

LAN COLOMBIA FLEET MI-27-23 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-23 - Artificial feel and rudder travel limiting actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-27-23 P 2/2

MEL 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-34 - Elevator and Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-34-01 Elevator Servo-Control

Ident.: MI-27-34-00008332.0001001 / 21 MAR 10
Applicable to: ALL

27-34-01A
Repair interval Nbr installed Nbr required Placard
4 4 No
All must be operative.

27-34-02 Elevator Servo-Control Position Transducer

Ident.: MI-27-34-00008334.0001001 / 12 SEP 11
Applicable to: ALL

27-34-02A
Repair interval Nbr installed Nbr required Placard
C 8 4 No
(m) One transducer per servo-control must be operative.
Reference(s)
(m) Refer to AMM 27-34-00-040-001

LAN COLOMBIA FLEET MI-27-34 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-34 - Elevator and Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-27-34 P 2/2

MEL 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-40 - Trimmable Horizontal Stabilizer (THS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-40-01 Stabilizer Mechanical Control

Ident.: MI-27-40-00008336.0001001 / 21 MAR 10
Applicable to: ALL

27-40-01A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

27-40-02 Stabilizer Actuator Electric Motor

Ident.: MI-27-40-00008338.0001001 / 12 SEP 11
Applicable to: ALL

27-40-02A Electric motor 3 inoperative

Repair interval Nbr installed Nbr required Placard
C 3 2 No
The stabilizer actuator electric motor 3 may be inoperative.

27-40-02B Electric motor 2 inoperative

Repair interval Nbr installed Nbr required Placard
C 3 2 No
The stabilizer actuator electric motor 2 may be inoperative provided that:
1) ETOPS is not conducted, and
2) ELAC 1 pitch channel is considered inoperative.
Refer to Item 27-93-01 ELAC 1

LAN COLOMBIA FLEET MI-27-40 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-40 - Trimmable Horizontal Stabilizer (THS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-27-40 P 2/2

MEL 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-51 - Flaps Electrical Control and Monitoring
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-51-01 SFCC Flap Channel

Ident.: MI-27-51-00008340.0001001 / 05 NOV 13
Applicable to: ALL

Note: RNP Item

27-51-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(o) (m) SFCC 2 flap channel may be inoperative provided that:
1) RNAV ( RNP ) operations are not conducted, and
2) It is deactivated, and
3) The slats and flaps are checked operative on SFCC 1, and
4) The SFCC 1 flap WTB is checked operative before each flight, and
5) All ELAC s, SEC s, LGCIU s, RA s, FAC s and ADIRS are operative, and
6) The minimum idle on ground is considered inoperative.
Refer to Item 73-20-05 Minimum Idle on Ground
Reference(s)
(o) Refer to OpsProc 27-51-01A SFCC Flap Channel
(m) Refer to AMM 27-51-00-040-001

27-51-02 SFCC Slat Channel

Ident.: MI-27-51-00008341.0001001 / 05 NOV 13
Applicable to: ALL

Note: RNP Item

Continued on the following page

LAN COLOMBIA FLEET MI-27-51 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-51 - Flaps Electrical Control and Monitoring
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

27-51-02A
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(o) (m) SFCC 2 slat channel may be inoperative provided that:
1) RNAV ( RNP ) operations are not conducted, and
2) It is deactivated, and
3) The slats and flaps are checked operative on SFCC 1, and
4) The SFCC 1 slat WTB is checked operative before each flight, and
5) All ELAC s, SEC s, LGCIU s, RA s, FAC s and ADIRS are operative, and
6) Takeoff is not performed in CONF 1+F.
Reference(s)
(o) Refer to OpsProc 27-51-02A SFCC Slat Channel
(m) Refer to AMM 27-51-00-040-005

27-51-03 Flap Wing Tip Brakes Solenoid

Ident.: MI-27-51-00009138.0001001 / 21 MAR 10
Applicable to: ALL

27-51-03A
Repair interval Nbr installed Nbr required Placard
C 4 2 No
(m) One or two solenoids associated with the SFCC 2 may be inoperative provided that the
SFCC 1 flap WTB is checked operative before each flight.
Reference(s)
(m) Refer to AMM 27-51-00-040-004

LAN COLOMBIA FLEET MI-27-51 P 2/2

MEL B to C 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-54 - Flaps Hydraulic Actuation and Power Transmission
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-54-01 Flap Hydraulic Motor

Ident.: MI-27-54-00008344.0001001 / 12 SEP 11
Applicable to: ALL

27-54-01A Green motor inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
Green motor may be inoperative.

27-54-01B Yellow motor inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
Yellow motor may be inoperative provided that the blue slat motor is operative.

27-54-02 Flap PCU Valve Block

Ident.: MI-27-54-00008345.0001001 / 14 SEP 10
Applicable to: ALL

27-54-02A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
The valve block associated with SFCC 2 may be inoperative provided that the SFCC 2 flap
channel is considered inoperative.
Refer to Item 27-51-01 SFCC Flap Channel

LAN COLOMBIA FLEET MI-27-54 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-54 - Flaps Hydraulic Actuation and Power Transmission
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-54-03 Flap Pressure-Off Brake

Ident.: MI-27-54-00008347.0001001 / 21 MAR 10
Applicable to: ALL

27-54-03A
Repair interval Nbr installed Nbr required Placard
2 2 No
Both must be operative.

LAN COLOMBIA FLEET MI-27-54 P 2/2

MEL C 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-64 - Spoiler Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-64-01 Spoiler 5
Ident.: MI-27-64-00008349.0002001 / 27 FEB 15
Applicable to: MSN 4516-5364

27-64-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) (m) The pair of spoilers 5 may be inoperative provided that:
1) The affected spoiler is deactivated in the retracted position, and
2) The pairs of spoilers 1, 2, 3, and 4 are operative.
Reference(s)
(o) Refer to OpsProc 27-64-01A Spoiler 5
(m) Refer to AMM 27-64-00-040-001

27-64-01 Spoiler 5
Ident.: MI-27-64-00008349.0008001 / 10 OCT 14
Applicable to: MSN 5443-5453

27-64-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) (m) The pair of spoilers 5 may be inoperative provided that:
1) The affected spoiler is deactivated in the retracted position, and
2) The pairs of spoilers 1, 2, 3, and 4 are operative, and
3) The MTOW is limited to 76 400 kg ( 168 430 lb ).
Reference(s)
(o) Refer to OpsProc 27-64-01A Spoiler 5
(m) Refer to AMM 27-64-00-040-001

LAN COLOMBIA FLEET MI-27-64 P 1/6

MEL A 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-64 - Spoiler Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-64-02 Spoiler 1 or 3
Ident.: MI-27-64-00008351.0001001 / 21 MAR 10
Applicable to: ALL

27-64-02A
Repair interval Nbr installed Nbr required Placard
C 4 2 No
(o) (m) One pair of spoilers 1 or 3 may be inoperative provided that:
1) The affected spoiler is deactivated in the retracted position, and
2) The pairs of spoilers 2, 4, and 5 are operative, and
3) The Flight Manual performance penalties are applied.
Reference(s)
(o) Refer to OpsProc 27-64-02A Spoiler 1 or 3
(m) Refer to AMM 27-64-00-040-001

27-64-03 Spoiler 2 or 4
Ident.: MI-27-64-00008354.0002001 / 27 FEB 15
Applicable to: MSN 4516-5364

27-64-03A
Repair interval Nbr installed Nbr required Placard
C 4 2 No
(o) (m) One pair of spoilers 2 or 4 may be inoperative in the retracted position provided that:
1) The affected spoiler is deactivated in the retracted position, and
2) The pairs of spoilers 1, 3, and 5 are operative, and
3) The SFCC 2 flap channel is operative, and
4) The Flight Manual performance penalties are applied.
Reference(s)
(o) Refer to OpsProc 27-64-03A Spoiler 2 or 4
(m) Refer to AMM 27-64-00-040-001

LAN COLOMBIA FLEET MI-27-64 P 2/6

MEL B to C 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-64 - Spoiler Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-64-03 Spoiler 2 or 4
Ident.: MI-27-64-00008354.0008001 / 10 OCT 14
Applicable to: MSN 5443-5453

27-64-03A
Repair interval Nbr installed Nbr required Placard
C 4 2 No
(o) (m) One pair of spoilers 2 or 4 may be inoperative in the retracted position provided that:
1) The affected spoiler is deactivated in the retracted position, and
2) The pairs of spoilers 1, 3, and 5 are operative, and
3) The SFCC 2 flap channel is operative, and
4) The Flight Manual performance penalties are applied, and
5) If the pair of spoilers 4 is inoperative, the MTOW is limited to 76 400 kg ( 168 430 lb ).
Reference(s)
(o) Refer to OpsProc 27-64-03A Spoiler 2 or 4
(m) Refer to AMM 27-64-00-040-001

27-64-04 Spoilers 1 and 2

Ident.: MI-27-64-00008357.0001001 / 21 MAR 10
Applicable to: ALL

27-64-04A
Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) (m) The pairs of spoilers 1 and 2 may be inoperative in the retracted position provided that:
1) The affected spoilers are deactivated in the retracted position, and
2) The pairs of spoilers 3, 4, and 5 are operative, and
3) The SFCC 2 flap channel is operative, and
4) The Flight Manual performance penalties are applied.
Reference(s)
(o) Refer to OpsProc 27-64-04A Spoilers 1 and 2
(m) Refer to AMM 27-64-00-040-001

LAN COLOMBIA FLEET MI-27-64 P 3/6

MEL C to D 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-64 - Spoiler Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-64-05 Spoilers 3 and 4

Ident.: MI-27-64-00008359.0002001 / 27 FEB 15
Applicable to: MSN 4516-5364

27-64-05A
Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) (m) The pairs of spoilers 3 and 4 may be inoperative in the retracted position provided that:
1) The affected spoilers are deactivated in the retracted position, and
2) The pairs of spoilers 1, 2, and 5 are operative, and
3) The TR 1 and TR 2 are operative, and
4) The DC TIE contactor 1PC1 is checked closed, and
5) The SFCC 2 flap channel is operative, and
6) The Flight Manual performance penalties are applied.
Reference(s)
(o) Refer to OpsProc 27-64-05A Spoilers 3 and 4
(m) Refer to AMM 27-64-00-040-001

27-64-05 Spoilers 3 and 4

Ident.: MI-27-64-00008359.0008001 / 10 OCT 14
Applicable to: MSN 5443-5453

27-64-05A
Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) (m) The pairs of spoilers 3 and 4 may be inoperative in the retracted position provided that:
1) The affected spoilers are deactivated in the retracted position, and
2) The pairs of spoilers 1, 2, and 5 are operative, and
3) The TR 1 and TR 2 are operative, and
4) The DC TIE contactor 1PC1 is checked closed, and
5) The SFCC 2 flap channel is operative, and
6) The Flight Manual performance penalties are applied, and
7) The MTOW is limited to 76 400 kg ( 168 430 lb ).
Continued on the following page

LAN COLOMBIA FLEET MI-27-64 P 4/6

MEL E 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-64 - Spoiler Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 27-64-05A Spoilers 3 and 4
(m) Refer to AMM 27-64-00-040-001

LAN COLOMBIA FLEET MI-27-64 P 5/6

MEL E 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-64 - Spoiler Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-27-64 P 6/6

MEL 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-81 - Slats Electrical Control and Monitoring
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-81-01 Slat Wing Tip Brakes Solenoids

Ident.: MI-27-81-00008366.0001001 / 21 MAR 10
Applicable to: ALL

27-81-01A
Repair interval Nbr installed Nbr required Placard
C 4 2 No
(m) One or two solenoids associated with the SFCC 2 may be inoperative provided that the
SFCC 1 slat WTB is checked operative before each flight.
Reference(s)
(m) Refer to AMM 27-81-00-040-001

LAN COLOMBIA FLEET MI-27-81 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-81 - Slats Electrical Control and Monitoring
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-27-81 P 2/2

MEL 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-84 - Slats Hydraulic Actuation and Power Transmission
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-84-01 Slats Hydraulic Motor

Ident.: MI-27-84-00008368.0001001 / 21 MAR 10
Applicable to: ALL

27-84-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative.

27-84-02 Slat PCU Valve Block

Ident.: MI-27-84-00008371.0001001 / 21 MAR 10
Applicable to: ALL

27-84-02A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
The valve block associated with SFCC 2 may be inoperative provided that the SFCC 2 slat
channel is considered inoperative.
Refer to Item 27-51-02 SFCC Slat Channel

27-84-03 Slat Pressure-Off Brake

Ident.: MI-27-84-00008373.0001001 / 21 MAR 10
Applicable to: ALL

27-84-03A
Repair interval Nbr installed Nbr required Placard
2 2 No
Both must be operative.

LAN COLOMBIA FLEET MI-27-84 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-84 - Slats Hydraulic Actuation and Power Transmission
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-27-84 P 2/2

MEL 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-92 - Electrical Flight Control System
COLOMBIA
LAN COLOMBIA AIRLINES (EFCS) Control Inputs and Power Supply
MINIMUM EQUIPMENT LIST

27-92-01 Speedbrake Control System

Ident.: MI-27-92-00008375.0001001 / 12 SEP 11
Applicable to: ALL

27-92-01A Speedbrake control system inoperative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) Speedbrake control system may be inoperative provided that the Flight Manual performance
penalties associated with the ground spoiler control system inoperative are applied.
Reference(s)
(o) Refer to OpsProc 27-92-01A Speedbrake Control System (speedbrake control system
inoperative)

27-92-01B Speedbrake 2 or speedbrakes 3 and 4 inoperative

Repair interval Nbr installed Nbr required Placard
C 1 1 No
(o) Speedbrake 2 or speedbrakes 3 and 4 may be inoperative provided that the Flight Manual
performance penalties associated with one or two pairs of spoilers inoperative are applied.
Reference(s)
(o) Refer to OpsProc 27-92-01B Speedbrake Control System (speedbrake 2 or speedbrakes 3
and 4 inoperative)

LAN COLOMBIA FLEET MI-27-92 P 1/4

MEL A 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-92 - Electrical Flight Control System
COLOMBIA
LAN COLOMBIA AIRLINES (EFCS) Control Inputs and Power Supply
MINIMUM EQUIPMENT LIST

27-92-02 Ground Spoiler Control System

Ident.: MI-27-92-00008377.0001001 / 27 NOV 12
Applicable to: ALL

27-92-02A Ground spoiler control system inoperative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that:
1) Both thrust reversers are not taken into account for performance computation, and
2) The autobrake function is not used, and
3) The Flight Manual performance penalties are applied, and
4) Do not dispatch to runways lower than 1900 mts lenght.
Note: Check aircraft performance on take off and landing at departure, destination
and alternate aerodromes.
Reference(s)
(o) Refer to OpsProc 27-92-02A Ground Spoiler Control System (ground spoiler control system
inoperative)

27-92-02B Spoilers 5 inoperative

Repair interval Nbr installed Nbr required Placard
C 1 1 No
(o) The pair of spoilers 5 may be inoperative.
Reference(s)
(o) Refer to OpsProc 27-92-02B Ground Spoiler Control System (pair of spoilers 5 inoperative)

27-92-02C Spoilers 1 and 2, or spoilers 3 and 4 inoperative

Repair interval Nbr installed Nbr required Placard
C 1 1 No
(o) The pairs of spoilers 1 and 2 or the pairs of spoilers 3 and 4 may be inoperative provided
that the Flight Manual performance penalties are applied.
Continued on the following page

LAN COLOMBIA FLEET MI-27-92 P 2/4

MEL B 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-92 - Electrical Flight Control System
COLOMBIA
LAN COLOMBIA AIRLINES (EFCS) Control Inputs and Power Supply
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 27-92-02C Ground Spoiler Control System (pairs of spoilers 1 and 2 or
pairs of spoilers 3 and 4 inoperative)

27-92-03 SIDESTICK PRIORITY light

Ident.: MI-27-92-00008380.0001001 / 21 MAR 10
Applicable to: ALL

27-92-03A
Repair interval Nbr installed Nbr required Placard
4 4 No
All must be operative.

27-92-04 Sidestick Dual Input Visual Warnings

Ident.: MI-27-92-00008382.0001001 / 21 MAR 10
Applicable to: ALL

27-92-04A
Repair interval Nbr installed Nbr required Placard
D 2 0 No
One or both may be inoperative.

27-92-05 Sidestick Dual Input Aural Warning

Ident.: MI-27-92-00008384.0001001 / 12 SEP 12
Applicable to: ALL

27-92-05A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-27-92 P 3/4

MEL B to E 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-92 - Electrical Flight Control System
COLOMBIA
LAN COLOMBIA AIRLINES (EFCS) Control Inputs and Power Supply
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-27-92 P 4/4

MEL 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-93 - ELAC System (Elevator Aileron Computer)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-93-01 ELAC 1
Ident.: MI-27-93-00008385.0008001 / 05 NOV 13
Applicable to: ALL

Note: RNP Item

27-93-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) (m) ** ELAC 1 or any ELAC 1 function may be inoperative provided that:
1) ETOPS and RNAV ( RNP ) operations are not conducted, and
2) All SEC s, SFCC s, LGCIU s, RA s, ADIRS and FAC s are operative, and
3) The pairs of spoilers 2, 3, 4, and 5 are operative, and
4) The TR 1 and the TR 2 are operative, and
5) Both accelerometers associated with the ELAC 2 are checked operative before each
flight, and
6) All sidesticks transducers associated with the ELAC 2 and the three SEC s are checked
operative before each flight, and
7) The DC TIE contactor 1PC1 is checked closed, before each flight, and
8) The elevators and roll spoilers control is checked operative through the SEC s before
each flight.
Note: F/O take-over pb cannot disengage AP 1.
Reference(s)
(o) Refer to OpsProc 27-93-01A ELAC 1
(m) Refer to AMM 27-93-00-040-001

27-93-02 ELAC 2
Ident.: MI-27-93-00008386.0001001 / 05 NOV 13
Applicable to: ALL

Note: RNP Item

Continued on the following page

LAN COLOMBIA FLEET MI-27-93 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-93 - ELAC System (Elevator Aileron Computer)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

27-93-02A
Repair interval Nbr installed Nbr required Placard
1 1 No
** Must be operative.

27-93-03 Pitch Normal Law

Ident.: MI-27-93-00008388.0001001 / 21 MAR 10
Applicable to: ALL

27-93-03A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

LAN COLOMBIA FLEET MI-27-93 P 2/2

MEL B to C 05 NOV 13
 MEL ITEMS
27 - FLIGHT CONTROLS
27-94 - SEC System (Spoiler and Elevator Computer)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-94-01 SEC 1
Ident.: MI-27-94-00008390.0002001 / 27 FEB 15
Applicable to: MSN 4516-5364

27-94-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) (m) May be inoperative provided that:
1) ETOPS is not conducted, and
2) It is deactivated, and
3) The SEC 2 and the SEC 3 are operative, and
4) All ELAC s, SFCC s, LGCIU s, RA s, FAC s and ADIRS are operative, and
5) The SFCC 2 flap channel is operative, and
6) All aileron servo-controls associated with the operative SEC s are operative, and
7) The TR 1 and TR 2 are operative, and
8) The sidestick transducers associated with the ELAC s and the operative SEC s are
checked operative before each flight, and
9) The DC TIE contactor 1PC1 is checked closed, before each flight, and
10) The elevators control through the SEC 2 and the ELAC s and the roll spoilers control
through the operative SEC s are checked operative before each flight, and
11) The Flight Manual performance penalties for the pairs of spoilers 3 and 4 inoperative
are applied.
Reference(s)
(o) Refer to OpsProc 27-94-01A SEC 1
(m) Refer to AMM 27-94-00-040-002

LAN COLOMBIA FLEET MI-27-94 P 1/6

MEL A 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-94 - SEC System (Spoiler and Elevator Computer)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-94-01 SEC 1
Ident.: MI-27-94-00008390.0012001 / 10 OCT 14
Applicable to: MSN 5443-5453

27-94-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) (m) May be inoperative provided that:
1) ETOPS is not conducted, and
2) It is deactivated, and
3) The SEC 2 and the SEC 3 are operative, and
4) All ELAC s, SFCC s, LGCIU s, RA s, FAC s and ADIRS are operative, and
5) The SFCC 2 flap channel is operative, and
6) All aileron servo-controls associated with the operative SEC s are operative, and
7) The TR 1 and TR 2 are operative, and
8) The sidestick transducers associated with the ELAC s and the operative SEC s are
checked operative before each flight, and
9) The DC TIE contactor 1PC1 is checked closed, before each flight, and
10) The elevators control through the SEC 2 and the ELAC s and the roll spoilers control
through the operative SEC s are checked operative before each flight, and
11) The Flight Manual performance penalties for the pairs of spoilers 3 and 4 inoperative
are applied, and
12) The MTOW is limited to 76 400 kg ( 168 430 lb ).
Reference(s)
(o) Refer to OpsProc 27-94-01A SEC 1
(m) Refer to AMM 27-94-00-040-002

LAN COLOMBIA FLEET MI-27-94 P 2/6

MEL A 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-94 - SEC System (Spoiler and Elevator Computer)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-94-02 SEC 2
Ident.: MI-27-94-00008392.0002001 / 27 FEB 15
Applicable to: MSN 4516-5364

27-94-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) (m) May be inoperative provided that:
1) It is deactivated, and
2) The SEC 1 and the SEC 3 are operative, and
3) All ELAC s, SFCC s, LGCIU s, RA s, FAC s and ADIRS are operative, and
4) All aileron servo-controls and roll spoilers associated with the operative SEC s are
operative, and
5) The sidestick transducers associated with the ELAC s and the operative SEC s are
checked operative before each flight, and
6) The elevators control through the SEC 1 and the ELAC s and the roll spoilers control
through the operative SEC s are checked operative before each flight.
Reference(s)
(o) Refer to OpsProc 27-94-02A SEC 2
(m) Refer to AMM Task 27-94-00-040-002

LAN COLOMBIA FLEET MI-27-94 P 3/6

MEL B 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-94 - SEC System (Spoiler and Elevator Computer)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-94-02 SEC 2
Ident.: MI-27-94-00008392.0012001 / 10 OCT 14
Applicable to: MSN 5443-5453

27-94-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) (m) May be inoperative provided that:
1) It is deactivated, and
2) The SEC 1 and the SEC 3 are operative, and
3) All ELAC s, SFCC s, LGCIU s, RA s, FAC s and ADIRS are operative, and
4) All aileron servo-controls and roll spoilers associated with the operative SEC s are
operative, and
5) The sidestick transducers associated with the ELAC s and the operative SEC s are
checked operative before each flight, and
6) The elevators control through the SEC 1 and the ELAC s and the roll spoilers control
through the operative SEC s are checked operative before each flight.
7) The MTOW is limited to 76 400 kg ( 168 430 lb ).
Reference(s)
(o) Refer to OpsProc 27-94-02A SEC 2
(m) Refer to AMM 27-94-00-040-002

LAN COLOMBIA FLEET MI-27-94 P 4/6

MEL B 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-94 - SEC System (Spoiler and Elevator Computer)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-94-03 SEC 3
Ident.: MI-27-94-00008394.0001001 / 10 OCT 14
Applicable to: ALL

27-94-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that:
1) It is deactivated, and
2) The SEC 1 and SEC 2 are operative, and
3) The SFCC 2 flap channel is operative, and
4) All aileron servo-controls and roll spoilers associated with the operative SEC s are
operative, and
5) The Flight Manual performance penalties for the pairs of spoilers 1 and 2 inoperative are
applied.
Reference(s)
(o) Refer to OpsProc 27-94-03A SEC 3

LAN COLOMBIA FLEET MI-27-94 P 5/6

MEL C 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-94 - SEC System (Spoiler and Elevator Computer)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-27-94 P 6/6

MEL 27 FEB 15
 MEL ITEMS
27 - FLIGHT CONTROLS
27-95 - FCDC System (Flight Control Data Concentrator)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-95-01 FCDC 1
Ident.: MI-27-95-00008395.0001001 / 21 MAR 10
Applicable to: ALL

27-95-01A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

27-95-02 FCDC 2
Ident.: MI-27-95-00008396.0001001 / 10 OCT 14
Applicable to: ALL

27-95-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 27-95-02A FCDC 2

LAN COLOMBIA FLEET MI-27-95 P 1/2

MEL A to B 10 OCT 14
 MEL ITEMS
27 - FLIGHT CONTROLS
27-95 - FCDC System (Flight Control Data Concentrator)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-27-95 P 2/2

MEL 10 OCT 14
 MEL ITEMS
28 - FUEL
28-00 - MAINTENANCE Message on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-00-01 FUEL MAINTENANCE Message

Ident.: MI-28-00-00008177.0001001 / 21 MAR 10
Applicable to: ALL

28-00-01A
Repair interval Nbr installed Nbr required Placard
C No
FUEL MAINTENANCE message may be displayed on the STATUS SD page.

LAN COLOMBIA FLEET MI-28-00 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
28 - FUEL
28-00 - MAINTENANCE Message on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-28-00 P 2/2

MEL 05 NOV 13
 MEL ITEMS
28 - FUEL
28-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 28-01-01 - FUEL Overhead Panel
MINIMUM EQUIPMENT LIST

28-01-01-01 Wing TK PUMP pb-sw FAULT light

Ident.: MI-28-01-01-00008178.0001001 / 21 MAR 10
Applicable to: ALL

28-01-01-01A
Repair interval Nbr installed Nbr required Placard
C 4 0 Yes
One or more may be inoperative provided that the corresponding pump is set to OFF when
the associated tank is empty.

28-01-01-02 Wing TK PUMP pb-sw OFF light

Ident.: MI-28-01-01-00008179.0001001 / 21 MAR 10
Applicable to: ALL

28-01-01-02A
Repair interval Nbr installed Nbr required Placard
C 4 0 Yes
One or more may be inoperative provided that the corresponding pump indication is
operative on the FUEL SD page.

28-01-01-03 X FEED pb-sw ON light

Ident.: MI-28-01-01-00008180.0001001 / 21 MAR 10
Applicable to: ALL

28-01-01-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that the X FEED indication is operative on the FUEL SD page.

LAN COLOMBIA FLEET MI-28-01-01 P 1/4

MEL A to C 10 OCT 14
 MEL ITEMS
28 - FUEL
28-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 28-01-01 - FUEL Overhead Panel
MINIMUM EQUIPMENT LIST

28-01-01-04 X FEED pb-sw OPEN light

Ident.: MI-28-01-01-00008181.0001001 / 21 MAR 10
Applicable to: ALL

28-01-01-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that the X FEED indication is operative on the FUEL SD page.

28-01-01-05 CTR TK PUMP pb-sw FAULT light

Ident.: MI-28-01-01-00008182.0002001 / 10 OCT 14
Applicable to: ALL

28-01-01-05A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative provided that the corresponding pump is set to OFF when
there is no fuel in the center tank.

28-01-01-06 CTR TK PUMP pb-sw OFF light

Ident.: MI-28-01-01-00008183.0002001 / 10 OCT 14
Applicable to: ALL

28-01-01-06A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative provided that the corresponding pump indication is
operative on the FUEL SD page.

LAN COLOMBIA FLEET MI-28-01-01 P 2/4

MEL D to F 10 OCT 14
 MEL ITEMS
28 - FUEL
28-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 28-01-01 - FUEL Overhead Panel
MINIMUM EQUIPMENT LIST

28-01-01-07 FUEL MODE SEL pb-sw FAULT light

Ident.: MI-28-01-01-00008184.0003001 / 10 OCT 14
Applicable to: ALL

28-01-01-07A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that all tank pumps indications are operative on the FUEL SD
page .
Reference(s)
(o) Refer to OpsProc 28-01-01-07A FUEL MODE SEL pb-sw FAULT light

LAN COLOMBIA FLEET MI-28-01-01 P 3/4

MEL G 10 OCT 14
 MEL ITEMS
28 - FUEL
28-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 28-01-01 - FUEL Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-28-01-01 P 4/4

MEL 10 OCT 14
 MEL ITEMS
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-01 - Fuel Quantity Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

28-07-01-01 Fuel On Board (FOB) Indication on the FUEL SD page

Ident.: MI-28-07-01-00008270.0001001 / 21 MAR 10
Applicable to: ALL

28-07-01-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 28-07-01-01A Fuel On Board (FOB) Indication on the FUEL SD page

28-07-01-02 Fuel Quantity Indication (FQI) in Degraded Mode on the FUEL SD page
Ident.: MI-28-07-01-00008271.0001001 / 12 SEP 11
Applicable to: ALL

28-07-01-02A
Repair interval Nbr installed Nbr required Placard
D 5 0 No
(o) One or more FQI may be in the degraded mode (with dashes on the two last digits)
provided that the loss of accuracy is taken into account for the fuel planning for each
affected tank.
Note: The Fuel On Board indication is also in the degraded mode.
Reference(s)
(o) Refer to OpsProc 28-07-01-02A Fuel Quantity Indication in Degraded Mode on the FUEL
SD page

LAN COLOMBIA FLEET MI-28-07-01 P 1/6

MEL A to B 10 OCT 14
 MEL ITEMS
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-01 - Fuel Quantity Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

28-07-01-03 Outer Tank Fuel Quantity Indication on the FUEL SD page

Ident.: MI-28-07-01-00008272.0001001 / 10 OCT 14
Applicable to: ALL

28-07-01-03A Check of fuel quantity in the associated tank after refueling

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) (m) One may be inoperative provided that:
1) The fuel quantity in the associated tank is checked after each refueling by the manual
magnetic indicators or by the corresponding fuel quantity indicator on refuel/defuel
control panel, and
2) The associated fuel used indication is operative, and
3) The associated inner tank indication is operative.
Reference(s)
(o) Refer to OpsProc 28-07-01-03A Outer Tank Fuel Quantity Indication on the FUEL SD page
(m) Refer to AMM 28-40-00-040-003

28-07-01-03B High level fuel detection system checked operative before refueling and
associated inner tank indication operative
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(m) One may be inoperative provided that:
1) The high level fuel detection system is checked operative before refueling, and
2) The tanks in both wings are full, and
3) The associated fuel used indication is operative, and
4) The associated inner tank indication is operative.
Reference(s)
(m) Refer to AMM 28-40-00-040-003
Continued on the following page

LAN COLOMBIA FLEET MI-28-07-01 P 2/6

MEL C 10 OCT 14
 MEL ITEMS
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-01 - Fuel Quantity Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

Continued from the previous page

28-07-01-03C Check of fuel quantity in the associated wing after refueling/defueling
Repair interval Nbr installed Nbr required Placard
B 2 1 No
(o) (m) One may be inoperative provided that:
1) The fuel quantity in the associated wing (inner and outer tanks) is checked after each
refueling/defueling by the manual magnetic indicators or by the corresponding fuel
quantity indicator on the refuel/defuel control panel, and
2) The associated fuel used indication is operative.
Reference(s)
(o) Refer to OpsProc 28-07-01-03C Outer Tank Fuel Quantity Indication on the FUEL SD page
(m) Refer to AMM 28-40-00-040-003

28-07-01-03D High level fuel detection system checked operative before refueling
Repair interval Nbr installed Nbr required Placard
B 2 1 No
(m) One may be inoperative provided that:
1) The high level fuel detection system is checked operative before refueling, and
2) The tanks in both wings are full, and
3) The associated fuel used indication is operative.
Reference(s)
(m) Refer to AMM 28-40-00-040-003

LAN COLOMBIA FLEET MI-28-07-01 P 3/6

MEL C 10 OCT 14
 MEL ITEMS
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-01 - Fuel Quantity Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

28-07-01-04 Inner Tank Fuel Quantity Indication on the FUEL SD page

Ident.: MI-28-07-01-00008273.0001001 / 10 OCT 14
Applicable to: ALL

28-07-01-04A Check of fuel quantity in the associated tank after refueling

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) (m) One may be inoperative provided that:
1) The fuel quantity in the associated tank is checked after each refueling by the manual
magnetic indicators or by the corresponding fuel quantity indicator on the refuel/defuel
control panel, and
2) The associated fuel used indication is operative.
Reference(s)
(o) Refer to OpsProc 28-07-01-04A Inner/Wing Tank Fuel Quantity Indication on the FUEL SD
page
(m) Refer to AMM 28-40-00-040-005

28-07-01-04B High level fuel detection system checked operative before refueling
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(m) One may be inoperative provided that:
1) The high level fuel detection system is checked operative before refueling, and
2) The tanks in both wings are full, and
3) The associated fuel used indication is operative.
Reference(s)
(m) Refer to AMM 28-40-00-040-005

LAN COLOMBIA FLEET MI-28-07-01 P 4/6

MEL D 10 OCT 14
 MEL ITEMS
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-01 - Fuel Quantity Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

28-07-01-05 Center Tank Fuel Quantity Indication on the FUEL SD page

Ident.: MI-28-07-01-00008274.0002001 / 12 SEP 11
Applicable to: ALL

28-07-01-05A Check of fuel quantity after refueling

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that:
1) The fuel quantity in the center tank is checked after each refueling by the manual
magnetic indicators or by the corresponding fuel quantity indicator on the refuel/defuel
control panel, and
2) All wing tanks fuel quantity indications are operative, and
3) Both fuel used indications are operative.
Reference(s)
(o) Refer to OpsProc 28-07-01-05A Center Tank Fuel Quantity Indication on the FUEL SD page
(m) Refer to AMM 28-40-00-040-006

28-07-01-05B Fuel in the center tank not usable

Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that there is no fuel in the center tank or the fuel in this tank
is considered as not usable and as part of the ZFW and is taken into account for CG
determination.

LAN COLOMBIA FLEET MI-28-07-01 P 5/6

MEL E 10 OCT 14
 MEL ITEMS
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-01 - Fuel Quantity Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-28-07-01 P 6/6

MEL 10 OCT 14
 MEL ITEMS
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-02 - Fuel Temperature Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

28-07-02-01 Fuel Temperature Indication on the FUEL SD page

Ident.: MI-28-07-02-00008276.0001001 / 10 OCT 14
Applicable to: ALL

28-07-02-01A
Repair interval Nbr installed Nbr required Placard
C 4 2 No
One in each wing or both in one wing may be inoperative.

LAN COLOMBIA FLEET MI-28-07-02 P 1/2

MEL A 10 OCT 14
 MEL ITEMS
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-02 - Fuel Temperature Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-28-07-02 P 2/2

MEL 10 OCT 14
 MEL ITEMS
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-03 - Tank Pump Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

28-07-03-01 Wing Tank Pump Indication on the FUEL SD page

Ident.: MI-28-07-03-00008277.0001001 / 21 MAR 10
Applicable to: ALL

28-07-03-01A
Repair interval Nbr installed Nbr required Placard
C 4 0 No
One or more may be inoperative.

28-07-03-02 Center Tank Pump Indication on the FUEL SD page

Ident.: MI-28-07-03-00008278.0003001 / 10 OCT 14
Applicable to: ALL

28-07-03-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

LAN COLOMBIA FLEET MI-28-07-03 P 1/2

MEL A to B 10 OCT 14
 MEL ITEMS
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-03 - Tank Pump Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-28-07-03 P 2/2

MEL 10 OCT 14
 MEL ITEMS
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-04 - Valve Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

28-07-04-01 Engine LP Fuel Valve Indication on the FUEL SD page

Ident.: MI-28-07-04-00008279.0001001 / 01 AUG 13
Applicable to: ALL

28-07-04-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(m) One or both may be inoperative provided that the associated LP valve is checked operative
before each flight.
Reference(s)
(m) Refer to AMM 28-40-00-040-009

28-07-04-02 APU LP Fuel Valve Indication on the FUEL SD page

Ident.: MI-28-07-04-00008280.0001001 / 21 MAR 10
Applicable to: ALL

28-07-04-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that:
1) The APU LP valve is secured in the closed position and,
2) The APU is not used.
Reference(s)
(m) Refer to AMM 28-40-00-040-001

LAN COLOMBIA FLEET MI-28-07-04 P 1/2

MEL A to B 10 OCT 14
 MEL ITEMS
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-04 - Valve Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

28-07-04-03 Crossfeed Valve Indication on the FUEL SD page

Ident.: MI-28-07-04-00008281.0001001 / 01 AUG 13
Applicable to: ALL

28-07-04-03A Non ETOPS flight

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(m) May be inoperative provided that:
1) ETOPS is not conducted, and
2) Operation of the crossfeed valve is checked before the first flight of each day.
Reference(s)
(m) Refer to AMM 28-40-00-040-002

28-07-04-04 Wing Transfer Valve Indication on the FUEL SD page

Ident.: MI-28-07-04-00008282.0001001 / 10 OCT 14
Applicable to: ALL

28-07-04-04A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) (m) One or both may be inoperative provided that:
1) The fuel quantity indications of the associated inner and outer tanks are operative, and
2) The transfer valve operation is checked before each flight and when used in flight.
Reference(s)
(o) Refer to OpsProc 28-07-04-04A Wing Transfer Valve Indication on the FUEL SD page
(m) Refer to AMM 28-40-00-040-004

LAN COLOMBIA FLEET MI-28-07-04 P 2/2

MEL C to D 10 OCT 14
 MEL ITEMS
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-05 - Fuel Flow Indication on the FUEL SD page
MINIMUM EQUIPMENT LIST

28-07-05-01 Fuel Flow 1+2 Indication on the FUEL SD page

Ident.: MI-28-07-05-00015815.0001001 / 27 FEB 15
Applicable to: ALL

28-07-05-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-28-07-05 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-05 - Fuel Flow Indication on the FUEL SD page
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-28-07-05 P 2/2

MEL 27 FEB 15
 MEL ITEMS
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-06 - Fuel Used Indication on the FUEL SD page
MINIMUM EQUIPMENT LIST

28-07-06-01 Fuel Used Indication on the FUEL SD page

Ident.: MI-28-07-06-00015816.0001001 / 27 FEB 15
Applicable to: ALL

28-07-06-01A
Repair interval Nbr installed Nbr required Placard

Refer to Item 73-07-01 Fuel Used Indication on the ENGINE SD page

28-07-06-02 Fuel Used 1+2 Indication on the FUEL SD page

Ident.: MI-28-07-06-00015817.0001001 / 27 FEB 15
Applicable to: ALL

28-07-06-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-28-07-06 P 1/2

MEL A to B 27 FEB 15
 MEL ITEMS
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-06 - Fuel Used Indication on the FUEL SD page
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-28-07-06 P 2/2

MEL 27 FEB 15
 MEL ITEMS
28 - FUEL
28-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-09-01 FUEL L(R) INNER(OUTER) TK HI TEMP Alert

Ident.: MI-28-09-00008287.0001001 / 10 OCT 14
Applicable to: ALL

28-09-01A One or two inoperative

Repair interval Nbr installed Nbr required Placard
C 4 2 No
(o) One in each wing or both in one wing may be displayed provided that:
1) The fuel temperature indications of the non affected tanks are operative on the FUEL SD
page , and
2) The fuel temperature is monitored before takeoff and during the flight.
Note: For fuel temperature limitations, Refer to AFM/LIM-28 Fuel Temperature Limits .
Reference(s)
(o) Refer to OpsProc 28-09-01A FUEL L(R) INNER(OUTER)/WING TK HI TEMP Alert

28-09-01B One or more inoperative

Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) One or more may be displayed provided that:
1) The fuel temperature indications are operative on the FUEL SD page , and
2) The fuel temperature is monitored before takeoff and during the flight.
Note: For fuel temperature limitations, Refer to AFM/LIM-28 Fuel Temperature Limits .
Reference(s)
(o) Refer to OpsProc 28-09-01B FUEL L(R) INNER(OUTER)/WING TK HI TEMP Alert

LAN COLOMBIA FLEET MI-28-09 P 1/2

MEL A 10 OCT 14
 MEL ITEMS
28 - FUEL
28-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-09-02 FUEL L(R) INNER(OUTER) TK LO TEMP Alert

Ident.: MI-28-09-00008288.0001001 / 10 OCT 14
Applicable to: ALL

28-09-02A One or two inoperative

Repair interval Nbr installed Nbr required Placard
C 4 2 No
(o) One in each wing or both in one wing may be displayed provided that:
1) The fuel temperature indications of the non affected tanks are operative on the FUEL SD
page , and
2) The fuel temperature is monitored before takeoff and during the flight.
Note: For fuel temperature limitations, Refer to AFM/LIM-28 Fuel Temperature Limits .
Reference(s)
(o) Refer to OpsProc 28-09-02A FUEL L(R) INNER(OUTER)/WING TK LO TEMP Alert

28-09-02B One or more inoperative

Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) One or more may be displayed provided that:
1) The fuel temperature indications are operative on the FUEL SD page , and
2) The fuel temperature is monitored before takeoff and during the flight.
Note: For fuel temperature limitations, Refer to AFM/LIM-28 Fuel Temperature Limits .
Reference(s)
(o) Refer to OpsProc 28-09-02B FUEL L(R) INNER(OUTER)/WING TK LO TEMP Alert

LAN COLOMBIA FLEET MI-28-09 P 2/2

MEL B 10 OCT 14
 MEL ITEMS
28 - FUEL
28-12 - Tank Venting System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-12-01 Overpressure Protector between the Inner and the Outer Tank
Ident.: MI-28-12-00008195.0001001 / 10 OCT 14
Applicable to: ALL

28-12-01A Inner tank temperature monitored

Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) One or both may be broken or missing provided that the fuel temperature of the inner tank is
monitored.
Reference(s)
(o) Refer to OpsProc 28-12-01A Overpressure Protector Between the Inner and the Outer Tank
(Inner tank fuel temperature monitored)

28-12-01B Transfer valves secured open

Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) (m) One or both may be broken or missing provided that the associated transfer valves are
secured in the open position after each refueling, or after each aircraft repowering.
Reference(s)
(o) Refer to OpsProc 28-12-01B Overpressure Protector Between the Inner and the Outer Tank
(Transfer valves opened)
(m) Refer to AMM Task 28-12-00-040-003

28-12-02 Overpressure Protector in the Vent Surge Tank

Ident.: MI-28-12-00008196.0001001 / 12 SEP 12
Applicable to: ALL

28-12-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) One or both may be broken or missing.
Continued on the following page

LAN COLOMBIA FLEET MI-28-12 P 1/2

MEL A to B 10 OCT 14
 MEL ITEMS
28 - FUEL
28-12 - Tank Venting System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 28-12-02A Overpressure Protector in the Vent Surge Tank

28-12-03 Overpressure Protector in the Inner Tank

Ident.: MI-28-12-00008197.0001001 / 10 OCT 14
Applicable to: ALL

28-12-03A
Repair interval Nbr installed Nbr required Placard
2 2 No
Both must be operative.

28-12-04 Overpressure Protector between the Center and the Inner Tank
Ident.: MI-28-12-00008198.0002001 / 10 OCT 14
Applicable to: ALL

28-12-04A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

LAN COLOMBIA FLEET MI-28-12 P 2/2

MEL B to D 10 OCT 14
 MEL ITEMS
28 - FUEL
28-15 - Intercell Transfer System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-15-01 LH Wing Transfer Valve

Ident.: MI-28-15-00008201.0001001 / 10 OCT 14
Applicable to: ALL

28-15-01A One or both inoperative open

Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) One or both may be inoperative in the open position.
Reference(s)
(o) Refer to OpsProc 28-15-01A LH Wing Transfer Valve (At least one transfer valve open)

28-15-01B One or both inoperative with not usable fuel

Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) One or both may be inoperative in the closed position provided that the fuel in the LH outer
tank is considered as not usable and as part of the ZFW .
Reference(s)
(o) Refer to OpsProc 28-15-01B LH Wing Transfer Valve (At least one transfer valve failed
closed)

28-15-01C One inoperative closed

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) (m) One may be inoperative in the closed position provided that the remaining LH wing transfer
valve is secured in the open position after each refueling, or after each aircraft repowering.
Reference(s)
(o) Refer to OpsProc 28-15-01C LH Wing Transfer Valve (At least one transfer valve open)
(m) Refer to AMM 28-15-00-040-001

LAN COLOMBIA FLEET MI-28-15 P 1/2

MEL A 10 OCT 14
 MEL ITEMS
28 - FUEL
28-15 - Intercell Transfer System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-15-02 RH Wing Transfer Valve

Ident.: MI-28-15-00008202.0001001 / 10 OCT 14
Applicable to: ALL

28-15-02A One or both inoperative open

Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) One or both may be inoperative in the open position.
Reference(s)
(o) Refer to OpsProc 28-15-02A RH Wing Transfer Valve (At least one transfer valve open)

28-15-02B One or both inoperative with not usable fuel

Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) One or both may be inoperative in the closed position provided that the fuel in the RH outer
tank is considered as not usable and as part of the ZFW .
Reference(s)
(o) Refer to OpsProc 28-15-02B RH Wing Transfer Valve (At least one transfer valve failed
closed)

28-15-02C One inoperative closed

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) (m) One may be inoperative in the closed position provided that the remaining RH wing transfer
valve is secured in the open position after each refueling, or after each aircraft repowering.
Reference(s)
(o) Refer to OpsProc 28-15-02C RH Wing Transfer Valve (At least one transfer valve open)
(m) Refer to AMM 28-15-00-040-002

LAN COLOMBIA FLEET MI-28-15 P 2/2

MEL B 10 OCT 14
 MEL ITEMS
28 - FUEL
28-20 - Distribution
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-20-01 Automatic Fuel Feed System

Ident.: MI-28-20-00008203.0006001 / 10 OCT 14
Applicable to: ALL

28-20-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 28-20-01A Automatic Fuel Feed System

LAN COLOMBIA FLEET MI-28-20 P 1/2

MEL A 10 OCT 14
 MEL ITEMS
28 - FUEL
28-20 - Distribution
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-28-20 P 2/2

MEL 10 OCT 14
 MEL ITEMS
28 - FUEL
28-21 - Main Fuel Pump System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-21-01 Wing Tank Pump

Ident.: MI-28-21-00008204.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

28-21-01A JP4/JET B not used

Repair interval Nbr installed Nbr required Placard
C 4 3 Yes
One pump may be inoperative provided that JP4/JET B is not used.

28-21-01B Use of JP4/JET B

Repair interval Nbr installed Nbr required Placard
C 4 3 Yes
(m) Pump 2 LH or pump 2 RH may be inoperative when JP4/JET B is used provided that:
1) The fuel return valve is checked operative before each flight, and
2) The fuel temperature is less than 30 C.
Reference(s)
(m) Refer to AMM 28-21-00-040-001

28-21-01 Wing Tank Pump

Ident.: MI-28-21-00008204.0002001 / 10 OCT 14
Applicable to: MSN 4516-4546

28-21-01A JP4/JET B not used

Repair interval Nbr installed Nbr required Placard
C 4 3 Yes
One pump may be inoperative provided that JP4/JET B is not used.
Continued on the following page

LAN COLOMBIA FLEET MI-28-21 P 1/4

MEL A 27 FEB 15
 MEL ITEMS
28 - FUEL
28-21 - Main Fuel Pump System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

28-21-01B Use of JP4/JET B
Repair interval Nbr installed Nbr required Placard
C 4 3 Yes
Pump 2 LH or pump 2 RH may be inoperative when JP4/JET B is used provided that the
fuel temperature is less than 30 C.

28-21-02 Center Tank Pump

Ident.: MI-28-21-00008205.0006001 / 10 OCT 14
Applicable to: ALL

28-21-02A One inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(o) One may be inoperative provided that the flight routes permit a landing at a suitable airport if
the remaining center tank pump fails with fuel in the center tank.
Reference(s)
(o) Refer to OpsProc 28-21-02A Center Tank Pump (One inoperative)

28-21-02D Both inoperative

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(o) Both may be inoperative provided that:
1) There is no fuel in the center tank or the fuel in the center tank is considered as not
usable and as part of the ZFW and is taken into account for CG determination, and
2) The center tank pumps are set to OFF.
Reference(s)
(o) Refer to OpsProc 28-21-02D Center Tank Pump (Both inoperative)

LAN COLOMBIA FLEET MI-28-21 P 2/4

MEL A to B 27 FEB 15
 MEL ITEMS
28 - FUEL
28-21 - Main Fuel Pump System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-21-03 Wing Tank Pump Sequence Valve

Ident.: MI-28-21-00008206.0003001 / 10 OCT 14
Applicable to: ALL

28-21-03A
Repair interval Nbr installed Nbr required Placard
C 4 3 No
One may be inoperative provided that the associated pump is set to OFF when the center
tank is feeding.

LAN COLOMBIA FLEET MI-28-21 P 3/4

MEL C 27 FEB 15
 MEL ITEMS
28 - FUEL
28-21 - Main Fuel Pump System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-28-21 P 4/4

MEL 27 FEB 15
 MEL ITEMS
28 - FUEL
28-22 - APU Fuel Pump System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-22-01 APU Fuel Pump

Ident.: MI-28-22-00008207.0002001 / 10 OCT 14
Applicable to: ALL

28-22-01A Non ETOPS flight

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that ETOPS is not conducted.
Reference(s)
(o) Refer to OpsProc 28-22-01A APU Fuel Pump

28-22-01B ETOPS 120 min flight

Repair interval Nbr installed Nbr required Placard
A 1 0 Yes
(o) May be inoperative for four flights provided that ETOPS beyond 120 min is not conducted.
Reference(s)
(o) Refer to OpsProc 28-22-01B APU Fuel Pump

LAN COLOMBIA FLEET MI-28-22 P 1/2

MEL A 10 OCT 14
 MEL ITEMS
28 - FUEL
28-22 - APU Fuel Pump System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-28-22 P 2/2

MEL 10 OCT 14
 MEL ITEMS
28 - FUEL
28-23 - Crossfeed System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-23-01 Crossfeed Valve

Ident.: MI-28-23-00008208.0001001 / 21 MAR 10
Applicable to: ALL

28-23-01A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

LAN COLOMBIA FLEET MI-28-23 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
28 - FUEL
28-23 - Crossfeed System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-28-23 P 2/2

MEL 05 NOV 13
 MEL ITEMS
28 - FUEL
28-24 - Engine LP Fuel Shutoff
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-24-01 Engine LP Fuel Valve Electrical Motor

Ident.: MI-28-24-00008209.0002001 / 21 MAR 10
Applicable to: ALL

28-24-01A
Repair interval Nbr installed Nbr required Placard
C 4 3 No
(m) One may be inoperative on one engine provided that:
1) The affected motor is deactivated, and
2) The remaining motor is checked operative.
Reference(s)
(m) Refer to AMM 28-24-00-040-002

LAN COLOMBIA FLEET MI-28-24 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
28 - FUEL
28-24 - Engine LP Fuel Shutoff
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-28-24 P 2/2

MEL 05 NOV 13
 MEL ITEMS
28 - FUEL
28-25 - Refuel/Defuel System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-25-01 Fuel Quantity Preselector

Ident.: MI-28-25-00008210.0001001 / 04 AUG 11
Applicable to: ALL

28-25-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

28-25-02 Fuel Quantity on the Refuel/Defuel Control Panel

Ident.: MI-28-25-00008211.0001001 / 25 MAY 11
Applicable to: ALL

28-25-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the fuel quantity is continuously monitored on the FUEL
SD page during refueling and defueling.

28-25-03 Refuel Valve

Ident.: MI-28-25-00008212.0003001 / 27 FEB 15
Applicable to: ALL

28-25-03A Manual refueling

Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
(m) One or more may be inoperative provided that the aircraft is manually refueled.
Reference(s)
(m) Refer to AMM 28-25-00-040-005

LAN COLOMBIA FLEET MI-28-25 P 1/2

MEL A to C 27 FEB 15
 MEL ITEMS
28 - FUEL
28-25 - Refuel/Defuel System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-25-04 Transfer Defuel Valve

Ident.: MI-28-25-00008213.0001001 / 21 MAR 10
Applicable to: ALL

28-25-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that the valve is secured in the closed position.
Reference(s)
(m) Refer to AMM 28-25-00-040-004

28-25-05 Exterior Refuel/Defuel Control Panel

Ident.: MI-28-25-00008214.0001001 / 05 APR 12
Applicable to: ALL

28-25-05A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that the aircraft is manually refueled.
Reference(s)
(m) Refer to AMM 28-25-00-040-008

LAN COLOMBIA FLEET MI-28-25 P 2/2

MEL D to E 27 FEB 15
 MEL ITEMS
28 - FUEL
28-29 - APU LP Fuel Shutoff
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-29-01 APU LP Fuel Valve

Ident.: MI-28-29-00008232.0001001 / 12 SEP 11
Applicable to: ALL

28-29-01A Checked closed on FUEL SD page

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that:
1) It is checked closed on the FUEL SD page , and
2) The APU is not used.
Reference(s)
(o) Refer to OpsProc 28-29-01A APU LP Fuel Valve

28-29-01B Secured closed

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that:
1) It is secured in the closed position, and
2) The APU is not used.
Reference(s)
(m) Refer to AMM 28-29-00-040-002

LAN COLOMBIA FLEET MI-28-29 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
28 - FUEL
28-29 - APU LP Fuel Shutoff
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-28-29 P 2/2

MEL 05 NOV 13
 MEL ITEMS
28 - FUEL
28-43 - Manual Magnetic Indicators
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-43-01 Manual Magnetic Indicators

Ident.: MI-28-43-00008233.0007001 / 10 OCT 14
Applicable to: ALL

28-43-01A Associated fuel quantity indication operative on the FUEL SD page

Repair interval Nbr installed Nbr required Placard
C 9 0 No
One or more may be inoperative provided that the associated fuel quantity indication is
operative on the FUEL SD page.

28-43-01B High level fuel detection and fuel used indication operative
Repair interval Nbr installed Nbr required Placard
C 9 0 No
(m) One or more may be inoperative provided that:
1) The high level fuel detection system is checked operative before refueling, and
2) The tanks in both wings are full, and
3) The associated fuel used indication is operative.
Reference(s)
(m) Refer to AMM 28-40-00-040-012

LAN COLOMBIA FLEET MI-28-43 P 1/2

MEL A 10 OCT 14
 MEL ITEMS
28 - FUEL
28-43 - Manual Magnetic Indicators
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-28-43 P 2/2

MEL 10 OCT 14
 MEL ITEMS
28 - FUEL
28-46 - Tank Level Sensing
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-46-01 High Level Detection System in the Inner Tank

Ident.: MI-28-46-00008235.0001001 / 10 OCT 14
Applicable to: ALL

28-46-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative provided that the fuel quantity is continuously monitored
during refueling.

28-46-02 High Level Detection System in the Center Tank

Ident.: MI-28-46-00008237.0002001 / 21 MAR 10
Applicable to: ALL

28-46-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the fuel quantity is continuously monitored during
refueling.

28-46-04 Low Level Detection System in the Inner Tank

Ident.: MI-28-46-00008240.0001001 / 10 OCT 14
Applicable to: ALL

28-46-04A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative.

LAN COLOMBIA FLEET MI-28-46 P 1/2

MEL A to C 10 OCT 14
 MEL ITEMS
28 - FUEL
28-46 - Tank Level Sensing
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-28-46 P 2/2

MEL 10 OCT 14
 MEL ITEMS
28 - FUEL
28-50 - Fuel Management
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-50-01 Fuel Quantity Indicating Computer ( FQIC ) Channel

Ident.: MI-28-50-00008242.0001001 / 21 MAR 10
Applicable to: ALL

28-50-01A
Repair interval Nbr installed Nbr required Placard
A 2 1 No
(o) One may be inoperative for 10 calendar days provided that ETOPS is not conducted.
Reference(s)
(o) Refer to OpsProc 28-50-01A Fuel Quantity Indicating Computer (FQIC) Channel

LAN COLOMBIA FLEET MI-28-50 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
28 - FUEL
28-50 - Fuel Management
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-28-50 P 2/2

MEL 05 NOV 13
 MEL ITEMS
29 - HYDRAULIC POWER
29-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 29-01-01 - HYD Overhead Panel
MINIMUM EQUIPMENT LIST

29-01-01-01 B(Y) ELEC PUMP pb-sw FAULT light

Ident.: MI-29-01-01-00008031.0001001 / 27 FEB 15
Applicable to: ALL

29-01-01-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative provided that the associated reservoir quantity indication is
operative on the HYD SD page .
Note: Simultaneous illumination of the BLUE ELEC PUMP pb-sw FAULT light and the
ENG 1(2) PUMP pb-sw FAULT light with engines off may be due to a failed engine
oil low pressure switch. In this case, the ENG 1(2) OIL LO PR alert is inoperative.
Refer to Item 79-09-01 ENG 1(2) OIL LO PR Alert

29-01-01-02 B ELEC PUMP pb-sw OFF light

Ident.: MI-29-01-01-00008034.0001001 / 21 MAR 10
Applicable to: ALL

29-01-01-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

29-01-01-03 Y ELEC PUMP pb-sw ON light

Ident.: MI-29-01-01-00008042.0001001 / 21 MAR 10
Applicable to: ALL

29-01-01-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-29-01-01 P 1/4

MEL A to C 27 FEB 15
 MEL ITEMS
29 - HYDRAULIC POWER
29-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 29-01-01 - HYD Overhead Panel
MINIMUM EQUIPMENT LIST

29-01-01-04 G(Y) ENG 1(2) PUMP pb-sw FAULT light

Ident.: MI-29-01-01-00008048.0001001 / 27 FEB 15
Applicable to: ALL

29-01-01-04A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative provided that the associated reservoir quantity indication is
operative on the HYD SD page .
Note: Simultaneous illumination of the BLUE ELEC PUMP pb-sw FAULT light and the
ENG 1(2) PUMP pb-sw FAULT light with engines off may be due to a failed engine
oil low pressure switch. In this case, the ENG 1(2) OIL LO PR alert is inoperative.
Refer to Item 79-09-01 ENG 1(2) OIL LO PR Alert

29-01-01-05 G(Y) ENG 1(2) PUMP pb-sw OFF light

Ident.: MI-29-01-01-00008049.0001001 / 21 MAR 10
Applicable to: ALL

29-01-01-05A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

29-01-01-06 PTU pb-sw FAULT light

Ident.: MI-29-01-01-00008050.0001001 / 21 MAR 10
Applicable to: ALL

29-01-01-06A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the quantity indications of the yellow and green reservoir
are operative on the HYD SD page.

LAN COLOMBIA FLEET MI-29-01-01 P 2/4

MEL D to F 27 FEB 15
 MEL ITEMS
29 - HYDRAULIC POWER
29-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 29-01-01 - HYD Overhead Panel
MINIMUM EQUIPMENT LIST

29-01-01-07 PTU pb-sw OFF light

Ident.: MI-29-01-01-00008051.0001001 / 21 MAR 10
Applicable to: ALL

29-01-01-07A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-29-01-01 P 3/4

MEL G 27 FEB 15
 MEL ITEMS
29 - HYDRAULIC POWER
29-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 29-01-01 - HYD Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-29-01-01 P 4/4

MEL 27 FEB 15
 MEL ITEMS
29 - HYDRAULIC POWER
29-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 29-01-02 - Maintenance HYD Overhead Panel
MINIMUM EQUIPMENT LIST

29-01-02-01 G(B)(Y) LEAK MEASUREMENT VALVES pb-sw OFF light

Ident.: MI-29-01-02-00008052.0001001 / 21 MAR 10
Applicable to: ALL

29-01-02-01A
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative.

LAN COLOMBIA FLEET MI-29-01-02 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
29 - HYDRAULIC POWER
29-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 29-01-02 - Maintenance HYD Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-29-01-02 P 2/2

MEL 05 NOV 13
 MEL ITEMS
29 - HYDRAULIC POWER
29-07 - Indications on the HYD SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-07-01 Yellow ELEC Pump Indication on the HYD SD page

Ident.: MI-29-07-00008078.0001001 / 21 MAR 10
Applicable to: ALL

29-07-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.

29-07-02 Pump Indication on the HYD SD page

Ident.: MI-29-07-00008079.0001001 / 26 JUN 11
Applicable to: ALL

29-07-02A
Repair interval Nbr installed Nbr required Placard
C 3 0 No
One or more may be inoperative.

29-07-03 Fire Valve Indication on the HYD SD page

Ident.: MI-29-07-00008080.0001001 / 21 MAR 10
Applicable to: ALL

29-07-03A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

LAN COLOMBIA FLEET MI-29-07 P 1/4

MEL A to C 05 NOV 13
 MEL ITEMS
29 - HYDRAULIC POWER
29-07 - Indications on the HYD SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-07-04 PTU Indication on the HYD SD page

Ident.: MI-29-07-00008081.0001001 / 21 MAR 10
Applicable to: ALL

29-07-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.

29-07-05 Reservoir Quantity Indication on the HYD SD page

Ident.: MI-29-07-00008082.0001001 / 21 MAR 10
Applicable to: ALL

29-07-05A
Repair interval Nbr installed Nbr required Placard
C 3 2 No
(m) One may be inoperative provided that:
1) The associated HYD B(G)(Y) RSVR LO LVL alert is checked operative, and
2) The associated reservoir quantity is checked before each flight.
Reference(s)
(m) Refer to AMM

29-07-06 RAT Indication on the HYD SD page

Ident.: MI-29-07-00008083.0001001 / 21 MAR 10
Applicable to: ALL

29-07-06A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that the RAT is visually checked to be stowed before each
flight.

LAN COLOMBIA FLEET MI-29-07 P 2/4

MEL D to F 05 NOV 13
 MEL ITEMS
29 - HYDRAULIC POWER
29-07 - Indications on the HYD SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-07-07 System Label Indication on the HYD SD page

Ident.: MI-29-07-00008084.0001001 / 21 MAR 10
Applicable to: ALL

29-07-07A
Repair interval Nbr installed Nbr required Placard
C 3 0 No
(o) One or more may be inoperative provided that the associated system pressure is checked
available before each flight.
Reference(s)
(o) Refer to OpsProc 29-07-07A System Label Indication on the HYD SD page

29-07-08 System Pressure Indication on the HYD SD page

Ident.: MI-29-07-00008085.0001001 / 21 MAR 10
Applicable to: ALL

29-07-08A
Repair interval Nbr installed Nbr required Placard
C 3 2 No
(o) One may be inoperative provided that the associated system label indication is checked
operative before each flight.
Reference(s)
(o) Refer to OpsProc 29-07-08A System Pressure Indication on the HYD SD page

LAN COLOMBIA FLEET MI-29-07 P 3/4

MEL G to H 05 NOV 13
 MEL ITEMS
29 - HYDRAULIC POWER
29-07 - Indications on the HYD SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-29-07 P 4/4

MEL 05 NOV 13
 MEL ITEMS
29 - HYDRAULIC POWER
29-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-09-01 HYD B(Y) ELEC PUMP LO PR Alert

Ident.: MI-29-09-00008086.0001001 / 21 MAR 10
Applicable to: ALL

29-09-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be displayed provided that the associated system pressure indication is
operative.

29-09-02 HYD B(Y) ELEC PUMP OVHT Alert

Ident.: MI-29-09-00008087.0001001 / 21 MAR 10
Applicable to: ALL

29-09-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be displayed.

29-09-03 HYD G(Y) ENG 1(2) PUMP LO PR Alert

Ident.: MI-29-09-00008088.0001001 / 21 MAR 10
Applicable to: ALL

29-09-03A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) One or both may be displayed provided that:
1) The associated system pressure indications are operative, and
2) The engine pumps are checked operative before each flight.
Reference(s)
(o) Refer to OpsProc 29-09-03A HYD G(Y) ENG 1(2) PUMP LO PR Alert

LAN COLOMBIA FLEET MI-29-09 P 1/4

MEL A to C 05 NOV 13
 MEL ITEMS
29 - HYDRAULIC POWER
29-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-09-04 HYD G(B)(Y) RSVR LO AIR PR Alert

Ident.: MI-29-09-00008090.0001001 / 21 MAR 10
Applicable to: ALL

29-09-04A
Repair interval Nbr installed Nbr required Placard
C 3 2 No
(m) One may be inoperative provided that the air pressure is checked on the associated
reservoir before each flight.
Reference(s)
(m) Refer to AMM

29-09-05 HYD G(B)(Y) RSVR LO LVL Alert

Ident.: MI-29-09-00008091.0001001 / 21 MAR 10
Applicable to: ALL

29-09-05A
Repair interval Nbr installed Nbr required Placard
C 3 2 No
One may be displayed provided that the associated reservoir quantity is checked on the
HYD SD page before each flight.
Note: 1. When the alert is displayed on the EWD , the associated PUMP pb-sw FAULT
light and the PTU pb-sw FAULT light (if the green or the yellow system is
affected) may simultaneously come on.
Refer to Item 29-01-01-01 B(Y) ELEC PUMP pb-sw FAULT light , and
Refer to Item 29-01-01-04 G(Y) ENG 1(2) PUMP pb-sw FAULT light , and
Refer to Item 29-01-01-06 PTU pb-sw FAULT light
2. If the blue reservoir is affected, EMER GEN may appear in the INOP SYS
column on the STATUS SD page before engine start.

LAN COLOMBIA FLEET MI-29-09 P 2/4

MEL D to E 05 NOV 13
 MEL ITEMS
29 - HYDRAULIC POWER
29-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-09-06 HYD G(B)(Y) RSVR OVHT Alert

Ident.: MI-29-09-00008092.0001001 / 21 MAR 10
Applicable to: ALL

29-09-06A
Repair interval Nbr installed Nbr required Placard
C 3 2 No
The HYD G RSVR OVHT alert or the HYD Y RSVR OVHT alert may be displayed.

29-09-07 HYD PTU FAULT Alert

Ident.: MI-29-09-00008093.0001001 / 21 MAR 10
Applicable to: ALL

29-09-07A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be displayed provided that the PTU is checked operative before each flight.
Reference(s)
(o) Refer to OpsProc 29-09-07A HYD PTU FAULT Alert

29-09-08 HYD RAT FAULT Alert

Ident.: MI-29-09-00008094.0001001 / 12 SEP 11
Applicable to: ALL

29-09-08A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(m) May be displayed provided that the RAT integrity is checked before each flight.
Reference(s)
(m) Refer to AMM 29-30-00-040-001

LAN COLOMBIA FLEET MI-29-09 P 3/4

MEL F to H 05 NOV 13
 MEL ITEMS
29 - HYDRAULIC POWER
29-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-09-09 HYD G(B)(Y)(B+G)(G+Y)(B+Y) SYS LO PR Alert

Ident.: MI-29-09-00008095.0001001 / 21 MAR 10
Applicable to: ALL

29-09-09A
Repair interval Nbr installed Nbr required Placard
C 3 0 No
(o) One or more may be displayed provided that the associated system pressure is checked
available before each flight.
Reference(s)
(o) Refer to OpsProc 29-09-09A HYD G(B)(Y)(B+G)(G+Y)(B+Y) SYS LO PR Alert

LAN COLOMBIA FLEET MI-29-09 P 4/4

MEL I 05 NOV 13
 MEL ITEMS
29 - HYDRAULIC POWER
29-10 - Main Hydraulic Power
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-10-01 Engine Driven Pump

Ident.: MI-29-10-00008055.0001001 / 21 MAR 10
Applicable to: ALL

29-10-01A
Repair interval Nbr installed Nbr required Placard
2 2 No
Both must be operative.

29-10-02 Engine Driven Pump Depressurization Function

Ident.: MI-29-10-00010628.0001001 / 21 MAR 10
Applicable to: ALL

29-10-02A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative.

29-10-03 Blue System Electric Pump

Ident.: MI-29-10-00008057.0001001 / 21 MAR 10
Applicable to: ALL

29-10-03A
Repair interval Nbr installed Nbr required Placard
C 1 1 No
(o) The automatic control may be inoperative provided that the pump is manually operated.
Reference(s)
(o) Refer to OpsProc 29-10-03A Blue System Electric Pump

LAN COLOMBIA FLEET MI-29-10 P 1/4

MEL A to C 27 FEB 15
 MEL ITEMS
29 - HYDRAULIC POWER
29-10 - Main Hydraulic Power
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-10-04 Hydraulic System Accumulator

Ident.: MI-29-10-00008061.0002001 / 27 FEB 15
Applicable to: ALL

29-10-04A
Repair interval Nbr installed Nbr required Placard
C 3 0 No
(m) One or more may be inoperative provided that the affected accumulator is deactivated.
Reference(s)
(m) Refer to AMM Task

29-10-05 Yellow Brake Accumulator

Ident.: MI-29-10-00008063.0001001 / 21 MAR 10
Applicable to: ALL

29-10-05A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

29-10-07 Engine Pump Fire Valve

Ident.: MI-29-10-00008067.0001001 / 21 MAR 10
Applicable to: ALL

29-10-07A
Repair interval Nbr installed Nbr required Placard
2 2 No
Both must be operative.

LAN COLOMBIA FLEET MI-29-10 P 2/4

MEL D to F 27 FEB 15
 MEL ITEMS
29 - HYDRAULIC POWER
29-10 - Main Hydraulic Power
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-10-08 Hydraulic System Filter

Ident.: MI-29-10-00008069.0001001 / 12 SEP 11
Applicable to: ALL

29-10-08A One LP filter inoperative

Repair interval Nbr installed Nbr required Placard
C 8 7 No
One LP filter may be inoperative.

29-10-08B Reservoir filling filter inoperative

Repair interval Nbr installed Nbr required Placard
C 8 7 No
The reservoir filling filter may be inoperative.

29-10-09 Hydraulic Case Drain Filter

Ident.: MI-29-10-00008072.0001001 / 21 MAR 10
Applicable to: ALL

29-10-09A
Repair interval Nbr installed Nbr required Placard
C 3 2 No
(m) One may be inoperative provided that it is removed.
Reference(s)
(m) Refer to AMM

LAN COLOMBIA FLEET MI-29-10 P 3/4

MEL G to H 27 FEB 15
 MEL ITEMS
29 - HYDRAULIC POWER
29-10 - Main Hydraulic Power
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-29-10 P 4/4

MEL 27 FEB 15
 MEL ITEMS
29 - HYDRAULIC POWER
29-22 - Blue Auxiliary Hydraulic Power
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-22-01 Ram Air Turbine

Ident.: MI-29-22-00008074.0001001 / 21 MAR 10
Applicable to: ALL

29-22-01A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

LAN COLOMBIA FLEET MI-29-22 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
29 - HYDRAULIC POWER
29-22 - Blue Auxiliary Hydraulic Power
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-29-22 P 2/2

MEL 05 NOV 13
 MEL ITEMS
29 - HYDRAULIC POWER
29-23 - Power Transfer
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-23-01 Power Transfer Unit ( PTU )

Ident.: MI-29-23-00008076.0001001 / 21 MAR 10
Applicable to: ALL

29-23-01A
Repair interval Nbr installed Nbr required Placard
C 1 1 No
(o) PTU may continuously run when set to AUTO provided that the operation of the PTU in both
directions is checked before the first flight of each day.
Reference(s)
(o) Refer to OpsProc 29-23-01A Power Transfer Unit

LAN COLOMBIA FLEET MI-29-23 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
29 - HYDRAULIC POWER
29-23 - Power Transfer
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-29-23 P 2/2

MEL 05 NOV 13
 MEL ITEMS
29 - HYDRAULIC POWER
29-24 - Yellow Auxiliary Hydraulic Power
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-24-01 Yellow System Electric Pump

Ident.: MI-29-24-00008077.0001001 / 21 MAR 10
Applicable to: ALL

29-24-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that the associated pb-sw is set to off.
Reference(s)
(o) Refer to OpsProc 29-24-01A Yellow System Electric Pump

LAN COLOMBIA FLEET MI-29-24 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
29 - HYDRAULIC POWER
29-24 - Yellow Auxiliary Hydraulic Power
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-29-24 P 2/2

MEL 05 NOV 13
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-00 - MAINTENANCE Message on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-00-01 ICE DETECT MAINTENANCE Message

Ident.: MI-30-00-00007863.0002001 / 27 FEB 15
Applicable to: ALL

30-00-01A
Repair interval Nbr installed Nbr required Placard
D No
ICE DETECT MAINTENANCE message may be displayed on the STATUS SD page.

LAN COLOMBIA FLEET MI-30-00 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-00 - MAINTENANCE Message on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-30-00 P 2/2

MEL 27 FEB 15
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 30-01-01 - ANTI ICE Overhead Panel
MINIMUM EQUIPMENT LIST

30-01-01-01 ANTI ICE ENG 1(2) pb-sw FAULT light

Ident.: MI-30-01-01-00007866.0001001 / 12 SEP 11
Applicable to: ALL

30-01-01-01A One inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
One may be inoperative provided that the associated engine anti-ice valve is considered
inoperative in the closed position.
Refer to Item 30-21-01A Engine Anti-Ice Valve

30-01-01-01B One or both inoperative

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative provided that the associated engine anti-ice valve is
considered inoperative in the open position.
Refer to Item 30-21-01 Engine Anti-Ice Valve

30-01-01-02 ANTI ICE ENG 1(2) pb-sw ON light

Ident.: MI-30-01-01-00007870.0001001 / 21 MAR 10
Applicable to: ALL

30-01-01-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

LAN COLOMBIA FLEET MI-30-01-01 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 30-01-01 - ANTI ICE Overhead Panel
MINIMUM EQUIPMENT LIST

30-01-01-03 ANTI ICE WING pb-sw FAULT light

Ident.: MI-30-01-01-00007882.0001001 / 12 SEP 11
Applicable to: ALL

30-01-01-03A Anti-ice arrow symbols operative on the BLEED SD page

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that the anti-ice arrow symbols are operative on the BLEED
SD page .
Reference(s)
(o) Refer to OpsProc 30-01-01-03A ANTI ICE WING pb-sw FAULT light

30-01-01-03B Non ETOPS flight

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that:
1) ETOPS is not conducted, and
2) The wing anti-ice control valves are deactivated in the closed position and considered
inoperative.
Refer to Item 30-11-01 Wing Anti-Ice Control Valve
Reference(s)
(m) Refer to AMM 30-11-00-040-002

30-01-01-04 ANTI ICE WING pb-sw ON light

Ident.: MI-30-01-01-00007885.0001001 / 21 MAR 10
Applicable to: ALL

30-01-01-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-30-01-01 P 2/2

MEL C to D 05 NOV 13
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 30-01-02 - WIPER Overhead Panel
MINIMUM EQUIPMENT LIST

30-01-02-01 Wiper High Speed Function (FAST Position)

Ident.: MI-30-01-02-00007890.0001001 / 21 MAR 10
Applicable to: ALL

30-01-02-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative provided that the associated low speed function is
operative.

30-01-02-02 Wiper Low Speed Function (SLOW Position)

Ident.: MI-30-01-02-00007893.0001001 / 21 MAR 10
Applicable to: ALL

30-01-02-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

LAN COLOMBIA FLEET MI-30-01-02 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 30-01-02 - WIPER Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-30-01-02 P 2/2

MEL 05 NOV 13
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-07 - Indications on the BLEED SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-07-01 ANTI ICE Indication on the BLEED SD page

Ident.: MI-30-07-00008019.0001001 / 21 MAR 10
Applicable to: ALL

30-07-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

30-07-02 Arrow Indication on the BLEED SD page

Ident.: MI-30-07-00008020.0001001 / 21 MAR 10
Applicable to: ALL

30-07-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

LAN COLOMBIA FLEET MI-30-07 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-07 - Indications on the BLEED SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-30-07 P 2/2

MEL 05 NOV 13
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-11 - Wing Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-11-01 Wing Anti-Ice Control Valve

Ident.: MI-30-11-00007897.0001001 / 12 SEP 11
Applicable to: ALL

30-11-01A Inoperative in the open position

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) (m) The RH valve may be inoperative in the open position provided that the associated ECAM
procedure is applied.
Reference(s)
(o) Refer to OpsProc 30-11-01A Wing Anti-Ice Control Valve
(m) Refer to AMM 30-11-00-040-004

30-11-01B Inoperative in the closed position

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(m) One or both may be inoperative in the closed position provided that:
1) ETOPS is not conducted, and
2) The aircraft is not operated in known or forecast icing conditions.
Reference(s)
(m) Refer to AMM 30-11-00-040-001

LAN COLOMBIA FLEET MI-30-11 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-11 - Wing Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-30-11 P 2/2

MEL 05 NOV 13
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-21 - Engine Air Intake Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-21-01 Engine Anti-Ice Valve

Ident.: MI-30-21-00007898.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

30-21-01A Inoperative in the closed position

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(m) One may be inoperative in the closed position provided that:
1) ETOPS is not conducted, and
2) The aircraft is not operated in known or forecast icing conditions.
Reference(s)
(m) Refer to AMM 30-21-00-040-001

30-21-01B Inoperative in the open position

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(o) (m) One or both may be inoperative in the open position provided that the Flight Manual
performance penalties are applied.
Reference(s)
(o) Refer to OpsProc 30-21-01B Engine Anti-Ice Valve
(m) Refer to AMM 30-21-00-040-002

30-21-01 Engine Anti-Ice Valve

Ident.: MI-30-21-00007898.0002001 / 10 OCT 14
Applicable to: MSN 4516-4546

30-21-01A Inoperative in the closed position

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(m) One may be inoperative in the closed position provided that:
1) ETOPS is not conducted, and
2) The aircraft is not operated in known or forecast icing conditions.
Continued on the following page

LAN COLOMBIA FLEET MI-30-21 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-21 - Engine Air Intake Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(m) Refer to AMM 30-21-00-040-020

30-21-01C Inoperative in the open position

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(o) (m) One or both may be inoperative in the open position provided that:
1) The Flight Manual performance penalties are applied, and
2) The OAT is below ISA + 35 C .
Reference(s)
(o) Refer to OpsProc 30-21-01C Engine Anti-Ice Valve
(m) Refer to AMM 30-21-00-040-010

LAN COLOMBIA FLEET MI-30-21 P 2/2

MEL A 27 FEB 15
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-31 - Probe Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-31-01 Probe Heat Computer ( PHC )

Ident.: MI-30-31-00007899.0001001 / 20 JUN 14
Applicable to: ALL

30-31-01A Associated probe heating operative

Repair interval Nbr installed Nbr required Placard
C 3 2 No
(m) One may be inoperative provided that the associated probe heating is checked operative
before each flight.
Reference(s)
(m) Refer to AMM Task 30-31-00-040-001

30-31-01B F/O PHC inoperative

Repair interval Nbr installed Nbr required Placard
C 3 2 No
(o) (m) The F/O PHC may be inoperative provided that the ADR s, heaters and failure alerts
associated with the operative computers are checked operative every day.
Reference(s)
(o) Refer to OpsProc 30-31-01B Probe Heat Computer
(m) Refer to AMM Task 30-31-00-040-002

30-31-01C STBY PHC inoperative

Repair interval Nbr installed Nbr required Placard
C 3 2 No
(m) The STBY PHC may be inoperative provided that:
1) The ADR s, heaters and failure alerts associated with the operative computers are
checked operative every day, and
2) The aircraft is not operated in visible moisture or in known or forecast icing conditions,
and
3) The OAT at the departure airport is above 5 C when the taxiway or the runway are
contaminated with water or slush.
Continued on the following page

LAN COLOMBIA FLEET MI-30-31 P 1/6

MEL A 10 OCT 14
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-31 - Probe Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(m) Refer to AMM Task 30-31-00-040-002

30-31-02 Pitot Heater

Ident.: MI-30-31-00007900.0001001 / 12 SEP 11
Applicable to: ALL

30-31-02A F/O pitot heater inoperative

Repair interval Nbr installed Nbr required Placard
C 3 2 No
(o) (m) The F/O pitot heater may be inoperative provided that the ADR s, heaters and failure alerts
associated with the CAPT and the STBY probes (pitot, static, AOA , TAT ) are checked
operative every day.
Reference(s)
(o) Refer to OpsProc 30-31-02A Pitot Heater
(m) Refer to AMM 30-31-00-040-002

30-31-02B CAPT pitot heater inoperative

Repair interval Nbr installed Nbr required Placard
C 3 2 No
(m) The CAPT pitot heater may be inoperative provided that:
1) The ADR s, heaters and failure alerts associated with the F/O and the STBY probes
(pitot, static, AOA , TAT ) are checked operative every day, and
2) The aircraft is not operated in visible moisture or in known or forecast icing conditions.
Reference(s)
(m) Refer to AMM 30-31-00-040-002
Continued on the following page

LAN COLOMBIA FLEET MI-30-31 P 2/6

MEL A to B 10 OCT 14
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-31 - Probe Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

30-31-02C STBY pitot heater inoperative
Repair interval Nbr installed Nbr required Placard
C 3 2 No
(m) The STBY pitot heater may be inoperative provided that:
1) The ADR s, heaters and failure alerts associated with the CAPT and the F/O probes
(pitot, static, AOA , TAT ) are checked operative every day, and
2) The aircraft is not operated in visible moisture or in known or forecast icing conditions.
Reference(s)
(m) Refer to AMM 30-31-00-040-002

30-31-03 Static Ports Heater

Ident.: MI-30-31-00007901.0001001 / 10 OCT 14
Applicable to: ALL

30-31-03A One STBY static port heater inoperative

Repair interval Nbr installed Nbr required Placard
C 6 5 No
One STBY static ports heater may be inoperative.

30-31-03B Both STBY static port heater inoperative

Repair interval Nbr installed Nbr required Placard
C 6 4 No
(m) Both STBY static ports heaters may be inoperative provided that:
1) The ADR s, heaters and failure alerts associated with the CAPT and the F/O probes
(pitot, static, AOA , TAT ) are checked operative every day, and
2) The OAT at the departure airport is above 5 C when the runway is contaminated with
water or slush.
Reference(s)
(m) Refer to AMM Task 30-31-00-040-002
Continued on the following page

LAN COLOMBIA FLEET MI-30-31 P 3/6

MEL B to C 10 OCT 14
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-31 - Probe Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

30-31-03C One or both F/O static port heater inoperative
Repair interval Nbr installed Nbr required Placard
C 6 4 No
(o) (m) One or both F/O static ports heaters may be inoperative provided that the ADR s, heaters
and failure alerts associated with the CAPT and the STBY probes (pitot, static, AOA , TAT )
are checked operative every day.
Reference(s)
(o) Refer to OpsProc 30-31-03C F/O Static Ports Heater
(m) Refer to AMM Task 30-31-00-040-002

30-31-03D One or both CAPT static port heater inoperative

Repair interval Nbr installed Nbr required Placard
C 6 4 No
(o) (m) One or both CAPT static ports heaters may be inoperative provided that:
1) The ADR s, heaters and failure alerts associated with the F/O and the STBY probes
(pitot, static, AOA , TAT ) are checked operative every day, and
2) The OAT at the departure airport is above 5 C when the runway is contaminated with
water or slush.
Reference(s)
(o) Refer to OpsProc 30-31-03D CAPT Static Ports Heater
(m) Refer to AMM Task 30-31-00-040-002

30-31-04 Angle of Attack ( AOA ) Probes Heating

Ident.: MI-30-31-00007902.0001001 / 20 JUN 14
Applicable to: ALL

30-31-04A F/O AOA inoperative

Repair interval Nbr installed Nbr required Placard
C 3 2 No
(o) (m) The F/O AOA probes heating may be inoperative provided that the ADR s, heaters and
failure alerts associated with the CAPT and the STBY probes (pitot, static, AOA , TAT ) are
checked operative every day
Continued on the following page

LAN COLOMBIA FLEET MI-30-31 P 4/6

MEL C to D 10 OCT 14
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-31 - Probe Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 30-31-04A Angle of Attack (AOA) Probe Heating (F/O inoperative)
(m) Refer to AMM Task 30-31-00-040-002

30-31-04B STBY AOA inoperative

Repair interval Nbr installed Nbr required Placard
C 3 2 No
(o) (m) The STBY AOA probes heating may be inoperative provided that the ADR s, heaters and
failure alerts associated with the CAPT and the F/O probes (pitot, static, AOA , TAT ) are
checked operative every day
Reference(s)
(o) Refer to OpsProc 30-31-04B Angle of Attack (AOA) Probe Heating (CAPT or STBY
inoperative)
(m) Refer to AMM Task 30-31-00-040-002

30-31-04C CAPT AOA inoperative

Repair interval Nbr installed Nbr required Placard
C 3 2 No
(o) (m) The CAPT AOA probes heating may be inoperative provided that:
1) The ADR s, heaters and failure alerts associated with the F/O and the STBY probes
(pitot, static, AOA , TAT ) are checked operative every day, and
2) The aircraft is not operated in visible moisture or in known or forecast icing conditions
Reference(s)
(o) Refer to OpsProc 30-31-04C Angle of Attack (AOA) Probe Heating (CAPT or STBY
inoperative)
(m) Refer to AMM Task 30-31-00-040-002

LAN COLOMBIA FLEET MI-30-31 P 5/6

MEL D 10 OCT 14
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-31 - Probe Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-31-05 TAT Probes Heating

Ident.: MI-30-31-00007903.0001001 / 12 SEP 11
Applicable to: ALL

30-31-05A One inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative.

30-31-05B Both inoperative

Repair interval Nbr installed Nbr required Placard
C 2 0 No
Both may be inoperative provided that the aircraft is not operated in visible moisture or in
known or forecast icing conditions.

LAN COLOMBIA FLEET MI-30-31 P 6/6

MEL E 10 OCT 14
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-42 - Windshield Anti-Icing and Defogging
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-42-01 Window Heat Computer

Ident.: MI-30-42-00007912.0001001 / 21 MAR 10
Applicable to: ALL

30-42-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) (m) One may be inoperative provided that:
1) The aircraft is not operated in known or forecast icing conditions, and
2) All heaters and failure alerts on the front and sliding windows associated with the
operative computer are checked operative every day.
Reference(s)
(o) Refer to OpsProc 30-42-01A Window Heat Computer
(m) Refer to AMM 30-42-00-040-001

30-42-02 Fixed Lateral Window and Sliding Window Heating

Ident.: MI-30-42-00007913.0001001 / 21 MAR 10
Applicable to: ALL

30-42-02A
Repair interval Nbr installed Nbr required Placard
C 4 0 No
One or more may be inoperative.

30-42-03 Windshield Heating

Ident.: MI-30-42-00007915.0001001 / 12 SEP 12
Applicable to: ALL

30-42-03A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) ** One may be inoperative provided that the aircraft is not operated in known or forecast
icing conditions.
Continued on the following page

LAN COLOMBIA FLEET MI-30-42 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-42 - Windshield Anti-Icing and Defogging
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 30-42-03A Windshield Heating

30-42-04 PROBES/WINDOW HEAT pb-sw AUTO Control

Ident.: MI-30-42-00007918.0001001 / 21 MAR 10
Applicable to: ALL

30-42-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
Automatic control may be inoperative provided that the PROBES/WINDOW HEAT system is
manually selected.

30-42-05 PROBES/WINDOW HEAT pb-sw ON light

Ident.: MI-30-42-00007921.0001001 / 21 MAR 10
Applicable to: ALL

30-42-05A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-30-42 P 2/2

MEL C to E 05 NOV 13
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-45 - Windshield Rain Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-45-01 Windshield Wiper

Ident.: MI-30-45-00007927.0001001 / 12 SEP 12
Applicable to: ALL

30-45-01A One inoperative on the PNF side

Repair interval Nbr installed Nbr required Placard
A 2 1 Yes
** One may be inoperative on the PNF side for three flights.

30-45-01B One or both inoperative

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(o) ** One or both may be inoperative provided that:
1) The aircraft is not operated in precipitation within departure and arrival areas, and
2) The approach minima do not require their use.
Reference(s)
(o) Refer to OpsProc 30-45-01B Windshield Wiper

30-45-01C Rain repellent system operative

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
** One may be inoperative provided that the associated rain repellent system is installed
and operative.

30-45-02 Windshield Wiper PARK Function

Ident.: MI-30-45-00007929.0001001 / 12 SEP 11
Applicable to: ALL

30-45-02A One or both inoperative

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative provided that the associated wipers can be positioned in a
location that will not obstruct forward vision.
Continued on the following page

LAN COLOMBIA FLEET MI-30-45 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-45 - Windshield Rain Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

30-45-02B One or both inoperative and removed
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(m) One or both may be inoperative provided that the associated wipers are removed.
Refer to Item 30-45-01 Windshield Wiper
Reference(s)
(m) Refer to AMM 30-45-00-040-003

30-45-03 Rain Repellent System

Ident.: MI-30-45-00007931.0001001 / 12 SEP 12
Applicable to: ALL

30-45-03A
Repair interval Nbr installed Nbr required Placard
D 2 0 Yes
** One or both may be inoperative.
Note: No entry in the logbook is required when it is installed but intentionally deactivated.

LAN COLOMBIA FLEET MI-30-45 P 2/2

MEL B to C 05 NOV 13
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-71 - Waste Water Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-71-01 Waste Water Drain Mast Heating System

Ident.: MI-30-71-00007934.0001001 / 21 MAR 10
Applicable to: ALL

30-71-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(m) One or both may be inoperative provided that:
1) The associated galleys and lavatories are not used, and
2) The associated lavatory water supplies are closed.
Reference(s)
(m) Refer to AMM 30-71-00-040-001

LAN COLOMBIA FLEET MI-30-71 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-71 - Waste Water Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-30-71 P 2/2

MEL 05 NOV 13
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-81 - Ice Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-81-01 Ice Detection System

Ident.: MI-30-81-00008016.0002001 / 27 FEB 15
Applicable to: ALL

30-81-01A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 30-81-01A Ice Detection System

30-81-02 External Visual Icing Indicator

Ident.: MI-30-81-00008017.0001001 / 21 MAR 10
Applicable to: ALL

30-81-02A
Repair interval Nbr installed Nbr required Placard
No
Refer to AFM/MCDL-30-01 Icing Indicator

30-81-03 Lighting of External Visual Icing Indicator

Ident.: MI-30-81-00008018.0001001 / 21 MAR 10
Applicable to: ALL

30-81-03A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 30-81-03A Lighting of External Visual Icing Indicator

LAN COLOMBIA FLEET MI-30-81 P 1/2

MEL A to C 27 FEB 15
 MEL ITEMS
30 - ICE AND RAIN PROTECTION
30-81 - Ice Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-30-81 P 2/2

MEL 27 FEB 15
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-00 - MAINTENANCE Message on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-00-02 ACMS MAINTENANCE Message

Ident.: MI-31-00-00007777.0002001 / 05 SEP 11
Applicable to: ALL

31-00-02A
Repair interval Nbr installed Nbr required Placard
D No
ACMS MAINTENANCE message may be displayed on the STATUS SD page.

31-00-04 CFDIU MAINTENANCE Message

Ident.: MI-31-00-00007779.0001001 / 21 MAR 10
Applicable to: ALL

31-00-04A
Repair interval Nbr installed Nbr required Placard
C No
CFDIU MAINTENANCE message may be displayed on the STATUS SD page.

31-00-05 DMC 1/3 MAINTENANCE Message

Ident.: MI-31-00-00007780.0001001 / 27 FEB 15
1 Applicable to: MSN 4892-4943, 5229, 5263-5364

31-00-05A
Repair interval Nbr installed Nbr required Placard
C No
DMC 1/3 MAINTENANCE message may be displayed on the STATUS SD page provided
that the DMC 2/3 MAINTENANCE message is not displayed on the STATUS SD page.

LAN COLOMBIA FLEET MI-31-00 P 1/2

MEL A to C 27 FEB 15
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-00 - MAINTENANCE Message on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-00-05 DMC 1/3 MAINTENANCE Message

Ident.: MI-31-00-00007780.0002001 / 27 FEB 15
2 Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453

31-00-05A
Repair interval Nbr installed Nbr required Placard
C No
DMC 1/3 MAINTENANCE message may be displayed on the STATUS SD page.

31-00-06 DMC 2/3 MAINTENANCE Message

Ident.: MI-31-00-00007781.0001001 / 21 MAR 10
Applicable to: ALL

31-00-06A
Repair interval Nbr installed Nbr required Placard
C No
DMC 2/3 MAINTENANCE message may be displayed on the STATUS SD page.

LAN COLOMBIA FLEET MI-31-00 P 2/2

MEL C to D 27 FEB 15
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-05 - Indications on the Primary Flight Display (PFD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-05-01 AP Related Indications on the FMA

Ident.: MI-31-05-00007820.0001001 / 21 MAR 10
Applicable to: ALL

31-05-01A
Repair interval Nbr installed Nbr required Placard

Refer to Item 22-05-01 AP Related Indications on the FMA

31-05-02 A/THR Related Indications on the FMA

Ident.: MI-31-05-00007821.0001001 / 21 MAR 10
Applicable to: ALL

31-05-02A
Repair interval Nbr installed Nbr required Placard

Refer to Item 22-05-02 A/THR Related Indications on the FMA

31-05-03 Approach and Landing Capabilities on the FMA

Ident.: MI-31-05-00007822.0001001 / 21 MAR 10
Applicable to: ALL

31-05-03A
Repair interval Nbr installed Nbr required Placard

Refer to Item 22-05-03 Approach and Landing Capabilities on the FMA

LAN COLOMBIA FLEET MI-31-05 P 1/6

MEL A to C 10 OCT 14
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-05 - Indications on the Primary Flight Display (PFD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-05-04 Special Messages on the FMA

Ident.: MI-31-05-00007823.0001001 / 21 MAR 10
Applicable to: ALL

31-05-04A
Repair interval Nbr installed Nbr required Placard

Refer to Item 22-05-04 Special Messages on the FMA

31-05-05 Actual Airspeed Reference Line and Scale Indications on the PFD
Ident.: MI-31-05-00007824.0001001 / 21 MAR 10
Applicable to: ALL

31-05-05A
Repair interval Nbr installed Nbr required Placard

Refer to Item 34-05-01 Actual Airspeed Reference Line and Scale Indication on the PFD

31-05-06 Mach Number Indication on the PFD

Ident.: MI-31-05-00007825.0001001 / 21 MAR 10
Applicable to: ALL

31-05-06A
Repair interval Nbr installed Nbr required Placard

Refer to Item 34-05-02 Mach Number Indication on the PFD

LAN COLOMBIA FLEET MI-31-05 P 2/6

MEL D to F 10 OCT 14
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-05 - Indications on the Primary Flight Display (PFD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-05-07 VMO / MMO Characteristic Speed Indication on the PFD

Ident.: MI-31-05-00007826.0001001 / 21 MAR 10
Applicable to: ALL

31-05-07A
Repair interval Nbr installed Nbr required Placard

Refer to Item 34-05-03 VMO/MMO Characteristic Speed Indication on the PFD

31-05-08 Altitude Indication on the PFD

Ident.: MI-31-05-00007827.0001001 / 21 MAR 10
Applicable to: ALL

31-05-08A
Repair interval Nbr installed Nbr required Placard

Refer to Item 34-05-04 Altitude Indication on the PFD

31-05-09 Vertical Speed Indication on the PFD

Ident.: MI-31-05-00007828.0001001 / 21 MAR 10
Applicable to: ALL

31-05-09A
Repair interval Nbr installed Nbr required Placard

Refer to Item 34-05-06 Vertical Speed in Inertial Mode Indication on the PFD

LAN COLOMBIA FLEET MI-31-05 P 3/6

MEL G to I 10 OCT 14
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-05 - Indications on the Primary Flight Display (PFD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-05-10 Other Air Data Related Indications on the PFD

Ident.: MI-31-05-00007829.0001001 / 21 MAR 10
Applicable to: ALL

31-05-10A
Repair interval Nbr installed Nbr required Placard

Refer to Item 34-05-07 Other Air Data Related Indications on the PFD

31-05-11 Attitude Indication on the PFD

Ident.: MI-31-05-00007830.0001001 / 21 MAR 10
Applicable to: ALL

31-05-11A
Repair interval Nbr installed Nbr required Placard

Refer to Item 34-05-08 Attitude Indication on the PFD

31-05-12 Heading Indication on the PFD

Ident.: MI-31-05-00007831.0001001 / 21 MAR 10
Applicable to: ALL

31-05-12A
Repair interval Nbr installed Nbr required Placard

Refer to Item 34-05-09 Heading Indication on the PFD

31-05-30 Lateral Deviation Scale (L/DEV)

Ident.: MI-31-05-20800890.9001001 / 10 OCT 14
Applicable to: ALL

Note: RNP item.

Continued on the following page

LAN COLOMBIA FLEET MI-31-05 P 4/6

MEL J to M 10 OCT 14
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-05 - Indications on the Primary Flight Display (PFD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

31-05-30A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
For RNP -AR < 0.3, both must be operative.

31-05-31 Vertical Deviation Scale (V/DEV)

Ident.: MI-31-05-20800891.9001001 / 10 OCT 14
Applicable to: ALL

Note: RNP item.

31-05-31A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
Both may be inoperative. ForRNAV ( GNSS ) , the operation is limited to LNAV minimums.
For RNP -AR operations, both scales must be operative.

LAN COLOMBIA FLEET MI-31-05 P 5/6

MEL M to N 10 OCT 14
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-05 - Indications on the Primary Flight Display (PFD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-31-05 P 6/6

MEL 10 OCT 14
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-06 - Indications on the Navigation Display (ND)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-06-01 Ground Speed Indication on the ND

Ident.: MI-31-06-00007832.0001001 / 21 MAR 10
Applicable to: ALL

31-06-01A
Repair interval Nbr installed Nbr required Placard

Refer to Item 34-06-01 Ground Speed Indication on the ND

31-06-02 True Air Speed Indication on the ND

Ident.: MI-31-06-00007834.0001001 / 21 MAR 10
Applicable to: ALL

31-06-02A
Repair interval Nbr installed Nbr required Placard

Refer to Item 34-06-02 True Air Speed Indication on the ND

31-06-03 Wind Indication on the ND

Ident.: MI-31-06-00007835.0001001 / 21 MAR 10
Applicable to: ALL

31-06-03A
Repair interval Nbr installed Nbr required Placard

Refer to Item 34-06-03 Wind Indication on the ND

LAN COLOMBIA FLEET MI-31-06 P 1/4

MEL A to C 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-06 - Indications on the Navigation Display (ND)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-06-04 Heading Indication on the ND

Ident.: MI-31-06-00007836.0001001 / 21 MAR 10
Applicable to: ALL

31-06-04A
Repair interval Nbr installed Nbr required Placard

Refer to Item 34-06-04 Heading Indication on the ND

31-06-05 Position (Aircraft Symbol) Indication on the ND

Ident.: MI-31-06-00007839.0001001 / 21 MAR 10
Applicable to: ALL

31-06-05A
Repair interval Nbr installed Nbr required Placard

Refer to Item 34-06-05 Position (Aircraft Symbol) Indication on the ND

31-06-06 Navigation Station Information on the ND

Ident.: MI-31-06-00007845.0001001 / 21 MAR 10
Applicable to: ALL

31-06-06A
Repair interval Nbr installed Nbr required Placard

Refer to Item 34-06-06 Radio Navaids Indications on the ND

LAN COLOMBIA FLEET MI-31-06 P 2/4

MEL D to F 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-06 - Indications on the Navigation Display (ND)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-06-07 Chrono Indication on the ND

Ident.: MI-31-06-00007846.0001001 / 21 MAR 10
Applicable to: ALL

31-06-07A
Repair interval Nbr installed Nbr required Placard

Refer to Item 34-06-07 Chrono Indication on the ND

LAN COLOMBIA FLEET MI-31-06 P 3/4

MEL G 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-06 - Indications on the Navigation Display (ND)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-31-06 P 4/4

MEL 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-07 - Indications on the System Display (SD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-07-01 Indications on the System Display pages

Ident.: MI-31-07-00007848.0001001 / 21 MAR 10
Applicable to: ALL

31-07-01A
Repair interval Nbr installed Nbr required Placard
No
Refer to corresponding item in the associated ATA chapter.

31-07-02 Permanent Data ( TAT , SAT , ISA , GLOAD -

ALT SEL, UTC , GW ) Indications on the SD
Ident.: MI-31-07-00007850.0003001 / 27 FEB 15
Applicable to: ALL

31-07-02A
Repair interval Nbr installed Nbr required Placard
C 7 1 No
(o) TAT indication must be available.
Reference(s)
(o) Refer to OpsProc 31-07-02A Permanent Data Indications on the SD

LAN COLOMBIA FLEET MI-31-07 P 1/2

MEL A to B 27 FEB 15
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-07 - Indications on the System Display (SD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-31-07 P 2/2

MEL 27 FEB 15
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-08 - Indications on the Engine Warning Display (EWD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-08-01 Engine Parameter Indications on the EWD

Ident.: MI-31-08-00007851.0001001 / 21 MAR 10
Applicable to: ALL

31-08-01A
Repair interval Nbr installed Nbr required Placard
No
Refer to 77-08

31-08-02 Fuel On Board ( FOB ) Indication on the EWD

Ident.: MI-31-08-00007852.0001001 / 21 MAR 10
Applicable to: ALL

31-08-02A
Repair interval Nbr installed Nbr required Placard

Refer to Item 28-07-01-01 Fuel On Board (FOB) Indication on the FUEL SD page

31-08-03 MEMO Messages on the EWD

Ident.: MI-31-08-00007853.0001001 / 12 SEP 11
Applicable to: ALL

31-08-03A
Repair interval Nbr installed Nbr required Placard
C 58 0 No
One or more may be inoperative.

LAN COLOMBIA FLEET MI-31-08 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-08 - Indications on the Engine Warning Display (EWD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-08-04 Slats/Flaps Position Indications on the EWD

Ident.: MI-31-08-00007854.0001001 / 21 MAR 10
Applicable to: ALL

31-08-04A
Repair interval Nbr installed Nbr required Placard

Refer to Item 27-08-01 Flap Position Indication on the EWD
Refer to Item 27-08-02 Slat Position Indication on the EWD
Note: Apply both MMEL Items.

LAN COLOMBIA FLEET MI-31-08 P 2/2

MEL D 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-20 - Independent Instruments
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-20-01 Electrical Clock Indicator

Ident.: MI-31-20-00007782.0001001 / 21 MAR 10
Applicable to: ALL

31-20-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that:
1) The UTC indication from the CFDIU is operative on the permanent data of the SD , and
2) A chrono indication is operative on at least one ND .
Reference(s)
(o) Refer to OpsProc 31-20-01A Electrical Clock Indicator

LAN COLOMBIA FLEET MI-31-20 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-20 - Independent Instruments
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-31-20 P 2/2

MEL 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-30 - Centralized Fault Display System (CFDS) and Data Recording System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-30-01 Centralized Fault Display System (CFDS)

Ident.: MI-31-30-00007784.0001001 / 21 MAR 10
Applicable to: ALL

31-30-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.

31-30-03 Digital Flight Data Recorder ( DFDR )

Ident.: MI-31-30-00007786.0001001 / 23 MAR 11
Applicable to: ALL

31-30-03A
Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative provided:
1) Cockpit Voice Recorder is operative Refer to Item 23-71-01 Cockpit Voice Recorder
(CVR) and
2) Repairs are made within three flight days.

31-30-04 Data Management (DMU or FDIMU Data Management function)

Ident.: MI-31-30-00007787.0002001 / 05 NOV 13
Applicable to: ALL

31-30-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-31-30 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-30 - Centralized Fault Display System (CFDS) and Data Recording System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-30-05 Flight Data Interface (FDIU or FDIMU Flight Data Interface function)
Ident.: MI-31-30-00007788.0001001 / 12 SEP 12
Applicable to: ALL

31-30-05A
Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative for three flight days.
Note: If FDIU or FDIMU Flight Data Interface function is inoperative the DFDR is
inoperative.
Refer to Item 31-30-03 Digital Flight Data Recorder (DFDR)

31-30-07 Printer
Ident.: MI-31-30-00007790.0001001 / 18 MAY 11
Applicable to: ALL

31-30-07A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-31-30 P 2/2

MEL D to E 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-38 - Up and Down Data Loading System
COLOMBIA
LAN COLOMBIA AIRLINES Acquisition/Interface and Equipment
MINIMUM EQUIPMENT LIST

31-38-01 DATA LOADING selector

Ident.: MI-31-38-00007791.0001001 / 21 MAR 10
Applicable to: ALL

31-38-01A
Repair interval Nbr installed Nbr required Placard
D 1 0 Yes
May be inoperative.

31-38-02 Data Loading Routing Box (DLRB)

Ident.: MI-31-38-00007792.0001001 / 21 MAR 10
Applicable to: ALL

31-38-02A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative.

31-38-03 Multipurpose Disk Drive Unit (MDDU)

Ident.: MI-31-38-00007793.0001001 / 10 OCT 14
Applicable to: MSN 4516-4972

31-38-03A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-31-38 P 1/2

MEL A to C 10 OCT 14
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-38 - Up and Down Data Loading System
COLOMBIA
LAN COLOMBIA AIRLINES Acquisition/Interface and Equipment
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-31-38 P 2/2

MEL 10 OCT 14
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-53 - Flight Warning Computer (FWC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-53-01 Flight Warning Computer ( FWC )

Ident.: MI-31-53-00007794.0001001 / 23 MAR 11
Applicable to: ALL

31-53-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) **
FWC 2 may be inoperative.
Reference(s)
(o) Refer to OpsProc 31-53-01A Flight Warning Computer (FWC)

31-53-02 MASTER CAUT Cancel Function

Ident.: MI-31-53-00007795.0001001 / 21 MAR 10
Applicable to: ALL

31-53-02A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative.

31-53-03 MASTER WARN Cancel Function

Ident.: MI-31-53-00007796.0001001 / 21 MAR 10
Applicable to: ALL

31-53-03A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative.

LAN COLOMBIA FLEET MI-31-53 P 1/4

MEL A to C 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-53 - Flight Warning Computer (FWC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-53-04 MASTER CAUT light

Ident.: MI-31-53-00007797.0001001 / 21 MAR 10
Applicable to: ALL

31-53-04A
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
One may be inoperative.

31-53-05 MASTER WARN light

Ident.: MI-31-53-00007798.0001001 / 21 MAR 10
Applicable to: ALL

31-53-05A
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
One may be inoperative.

31-53-06 Altitude Alert

Ident.: MI-31-53-00007799.0001001 / 04 AUG 11
Applicable to: ALL

Note: RVSM item.

31-53-06A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) One may be inoperative.
Reference(s)
(o) Refer to OpsProc 31-53-06A Altitude Alert
Continued on the following page

LAN COLOMBIA FLEET MI-31-53 P 2/4

MEL D to F 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-53 - Flight Warning Computer (FWC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

31-53-06B
Repair interval Nbr installed Nbr required Placard
A 2 0 No
Both may be inoperative provided :
1) One A/P ALT mode is operative, and
2) Rectification is made within three flight days.
3) For RVSM operation one Altitude alert must be operative.

LAN COLOMBIA FLEET MI-31-53 P 3/4

MEL F 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-53 - Flight Warning Computer (FWC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-31-53 P 4/4

MEL 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-55 - System Data Acquisition Concentrator (SDAC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-55-01 System Data Acquisition Concentrator (SDAC)

Ident.: MI-31-55-00007800.0001001 / 14 SEP 10
Applicable to: ALL

31-55-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
SDAC 2 may be inoperative.

LAN COLOMBIA FLEET MI-31-55 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-55 - System Data Acquisition Concentrator (SDAC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-31-55 P 2/2

MEL 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-56 - ECAM Control Panel (ECP)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-56-01 System Page Manual Call pb on the ECP

Ident.: MI-31-56-00007801.0001001 / 21 MAR 10
Applicable to: ALL

31-56-01A
Repair interval Nbr installed Nbr required Placard
C 11 0 Yes
One or more may be inoperative.

31-56-02 ALL pb on the ECP

Ident.: MI-31-56-00007802.0001001 / 21 MAR 10
Applicable to: ALL

31-56-02A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

31-56-03 CLR pb on the ECP

Ident.: MI-31-56-00007803.0001001 / 21 MAR 10
Applicable to: ALL

31-56-03A
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
One may be inoperative.

LAN COLOMBIA FLEET MI-31-56 P 1/4

MEL A to C 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-56 - ECAM Control Panel (ECP)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-56-04 EMER CANC pb on the ECP

Ident.: MI-31-56-00007804.0001001 / 21 MAR 10
Applicable to: ALL

31-56-04A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

31-56-05 RCL pb on the ECP

Ident.: MI-31-56-00007805.0001001 / 21 MAR 10
Applicable to: ALL

31-56-05A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

31-56-06 STS pb on the ECP

Ident.: MI-31-56-00007806.0001001 / 21 MAR 10
Applicable to: ALL

31-56-06A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-31-56 P 2/4

MEL D to F 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-56 - ECAM Control Panel (ECP)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-56-07 T.O CONFIG pb on the ECP

Ident.: MI-31-56-00007807.0001001 / 21 MAR 10
Applicable to: ALL

31-56-07A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 31-56-07A T.O CONFIG pb on the ECP

LAN COLOMBIA FLEET MI-31-56 P 3/4

MEL G 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-56 - ECAM Control Panel (ECP)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-31-56 P 4/4

MEL 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-62 - Display Management Computer (DMC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-62-01 DMC 1
Ident.: MI-31-62-00007808.0005001 / 27 FEB 15
Applicable to: ALL

31-62-01B
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative provided that:
1) The DMC 2 and DMC 3 are operative, and
2) The ISIS airspeed indication is operative, and
3) The ISIS altitude indication is operative, and
4) The ISIS attitude indication is operative, and
5) The standby compass is operative, and
6) The EIS DMC SWITCHING selector is set to CAPT 3.
Reference(s)
(o) Refer to OpsProc 31-62-01B DMC 1

31-62-02 DMC 2
Ident.: MI-31-62-00007809.0002001 / 27 FEB 15
Applicable to: ALL

31-62-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that:
1) The DMC 1 and DMC 3 are operative, and
2) The ISIS airspeed indication is operative, and
3) The ISIS altitude indication is operative, and
4) The ISIS attitude indication is operative, and
5) The standby compass is operative, and
6) The EIS DMC SWITCHING selector is set to F/O 3, and
7) The AC ESS FEED control is checked operative every day, and
8) The AC ESS FEED pb-sw FAULT light is checked operative every day.
Continued on the following page

LAN COLOMBIA FLEET MI-31-62 P 1/2

MEL A to B 27 FEB 15
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-62 - Display Management Computer (DMC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 31-62-02A DMC 2
(m) Refer to AMM Task 31-68-00-040-005

31-62-03 DMC 3
Ident.: MI-31-62-00007810.0004001 / 27 FEB 15
Applicable to: ALL

31-62-03B
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative provided that:
1) The DMC 1 and DMC 2 are operative, and
2) The ISIS airspeed indication is operative, and
3) The ISIS altitude indication is operative, and
4) The ISIS attitude indication is operative, and
5) The standby compass is operative.
Reference(s)
(o) Refer to OpsProc 31-62-03B DMC 3

LAN COLOMBIA FLEET MI-31-62 P 2/2

MEL B to C 27 FEB 15
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-63 - Display Unit (DU)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-63-01 PFDU 1
Ident.: MI-31-63-00009664.0001001 / 04 AUG 11
Applicable to: ALL

Note: RVSM item.

Note: RNP item.
Note: For RVSM operation two PFD data information must be displayed in any screen.

31-63-01A
Repair interval Nbr installed Nbr required Placard
1 1 No
** Must be operative.

31-63-02 PFDU 2
Ident.: MI-31-63-00007811.0001001 / 02 NOV 11
Applicable to: ALL

Note: RVSM item.

Note: RNP item.
Note: RNAV item.
Note: For RVSM operation two PFD data information must be displayed in any screen.

31-63-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) ** Except for ETOPS , RNAV ( RNP ), and RNAV ( GNSS ), may be inoperative provided
that PFDU 1, NDU 1, NDU 2, EWDU and SDU are operative.
Reference(s)
(o) Refer to OpsProc 31-63-02A PFDU 2

LAN COLOMBIA FLEET MI-31-63 P 1/4

MEL A to B 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-63 - Display Unit (DU)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-63-03 NDU 1
Ident.: MI-31-63-00007812.0001001 / 01 AUG 13
Applicable to: ALL

Note: RVSM item.

Note: RVSM operation is ensured due to the minimum equipment is covered in the remark of this
Item.
Note: RNP item.
Note: RNAV item.

31-63-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) ** Except for RNAV ( RNP ) and RNAV ( GNSS ) operations, may be inoperative provided
that PFDU 1, PFDU 2, NDU 2, EWDU and SDU are operative.
Reference(s)
(o) Refer to OpsProc 31-63-03A NDU 1

31-63-04 NDU 2
Ident.: MI-31-63-00007813.0001001 / 01 AUG 13
Applicable to: ALL

Note: RVSM item.

Note: RVSM operation is ensured due to the minimum equipment is covered in the remark of this
Item.
Note: RNP item.
Note: RNAV item.

Continued on the following page

LAN COLOMBIA FLEET MI-31-63 P 2/4

MEL C to D 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-63 - Display Unit (DU)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

31-63-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) ** Except for RNAV ( RNP ) and RNAV ( GNSS ) operations may be inoperative provided
that PFDU 1, PFDU 2, NDU 1, EWDU and SDU are operative.
Reference(s)
(o) Refer to OpsProc 31-63-04A NDU 2

31-63-05 SDU
Ident.: MI-31-63-00007814.0001001 / 01 AUG 13
Applicable to: ALL

Note: RVSM item.

Note: RVSM operation is ensured due to the minimum equipment is covered in the remark of this
Item.

31-63-05A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) (m) May be inoperative provided that:
1) The PFDU 1, PFDU 2, NDU 1, NDU 2 and EWDU are operative, and
2) The AC ESS FEED control is checked operative every day, and
3) The AC ESS FEED pb-sw FAULT light is checked operative every day.
Reference(s)
(o) Refer to OpsProc 31-63-05A SDU
(m) Refer to AMM 31-68-00-040-006

LAN COLOMBIA FLEET MI-31-63 P 3/4

MEL D to E 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-63 - Display Unit (DU)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-63-06 EWDU
Ident.: MI-31-63-00009604.0001001 / 23 MAR 11
Applicable to: ALL

31-63-06A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

LAN COLOMBIA FLEET MI-31-63 P 4/4

MEL F 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-68 - Switching Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-68-01 AIR DATA SWITCHING selector on the Center Pedestal

Ident.: MI-31-68-00007815.0001001 / 21 MAR 10
Applicable to: ALL

31-68-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that the AIR DATA SWITCHING selector is set to NORM.

31-68-02 ATT HDG SWITCHING selector on the Center Pedestal

Ident.: MI-31-68-00007816.0001001 / 21 MAR 10
Applicable to: ALL

31-68-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that the ATT HDG SWITCHING selector is set to NORM.

31-68-03 ECAM/ND XFR SWITCHING selector on the Center Pedestal

Ident.: MI-31-68-00007817.0001001 / 21 MAR 10
Applicable to: ALL

31-68-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that:
1) Both ECAM DU are operative, and
2) The ECAM/ND XFR SWITCHING selector is set to NORM.

LAN COLOMBIA FLEET MI-31-68 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
31 - INDICATING/RECORDING SYSTEMS
31-68 - Switching Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-68-04 EIS DMC SWITCHING selector on the Center Pedestal

Ident.: MI-31-68-00007818.0001001 / 21 MAR 10
Applicable to: ALL

31-68-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that the EIS DMC SWITCHING selector is set to NORM.

31-68-05 PFD/ND XFR pb on the Lateral Instrument Panel

Ident.: MI-31-68-00007819.0001001 / 21 MAR 10
Applicable to: ALL

31-68-05A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(o) One or both may be inoperative provided that:
1) The PFD and ND units are operative, and
2) The PFD to ND automatic switching is checked operative on the PF side before each
flight.
Reference(s)
(o) Refer to OpsProc 31-68-05A PFD/ND XFR pb on the Lateral Instrument Panel

LAN COLOMBIA FLEET MI-31-68 P 2/2

MEL D to E 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-07 - Indications on the WHEEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-07-01 Brakes Temperature Indication on the WHEEL SD page

Ident.: MI-32-07-00007761.0001001 / 12 SEP 11
Applicable to: ALL

32-07-01A BRAKES HOT alert not displayed

Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) One or more may be inoperative provided that the ground brake cooling time is applied.
Reference(s)
(o) Refer to OpsProc 32-07-01A Brakes Temperature Indication on the WHEEL SD page

32-07-01B BRAKES HOT alert displayed

Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) (m) One or more may be inoperative provided that:
1) The associated sensor is deactivated if the BRAKES HOT alert is displayed on the EWD
, and
2) The ground brake cooling time is applied.
Reference(s)
(o) Refer to OpsProc 32-07-01B Brakes Temperature Indication on the WHEEL SD page
(m) Refer to AMM 32-47-00-040-001

32-07-02 L/G Position Indication on the WHEEL SD page

Ident.: MI-32-07-00007762.0001001 / 21 MAR 10
Applicable to: ALL

32-07-02A
Repair interval Nbr installed Nbr required Placard
C 6 0 No
One or more may be inoperative provided that the L/G gear position indications are
operative on the LDG GEAR indicator panel.

LAN COLOMBIA FLEET MI-32-07 P 1/6

MEL A to B 27 FEB 15
 MEL ITEMS
32 - LANDING GEAR
32-07 - Indications on the WHEEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-07-03 L/G Doors Position Indication on the WHEEL SD page

Ident.: MI-32-07-00007763.0001001 / 21 MAR 10
Applicable to: ALL

32-07-03A
Repair interval Nbr installed Nbr required Placard
C 3 0 No
(o) One or more may be inoperative.
Reference(s)
(o) Refer to OpsProc 32-07-03A L/G Doors Position Indication on the WHEEL SD page

32-07-04 L/G CTL Indication on the WHEEL SD page

Ident.: MI-32-07-00007764.0001001 / 21 MAR 10
Applicable to: ALL

32-07-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.

32-07-05 UP LOCK Indication on the WHEEL SD page

Ident.: MI-32-07-00007765.0001001 / 21 MAR 10
Applicable to: ALL

32-07-05A
Repair interval Nbr installed Nbr required Placard
C 3 0 No
One or more may be inoperative.

LAN COLOMBIA FLEET MI-32-07 P 2/6

MEL C to E 27 FEB 15
 MEL ITEMS
32 - LANDING GEAR
32-07 - Indications on the WHEEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-07-06 [Y] N/W STEERING Indication on the WHEEL SD page

Ident.: MI-32-07-00007766.0002001 / 27 FEB 15
Applicable to: ALL

32-07-06A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

32-07-08 ANTI SKID, [1], [2] Indication on the WHEEL SD page

Ident.: MI-32-07-00007768.0003001 / 27 FEB 15
Applicable to: ALL

32-07-08A
Repair interval Nbr installed Nbr required Placard
C 3 0 No
One or more may be inoperative.

32-07-09 AUTO BRK Indication on the WHEEL SD page

Ident.: MI-32-07-00007769.0001001 / 21 MAR 10
Applicable to: ALL

32-07-09A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-32-07 P 3/6

MEL F to H 27 FEB 15
 MEL ITEMS
32 - LANDING GEAR
32-07 - Indications on the WHEEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-07-10 [G] NORM BRK Indication on the WHEEL SD page

Ident.: MI-32-07-00007770.0002001 / 27 FEB 15
Applicable to: ALL

32-07-10A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

32-07-11 Release Brake Indication on the WHEEL SD page

Ident.: MI-32-07-00007771.0001001 / 21 MAR 10
Applicable to: ALL

32-07-11A
Repair interval Nbr installed Nbr required Placard
C 4 0 No
One or more may be inoperative.

32-07-12 ACCU PRESS/ACCU ONLY Indication on the WHEEL SD page

Ident.: MI-32-07-00007772.0002001 / 27 FEB 15
Applicable to: ALL

32-07-12A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-32-07 P 4/6

MEL I to K 27 FEB 15
 MEL ITEMS
32 - LANDING GEAR
32-07 - Indications on the WHEEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-07-13 [Y] ALTN BRK Indication on the WHEEL SD page

Ident.: MI-32-07-00007773.0002001 / 27 FEB 15
Applicable to: ALL

32-07-13A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

LAN COLOMBIA FLEET MI-32-07 P 5/6

MEL L 27 FEB 15
 MEL ITEMS
32 - LANDING GEAR
32-07 - Indications on the WHEEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-32-07 P 6/6

MEL 27 FEB 15
 MEL ITEMS
32 - LANDING GEAR
32-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-09-01 BRAKES-N/WS MINOR FAULT Alert

Ident.: MI-32-09-00007774.0005001 / 27 FEB 15
Applicable to: ALL

32-09-01A Fault on an alternate braking system pressure transducer

Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be displayed provided that:
1) The alert is confirmed to be caused by a fault on an alternate braking system pressure
transducer by troubleshooting, and
2) The associated BRAKES pressure indicator is considered inoperative.
Refer to Item 32-44-03 BRAKES Pressure Indicator

32-09-01C Both BRAKES pressure indicators operative

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be displayed provided that:
1) Both BRAKES pressure indicators are operative, and
2) The alternate braking system is checked operative before the first flight of each day, and
3) It is checked before each flight that the CFDS failure message related to the
BRAKES-N/WS MINOR FAULT alert do not report a fault on an alternate pressure
transducer.
Reference(s)
(o) Refer to OpsProc 32-09-01C BRAKES-N/WS MINOR FAULT Alert (Alternate braking
checked operative)
(m) Refer to AMM 32-46-00-040-001

LAN COLOMBIA FLEET MI-32-09 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
32 - LANDING GEAR
32-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-32-09 P 2/2

MEL 27 FEB 15
 MEL ITEMS
32 - LANDING GEAR
32-11 - Main Gear
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-11-01 Main Gear Torque Link Damper

Ident.: MI-32-11-00007682.0002001 / 21 MAR 10
Applicable to: ALL

32-11-01A
Repair interval Nbr installed Nbr required Placard
A 2 0 No
One or both may be inoperative for 7 flights.

LAN COLOMBIA FLEET MI-32-11 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-11 - Main Gear
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-32-11 P 2/2

MEL 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-12 - Main Gear Doors
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-12-01 Main Gear Door Ground Opening Cable

Ident.: MI-32-12-00007686.0001001 / 02 NOV 11
Applicable to: ALL

32-12-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(m) One or both may be broken or missing.
Reference(s)
(m) Refer to AMM 32-12-00-040-006

LAN COLOMBIA FLEET MI-32-12 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-12 - Main Gear Doors
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-32-12 P 2/2

MEL 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-31 - Normal Extension and Retraction
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-31-01 Landing Gear Control and Interface Unit ( LGCIU )

Ident.: MI-32-31-00007688.0002001 / 21 MAR 10
Applicable to: ALL

32-31-01A
Repair interval Nbr installed Nbr required Placard
A 2 1 No
(o) The LGCIU 2 may be inoperative for 7 flights provided that:
1) All ELAC s, SEC s, SFCC s, RA s, FAC s, and ADIRS s are operative, and
2) Both air conditioning packs are operative, and
3) The FLEX Takeoff Mode is not used, and
4) The operation of avionics equipment is time limited on ground.
Reference(s)
(o) Refer to OpsProc 32-31-01A Landing Gear Control and Interface Unit (LGCIU)

32-31-02 Landing Gear Retracting System

Ident.: MI-32-31-00007690.0001001 / 12 SEP 12
Applicable to: ALL

32-31-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) (m) May be inoperative provided that:
1) ETOPS is not conducted, and
2) The aircraft is operated in accordance with the Flight Manual supplement for the flight
with landing gear down.
Reference(s)
(o) Refer to OpsProc 32-31-02A Landing Gear Retracting System
(m) Refer to AMM 32-31-00-040-803

LAN COLOMBIA FLEET MI-32-31 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-31 - Normal Extension and Retraction
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-32-31 P 2/2

MEL 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-32-01 LGCIU 1 Proximity Detector

Ident.: MI-32-32-00007693.0001001 / 21 MAR 10
Applicable to: ALL

32-32-01A
Repair interval Nbr installed Nbr required Placard
16 16 No
All must be operative.

32-32-02 LGCIU 2 RH L/G Shock Absorber Proximity Detector

Ident.: MI-32-32-00007694.0001001 / 21 MAR 10
Applicable to: ALL

32-32-02A
Repair interval Nbr installed Nbr required Placard
A 1 0 No
(o) (m) May be inoperative for 7 flights provided that:
1) Both radio altimeters are operative, and
2) The other proximity detectors are operative, and
3) The origin of the failure is checked to be electrical.
Reference(s)
(o) Refer to OpsProc 32-32-02A LGCIU 2 RH L/G Shock Absorber Proximity Detector
(m) Refer to AMM 32-31-00-040-003

32-32-02B
Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative for 7 flights provided that the LGCIU 2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)

LAN COLOMBIA FLEET MI-32-32 P 1/12

MEL A to B 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-32-03 LGCIU 2 LH L/G Shock Absorber Proximity Detector

Ident.: MI-32-32-00007695.0001001 / 21 MAR 10
Applicable to: ALL

32-32-03A
Repair interval Nbr installed Nbr required Placard
A 1 0 No
(o) (m) May be inoperative for 7 flights provided that:
1) Both radio altimeters are operative, and
2) The other proximity detectors are operative, and
3) The origin of the failure is checked to be electrical.
Reference(s)
(o) Refer to OpsProc 32-32-03A LGCIU 2 LH L/G Shock Absorber Proximity Detector
(m) Refer to AMM 32-31-00-040-003

32-32-03B
Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative for 7 flights provided that the LGCIU 2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)

32-32-04 LGCIU 2 Nose L/G Shock Absorber Proximity Detector

Ident.: MI-32-32-00007696.0001001 / 12 SEP 11
Applicable to: ALL

32-32-04A Other proximity detectors operative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
(o) (m) May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
Continued on the following page

LAN COLOMBIA FLEET MI-32-32 P 2/12

MEL C to D 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 32-32-04A LGCIU 2 Nose L/G Shock Absorber Proximity Detector
(m) Refer to AMM 32-31-00-040-003

32-32-04B LGCIU 2 considered inoperative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative for 7 flights provided that the LGCIU 2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)

32-32-05 LGCIU 2 RH L/G Down Lock Proximity Detector

Ident.: MI-32-32-00007699.0001001 / 12 SEP 11
Applicable to: ALL

32-32-05A Other proximity detectors operative

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
Reference(s)
(o) Refer to OpsProc 32-32-05A LGCIU 2 RH L/G Down Lock Proximity Detector
(m) Refer to AMM 32-31-00-040-003

32-32-05B LGCIU 2 considered inoperative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative for 7 flights provided that the LGCIU 2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)

LAN COLOMBIA FLEET MI-32-32 P 3/12

MEL D to E 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-32-06 LGCIU 2 LH L/G Down Lock Proximity Detector

Ident.: MI-32-32-00007700.0001001 / 12 SEP 11
Applicable to: ALL

32-32-06A Other proximity detectors operative

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
Reference(s)
(o) Refer to OpsProc 32-32-06A LGCIU 2 LH L/G Down Lock Proximity Detector
(m) Refer to AMM 32-31-00-040-003

32-32-06B LGCIU 2 considered inoperative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative for 7 flights provided that the LGCIU 2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)

32-32-07 LGCIU 2 Nose L/G Down Lock Proximity Detector

Ident.: MI-32-32-00007701.0001001 / 12 SEP 11
Applicable to: ALL

32-32-07A Other proximity detectors operative

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
Reference(s)
(o) Refer to OpsProc 32-32-07A LGCIU 2 Nose L/G Down Lock Proximity Detector
(m) Refer to AMM 32-31-00-040-003
Continued on the following page

LAN COLOMBIA FLEET MI-32-32 P 4/12

MEL F to G 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

32-32-07B LGCIU 2 considered inoperative
Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative for 7 flights provided that the LGCIU 2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)

32-32-08 LGCIU 2 RH L/G Up Lock Proximity Detector

Ident.: MI-32-32-00007702.0001001 / 12 SEP 11
Applicable to: ALL

32-32-08A Other proximity detectors operative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
(o) (m) May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
Reference(s)
(o) Refer to OpsProc 32-32-08A LGCIU 2 RH L/G Up Lock Proximity Detector
(m) Refer to AMM 32-31-00-040-003

32-32-08B LGCIU 2 considered inoperative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative for 7 flights provided that the LGCIU 2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)

LAN COLOMBIA FLEET MI-32-32 P 5/12

MEL G to H 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-32-09 LGCIU 2 LH L/G Up Lock Proximity Detector

Ident.: MI-32-32-00007712.0001001 / 12 SEP 11
Applicable to: ALL

32-32-09A Other proximity detectors operative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
(o) (m) May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
Reference(s)
(o) Refer to OpsProc 32-32-09A LGCIU 2 LH L/G Up Lock Proximity Detector
(m) Refer to AMM 32-31-00-040-003

32-32-09B LGCIU 2 considered inoperative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative for 7 flights provided that the LGCIU 2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)

32-32-10 LGCIU 2 Nose L/G Up Lock Proximity Detector

Ident.: MI-32-32-00007726.0001001 / 12 SEP 11
Applicable to: ALL

32-32-10A Other proximity detectors operative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
(o) (m) May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
Reference(s)
(o) Refer to OpsProc 32-32-10A LGCIU 2 Nose L/G Up Lock Proximity Detector
(m) Refer to AMM 32-31-00-040-003
Continued on the following page

LAN COLOMBIA FLEET MI-32-32 P 6/12

MEL I to J 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

32-32-10B LGCIU 2 considered inoperative
Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative for 7 flights provided that the LGCIU 2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)

32-32-11 LGCIU 2 RH L/G Doors Open Proximity Detector

Ident.: MI-32-32-00007727.0001001 / 12 SEP 11
Applicable to: ALL

32-32-11A Other proximity detectors operative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
(o) (m) May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
Reference(s)
(o) Refer to OpsProc 32-32-11A LGCIU 2 RH L/G Doors Open Proximity Detector
(m) Refer to AMM 32-31-00-040-003

32-32-11B LGCIU 2 considered inoperative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative for 7 flights provided that the LGCIU 2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)

LAN COLOMBIA FLEET MI-32-32 P 7/12

MEL J to K 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-32-12 LGCIU 2 LH L/G Doors Open Proximity Detector

Ident.: MI-32-32-00007728.0001001 / 12 SEP 11
Applicable to: ALL

32-32-12A Other proximity detectors operative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
(o) (m) May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
Reference(s)
(o) Refer to OpsProc 32-32-12A LGCIU 2 LH L/G Doors Open Proximity Detector
(m) Refer to AMM 32-31-00-040-003

32-32-12B LGCIU 2 considered inoperative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative for 7 flights provided that the LGCIU 2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)

32-32-13 LGCIU 2 Nose L/G Doors Open Proximity Detector

Ident.: MI-32-32-00007729.0001001 / 12 SEP 11
Applicable to: ALL

32-32-13A Other proximity detectors operative

Repair interval Nbr installed Nbr required Placard
A 2 0 No
(o) (m) One or both may be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
Reference(s)
(o) Refer to OpsProc 32-32-13A LGCIU 2 Nose L/G Doors Open Proximity Detector
(m) Refer to AMM 32-31-00-040-003
Continued on the following page

LAN COLOMBIA FLEET MI-32-32 P 8/12

MEL L to M 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

32-32-13B LGCIU 2 considered inoperative
Repair interval Nbr installed Nbr required Placard
A 2 0 No
One or both may be inoperative for 7 flights provided that the LGCIU 2 is considered
inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)

32-32-14 LGCIU 2 RH L/G Doors Closed Proximity Detector

Ident.: MI-32-32-00007730.0001001 / 12 SEP 11
Applicable to: ALL

32-32-14A Other proximity detectors operative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
(o) (m) May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
Reference(s)
(o) Refer to OpsProc 32-32-14A LGCIU 2 RH L/G Doors Closed Proximity Detector
(m) Refer to AMM 32-31-00-040-003

32-32-14B LGCIU 2 considered inoperative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative for 7 flights provided that the LGCIU 2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)

LAN COLOMBIA FLEET MI-32-32 P 9/12

MEL M to N 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-32-15 LGCIU 2 LH L/G Doors Closed Proximity Detector

Ident.: MI-32-32-00007731.0001001 / 12 SEP 11
Applicable to: ALL

32-32-15A Other proximity detectors operative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
(o) (m) May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
Reference(s)
(o) Refer to OpsProc 32-32-15A LGCIU 2 LH L/G Doors Closed Proximity Detector
(m) Refer to AMM 32-31-00-040-003

32-32-15B LGCIU 2 considered inoperative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative for 7 flights provided that the LGCIU 2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)

32-32-16 LGCIU 2 Nose L/G Doors Closed Proximity Detector

Ident.: MI-32-32-00007732.0001001 / 12 SEP 11
Applicable to: ALL

32-32-16A Other proximity detectors operative

Repair interval Nbr installed Nbr required Placard
A 1 0 No
(o) (m) May be inoperative for 7 flights provided that:
1) The other proximity detectors are operative, and
2) The origin of the failure is checked to be electrical.
Reference(s)
(o) Refer to OpsProc 32-32-16A LGCIU 2 Nose L/G Doors Closed Proximity Detector
(m) Refer to AMM 32-31-00-040-003
Continued on the following page

LAN COLOMBIA FLEET MI-32-32 P 10/12

MEL O to P 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

32-32-16B LGCIU 2 considered inoperative
Repair interval Nbr installed Nbr required Placard
A 1 0 No
May be inoperative for 7 flights provided that the LGCIU 2 is considered inoperative.
Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)

LAN COLOMBIA FLEET MI-32-32 P 11/12

MEL P 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-32-32 P 12/12

MEL 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-33 - Free Fall Extension
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-33-01 Landing Gear Gravity Extension System

Ident.: MI-32-33-00007734.0001001 / 12 SEP 12
Applicable to: ALL

32-33-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) (m) May be inoperative provided that:
1) ETOPS is not conducted, and
2) The aircraft is operated in accordance with the Flight Manual supplement for the flight
with landing gear down.
Reference(s)
(o) Refer to OpsProc 32-33-01A Landing Gear Gravity Extension System
(m) Refer to AMM 32-31-00-040-802

LAN COLOMBIA FLEET MI-32-33 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-33 - Free Fall Extension
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-32-33 P 2/2

MEL 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-41 - Wheels
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-41-01 Nose Wheel Tie Bolt

Ident.: MI-32-41-00007735.0001001 / 12 SEP 12
Applicable to: ALL

32-41-01A
Repair interval Nbr installed Nbr required Placard
A 6 5 No
(m) One tie bolt on one wheel may be broken or missing for 15 flights provided that:
1) The affected wheel tie bolt is removed, and
2) The affected wheel is checked for absence of damage.
Reference(s)
(m) Refer to AMM 32-41-00-040-002

32-41-02 Main Wheel Tie Bolt

Ident.: MI-32-41-00007736.0001001 / 20 JUN 14
Applicable to: ALL

32-41-02A
Repair interval Nbr installed Nbr required Placard
A 8 7 No
(m) One tie bolt on one wheel may be broken or missing for 15 flights provided that:
1) The affected wheel tie bolt is removed, and
2) The affected wheel and the associated brake are checked for absence of damage.
Reference(s)
(m) Refer to AMM Task 32-41-00-040-003

LAN COLOMBIA FLEET MI-32-41 P 1/2

MEL A to B 20 JUN 14
 MEL ITEMS
32 - LANDING GEAR
32-41 - Wheels
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-32-41 P 2/2

MEL 20 JUN 14
 MEL ITEMS
32 - LANDING GEAR
32-42 - Normal Braking
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-42-01 Main Wheel Brake

Ident.: MI-32-42-00007737.0001001 / 27 NOV 12
Applicable to: ALL

32-42-01A
Repair interval Nbr installed Nbr required Placard
C 4 3 No
(o) (m) One may be inoperative provided that:
1) The nose wheel steering is operative, and
2) Both thrust reversers are operative, and
3) The green and yellow systems are operative on operative brakes, and
4) The affected brake is deactivated or removed, and
5) The runway width at departure, alternate and arrival airports are at least 45 m , and
6) The Flight Manual performance penalties are applied.
Reference(s)
(o) Refer to OpsProc 32-42-01A Main Wheel Brake
(m) Refer to AMM 32-42-00-040-003

32-42-02 Green System Brake

Ident.: MI-32-42-00007738.0001001 / 21 MAR 10
Applicable to: ALL

32-42-02A
Repair interval Nbr installed Nbr required Placard
C 1 1 No
(o) (m) Braking on one wheel may be inoperative provided that:
1) The nose wheel steering is operative, and
2) Both thrust reversers are operative, and
3) The green hydraulic supply of affected brake is deactivated, and
4) The runway width at departure and arrival airports is at least 45 m , and
5) The Flight Manual performance penalties are applied.
Reference(s)
(o) Refer to OpsProc 32-42-02A Green System Brake
(m) Refer to AMM 32-42-00-040-002

LAN COLOMBIA FLEET MI-32-42 P 1/4

MEL A to B 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-42 - Normal Braking
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-42-03 Braking/Steering Control Unit ( BSCU ) System 1

Ident.: MI-32-42-00007739.0002001 / 12 SEP 12
Applicable to: ALL

32-42-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(m) ** May be inoperative provided that:
1) The BSCU system 2 is operative, and
2) The affected system is deactivated, and
3) It is checked that the CFDS does not report a fault related to the L/G SYS DISAGREE
alert before each flight, and
4) The AUTO/BRK (LO, MED, MAX) pb-sw DECEL light and the AUTO/BRK (LO, MED,
MAX) pb-sw ON light are considered inoperative.
Refer to Item 32-42-08 AUTO/BRK (LO, MED, MAX) pb-sw DECEL light , and
Refer to Item 32-42-09 AUTO/BRK (LO, MED, MAX) pb-sw ON light
Reference(s)
(m) Refer to AMM 32-42-00-040-007

32-42-04 Braking/Steering Control Unit (BSCU) System 2

Ident.: MI-32-42-00007740.0002001 / 12 SEP 12
Applicable to: ALL

32-42-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(m) ** May be inoperative provided that:
1) The affected system is deactivated, and
2) It is checked that the CFDS does not report a fault related to the L/G SYS DISAGREE
alert before each flight.
Reference(s)
(m) Refer to AMM 32-42-00-040-007

LAN COLOMBIA FLEET MI-32-42 P 2/4

MEL C to D 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-42 - Normal Braking
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-42-05 AUTO/BRK Function

Ident.: MI-32-42-00007741.0001001 / 27 NOV 12
Applicable to: ALL

32-42-05A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative if aircraft is not dispatched to runways less than 1900 mts lenght.
Reference(s)
(o) Refer to OpsProc 32-42-05A AUTO/BRK Function

32-42-06 Tachometer
Ident.: MI-32-42-00007742.0001001 / 21 MAR 10
Applicable to: ALL

32-42-06B
Repair interval Nbr installed Nbr required Placard
4 4 No
Must be operative.

32-42-08 AUTO/BRK (LO, MED, MAX) pb-sw DECEL light

Ident.: MI-32-42-00007744.0001001 / 21 MAR 10
Applicable to: ALL

32-42-08A
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative.

LAN COLOMBIA FLEET MI-32-42 P 3/4

MEL E to G 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-42 - Normal Braking
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-42-09 AUTO/BRK (LO, MED, MAX) pb-sw ON light

Ident.: MI-32-42-00007745.0001001 / 12 SEP 11
Applicable to: ALL

32-42-09A AUTO/BRK mode arming displayed on the WHEEL SD page

Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative provided that, when appropriate, the associated
AUTO/BRK mode arming is displayed on the WHEEL SD page .

32-42-09B AUTO/BRK function considered inoperative

Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative provided that the AUTO/BRK function is considered
inoperative.
Refer to Item 32-42-05 AUTO/BRK Function

LAN COLOMBIA FLEET MI-32-42 P 4/4

MEL H 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-44 - Alternate Braking
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-44-01 Yellow System Brake

Ident.: MI-32-44-00007746.0001001 / 21 MAR 10
Applicable to: ALL

32-44-01A
Repair interval Nbr installed Nbr required Placard
C 1 1 No
(m) Braking on one wheel may be inoperative provided that:
1) Both thrust reversers are operative, and
2) The yellow hydraulic supply of the affected brake is deactivated.
Reference(s)
(m) Refer to AMM 32-43-00-040-001

32-44-02 ACCU PRESS Indicator

Ident.: MI-32-44-00007747.0002001 / 27 FEB 15
Applicable to: ALL

32-44-02A Brakes pressure indicator operative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that:
1) Both brakes pressure indicators are operative, and
2) The pressure on both brakes pressure indicators is checked with parking brake ON
before each flight.

32-44-02B Checks on WHEEL SD page

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that:
1) The ACCU PRESS/ACCU ONLY indication is operative on the WHEEL SD page, and
2) The hydraulic pressure of the brake accumulator is checked on the WHEEL SD page
before each flight.

LAN COLOMBIA FLEET MI-32-44 P 1/2

MEL A to B 27 FEB 15
 MEL ITEMS
32 - LANDING GEAR
32-44 - Alternate Braking
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-44-03 BRAKES Pressure Indicator

Ident.: MI-32-44-00007748.0002001 / 21 MAR 10
Applicable to: ALL

32-44-03A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative provided that the BSCU system 1 and the BSCU system 2
are operative.

32-44-04 Alternate Braking Control Unit (ABCU)

Ident.: MI-32-44-00007749.0003001 / 27 FEB 15
Applicable to: ALL

32-44-04A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

LAN COLOMBIA FLEET MI-32-44 P 2/2

MEL C to D 27 FEB 15
 MEL ITEMS
32 - LANDING GEAR
32-45 - Parking/Ultimate Emergency Braking
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-45-01 Parking Brake Control Valve Electrical Motor

Ident.: MI-32-45-00007750.0001001 / 21 MAR 10
Applicable to: ALL

32-45-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(m) One may be inoperative provided that:
1) Both thrust reversers are operative, and
2) The aircraft is not towed if the STBY motor is affected and when the batteries supply the
aircraft.
Reference(s)
(m) Refer to AMM 32-45-00-040-001

LAN COLOMBIA FLEET MI-32-45 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-45 - Parking/Ultimate Emergency Braking
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-32-45 P 2/2

MEL 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-47 - Brake Temperature System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-47-01 Brake Temperature Monitoring Unit ( BTMU )

Ident.: MI-32-47-00007751.0001001 / 21 MAR 10
Applicable to: ALL

32-47-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) One or both may be inoperative provided that the ground brake cooling time is applied.
Reference(s)
(o) Refer to OpsProc 32-47-01A Brake Temperature Monitoring Unit (BTMU)

LAN COLOMBIA FLEET MI-32-47 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-47 - Brake Temperature System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-32-47 P 2/2

MEL 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-48 - Brake Cooling
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-48-01 Brake Fan System

Ident.: MI-32-48-00007752.0001001 / 18 MAY 11
Applicable to: ALL

32-48-01A
Repair interval Nbr installed Nbr required Placard
D 1 0 Yes
May be inoperative.

32-48-02 BRK FAN pb-sw HOT light

Ident.: MI-32-48-00007753.0001001 / 18 MAY 11
Applicable to: ALL

32-48-02A
Repair interval Nbr installed Nbr required Placard
D 1 0 Yes
May be inoperative.

32-48-03 BRK FAN pb-sw ON light

Ident.: MI-32-48-00007754.0001001 / 18 MAY 11
Applicable to: ALL

32-48-03A
Repair interval Nbr installed Nbr required Placard
D 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-32-48 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-48 - Brake Cooling
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-32-48 P 2/2

MEL 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-51 - Steering
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-51-01 Nose Wheel Steering Control System

Ident.: MI-32-51-00007755.0002001 / 27 NOV 12
Applicable to: ALL

32-51-01A
Repair interval Nbr installed Nbr required Placard
A 1 0 Yes
(o) ** May be inoperative for three flights provided that:
1) The failure is detected by the BSCU (the WHEEL N/W STRG FAULT alert is displayed
on the EWD ), and
2) The runway width at departure, alternate and arrival airports is at least 45 m , and
3) The runway is not contaminated, and
4) The crosswind component is below 20 kt at departure and arrival airports, and
5) Revenue flight is not dispatched.
Note: For nose wheel steering offset, Refer to FCOM/PRO-SUP-32 Operation with
Nosewheel Steering Offset .
Reference(s)
(o) Refer to OpsProc 32-51-01A Nose Wheel Steering Control System

32-51-02 Rudder PEDALS DISC pb

Ident.: MI-32-51-00007756.0001001 / 14 SEP 10
Applicable to: ALL

32-51-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(o) One or both may be inoperative (no disconnection is possible).
Reference(s)
(o) Refer to OpsProc 32-51-02A Rudder PEDALS DISC pb

LAN COLOMBIA FLEET MI-32-51 P 1/4

MEL A to B 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-51 - Steering
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-51-03 NWS Electrical Deactivation Box

Ident.: MI-32-51-00007757.0001001 / 12 SEP 11
Applicable to: ALL

32-51-03A No towing mode when lever in the TOWING position

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative.
Note: The towing mode is not available when the lever is in the TOWING position.
Reference(s)
(o) Refer to OpsProc 32-51-03A NWS Electrical Deactivation Box (towing mode is not available
when the lever is in the TOWING position)

32-51-03B NWS electrical deactivation box deactivated

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that the NWS electrical deactivation box is deactivated.
Reference(s)
(o) Refer to OpsProc 32-51-03B NWS Electrical Deactivation Box (NWS Electrical Deactivation
Box deactivated)
(m) Refer to AMM 32-51-00-040-002

32-51-04 PARKING BRAKE light on the NWS Electrical Deactivation Box

Ident.: MI-32-51-00007758.0001001 / 21 MAR 10
Applicable to: ALL

32-51-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative.
Continued on the following page

LAN COLOMBIA FLEET MI-32-51 P 2/4

MEL C to D 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-51 - Steering
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 32-51-04A PARKING BRAKE light on the NWS Electrical Deactivation
Box

LAN COLOMBIA FLEET MI-32-51 P 3/4

MEL D 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-51 - Steering
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-32-51 P 4/4

MEL 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-61 - Landing Gear Panel on the Center Instrument Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-61-01 LDG GEAR Indicator Panel

Ident.: MI-32-61-00007759.0001001 / 21 MAR 10
Applicable to: ALL

32-61-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

32-61-02 DOWN Red Arrow light on the Landing Gear lever

Ident.: MI-32-61-00007760.0001001 / 14 SEP 10
Applicable to: ALL

32-61-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that the L/G GEAR NOT DOWN alert and the L/G GEAR NOT
DOWNLOCKED alert are checked operative.
Reference(s)
(m) Refer to AMM 32-61-00-040-001

LAN COLOMBIA FLEET MI-32-61 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
32 - LANDING GEAR
32-61 - Landing Gear Panel on the Center Instrument Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-32-61 P 2/2

MEL 05 NOV 13
 MEL ITEMS
33 - LIGHTS
33-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 33-01-01 - ANN LT Overhead Panel
MINIMUM EQUIPMENT LIST

33-01-01-01 TEST Function of ANN LT sw

Ident.: MI-33-01-01-00007633.0001001 / 21 MAR 10
Applicable to: ALL

33-01-01-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.

33-01-01-02 DIM Function of ANN LT sw

Ident.: MI-33-01-01-00007635.0001001 / 21 MAR 10
Applicable to: ALL

33-01-01-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
Dim lighting may be inoperative provided that the bright lighting is operative.

33-01-01-03 BRT Function of ANN LT sw

Ident.: MI-33-01-01-00007636.0001001 / 21 MAR 10
Applicable to: ALL

33-01-01-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
Bright lighting may be inoperative for night operation.

LAN COLOMBIA FLEET MI-33-01-01 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
33 - LIGHTS
33-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 33-01-01 - ANN LT Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-33-01-01 P 2/2

MEL 05 NOV 13
 MEL ITEMS
33 - LIGHTS
33-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 33-01-02 - SIGNS Overhead Panel
MINIMUM EQUIPMENT LIST

33-01-02-01 EMER EXIT LT OFF light

Ident.: MI-33-01-02-00007637.0001001 / 12 SEP 12
Applicable to: ALL

33-01-02-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

33-01-02-02 AUTO Function of SEAT BELT SIGNS sw

Ident.: MI-33-01-02-00007638.0001001 / 18 MAY 11
Applicable to: ALL

33-01-02-02A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 33-01-02-02A AUTO Function of SEAT BELT SIGNS selector

33-01-02-03 AUTO Function of NO SMOKING SIGNS sw

Ident.: MI-33-01-02-00007639.0001001 / 21 MAR 10
Applicable to: ALL

33-01-02-03A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
(o) May be inoperative.
Reference(s)
(o) Refer to OpsProc 33-01-02-03A AUTO Function of NO SMOKING/EXIT/NO PORTABLE
SIGNS selector

LAN COLOMBIA FLEET MI-33-01-02 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
33 - LIGHTS
33-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 33-01-02 - SIGNS Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-33-01-02 P 2/2

MEL 05 NOV 13
 MEL ITEMS
33 - LIGHTS
33-10 - Cockpit General Illumination
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

33-10-01 Cockpit General Illumination (Center & Main Instrument

Lighting, Console and Floor Lighting, Dome lights
and Lighting Strips, Instrument and Panel Integral
Lighting, Map Holder Lighting, Center Pedestal Lighting)
Ident.: MI-33-10-00007640.0004001 / 27 FEB 15
Applicable to: ALL

33-10-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that:
1) The lighting is sufficient for all instruments and controls, and
2) The RH dome light is operative.

LAN COLOMBIA FLEET MI-33-10 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
33 - LIGHTS
33-10 - Cockpit General Illumination
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-33-10 P 2/2

MEL 27 FEB 15
 MEL ITEMS
33 - LIGHTS
33-20 - Cabin General Illumination
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

33-20-01 Cabin General Illumination

Ident.: MI-33-20-00007641.0001001 / 02 NOV 11
Applicable to: ALL

33-20-01A
Repair interval Nbr installed Nbr required Placard
C 3 0 No
The lighting must be sufficient for cabin attendants to perform their duties.

33-20-02 Cabin Signs (No Smoking/No Electronic

Devices/Fasten Seat Belt/Return to Seat)
Ident.: MI-33-20-00007642.0001001 / 10 OCT 14
Applicable to: ALL

33-20-02A Affected seat occupied

Repair interval Nbr installed Nbr required Placard
C 41 0 No
One or more may be inoperative and the affected passenger seat may be occupied
provided that:
1) The passenger address system is operative, and can be heard throughout the cabin
during the flight, and
2) The passenger address system is used to alert the passengers when return to seat is
requested, seat belts should be fastened and smoking is prohibited.

33-20-02B Affected seat not occupied

Repair interval Nbr installed Nbr required Placard
C 41 Yes
(m) One or more No Smoking/No Electronic Devices/Fasten Seat Belt sign may be inoperative
provided that:
1) No passenger seat is occupied from which a passenger cannot see a readily legible No
smoking/No Electronic Devices/Fasten Seat Belt sign, and
2) The affected seat is blocked and placarded inoperative.
Continued on the following page

LAN COLOMBIA FLEET MI-33-20 P 1/2

MEL A to B 10 OCT 14
 MEL ITEMS
33 - LIGHTS
33-20 - Cabin General Illumination
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(m) Refer to AMM Task 33-20-00-040-001

33-20-03 Lavatory Sign (Return to seat)

Ident.: MI-33-20-00007643.0001001 / 10 OCT 14
Applicable to: ALL

33-20-03A
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
(o) One or more may be inoperative and the affected lavatory may be used provided that:
1) The passenger address system is checked operative in the affected lavatory, and
2) The passenger address system is used to alert the occupant to return to his seat.
Reference(s)
(o) Refer to OpsProc 33-20-03A Lavatory Sign (Return to seat)

LAN COLOMBIA FLEET MI-33-20 P 2/2

MEL B to C 10 OCT 14
 MEL ITEMS
33 - LIGHTS
33-30 - Cargo and Service Compartment Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

33-30-01 Cargo and Service Compartment Lighting System

Ident.: MI-33-30-00007644.0001001 / 21 MAR 10
Applicable to: ALL

33-30-01A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-33-30 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
33 - LIGHTS
33-30 - Cargo and Service Compartment Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-33-30 P 2/2

MEL 05 NOV 13
 MEL ITEMS
33 - LIGHTS
33-40 - Exterior Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

33-40-01 Navigation light System 1

Ident.: MI-33-40-00007645.0002001 / 12 SEP 12
Applicable to: ALL

33-40-01A Navigation light system 1 and 2 inoperative

Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative for daylight operations.

33-40-01B Navigation light system 2 operative

Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative provided that the Navigation light system 2 is operative.

33-40-02 Navigation light System 2

Ident.: MI-33-40-00007646.0001001 / 21 MAR 10
Applicable to: ALL

33-40-02A
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative.

33-40-03 Landing light

Ident.: MI-33-40-00007647.0001001 / 12 SEP 12
Applicable to: ALL

33-40-03A Taxi and takeoff lights operative

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
One may be inoperative provided that both taxi and takeoff lights are operative.
Continued on the following page

LAN COLOMBIA FLEET MI-33-40 P 1/6

MEL A to C 05 NOV 13
 MEL ITEMS
33 - LIGHTS
33-40 - Exterior Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

33-40-03B Daylight operations
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative for daylight operations.

33-40-04 Landing light Extension/Retraction System

Ident.: MI-33-40-00007651.0001001 / 12 SEP 11
Applicable to: ALL

33-40-04A Inoperative in extended position

Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) One or both may be inoperative in the extended position.
Reference(s)
(o) Refer to OpsProc 33-40-04A Landing light Extension/Retraction System

33-40-04B Inoperative in retracted position

Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative in the retracted position provided that the associated light is
considered inoperative.
Refer to Item 33-40-03 Landing light

LAN COLOMBIA FLEET MI-33-40 P 2/6

MEL C to D 05 NOV 13
 MEL ITEMS
33 - LIGHTS
33-40 - Exterior Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

33-40-05 Runway Turnoff light

Ident.: MI-33-40-00007654.0001001 / 21 MAR 10
Applicable to: ALL

33-40-05A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

33-40-06 Taxi and Takeoff light

Ident.: MI-33-40-00007657.0001001 / 21 MAR 10
Applicable to: ALL

33-40-06A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

33-40-07 Logo light

Ident.: MI-33-40-00007658.0001001 / 21 MAR 10
Applicable to: ALL

33-40-07A
Repair interval Nbr installed Nbr required Placard
D 2 0 Yes
One or both may be inoperative.

LAN COLOMBIA FLEET MI-33-40 P 3/6

MEL E to G 05 NOV 13
 MEL ITEMS
33 - LIGHTS
33-40 - Exterior Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

33-40-08 Beacon light

Ident.: MI-33-40-00007659.0002001 / 12 SEP 11
Applicable to: ALL

33-40-08A Daylight operations

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(o) One or both may be inoperative for daylight operations.
Reference(s)
(o) Refer to OpsProc 33-40-08A Beacon light

33-40-08B Strobe lights operative

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(o) One or both may be inoperative provided that the Strobe lights are operative.
Reference(s)
(o) Refer to OpsProc 33-40-08B Beacon light

33-40-09 Wing Scan light

Ident.: MI-33-40-00007662.0001001 / 12 SEP 11
Applicable to: ALL

33-40-09A Daylight operations

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative for daylight operations.

33-40-09B Night operations

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
One may be inoperative for night operations.

LAN COLOMBIA FLEET MI-33-40 P 4/6

MEL H to I 05 NOV 13
 MEL ITEMS
33 - LIGHTS
33-40 - Exterior Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

33-40-10 Strobe light

Ident.: MI-33-40-00007664.0001001 / 21 MAR 10
Applicable to: ALL

33-40-10A
Repair interval Nbr installed Nbr required Placard
D 3 0 Yes
One or more may be inoperative.

LAN COLOMBIA FLEET MI-33-40 P 5/6

MEL J 05 NOV 13
 MEL ITEMS
33 - LIGHTS
33-40 - Exterior Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-33-40 P 6/6

MEL 05 NOV 13
 MEL ITEMS
33 - LIGHTS
33-51 - Cabin Emergency Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

33-51-01 Exit Marking Sign

Ident.: MI-33-51-00007667.0004001 / 10 OCT 14
Applicable to: ALL

33-51-01B A maximum of three non-adjacent LED s inoperative

Repair interval Nbr installed Nbr required Placard
C 6 6 No
A maximum of three non-adjacent LED s may be inoperative in one or more signs.

33-51-01C Associated exit considered inoperative

Repair interval Nbr installed Nbr required Placard
B 6 5 No
One may be inoperative provided that the associated exit is considered inoperative.
Refer to Item 52-10-01 Cabin Passenger Door , and
Refer to Item 52-10-02 Overwing Emergency Exit

33-51-02 Exit Location Sign in the Main Aisle

Ident.: MI-33-51-00007668.0002001 / 10 OCT 14
Applicable to: ALL

33-51-02A
Repair interval Nbr installed Nbr required Placard
C 2 2 No
A maximum of three non-adjacent LEDs may be inoperative in one or more signs.

LAN COLOMBIA FLEET MI-33-51 P 1/6

MEL A to B 27 FEB 15
 MEL ITEMS
33 - LIGHTS
33-51 - Cabin Emergency Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

33-51-03 Overhead Emergency Lighting System in the Main Aisle

Ident.: MI-33-51-00007669.0001001 / 27 FEB 15
Applicable to: ALL

33-51-03A
Repair interval Nbr installed Nbr required Placard
C 8 5 No
A maximum of three non-adjacent overhead emergency lights may be inoperative.

33-51-04 Overhead Emergency Lighting System in the Door Vicinity

Ident.: MI-33-51-00007670.0004001 / 10 OCT 14
Applicable to: ALL

33-51-04A
Repair interval Nbr installed Nbr required Placard
No
One or more may be inoperative provided that the associated exit is considered inoperative.
Refer to Item 52-10-01 Cabin Passenger Door

LAN COLOMBIA FLEET MI-33-51 P 2/6

MEL C to D 27 FEB 15
 MEL ITEMS
33 - LIGHTS
33-51 - Cabin Emergency Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

33-51-05 Floor Proximity Emergency Escape

Path Marking System in the Main Aisle
Ident.: MI-33-51-00007671.0001001 / 02 NOV 11
Applicable to: ALL

33-51-05A
Repair interval Nbr installed Nbr required Placard
C 1 1 No
Each of the photoluminescent strips of an aisle may be partly inoperative up to a 25% of its
length provided:
1) None of the inoperative strips are adjacent to each other, and
2) None of the inoperative strips are closer than 2.0 m. between them.
3) The inoperative strips are not in the intersection with the cross aisle floor strip.
4) The inoperative strips are not directly opposite to each other.
5) No more than 4 such inoperative parts are allowed.
Note: A photoluminescent strip has a maximum length of 1,4 meters.
Note: Cabin crew must be briefed of this situation.

33-51-07 Floor Proximity Emergency Escape Path Marking System Exit Marker
Ident.: MI-33-51-00007673.0001001 / 10 OCT 14
Applicable to: ALL

33-51-07A
Repair interval Nbr installed Nbr required Placard
B 8 7 No
One may be inoperative provided that the associated exit is considered inoperative.
Refer to Item 52-10-01 Cabin Passenger Door , and
Refer to Item 52-10-02 Overwing Emergency Exit

LAN COLOMBIA FLEET MI-33-51 P 3/6

MEL E to F 27 FEB 15
 MEL ITEMS
33 - LIGHTS
33-51 - Cabin Emergency Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

33-51-08 Overwing Emergency light

Ident.: MI-33-51-00007674.0001001 / 10 OCT 14
Applicable to: ALL

33-51-08A Daylight operations

Repair interval Nbr installed Nbr required Placard
C 4 0 No
One or more may be inoperative for daylight operations.

33-51-08B Associated exit considered inoperative

Repair interval Nbr installed Nbr required Placard
B 4 3 No
One or more may be inoperative provided that the associated exit is considered inoperative.
Refer to Item 52-10-02 Overwing Emergency Exit

33-51-09 Overwing Exit Handle light

Ident.: MI-33-51-00007675.0001001 / 10 OCT 14
Applicable to: ALL

33-51-09A
Repair interval Nbr installed Nbr required Placard
C 4 0 No
One or more may be inoperative.

33-51-10 Escape Slide Lighting

Ident.: MI-33-51-00007676.0001001 / 10 OCT 14
Applicable to: ALL

33-51-10A Daylight operations

Repair interval Nbr installed Nbr required Placard
C 6 0 No
May be inoperative for daylight operations.
Continued on the following page

LAN COLOMBIA FLEET MI-33-51 P 4/6

MEL G to I 27 FEB 15
 MEL ITEMS
33 - LIGHTS
33-51 - Cabin Emergency Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

33-51-10B Associated exit considered inoperative
Repair interval Nbr installed Nbr required Placard
B 6 5 No
May be inoperative provided that the associated exit is considered inoperative.
Refer to Item 52-10-01 Cabin Passenger Door , and
Refer to Item 52-10-02 Overwing Emergency Exit

33-51-11 Lavatory Auxiliary light

Ident.: MI-33-51-00007677.0001001 / 10 OCT 14
Applicable to: ALL

33-51-11A
Repair interval Nbr installed Nbr required Placard
C 3 0 No
One or more may be inoperative.

LAN COLOMBIA FLEET MI-33-51 P 5/6

MEL I to J 27 FEB 15
 MEL ITEMS
33 - LIGHTS
33-51 - Cabin Emergency Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-33-51 P 6/6

MEL 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-00 - MAINTENANCE Messages on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-00-01 ADR MAINTENANCE Message

Ident.: MI-34-00-00008503.0002001 / 27 FEB 15
Applicable to: ALL

34-00-01A
Repair interval Nbr installed Nbr required Placard
C No
ADR MAINTENANCE message may be displayed on the STATUS SD page.

34-00-02 IR MAINTENANCE Message

Ident.: MI-34-00-00008504.0001001 / 21 MAR 10
Applicable to: ALL

34-00-02A
Repair interval Nbr installed Nbr required Placard
C No
IR MAINTENANCE message may be displayed on the STATUS SD page.

LAN COLOMBIA FLEET MI-34-00 P 1/2

MEL A to B 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-00 - MAINTENANCE Messages on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-34-00 P 2/2

MEL 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 34-01-01 - ADIRS Overhead Panel
MINIMUM EQUIPMENT LIST

34-01-01-01 ADR pb-sw FAULT light

Ident.: MI-34-01-01-00008505.0001001 / 21 MAR 10
Applicable to: ALL

34-01-01-01A
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative.

34-01-01-02 ADR pb-sw OFF light

Ident.: MI-34-01-01-00008506.0001001 / 21 MAR 10
Applicable to: ALL

34-01-01-02A
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative.

34-01-01-03 IR pb-sw FAULT light

Ident.: MI-34-01-01-00008509.0002001 / 27 FEB 15
Applicable to: ALL

34-01-01-03A
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative.

LAN COLOMBIA FLEET MI-34-01-01 P 1/4

MEL A to C 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 34-01-01 - ADIRS Overhead Panel
MINIMUM EQUIPMENT LIST

34-01-01-04 IR pb-sw OFF light

Ident.: MI-34-01-01-00008510.0002001 / 27 FEB 15
Applicable to: ALL

34-01-01-04A
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative.

34-01-01-05 ON BAT light

Ident.: MI-34-01-01-00008511.0001001 / 21 MAR 10
Applicable to: ALL

34-01-01-05A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

34-01-01-31 ADR pb-sw

Ident.: MI-34-01-01-00008512.0001001 / 21 MAR 10
Applicable to: ALL

34-01-01-31A
Repair interval Nbr installed Nbr required Placard
C 3 2 Yes
(o) ADR 2 or ADR 3 pb-sw may be inoperative provided that:
1) The associated mode selector is operative, and
2) The two ADR s and the two IR s associated with the two operative ADRs pb-sw are
operative.
Reference(s)
(o) Refer to OpsProc 34-01-01-31A ADR pb-sw

LAN COLOMBIA FLEET MI-34-01-01 P 2/4

MEL D to F 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 34-01-01 - ADIRS Overhead Panel
MINIMUM EQUIPMENT LIST

34-01-01-32 IR pb-sw
Ident.: MI-34-01-01-00008513.0001001 / 27 FEB 15
Applicable to: ALL

34-01-01-32A
Repair interval Nbr installed Nbr required Placard
C 3 2 Yes
(o) IR 2 or IR 3 pb-sw may be inoperative provided that:
1) The associated mode selector is operative, and
2) The two ADR s and the two IR s associated with the two operative IRs pb-sw are
operative.
Reference(s)
(o) Refer to OpsProc 34-01-01-32A IR pb-sw

34-01-01-33 IR Mode selector

Ident.: MI-34-01-01-00008516.0002001 / 27 FEB 15
Applicable to: ALL

34-01-01-33A
Repair interval Nbr installed Nbr required Placard
C 3 2 Yes
One may be inoperative.

LAN COLOMBIA FLEET MI-34-01-01 P 3/4

MEL G to H 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 34-01-01 - ADIRS Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-34-01-01 P 4/4

MEL 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 34-01-02 - GPWS Overhead Panel
MINIMUM EQUIPMENT LIST

34-01-02-01 GPWS SYS FAULT light

Ident.: MI-34-01-02-00008534.0001001 / 05 NOV 13
Applicable to: ALL

34-01-02-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided GPWS is considered inoperative. Refer to Item 34-40-01
Ground Proximity Warning System (GPWS)/Terrain Awareness and Warning System
(TAWS)

LAN COLOMBIA FLEET MI-34-01-02 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
34 - NAVIGATION
34-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 34-01-02 - GPWS Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-34-01-02 P 2/2

MEL 05 NOV 13
 MEL ITEMS
34 - NAVIGATION
34-05 - Indications on the Primary Flight Display (PFD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-05-01 Actual Airspeed Reference Line and Scale Indication on the PFD
Ident.: MI-34-05-00008711.0001001 / 21 MAR 10
Applicable to: ALL

34-05-01A
Repair interval Nbr installed Nbr required Placard
2 2 No
Both must be operative.

34-05-02 Mach Number Indication on the PFD

Ident.: MI-34-05-00008712.0002001 / 27 FEB 15
Applicable to: ALL

34-05-02A One indication inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative.

34-05-02B Both indications inoperative - FCU operative

Repair interval Nbr installed Nbr required Placard
C 2 0 No
Both may be inoperative provided that the SPD/MACH selection window on the FCU is
operative.

34-05-02C Both indications inoperative - FL limitation

Repair interval Nbr installed Nbr required Placard
C 2 0 No
Both may be inoperative provided that the flight altitude is limited to 25 000 ft.
Continued on the following page

LAN COLOMBIA FLEET MI-34-05 P 1/4

MEL A to B 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-05 - Indications on the Primary Flight Display (PFD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

34-05-02D Both indications inoperative - ISIS Mach Number Indication operative
Repair interval Nbr installed Nbr required Placard
C 2 0 No
Both may be inoperative provided that the ISIS Mach Number indication is operative.

34-05-03 VMO/MMO Characteristic Speed Indication on the PFD

Ident.: MI-34-05-00008713.0001001 / 21 MAR 10
Applicable to: ALL

34-05-03A
Repair interval Nbr installed Nbr required Placard
2 2 No
Both must be operative.

34-05-04 Altitude Indication on the PFD

Ident.: MI-34-05-00008714.0001001 / 21 MAR 10
Applicable to: ALL

34-05-04A
Repair interval Nbr installed Nbr required Placard
2 2 No
Both must be operative.

34-05-05 Baro Reference Indication on the PFD

Ident.: MI-34-05-00008715.0001001 / 12 SEP 11
Applicable to: ALL

34-05-05A
Repair interval Nbr installed Nbr required Placard
2 2 No
Both must be operative.

LAN COLOMBIA FLEET MI-34-05 P 2/4

MEL B to E 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-05 - Indications on the Primary Flight Display (PFD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-05-06 Vertical Speed in Inertial Mode Indication on the PFD

Ident.: MI-34-05-00008716.0001001 / 21 MAR 10
Applicable to: ALL

34-05-06A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

34-05-07 Other Air Data Related Indications on the PFD

Ident.: MI-34-05-00008717.0001001 / 02 NOV 11
Applicable to: ALL

34-05-07A
Repair interval Nbr installed Nbr required Placard
C 6 0 No
(o) One or more may be inoperative.
Reference(s)
(o) Refer to OpsProc 34-05-07A Other Air Data Related Indications on the PFD

34-05-08 Attitude Indication on the PFD

Ident.: MI-34-05-00008718.0001001 / 23 MAR 11
Applicable to: ALL

34-05-08A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) **
One may be inoperative provided that:
1) ETOPS is not conducted, and
2) The aircraft is operated in day VMC conditions.
Continued on the following page

LAN COLOMBIA FLEET MI-34-05 P 3/4

MEL F to H 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-05 - Indications on the Primary Flight Display (PFD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 34-05-08A Attitude Indication on the PFD

34-05-09 Heading Indication on the PFD

Ident.: MI-34-05-00008719.0001001 / 21 MAR 10
Applicable to: ALL

34-05-09A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative.

LAN COLOMBIA FLEET MI-34-05 P 4/4

MEL H to I 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-06 - Indications on the Navigation Display (ND)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-06-01 Ground Speed Indication on the ND

Ident.: MI-34-06-00008720.0001001 / 21 MAR 10
Applicable to: ALL

34-06-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

34-06-02 True Air Speed Indication on the ND

Ident.: MI-34-06-00008721.0001001 / 21 MAR 10
Applicable to: ALL

34-06-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

34-06-03 Wind Indication on the ND

Ident.: MI-34-06-00008722.0001001 / 21 MAR 10
Applicable to: ALL

34-06-03A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

LAN COLOMBIA FLEET MI-34-06 P 1/4

MEL A to C 05 NOV 13
 MEL ITEMS
34 - NAVIGATION
34-06 - Indications on the Navigation Display (ND)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-06-04 Heading Indication on the ND

Ident.: MI-34-06-00008723.0001001 / 14 SEP 10
Applicable to: ALL

34-06-04A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative provided that the heading indications are operative on both PFDs.

34-06-05 Position (Aircraft Symbol) Indication on the ND

Ident.: MI-34-06-00008724.0001001 / 05 APR 12
Applicable to: ALL

Note: RNAV item.

RNP item.

34-06-05A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
Except for RNAV -1, RNAV -5, RNAV ( GNSS ) and RNAV ( RNP ) operations, both may
be inoperative.

34-06-05B
Repair interval Nbr installed Nbr required Placard
C 2 1 No
For RNAV -1, RNAV -5 and RNAV ( GNSS ) operations, one must be operative on Pilot
Flying Side.
Continued on the following page

LAN COLOMBIA FLEET MI-34-06 P 2/4

MEL D to E 05 NOV 13
 MEL ITEMS
34 - NAVIGATION
34-06 - Indications on the Navigation Display (ND)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

34-06-05C
Repair interval Nbr installed Nbr required Placard
2 2 No
Both must be operative for RNAV ( RNP ) operations.

34-06-06 Radio Navaids Indications on the ND

Ident.: MI-34-06-00008725.0001001 / 12 DEC 11
Applicable to: ALL

34-06-06A
Repair interval Nbr installed Nbr required Placard
C 8 3 No
Radio Navaids indications required for the intended flight must be operative.

34-06-07 Chrono Indication on the ND

Ident.: MI-34-06-00008726.0001001 / 21 MAR 10
Applicable to: ALL

34-06-07A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

LAN COLOMBIA FLEET MI-34-06 P 3/4

MEL E to G 05 NOV 13
 MEL ITEMS
34 - NAVIGATION
34-06 - Indications on the Navigation Display (ND)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-34-06 P 4/4

MEL 05 NOV 13
 MEL ITEMS
34 - NAVIGATION
34-10 - Air Data/Inertial Reference System (ADIRS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-10-01 ADR 1
Ident.: MI-34-10-00008541.0001001 / 12 SEP 12
Applicable to: ALL

Note: RVSM item.

Note: RVSM operation is ensured due to the minimum equipment is covered in the remark of this
Item.

34-10-01A
Repair interval Nbr installed Nbr required Placard
1 1 No
**
Must be operative.

34-10-02 ADR 2
Ident.: MI-34-10-00008542.0001001 / 10 OCT 14
Applicable to: ALL

Note: RVSM item.

Note: RVSM operation is ensured due to the minimum equipment is covered in the remark of this
Item.

34-10-02B
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) **
May be inoperative provided that:
1) The IR 1, IR 3, ADR 1 and ADR 3 are operative, and
2) The takeoff is not performed in CONF 1+F.
Continued on the following page

LAN COLOMBIA FLEET MI-34-10 P 1/10

MEL A to B 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-10 - Air Data/Inertial Reference System (ADIRS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 34-10-02B ADR 2

34-10-03 ADR 3
Ident.: MI-34-10-00008545.0001001 / 01 AUG 13
Applicable to: ALL

Note: RVSM item.

Note: For RVSM Operations, CC-COF must have ADR 1 and ADR 2 operative.
Note: RVSM operation is ensured due to the minimum equipment is covered in the remark of this
Item.

34-10-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) **
May be inoperative provided that the IR 1, IR 2, ADR 1 and ADR 2 are operative.
Reference(s)
(o) Refer to OpsProc 34-10-03A ADR 3

34-10-04 IR 1
Ident.: MI-34-10-00008547.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

Note: RNAV item.

Note: RNP item.

Continued on the following page

LAN COLOMBIA FLEET MI-34-10 P 2/10

MEL B to D 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-10 - Air Data/Inertial Reference System (ADIRS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

34-10-04B GPS 1 operative
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) ** The NAV mode may be inoperative provided that:
1) The IR 1 is operated in ATT mode, and
2) The IR 2 and IR 3 are operative, and
3) The GPS 1 is operative, and
4) The terrain function of the TAWS is considered inoperative.
Refer to Item 34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness
and Warning System (TAWS)
5) Do not perform RNAV ( RNP ) and RNAV ( GNSS ) operations.
Reference(s)
(o) Refer to OpsProc 34-10-04B IR 1 (only NAV mode of IR 1 inoperative)

34-10-04C GPS 1 inoperative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) ** The NAV mode may be inoperative provided that:
1) The IR 1 is operated in ATT mode, and
2) The IR 2 and IR 3 are operative, and
3) The Flight remains within radio navaids coverage, and
4) The terrain function of the TAWS is considered inoperative.
Refer to Item 34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness
and Warning System (TAWS)
5) Do not perform RNAV ( RNP ) and RNAV ( GNSS ) operations.
Reference(s)
(o) Refer to OpsProc 34-10-04C IR 1 (only NAV mode of IR 1 inoperative)
Continued on the following page

LAN COLOMBIA FLEET MI-34-10 P 3/10

MEL D 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-10 - Air Data/Inertial Reference System (ADIRS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

34-10-04D
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative for RNAV ( RNP ) and RNAV ( GNSS ) operations.

34-10-04 IR 1
Ident.: MI-34-10-00008547.0006001 / 10 OCT 14
Applicable to: MSN 4516-4546

Note: RNAV item.

Note: RNP item.

34-10-04B GPS 1 operative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) ** The NAV mode may be inoperative provided that:
1) The IR 1 is operated in ATT mode, and
2) The IR 2 and IR 3 are operative, and
3) The GPS 1 is operative, and
4) The terrain function of the TAWS is considered inoperative
Refer to Item 34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness
and Warning System (TAWS) , and
5) Do not perform RNAV ( RNP ) and RNAV ( GNSS ) operations.
6) The FMGC 1 is considered inoperative.
Refer to Item 22-83-01 Flight Management and Guidance Computer (FMGC)
Reference(s)
(o) Refer to OpsProc 34-10-04B IR 1 (only NAV mode of IR 1 inoperative)
Continued on the following page

LAN COLOMBIA FLEET MI-34-10 P 4/10

MEL D 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-10 - Air Data/Inertial Reference System (ADIRS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

34-10-04C GPS 1 inoperative
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) ** The NAV mode may be inoperative provided that:
1) The IR 1 is operated in ATT mode, and
2) The IR 2 and IR 3 are operative, and
3) The Flight remains within radio navaids coverage, and
4) The terrain function of the TAWS is considered inoperative
Refer to Item 34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness
and Warning System (TAWS) , and
5) Do not perform RNAV ( RNP ) and RNAV ( GNSS ) operations.
6) The FMGC 1 is considered inoperative.
Refer to Item 22-83-01 Flight Management and Guidance Computer (FMGC)
Reference(s)
(o) Refer to OpsProc 34-10-04C IR 1 (only NAV mode of IR 1 inoperative)

34-10-04D
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative for RNAV ( RNP ) and RNAV ( GNSS ) operations.

34-10-05 IR 2
Ident.: MI-34-10-00008549.0013001 / 10 OCT 14
Applicable to: MSN 4516-4546

Note: RNAV item.

Note: RNP item.
Note: For RNP -10 Operations: a) IR 2 may be inoperative without flight time limitations if one
GPS is operative. b) IR 2 may be inoperative if both GPS are inoperative with the following
limitations: 1) 6.2 hours since IRS Ground Alignment, or 2) 5.7 hours since last FM radio
update.
Continued on the following page

LAN COLOMBIA FLEET MI-34-10 P 5/10

MEL D to E 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-10 - Air Data/Inertial Reference System (ADIRS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Note: For RNAV -1 and RNAV -5 Operations: IR 2 may be inoperative.

34-10-05B IR 2 totally inoperative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) ** May be inoperative provided that:
1) The IR 2 pb-sw is set to OFF, and
2) The IR 1, the IR 3, and two ADR s are operative, and
3) The FMGC 2 is considered inoperative. Refer to Item 22-83-01 Flight Management and
Guidance Computer (FMGC)
4) Do not perform RNAV ( RNP ) and RNAV ( GNSS ) operations.
Reference(s)
(o) Refer to OpsProc 34-10-05B IR 2 (IR 2 totally inoperative)

34-10-05C Only NAV mode of IR 2 inoperative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) ** The NAV mode may be inoperative provided that:
1) The IR 2 is operated in ATT mode, and
2) The IR 1 and the IR 3 are operative.
3) Do not perform RNAV ( RNP ) and RNAV ( GNSS ) operations.
4) The FMGC 2 is considered inoperative.
Refer to Item 22-83-01 Flight Management and Guidance Computer (FMGC)
Reference(s)
(o) Refer to OpsProc 34-10-05C IR 2 (only NAV mode of IR 2 inoperative)

34-10-05D
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative for RNAV ( RNP ) and RNAV ( GNSS ) operations.

LAN COLOMBIA FLEET MI-34-10 P 6/10

MEL E 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-10 - Air Data/Inertial Reference System (ADIRS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-10-05 IR 2
Ident.: MI-34-10-00008549.0002001 / 27 FEB 15
Applicable to: MSN 4758-5453

Note: RNAV item.

Note: RNP item.
Note: For RNP -10 Operations: a) IR 2 may be inoperative without flight time limitations if one
GPS is operative. b) IR 2 may be inoperative if both GPS are inoperative with the following
limitations: 1) 6.2 hours since IRS Ground Alignment, or 2) 5.7 hours since last FM radio
update.
Note: For RNAV -1 and RNAV -5 Operations: IR 2 may be inoperative.

34-10-05B IR 2 totally inoperative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) ** May be inoperative provided that:
1) The IR 2 pb-sw is set to OFF, and
2) The IR 1, the IR 3 and two ADR s are operative.
3) Do not perform RNAV ( RNP ) and RNAV ( GNSS ) operations.
Reference(s)
(o) Refer to OpsProc 34-10-05B IR 2 (IR 2 totally inoperative)

34-10-05C Only NAV mode of IR 2 inoperative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) The NAV mode may be inoperative provided that:
1) The IR 2 is operated in ATT mode, and
2) The IR 1 and the IR 3 are operative.
3) Do not perform RNAV ( RNP ) and RNAV ( GNSS ) operations.
Reference(s)
(o) Refer to OpsProc 34-10-05C IR 2 (only NAV mode of IR 2 inoperative)
Continued on the following page

LAN COLOMBIA FLEET MI-34-10 P 7/10

MEL E 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-10 - Air Data/Inertial Reference System (ADIRS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

34-10-05D
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative for RNAV ( RNP ) and RNAV ( GNSS ) operations.

34-10-06 IR 3
Ident.: MI-34-10-00008552.0002001 / 27 FEB 15
Applicable to: ALL

Note: RNAV item.

Note: RNP item.
Note: For RNP -10 Operations: a) IR 3 may be inoperative without flight time limitations if one
GPS is operative. b) IR 3 may be inoperative if both GPS are inoperative with the following
limitations: 1) 6.2 hours since IRS Ground Alignment, or 2) 5.7 hours since last FM radio
update.

34-10-06A IR 3 pb-sw set to OFF

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) ** May be inoperative provided that:
1) The IR 3 pb-sw is set to OFF, and
2) The IR 1, the IR 2, the ADR 1 and the ADR 2 are operative.
3) Do not perform RNAV ( RNP ) and RNAV ( GNSS ) operations.
Reference(s)
(o) Refer to OpsProc 34-10-06A IR 3 ( ADIRU with IR 3 totally inoperative)
Continued on the following page

LAN COLOMBIA FLEET MI-34-10 P 8/10

MEL E to F 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-10 - Air Data/Inertial Reference System (ADIRS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

34-10-06B IR 3 operated in ATT mode
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) ** The NAV mode may be inoperative provided that:
1) The IR 3 is operated in ATT mode, and
2) The IR 1 and the IR 2 are operative.
3) Do not perform RNAV ( RNP ) and RNAV ( GNSS ) operations.
Reference(s)
(o) Refer to OpsProc 34-10-06B IR 3 ( ADIRU with only NAV mode of IR 3 inoperative)

34-10-06D
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative for RNAV ( RNP ) and RNAV ( GNSS ) operations.

LAN COLOMBIA FLEET MI-34-10 P 9/10

MEL F 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-10 - Air Data/Inertial Reference System (ADIRS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-34-10 P 10/10

MEL 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-11 - Sensors
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-11-01 Angle of Attack ( AOA ) Sensor

Ident.: MI-34-11-00008558.0001001 / 12 SEP 12
Applicable to: ALL

34-11-01A
Repair interval Nbr installed Nbr required Placard
C 3 2 No
The F/O or the STBY Angle Of Attack sensor may be inoperative provided that the
associated ADR is considered inoperative.
Refer to Item 34-10-02 ADR 2 , or
Refer to Item 34-10-03 ADR 3

34-11-02 CAPT Total Air Temperature ( TAT )

Sensor Element Connected to the ADR 1
Ident.: MI-34-11-00008560.0001001 / 02 NOV 11
Applicable to: ALL

34-11-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative provided that:
1) The CAPT sensor element connected to the ADR 3 is operative, and
2) The F/O sensor connected to the ADR 2 is operative, and
3) The ADR 2 and the ADR 3 are operative, and
4) The TAT indication on the SD is checked operative, and
5) The TAS indication on the ND 1 is considered inoperative.
Refer to Item 34-06-02 True Air Speed Indication on the ND
Reference(s)
(o) Refer to OpsProc 34-11-02A CAPT Total Air Temperature (TAT) Sensor Element
Connected to ADR 1

LAN COLOMBIA FLEET MI-34-11 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
34 - NAVIGATION
34-11 - Sensors
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-11-03 CAPT Total Air Temperature ( TAT )

Sensor Element Connected to the ADR 3
Ident.: MI-34-11-00008561.0001001 / 02 NOV 11
Applicable to: ALL

34-11-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative provided that:
1) The CAPT sensor element connected to the ADR 1 is operative, and
2) The F/O sensor connected to the ADR 2 is operative, and
3) The ADR 1 and the ADR 2 are operative, and
4) The TAT indication on the SD is checked operative.
Reference(s)
(o) Refer to OpsProc 34-11-03A CAPT Total Air Temperature (TAT) Sensor Element
Connected to ADR 3

34-11-04 F/O Total Air Temperature ( TAT )

Sensor Element Connected to the ADR 2
Ident.: MI-34-11-00008562.0001001 / 02 NOV 11
Applicable to: ALL

34-11-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative provided that:
1) Both CAPT TAT sensor elements are operative, and
2) The ADR 1 and the ADR 3 are operative, and
3) The TAT indication on the SD is checked operative, and
4) The TAS indications on the ND 2 is considered inoperative.
Refer to Item 34-06-02 True Air Speed Indication on the ND
Reference(s)
(o) Refer to OpsProc 34-11-04A F/O Total Air Temperature (TAT) Sensor Element Connected
to ADR 2

LAN COLOMBIA FLEET MI-34-11 P 2/2

MEL C to D 05 NOV 13
 MEL ITEMS
34 - NAVIGATION
34-22 - Attitude and Heading Standby Data
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-22-01 Standby Compass Indicator

Ident.: MI-34-22-00008615.0005001 / 27 FEB 15
Applicable to: ALL

34-22-01B
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that:
1) The three IR s are operative, and
2) The ATT/HDG SWITCHING selector , the EIS DMC SWITCHING selector and the
PFD/ND XFR pb are checked operative.
Reference(s)
(o) Refer to OpsProc 34-22-01B Standby Compass Indicator

34-22-02 Standby Compass Lighting

Ident.: MI-34-22-00008616.0001001 / 21 MAR 10
Applicable to: ALL

34-22-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-34-22 P 1/2

MEL A to B 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-22 - Attitude and Heading Standby Data
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-34-22 P 2/2

MEL 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-23 - Integrated Standby Instrument System (ISIS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-23-01 ISIS Altitude Indication

Ident.: MI-34-23-00008618.0001001 / 27 FEB 15
Applicable to: ALL

34-23-01A
Repair interval Nbr installed Nbr required Placard
B 1 0 No
May be inoperative provided that the aircraft is operated in day VMC conditions.

34-23-02 ISIS Airspeed Indication

Ident.: MI-34-23-00008619.0005001 / 27 FEB 15
Applicable to: ALL

34-23-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that:
1) The ISIS attitude indication is operative, and
2) The ADRs, DMCs and probe heat computers are operative, and
3) The AIR DATA SWITCHING selector, the EIS DMC SWITCHING selector and the
PFD/ND XFR pb are operative.

34-23-03 ISIS Bugs Indication

Ident.: MI-34-23-00008620.0001001 / 27 FEB 15
Applicable to: ALL

34-23-03A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-34-23 P 1/2

MEL A to C 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-23 - Integrated Standby Instrument System (ISIS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-23-04 ISIS Attitude Indication

Ident.: MI-34-23-00008621.0001001 / 27 FEB 15
Applicable to: ALL

34-23-04B
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

34-23-05 ISIS ILS Indication

Ident.: MI-34-23-00008622.0001001 / 27 FEB 15
Applicable to: ALL

34-23-05A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative.

34-23-06 ISIS Mach Number Indication

Ident.: MI-34-23-00008623.0001001 / 27 FEB 15
Applicable to: ALL

34-23-06A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-34-23 P 2/2

MEL D to F 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-30 - Landing and Taxiing Aid
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-30-04 Instrument Landing System ( ILS )

Ident.: MI-34-30-00008627.0002001 / 20 JUN 14
Applicable to: ALL

34-30-04A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) **
Note: For ETOPS , if ILS is required, ILS 1 must be operative
When the ILS 1 is inoperative, the GPWS / TAWS G/S mode (mode 5) is also
inoperative.
Refer to Item 34-40-01 Ground Proximity Warning System (GPWS)/Terrain
Awareness and Warning System (TAWS)
Reference(s)
(o) Refer to OpsProc 34-30-04A Instrument Landing System (ILS)

LAN COLOMBIA FLEET MI-34-30 P 1/2

MEL A 18 JUL 14
 MEL ITEMS
34 - NAVIGATION
34-30 - Landing and Taxiing Aid
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-34-30 P 2/2

MEL 18 JUL 14
 MEL ITEMS
34 - NAVIGATION
34-40 - GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-40-01 Ground Proximity Warning System (GPWS)/Terrain

Awareness and Warning System (TAWS)
Ident.: MI-34-40-00008697.0001001 / 05 NOV 13
Applicable to: ALL

Note: RNP item.

34-40-01A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative

34-40-02 Radio Altimeter Automatic Callout

Ident.: MI-34-40-00008698.0001001 / 23 MAR 11
Applicable to: ALL

34-40-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) **
May be inoperative.
Reference(s)
(o) Refer to OpsProc 34-40-02A Radio Altimeter Automatic Callout

34-40-03 Radio Altimeter System

Ident.: MI-34-40-00008699.0001001 / 27 FEB 15
Applicable to: ALL

Note: RNP item.

Continued on the following page

LAN COLOMBIA FLEET MI-34-40 P 1/4

MEL A to C 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-40 - GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

34-40-03A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) **
Except for RNAV ( RNP ) operations one may be inoperative provided that both FCU
channels, all ELAC s, SEC s, ADIRU s, SFCC s, LGCIU s and FAC s are operative.
Note: When the radio altimeter 1 is inoperative, the GPWS is inoperative.
Refer to Item 34-40-01 Ground Proximity Warning System (GPWS)/Terrain
Awareness and Warning System (TAWS)
Reference(s)
(o) Refer to OpsProc 34-40-03A Radio Altimeter System

34-40-04 Traffic Collision Avoidance System (TCAS)

Ident.: MI-34-40-00008700.0002001 / 27 FEB 15
Applicable to: ALL

34-40-04A
Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

34-40-05 Weather Radar System

Ident.: MI-34-40-00008701.0001001 / 27 FEB 15
Applicable to: ALL

34-40-05A
Repair interval Nbr installed Nbr required Placard
1 1 Yes
Must be operative

LAN COLOMBIA FLEET MI-34-40 P 2/4

MEL C to E 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-40 - GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-40-06 Predictive Windshear Detection Function

Ident.: MI-34-40-00007541.0001001 / 27 FEB 15
Applicable to: ALL

34-40-06A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided Windshear Detection System Reactive is operative.

34-40-07 PULL UP-GPWS pb-sw

Ident.: MI-34-40-00008702.0002001 / 27 FEB 15
Applicable to: ALL

34-40-07A One inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(o) One may be inoperative provided that the GPWS or the TAWS aural and visual warnings
are checked operative.
Reference(s)
(o) Refer to OpsProc 34-40-07A GPWS/PULL UP-G/S pb-sw

34-40-07B Both inoperative

Repair interval Nbr installed Nbr required Placard
2 0 Yes
Both may be inoperative provided that the GPWS or the TAWS is considered inoperative.
Refer to Item 34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness and
Warning System (TAWS)

LAN COLOMBIA FLEET MI-34-40 P 3/4

MEL F to G 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-40 - GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-34-40 P 4/4

MEL 27 FEB 15
 MEL ITEMS
34 - NAVIGATION
34-50 - ATC and Radio / GPS Navigation Systems
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-50-01 ATC
Ident.: MI-34-50-00008703.0001001 / 20 JUN 14
Applicable to: ALL

Note: RVSM item.

34-50-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) For RVSM operations mode C must be operative.
Note: If no ATC is available, the TCAS is also inoperative.
Refer to Item 34-40-04 Traffic Collision Avoidance System (TCAS)
Reference(s)
(o) Refer to OpsProc 34-50-01A ATC

34-50-03 ADF
Ident.: MI-34-50-00008705.0001001 / 18 MAY 11
Applicable to: ALL

34-50-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided :
1) Both VOR Systems are operative, and
2) At least two Inertial Reference must be operative Refer to Item 34-10-04 IR 1 Refer to
Item 34-10-05 IR 2 Refer to Item 34-10-06 IR 3 , and
3) Navigation is not based on the use of ADF .

LAN COLOMBIA FLEET MI-34-50 P 1/4

MEL A to B 10 OCT 14
 MEL ITEMS
34 - NAVIGATION
34-50 - ATC and Radio / GPS Navigation Systems
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-50-04 DME
Ident.: MI-34-50-00008706.0001001 / 05 APR 12
Applicable to: ALL

Note: RNAV item.

Note: RNP item.

34-50-04A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
Except for RNAV-1 and RNAV-5 one may be inoperative.

34-50-04B
Repair interval Nbr installed Nbr required Placard
C 2 1 No
For RNAV-1 and RNAV-5 one may be inoperative provided GPS based Navigation is used.

34-50-05 VOR
Ident.: MI-34-50-00008707.0001001 / 18 MAY 11
Applicable to: ALL

Note: RNAV item.

Note: RNP item.

34-50-05A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative provided:
1) Two GPS receivers operates normally, and
2) IR 1 and IR 2 operates normally.
Continued on the following page

LAN COLOMBIA FLEET MI-34-50 P 2/4

MEL C to D 10 OCT 14
 MEL ITEMS
34 - NAVIGATION
34-50 - ATC and Radio / GPS Navigation Systems
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

34-50-05B
Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative provided:
1) Two GPS receivers operate normally, and
2) IR 1 and IR 3 operate normally.

34-50-06 MARKER
Ident.: MI-34-50-00009155.0001001 / 23 MAR 11
Applicable to: ALL

34-50-06A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided approach procedures are not predicated on its use.

34-50-09 Global Positioning System (GPS)

Ident.: MI-34-50-00008710.0001001 / 05 NOV 13
Applicable to: ALL

Note: RNAV item.

Note: RNP item.

34-50-09A
Repair interval Nbr installed Nbr required Placard
D 2 0 No
Except forRNAV-1 ,RNAV ( RNP ) and RNAV ( GNSS ) operations and dispatch for Mount
Pleasant (MPN), both may be inoperative.
Continued on the following page

LAN COLOMBIA FLEET MI-34-50 P 3/4

MEL D to F 10 OCT 14
 MEL ITEMS
34 - NAVIGATION
34-50 - ATC and Radio / GPS Navigation Systems
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

34-50-09B
Repair interval Nbr installed Nbr required Placard
2 2 No
Must be operative for dispatch to Mount Pleasant (MPN), RNAV-1 , RNAV ( GNSS )
and RNAV ( RNP ) operations.

34-50-09C
Repair interval Nbr installed Nbr required Placard
D 2 0 No
Both may be inoperative for RNAV-10 operations with the following limitations:
1) 6.2 hours since IRS Ground Alignment, or
2) 5.7 hours since last FM radio update.

34-50-09D
Repair interval Nbr installed Nbr required Placard
D 2 1 No
One may be inoperative for RNAV-10 operations without flight time limitations.

LAN COLOMBIA FLEET MI-34-50 P 4/4

MEL F 10 OCT 14
 MEL ITEMS
35 - OXYGEN
35-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 35-01-01 - OXYGEN Overhead Panel
MINIMUM EQUIPMENT LIST

35-01-01-01 CREW SUPPLY pb-sw OFF light

Ident.: MI-35-01-01-00008727.0001001 / 21 MAR 10
Applicable to: ALL

35-01-01-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

35-01-01-02 PASSENGER SYS ON light

Ident.: MI-35-01-01-00008729.0001001 / 21 MAR 10
Applicable to: ALL

35-01-01-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

35-01-01-03 HI ALT LANDING pb-sw ON light

Ident.: MI-35-01-01-00008730.0001001 / 27 FEB 15
Applicable to: ALL

35-01-01-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-35-01-01 P 1/4

MEL A to C 27 FEB 15
 MEL ITEMS
35 - OXYGEN
35-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 35-01-01 - OXYGEN Overhead Panel
MINIMUM EQUIPMENT LIST

35-01-01-31 MANUAL Control of the MASK MAN ON pb

Ident.: MI-35-01-01-00008731.0001001 / 12 SEP 11
Applicable to: ALL

35-01-01-31A AUTO control function checked operative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that the AUTO control function is checked operative.
Reference(s)
(m) Refer to AMM 35-23-00-040-008

35-01-01-31B FL limitation
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that:
1) The operating altitude is limited to FL 250 , and
2) The minimum operating altitude is in accordance with applicable operating regulations,
and
3) The portable oxygen units (supplemental oxygen) are provided in accordance with
applicable regulations.
Reference(s)
(o) Refer to OpsProc 35-01-01-31B MANUAL Control of the MASK MAN ON pb

35-01-01-32 AUTO Control of the MASK MAN ON pb

Ident.: MI-35-01-01-00008732.0001001 / 10 OCT 14
Applicable to: ALL

35-01-01-32A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that:
1) The MANUAL Control of the passengers oxygen masks is checked operative, and
2) The operating altitude is limited to FL 300.
Continued on the following page

LAN COLOMBIA FLEET MI-35-01-01 P 2/4

MEL D to E 27 FEB 15
 MEL ITEMS
35 - OXYGEN
35-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 35-01-01 - OXYGEN Overhead Panel
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(m) Refer to AMM 35-23-00-040-802

35-01-01-33 HI ALT LANDING pb-sw

Ident.: MI-35-01-01-00008735.0001001 / 27 FEB 15
Applicable to: ALL

35-01-01-33A Passenger oxygen AUTO control checked operative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) (m) May be inoperative provided that the passenger oxygen AUTO control is checked operative.
Reference(s)
(o) Refer to OpsProc 35-01-01-33A HI ALT LANDING pb-sw
(m) Refer to AMM 35-23-00-040-001

35-01-01-33B Passenger oxygen AUTO control considered inoperative

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the passenger oxygen AUTO control is considered
inoperative.
Refer to Item 35-01-01-32 AUTO Control of the MASK MAN ON pb

LAN COLOMBIA FLEET MI-35-01-01 P 3/4

MEL E to F 27 FEB 15
 MEL ITEMS
35 - OXYGEN
35-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 35-01-01 - OXYGEN Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-35-01-01 P 4/4

MEL 27 FEB 15
 MEL ITEMS
35 - OXYGEN
35-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

35-07-01 Crew OXY High Pressure Indication on the DOOR/OXY SD page

Ident.: MI-35-07-00008771.0001001 / 21 MAR 10
Applicable to: ALL

35-07-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that the oxygen pressure is checked by direct reading before
each flight.
Reference(s)
(o) Refer to OpsProc 35-07-01A Crew OXY High Pressure Indication on the DOOR/OXY SD
page
(m) Refer to AMM 35-10-00-040-001

35-07-02 Crew Oxygen REGUL LO PR Indication on the DOOR/OXY SD page

Ident.: MI-35-07-00008773.0001001 / 21 MAR 10
Applicable to: ALL

35-07-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) (m) May be inoperative provided that the oxygen pressure is checked before the first flight of
each day.
Reference(s)
(o) Refer to OpsProc 35-07-02A Crew Oxygen REGUL LO PR Indication on the DOOR/OXY
SD page
(m) Refer to AMM 35-10-00-040-002

LAN COLOMBIA FLEET MI-35-07 P 1/2

MEL A to B 05 NOV 13
 MEL ITEMS
35 - OXYGEN
35-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-35-07 P 2/2

MEL 05 NOV 13
 MEL ITEMS
35 - OXYGEN
35-10 - Crew Oxygen
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

35-10-01 Crew Oxygen Mask

Ident.: MI-35-10-00008748.0001001 / 01 AUG 13
Applicable to: ALL

35-10-01A
Repair interval Nbr installed Nbr required Placard
C 4 2 Yes
Each occupant of the cockpit must have his assigned mask operative.

35-10-02 Crew Oxygen Mask Microphone

Ident.: MI-35-10-00008749.0001001 / 23 MAR 11
Applicable to: ALL

35-10-02A
Repair interval Nbr installed Nbr required Placard
C 4 2 Yes
One must be operative for each pilot.

35-10-03 Exterior Crew Oxygen Overpressure Indicator Disc (Green Disc)

Ident.: MI-35-10-00008751.0001001 / 23 MAR 11
Applicable to: ALL

35-10-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be missing or damaged.
Reference(s)
(o) Refer to OpsProc 35-10-03A Exterior Crew Oxygen Overpressure Indicator Disc (Green
Disc)

LAN COLOMBIA FLEET MI-35-10 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
35 - OXYGEN
35-10 - Crew Oxygen
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-35-10 P 2/2

MEL 05 NOV 13
 MEL ITEMS
35 - OXYGEN
35-20 - Passenger Oxygen
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

35-20-01 Passenger Oxygen Unit

Ident.: MI-35-20-00008753.0001001 / 12 SEP 11
Applicable to: ALL

35-20-01A Associated seats considered inoperative

Repair interval Nbr installed Nbr required Placard
D 56 0 No
One or more may be inoperative provided that the associated seats are considered
inoperative.
Refer to Item 25-20-01-01 Passenger Seat

35-20-01B FL limitation
Repair interval Nbr installed Nbr required Placard
C 56 0 Yes
(o) One or more may be inoperative and the associated seats may be occupied provided that:
1) The operating altitude is limited to FL 250 , and
2) The minimum operating altitude is in accordance with applicable operating regulations,
and
3) Portable oxygen units (supplemental oxygen) are provided.
Reference(s)
(o) Refer to OpsProc 35-20-01B Passenger Oxygen Unit

35-20-02 Cabin Attendant Oxygen Unit

Ident.: MI-35-20-00008755.0001001 / 12 SEP 11
Applicable to: ALL

35-20-02A Associated seats considered inoperative

Repair interval Nbr installed Nbr required Placard
3 0 No
One or more may be inoperative provided that the associated seats are considered
inoperative.
Refer to Item 25-20-03 Cabin Attendant Seat
Continued on the following page

LAN COLOMBIA FLEET MI-35-20 P 1/4

MEL A to B 10 OCT 14
 MEL ITEMS
35 - OXYGEN
35-20 - Passenger Oxygen
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

35-20-02B FL limitation
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
(o) One or more may be inoperative and the associated seats may be occupied provided that:
1) The operating altitude is limited to FL 250 , and
2) The minimum operating altitude is in accordance with applicable operating regulations,
and
3) Portable oxygen units (supplemental oxygen) are provided.
Reference(s)
(o) Refer to OpsProc 35-20-02B Cabin Attendant Oxygen Unit

35-20-03 Lavatory Oxygen Unit

Ident.: MI-35-20-00008756.9001002 / 10 OCT 14
Applicable to: ALL

35-20-03A
Repair interval Nbr installed Nbr required Placard
C 3 1 Yes
One or more may be inoperative provided that:
1) The associated lavatory door is placarded inoperative and locked closed, and
2) The lavatory is not used for storage or any other purpose.
Note: If forward lavatory is locked closed, it can be used only by pilots on duty when
flight time is more than 1:30 hour.

35-20-03B
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
All may be inoperative or missing provided that:
1) The lavatories are locked closed and placarded inoperative,
2) Lavatory(ies) is(are) only used by crew members,and
3) Only non revenue flight is permitted.

LAN COLOMBIA FLEET MI-35-20 P 2/4

MEL B to C 10 OCT 14
 MEL ITEMS
35 - OXYGEN
35-20 - Passenger Oxygen
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

35-20-04 Galley Oxygen Unit

Ident.: MI-35-20-00008757.0001001 / 14 FEB 13
Applicable to: ALL

Note: For an inoperative cabin attendant oxygen unit located within the galley area:
Refer to Item 35-20-02 Cabin Attendant Oxygen Unit

35-20-04A Adjacent cabin attendant oxygen unit available

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(o) One or more may be inoperative and the associated galley area may be occupied provided
that an adjacent cabin attendant individual oxygen unit is available for each occupants of
the associated galley area.
Reference(s)
(o) Refer to OpsProc 35-20-04A Galley Oxygen Unit (cabin attendant oxygen unit available
near the galley)

35-20-04B Portable oxygen available in the associated galley area

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(o) One or more may be inoperative and the associated galley area may be occupied provided
that a cabin attendant portable oxygen device is available for each occupants of the
associated galley area.
Reference(s)
(o) Refer to OpsProc 35-20-04B Galley Oxygen Unit (cabin attendant portable oxygen device
available near the galley)

35-20-04D Associated galley area not occupied

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or more may be inoperative provided that the associated galley area is not occupied.

LAN COLOMBIA FLEET MI-35-20 P 3/4

MEL D 10 OCT 14
 MEL ITEMS
35 - OXYGEN
35-20 - Passenger Oxygen
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

35-20-05 Manual Release Tool

Ident.: MI-35-20-00008758.0001001 / 23 MAR 11
Applicable to: ALL

35-20-05A
Repair interval Nbr installed Nbr required Placard
D 4 1 No
One must be available.

LAN COLOMBIA FLEET MI-35-20 P 4/4

MEL E 10 OCT 14
 MEL ITEMS
35 - OXYGEN
35-30 - Portable Oxygen
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

35-30-01 Flight Crew Portable Device

Ident.: MI-35-30-00008767.0001001 / 23 MAR 11
Applicable to: ALL

35-30-01A Protective Breathing Equipment (PBE)

Repair interval Nbr installed Nbr required Placard
1 1 No
Must be operative.

35-30-02 Cabin Attendant Portable Device

Ident.: MI-35-30-00008769.9001004 / 27 FEB 15
Applicable to: ALL

35-30-02A Bottle with Mask For Revenue Flights

Repair interval Nbr installed Nbr required Placard
C 5 4 Yes
Any in excess of those required by Flight Attendant on duty may be unserviceable or
missing provided :
1) One bottle for each Cabin Attendant on duty must be in fully operational condition, and
2) Unserviceable bottle(s) must be removed at next Maintenance facility , and
3) Required distribution of serviceable bottles is maintained throughout aircraft, and
4) Repairs are made at SCL maintenance base.

35-30-02B Bottle with Mask For Non Revenue Flights

Repair interval Nbr installed Nbr required Placard
C 5 Yes
Any in excess of those required by Flight Attendant on duty may be unserviceable or
missing provided :
1) One bottle for each Cabin Attendant on duty must be in fully operational condition, and
2) Unserviceable bottle(s) must be removed at next Maintenance facility , and
3) Required distribution of serviceable bottles is maintained throughout aircraft, and
4) Repairs are made at SCL maintenance base, and
5) Only non revenue flight is permitted.

LAN COLOMBIA FLEET MI-35-30 P 1/2

MEL A to B 27 FEB 15
 MEL ITEMS
35 - OXYGEN
35-30 - Portable Oxygen
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

35-30-03 Cabin Attendant Portable Device

1 Ident.: MI-35-30-20800295.9001001 / 27 FEB 15
Applicable to: ALL

35-30-03A Protective Breathing Equipment (PBE)

Repair interval Nbr installed Nbr required Placard

C 5 4 No
Any in excess of those required by Flight Attendant on duty may be inoperative or missing
provided :
1) One PBE for each Cabin Attendant on duty must be in fully operational condition, and
2) Required distribution of operative PBEs is maintained throughout aircraft, and
3) PBE inoperative(s) is (are) replaced or removed at next available maintenance facility.

LAN COLOMBIA FLEET MI-35-30 P 2/2

MEL C 27 FEB 15
 MEL ITEMS
36 - PNEUMATIC
36-00 - MAINTENANCE Message on the STATUS SD Page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

36-00-01 AIR BLEED MAINTENANCE Message

Ident.: MI-36-00-00016004.0002001 / 27 FEB 15
Applicable to: ALL

36-00-01D No fault on the APU leak detection loop

Repair interval Nbr installed Nbr required Placard
C No
(m) AIR BLEED MAINTENANCE message may be displayed on the STATUS SD page provided
that it is checked that the CFDS does not report a fault on the APU leak detection loop.
Reference(s)
(m) Refer to AMM Task 36-11-00-040-004

36-00-01E APU leak detection loop affected

Repair interval Nbr installed Nbr required Placard
C No
AIR BLEED MAINTENANCE message may be displayed on the STATUS SD page provided
that the APU leak detection loop is considered inoperative.
Refer to Item 36-22-03 APU Leak Detection Loop

LAN COLOMBIA FLEET MI-36-00 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
36 - PNEUMATIC
36-00 - MAINTENANCE Message on the STATUS SD Page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-36-00 P 2/2

MEL 27 FEB 15
 MEL ITEMS
36 - PNEUMATIC
36-01 - AIR COND Overhead Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

36-01-01 ENG BLEED pb-sw FAULT light

Ident.: MI-36-01-00008778.0001001 / 21 MAR 10
Applicable to: ALL

36-01-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

36-01-02 ENG BLEED pb-sw OFF light

Ident.: MI-36-01-00008783.0001001 / 21 MAR 10
Applicable to: ALL

36-01-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

36-01-03 APU BLEED pb-sw FAULT light

Ident.: MI-36-01-00008785.0001001 / 21 MAR 10
Applicable to: ALL

36-01-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-36-01 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
36 - PNEUMATIC
36-01 - AIR COND Overhead Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

36-01-04 APU BLEED pb-sw ON light

Ident.: MI-36-01-00008787.0001001 / 21 MAR 10
Applicable to: ALL

36-01-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-36-01 P 2/2

MEL D 05 NOV 13
 MEL ITEMS
36 - PNEUMATIC
36-07 - Indications on the BLEED SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

36-07-01 APU Bleed Valve Indication on the BLEED SD page

Ident.: MI-36-07-00008807.0001001 / 21 MAR 10
Applicable to: ALL

36-07-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.

36-07-02 Engine Bleed Valve Indication on the BLEED SD page

Ident.: MI-36-07-00008808.0001001 / 21 MAR 10
Applicable to: ALL

36-07-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

36-07-03 Engine Bleed HP Valve Indication on the BLEED SD page

Ident.: MI-36-07-00008809.0001001 / 21 MAR 10
Applicable to: ALL

36-07-03A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

LAN COLOMBIA FLEET MI-36-07 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
36 - PNEUMATIC
36-07 - Indications on the BLEED SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

36-07-04 Engine Bleed Precooler Inlet Pressure

Indication on the BLEED SD page
Ident.: MI-36-07-00008810.0001001 / 21 MAR 10
Applicable to: ALL

36-07-04A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

36-07-05 Engine Bleed Precooler Outlet Temperature

Indication on the BLEED SD page
Ident.: MI-36-07-00008811.0001001 / 21 MAR 10
Applicable to: ALL

36-07-05A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

36-07-06 X Bleed Valve Indication on the BLEED SD page

Ident.: MI-36-07-00008812.0001001 / 21 MAR 10
Applicable to: ALL

36-07-06A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-36-07 P 2/2

MEL D to F 05 NOV 13
 MEL ITEMS
36 - PNEUMATIC
36-11 - Engine Bleed Air Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

36-11-01 Engine Bleed Air Supply System

Ident.: MI-36-11-00008788.0002001 / 27 FEB 15
Applicable to: ALL

Note: The HP ground connection is near the engine 1 hazardous area. If the bleed air supply
system 2 is inoperative, it is better to use the APU bleed for engine start. If the APU bleed
is not available, a ground cart can be used as long as the pneumatic pipe is kept out of the
hazardous area.

36-11-01A Non ETOPS flight - no FL limitation

Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(o) One may be inoperative provided that:
1) ETOPS is not conducted, and
2) The associated ENG BLEED pb-sw is set to OFF, and
3) The X-BLEED selector is set to OPEN, and
4) The speedbrakes are operative, and
5) The airplane flies higher than MOCA ( Minimum Obstruction Clearence Altitude ) or the
airplane flies higher than Grid MORA ( Minimum Off Route Altitude ).
Note: During the takeoff briefing review the procedure with two air conditioning packs
failed.
Reference(s)
(o) Refer to OpsProc 36-11-01A Engine Bleed Air Supply System (non-ETOPS flights)
Continued on the following page

LAN COLOMBIA FLEET MI-36-11 P 1/6

MEL A 27 FEB 15
 MEL ITEMS
36 - PNEUMATIC
36-11 - Engine Bleed Air Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

36-11-01E Non ETOPS flight - limitation to 31 500 ft
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(o) One may be inoperative provided that:
1) ETOPS is not conducted, and
2) The associated ENG BLEED pb-sw is set to OFF, and
3) The X-BLEED selector is set to OPEN, and
4) The altitude is limited to 31 500 ft ( 9 600 m ), and
5) The airplane flies higher than MOCA ( Minimum Obstruction Clearence Altitude ) or the
airplane flies higher than Grid MORA ( Minimum Off Route Altitude ).
Note: During the takeoff briefing review the procedure with two air conditioning packs
failed.
Reference(s)
(o) Refer to OpsProc 36-11-01E Engine Bleed Air Supply System (non-ETOPS flights)

36-11-02 Engine Bleed Valve ( PRV )

Ident.: MI-36-11-00008790.0001001 / 12 SEP 11
Applicable to: ALL

36-11-02A
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
(m) One may be inoperative provided that:
1) The affected engine bleed valve is secured in the closed position, and
2) The associated bleed air supply system is considered inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System
Reference(s)
(m) Refer to AMM 36-11-00-040-001

LAN COLOMBIA FLEET MI-36-11 P 2/6

MEL A to B 27 FEB 15
 MEL ITEMS
36 - PNEUMATIC
36-11 - Engine Bleed Air Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

36-11-03 Engine Bleed Overpressure Valve

Ident.: MI-36-11-00008792.0001001 / 12 SEP 11
Applicable to: ALL

36-11-03A Associated bleed considered inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative provided that the associated bleed air supply system is considered
inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System

36-11-03B Associated Bleed still available

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative provided that the associated AIR ENG 1(2) BLEED FAULT
alert or the AIR ENG 1(2) BLEED ABNORM PR alert was not displayed during the previous
flight.

36-11-04 Engine Bleed Fan Air Valve

Ident.: MI-36-11-00008794.0001001 / 12 SEP 11
Applicable to: ALL

36-11-04A
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
One may be inoperative provided that the associated engine bleed air supply system is
considered inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System

LAN COLOMBIA FLEET MI-36-11 P 3/6

MEL C to D 27 FEB 15
 MEL ITEMS
36 - PNEUMATIC
36-11 - Engine Bleed Air Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

36-11-05 Engine Bleed Air Precooler

Ident.: MI-36-11-00008796.0001001 / 12 SEP 11
Applicable to: ALL

36-11-05A
Repair interval Nbr installed Nbr required Placard
C 2 1 Yes
One may be inoperative provided that the associated engine bleed air supply system is
considered inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System

36-11-06 Engine Bleed IP Check Valve

Ident.: MI-36-11-00008797.0001001 / 27 FEB 15
Applicable to: ALL

36-11-06A Associated bleed considered inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative provided that the associated engine bleed air supply system is
considered inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System

36-11-06B Associated HP valve secured in the closed position

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) (m) One may be inoperative in the open position provided that:
1) The associated HP valve is secured in the closed position, and
2) The opposite engine bleed supply system is operative.
Reference(s)
(o) Refer to OpsProc 36-11-06B Engine Bleed IP Check Valve
(m) Refer to AMM Task 36-11-00-040-002

LAN COLOMBIA FLEET MI-36-11 P 4/6

MEL E to F 27 FEB 15
 MEL ITEMS
36 - PNEUMATIC
36-11 - Engine Bleed Air Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

36-11-07 Engine Bleed HP Valve

Ident.: MI-36-11-00008798.0001001 / 27 FEB 15
Applicable to: ALL

36-11-07A Associated bleed considered inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative in the closed position provided that the associated engine bleed air
supply system is considered inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System

36-11-07B HP valve secured in the closed position

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) (m) One may be inoperative provided that:
1) The affected engine bleed HP valve is secured in the closed position, and
2) The opposite engine bleed supply system is operative.
Reference(s)
(o) Refer to OpsProc 36-11-07B Engine Bleed HP Valve
(m) Refer to AMM Task 36-11-00-040-003

36-11-08 Bleed Monitoring Computer ( BMC )

Ident.: MI-36-11-00008799.0012001 / 27 FEB 15
Applicable to: ALL

36-11-08A BMC 1 inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
BMC 1 may be inoperative provided that:
1) ETOPS is not conducted, and
2) The engine 1 bleed air supply system is considered inoperative
Refer to Item 36-11-01 Engine Bleed Air Supply System , and
3) The APU leak detection loop is considered inoperative.
Refer to Item 36-22-03 APU Leak Detection Loop
Continued on the following page

LAN COLOMBIA FLEET MI-36-11 P 5/6

MEL G to H 27 FEB 15
 MEL ITEMS
36 - PNEUMATIC
36-11 - Engine Bleed Air Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

36-11-08B BMC 2 inoperative
Repair interval Nbr installed Nbr required Placard
C 2 1 No
BMC 2 may be inoperative provided that the engine 2 bleed air supply system is considered
inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System

LAN COLOMBIA FLEET MI-36-11 P 6/6

MEL H 27 FEB 15
 MEL ITEMS
36 - PNEUMATIC
36-12 - APU Bleed Air Supply and Crossbleed Systems
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

36-12-01 APU Bleed Air Supply System

Ident.: MI-36-12-00008800.0001001 / 27 NOV 12
Applicable to: ALL

36-12-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided:
1) APU BLEED pb-sw is set to OFF, and
2) Do not dispatch to an airport where ASU (Air Supply Unit) is not available or: Refer to
FCOM/ Crossbleed Engine Start

36-12-02 APU Bleed Valve

Ident.: MI-36-12-00008801.0001001 / 12 SEP 12
Applicable to: ALL

36-12-02A Inoperative in the closed position

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative provided that:
1) The APU bleed valve is deactivated in the closed position, and
2) The APU bleed air supply system is considered inoperative.
Refer to Item 36-12-01 APU Bleed Air Supply System
Reference(s)
(m) Refer to AMM

36-12-02B Inoperative in the open position

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative in the open position provided that the APU is not used in flight.
Refer to Item 49-10-01 Power Plant (APU)
Continued on the following page

LAN COLOMBIA FLEET MI-36-12 P 1/4

MEL A to B 27 FEB 15
 MEL ITEMS
36 - PNEUMATIC
36-12 - APU Bleed Air Supply and Crossbleed Systems
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 36-12-02B APU Bleed Valve

36-12-03 APU Bleed Check Valve

Ident.: MI-36-12-00008802.0001001 / 21 MAR 10
Applicable to: ALL

36-12-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that the APU bleed air supply system is considered
inoperative.
Refer to Item 36-12-01 APU Bleed Air Supply System

36-12-04 Automatic Control of the X Bleed Valve

Ident.: MI-36-12-00008803.0001001 / 21 MAR 10
Applicable to: ALL

36-12-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that the manual control is checked operative.
Reference(s)
(o) Refer to OpsProc 36-12-04A Automatic control of the X Bleed Valve

LAN COLOMBIA FLEET MI-36-12 P 2/4

MEL B to D 27 FEB 15
 MEL ITEMS
36 - PNEUMATIC
36-12 - APU Bleed Air Supply and Crossbleed Systems
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

36-12-05 Manual Control of the X Bleed Valve

Ident.: MI-36-12-00015756.0001001 / 27 FEB 15
Applicable to: ALL

36-12-05A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative provided that the Automatic Control is checked operative.
Reference(s)
(o) Refer to OpsProc 36-12-05A Manual Control of the X Bleed Valve

LAN COLOMBIA FLEET MI-36-12 P 3/4

MEL E 27 FEB 15
 MEL ITEMS
36 - PNEUMATIC
36-12 - APU Bleed Air Supply and Crossbleed Systems
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-36-12 P 4/4

MEL 27 FEB 15
 MEL ITEMS
36 - PNEUMATIC
36-22 - Leak Detection Loop
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

36-22-01 Pylon Leak Detection System

Ident.: MI-36-22-00008804.0008001 / 27 FEB 15
Applicable to: ALL

36-22-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(m) One may be inoperative provided that:
1) The associated pylon leak detection loop is deactivated, and
2) The AIR ENG 1(2) BLEED LEAK alert is confirmed to be false by troubleshooting, and
3) The associated bleed air supply system is considered inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System
Reference(s)
(m) Refer to AMM 36-22-00-040-001

36-22-02 Wing Leak Detection System

Ident.: MI-36-22-00008805.0001001 / 21 MAR 10
Applicable to: ALL

36-22-02A
Repair interval Nbr installed Nbr required Placard
2 2 No
Must be operative.
Note: Failure of one loop in one or both wing leading edges is indicated by a
MAINTENANCE message displayed on the STATUS SD page .
Refer to 00008776 **Not found**

LAN COLOMBIA FLEET MI-36-22 P 1/4

MEL A to B 27 FEB 15
 MEL ITEMS
36 - PNEUMATIC
36-22 - Leak Detection Loop
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

36-22-03 APU Leak Detection Loop

Ident.: MI-36-22-00008806.0003001 / 27 FEB 15
Applicable to: ALL

36-22-03A APU bleed check valve replaced by a plate

Repair interval Nbr installed Nbr required Placard
C 1 0 No
(m) May be inoperative provided that:
1) The APU bleed check valve is removed and replaced by a plate, and
2) The APU bleed air supply system is considered inoperative.
Refer to Item 36-12-01 APU Bleed Air Supply System
Reference(s)
(m) Refer to AMM Task 36-12-00-040-XXX

36-22-03B No FL limitation
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative provided that:
1) ETOPS is not conducted, and
2) The AIR APU BLEED LEAK alert was not displayed during the previous flight, and
3) The ENG 1 BLEED pb-sw is set to OFF, and
4) The PACK 1 pb-sw is set to OFF, and
5) The X BLEED selector is set to SHUT, and
6) The APU BLEED pb-sw is set to OFF, and
7) The aircraft is not operated in known or forecast icing conditions, and
8) The speedbrakes are operative.
Reference(s)
(o) Refer to OpsProc 36-22-03B APU Leak Detection Loop
Continued on the following page

LAN COLOMBIA FLEET MI-36-22 P 2/4

MEL C 27 FEB 15
 MEL ITEMS
36 - PNEUMATIC
36-22 - Leak Detection Loop
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

36-22-03C Limitation to 31 500 ft
Repair interval Nbr installed Nbr required Placard
C 1 0 No
(o) May be inoperative provided that:
1) ETOPS is not conducted, and
2) The AIR APU BLEED LEAK alert was not displayed during the previous flight, and
3) The ENG 1 BLEED pb-sw is set to OFF, and
4) The PACK 1 pb-sw is set to OFF, and
5) The X BLEED selector is set to SHUT, and
6) The APU BLEED pb-sw is set to OFF, and
7) The aircraft is not operated in known or forecast icing conditions, and
8) The altitude is limited to 31 500 ft ( 9 600 m ).
Reference(s)
(o) Refer to OpsProc 36-22-03C APU Leak Detection Loop

LAN COLOMBIA FLEET MI-36-22 P 3/4

MEL C 27 FEB 15
 MEL ITEMS
36 - PNEUMATIC
36-22 - Leak Detection Loop
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-36-22 P 4/4

MEL 27 FEB 15
 MEL ITEMS
46 - INFORMATION SYSTEMS
46-21 - Air Traffic and Information Management System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

46-21-01 Air Traffic Service Unit (ATSU)

Ident.: MI-46-21-00008795.0002001 / 23 MAR 11
Applicable to: ALL

46-21-01A
Repair interval Nbr installed Nbr required Placard
D 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-46-21 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
46 - INFORMATION SYSTEMS
46-21 - Air Traffic and Information Management System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-46-21 P 2/2

MEL 05 NOV 13
 MEL ITEMS
47 - INERT GAS SYSTEM
47-00 - MAINTENANCE Message on the STATUS SD Page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

47-00-01 FUEL INERT MAINTENANCE Message

Ident.: MI-47-00-00010615.0001001 / 27 FEB 15
1 Applicable to: MSN 5229, 5263-5364

47-00-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
FUEL INERT MAINTENANCE Message may be displayed on the STATUS SD page.

LAN COLOMBIA FLEET MI-47-00 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
47 - INERT GAS SYSTEM
47-00 - MAINTENANCE Message on the STATUS SD Page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-47-00 P 2/2

MEL 27 FEB 15
 MEL ITEMS
47 - INERT GAS SYSTEM
47-10 - Generation/Storage
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

47-10-01 Fuel Tank Inerting System

Ident.: MI-47-10-00014411.0002001 / 27 FEB 15
1 Applicable to: MSN 5178, 5234, 5443-5453

47-10-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative.

LAN COLOMBIA FLEET MI-47-10 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
47 - INERT GAS SYSTEM
47-10 - Generation/Storage
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-47-10 P 2/2

MEL 27 FEB 15
 MEL ITEMS
49 - AIRBORNE AUXILIARY POWER
49-00 - MAINTENANCE Message on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

49-00-01 APU MAINTENANCE Message

Ident.: MI-49-00-00008813.0001001 / 21 MAR 10
Applicable to: ALL

49-00-01A
Repair interval Nbr installed Nbr required Placard
C No
APU MAINTENANCE message may be displayed on the STATUS SD page.

LAN COLOMBIA FLEET MI-49-00 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
49 - AIRBORNE AUXILIARY POWER
49-00 - MAINTENANCE Message on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-49-00 P 2/2

MEL 05 NOV 13
 MEL ITEMS
49 - AIRBORNE AUXILIARY POWER
49-01 - APU Overhead Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

49-01-01 APU MASTER SW pb-sw FAULT light

Ident.: MI-49-01-00008814.0001001 / 21 MAR 10
Applicable to: ALL

49-01-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the N and the EGT indications are operative on the APU
SD page.

49-01-02 APU MASTER SW pb-sw ON light

Ident.: MI-49-01-00008816.0001001 / 21 MAR 10
Applicable to: ALL

49-01-02A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

49-01-03 APU START pb-sw AVAIL light

Ident.: MI-49-01-00008817.0001001 / 21 MAR 10
Applicable to: ALL

49-01-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided that the N indication is operative on the APU SD page.

LAN COLOMBIA FLEET MI-49-01 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
49 - AIRBORNE AUXILIARY POWER
49-01 - APU Overhead Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

49-01-04 APU START pb-sw ON light

Ident.: MI-49-01-00008818.0001001 / 21 MAR 10
Applicable to: ALL

49-01-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative.

LAN COLOMBIA FLEET MI-49-01 P 2/2

MEL D 05 NOV 13
 MEL ITEMS
49 - AIRBORNE AUXILIARY POWER
49-07 - Indications on the APU SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

49-07-01 Indications on the APU SD page

Ident.: MI-49-07-00008821.0001001 / 23 MAR 11
Applicable to: ALL

49-07-01A
Repair interval Nbr installed Nbr required Placard
C 10 0 No
One or more may be inoperative.

LAN COLOMBIA FLEET MI-49-07 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
49 - AIRBORNE AUXILIARY POWER
49-07 - Indications on the APU SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-49-07 P 2/2

MEL 05 NOV 13
 MEL ITEMS
49 - AIRBORNE AUXILIARY POWER
49-10 - Power Plant
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

49-10-01 Power Plant ( APU )

Ident.: MI-49-10-00008819.0002001 / 27 FEB 15
Applicable to: ALL

49-10-01A Non ETOPS flight

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative provided that ETOPS is not conducted.
Reference(s)
(o) Refer to OpsProc 49-10-01A Power Plant (APU)

49-10-01B ETOPS 120 min flight

Repair interval Nbr installed Nbr required Placard
A 1 0 Yes
(o) May be inoperative for four flights provided that ETOPS beyond 120 min is not conducted.
Reference(s)
(o) Refer to OpsProc 49-10-01B Power Plant (APU)

49-10-01C APU deactivated or removed

Repair interval Nbr installed Nbr required Placard
D 1 0 Yes
(o) (m) May be inoperative provided that:
1) ETOPS is not conducted, and
2) The APU is deactivated or removed.
Reference(s)
(o) Refer to OpsProc 49-10-01C Power Plant (APU)
(m) Refer to AMM

LAN COLOMBIA FLEET MI-49-10 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
49 - AIRBORNE AUXILIARY POWER
49-10 - Power Plant
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

49-10-02 APU Air Intake Flap

Ident.: MI-49-10-00008820.0001001 / 12 SEP 11
Applicable to: ALL

49-10-02A APU not used

Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative in the closed position provided that the APU is not used.

49-10-02B APU used

Repair interval Nbr installed Nbr required Placard
A 1 0 No
(m) May be inoperative in the open position for 10 days.
Reference(s)
(m) Refer to AMM

LAN COLOMBIA FLEET MI-49-10 P 2/2

MEL B 27 FEB 15
 MEL ITEMS
52 - DOORS
52-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 52-01-01 - CKPT DOOR CONT Normal Overhead Panel
MINIMUM EQUIPMENT LIST

52-01-01-01 CHAN (1, 2) LEDs on the CKPT DOOR CONT Overhead Panel
Ident.: MI-52-01-01-00008677.0001001 / 23 MAR 11
Applicable to: ALL

52-01-01-01A On Normal CKPT DOOR CONT Panel

Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or more may be inoperative provided the FAULT light on the COCKPIT DOOR Panel is
checked operative.

52-01-01-02 STRIKE (TOP, MID, BOT) LEDs on the

CKPT DOOR CONT Overhead Panel
Ident.: MI-52-01-01-00008678.0001001 / 23 MAR 11
Applicable to: ALL

52-01-01-02A
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
One or more may be inoperative provided the FAULT light on the COCKPIT DOOR Panel is
checked operative.

52-01-01-03 Pressure Rate Sensor on the CKPT DOOR CONT Overhead Panel
Ident.: MI-52-01-01-00008679.0001001 / 10 OCT 14
Applicable to: ALL

52-01-01-03A One inoperative

Repair interval Nbr installed Nbr required Placard
A 2 1 Yes
(m) One may be inoperative for 60 consecutive calendar days provided that the remaining
pressure rate sensor is checked operative.
Reference(s)
(m) Refer to AMM 52-51-00-040-011
Continued on the following page

LAN COLOMBIA FLEET MI-52-01-01 P 1/2

MEL A to C 10 OCT 14
 MEL ITEMS
52 - DOORS
52-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 52-01-01 - CKPT DOOR CONT Normal Overhead Panel
MINIMUM EQUIPMENT LIST

Continued from the previous page

52-01-01-03B Both inoperative
Repair interval Nbr installed Nbr required Placard
A 2 0 No
Both may be inoperative for two flight days provided that the CDLS normal system is
considered inoperative.
Refer to Item 52-51-01 CDLS Normal System(Normal Control Unit, Toggle Switch and
Lights on Cockpit Door Panel, Buzzer, Keypad, Door Strike Release). .

LAN COLOMBIA FLEET MI-52-01-01 P 2/2

MEL C 10 OCT 14
 MEL ITEMS
52 - DOORS
52-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-07-01 Passenger Door Permanently Indicated

Open on the DOOR/OXY SD page
Ident.: MI-52-07-00008777.0001001 / 10 OCT 14
Applicable to: ALL

52-07-01A Check of associated door and 'C' repair interval

Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) One or more may be permanently indicated open when actually closed provided that:
1) The associated door is visually checked to be closed and locked before each flight, and
2) The white SLIDE ARMED light on the associated door does not come on when the door
is closed and locked and the slide arming lever is in the armed position.
Reference(s)
(o) Refer to OpsProc 52-07-01A Passenger Door/Emergency Exit Permanently Indicated Open
on the DOOR/OXY SD page (SLIDE ARMED light operative)

52-07-01B Check of associated door and 'B' repair interval

Repair interval Nbr installed Nbr required Placard
B 4 0 No
(o) One or more may be permanently indicated open when actually closed provided that the
associated door is visually checked to be closed and locked before each flight.
Reference(s)
(o) Refer to OpsProc 52-07-01B Passenger Door/Emergency Exit Permanently Indicated Open
on the DOOR/OXY SD page (SLIDE ARMED light may be permanently illuminated)

52-07-01C No night operations

Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) One or more may be permanently indicated open when actually closed provided that:
1) The aircraft is not operated at night, and
2) The associated door is visually checked to be closed and locked before each flight.
Continued on the following page

LAN COLOMBIA FLEET MI-52-07 P 1/6

MEL A 10 OCT 14
 MEL ITEMS
52 - DOORS
52-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 52-07-01C Passenger Door/Emergency Exit Permanently Indicated Open
on the DOOR/OXY SD page (SLIDE ARMED light may be permanently illuminated)

52-07-01D Slide of the associated door not armed

Repair interval Nbr installed Nbr required Placard
B 4 3 No
(o) One may be permanently indicated open when actually closed provided that:
1) The associated door is visually checked to be closed and locked before each flight, and
2) The slide of the associated door is not armed, and
3) The associated door is considered inoperative.
Refer to Item 52-10-01 Cabin Passenger Door
Reference(s)
(o) Refer to OpsProc 52-07-01D Passenger Door/Emergency Exit Permanently Indicated Open
on the DOOR/OXY SD page (SLIDE ARMED light may be permanently illuminated)

52-07-02 Passenger Door Permanently Indicated

Closed on the DOOR/OXY SD page
Ident.: MI-52-07-00008779.0001001 / 10 OCT 14
Applicable to: ALL

52-07-02A No night operations

Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) One or more may be permanently indicated closed when actually open provided that:
1) The aircraft is not operated at night, and
2) The associated door is visually checked to be closed and locked before each flight.
Reference(s)
(o) Refer to OpsProc 52-07-02A Passenger Door/Emergency Exit Permanently Indicated
Closed on the DOOR/OXY SD page
Continued on the following page

LAN COLOMBIA FLEET MI-52-07 P 2/6

MEL A to B 10 OCT 14
 MEL ITEMS
52 - DOORS
52-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

52-07-02B Check of associated door
Repair interval Nbr installed Nbr required Placard
B 4 3 No
(o) One may be permanently indicated closed when actually open provided that:
1) The associated door is visually checked to be closed and locked before each flight, and
2) The associated door is considered inoperative.
Refer to Item 52-10-01 Cabin Passenger Door
Reference(s)
(o) Refer to OpsProc 52-07-02B Passenger Door/Emergency Exit Permanently Indicated
Closed on the DOOR/OXY SD page

52-07-03 Overwing Emergency Exit Permanently

Indicated Open on the DOOR/OXY SD page
Ident.: MI-52-07-00008780.0001001 / 10 OCT 14
Applicable to: ALL

52-07-03A Check of associated exit and 'C' repair interval

Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) (m) One or more may be permanently indicated open when actually closed provided that:
1) The associated exit is visually checked to be closed and locked before each flight, and
2) The associated SLIDE indication is displayed in white on the DOOR/OXY SD page .
Reference(s)
(o) Refer to OpsProc 52-07-03A Overwing Emergency Exit Permanently Indicated Open on the
DOOR/OXY SD page
(m) Refer to AMM 52-70-00-040-010

52-07-03B Check of associated exit and 'B' repair interval

Repair interval Nbr installed Nbr required Placard
B 4 0 No
(o) (m) One or more may be permanently indicated open when actually closed provided that the
associated exit is visually checked to be closed and locked before each flight.
Continued on the following page

LAN COLOMBIA FLEET MI-52-07 P 3/6

MEL B to C 10 OCT 14
 MEL ITEMS
52 - DOORS
52-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 52-07-03B Overwing Emergency Exit Permanently Indicated Open on the
DOOR/OXY SD page
(m) Refer to AMM 52-70-00-040-010

52-07-03C No night operations

Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) (m) One or more may be permanently indicated open when actually closed provided that:
1) The aircraft is not operated at night, and
2) The associated exit is visually checked to be closed and locked before each flight.
Reference(s)
(o) Refer to OpsProc 52-07-03C Overwing Emergency Exit Permanently Indicated Open on the
DOOR/OXY SD page
(m) Refer to AMM 52-70-00-040-010

52-07-03D Both exits on the same side considered inoperative

Repair interval Nbr installed Nbr required Placard
B 4 3 No
(o) (m) One may be permanently indicated open when actually closed provided that:
1) The associated exit is visually checked to be closed and locked before each flight, and
2) Both exits on the same side are considered inoperative.
Refer to Item 52-10-02 Overwing Emergency Exit
Reference(s)
(o) Refer to OpsProc 52-07-03D Overwing Emergency Exit Permanently Indicated Open on the
DOOR/OXY SD page
(m) Refer to AMM 52-70-00-040-010

LAN COLOMBIA FLEET MI-52-07 P 4/6

MEL C 10 OCT 14
 MEL ITEMS
52 - DOORS
52-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-07-04 Overwing Emergency Exit Permanently

Indicated Closed on the DOOR/OXY SD page
Ident.: MI-52-07-00008781.0001001 / 10 OCT 14
Applicable to: ALL

52-07-04A No night operations

Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) (m) One or more may be permanently indicated closed when actually open provided that:
1) The aircraft is not operated at night, and
2) The associated exit is visually checked to be closed and locked before each flight.
Reference(s)
(o) Refer to OpsProc 52-07-04A Overwing Emergency Exit Permanently Indicated Closed on
the DOOR/OXY SD page
(m) Refer to AMM 52-70-00-040-011

52-07-04B Both exits on the same side considered inoperative

Repair interval Nbr installed Nbr required Placard
B 4 3 No
(o) (m) One may be permanently indicated closed when actually open provided that:
1) The associated exit is visually checked to be closed and locked before each flight, and
2) Both exits on the same side are considered inoperative.
Refer to Item 52-10-02 Overwing Emergency Exit
Reference(s)
(o) Refer to OpsProc 52-07-04B Overwing Emergency Exit Permanently Indicated Closed on
the DOOR/OXY SD page
(m) Refer to AMM 52-70-00-040-011

LAN COLOMBIA FLEET MI-52-07 P 5/6

MEL D 10 OCT 14
 MEL ITEMS
52 - DOORS
52-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-07-05 Cargo Door Indication on the DOOR/OXY SD page

Ident.: MI-52-07-00008782.0001001 / 23 MAR 11
Applicable to: ALL

52-07-05A
Repair interval Nbr installed Nbr required Placard
C 3 0 No
(o) (m) One or more may be inoperative provided that the associated door is visually checked to be
closed and locked before each flight.
Reference(s)
(o) Refer to OpsProc 52-07-05A Cargo Door Indication on the DOOR/OXY SD page
(m) Refer to AMM 52-70-00-040-001

52-07-06 Avionics Compartment Access Door

Indication on the DOOR/OXY SD page
Ident.: MI-52-07-00008784.0001001 / 23 MAR 11
Applicable to: ALL

52-07-06A
Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) (m) One or more may be inoperative provided that the associated door is visually checked to be
closed and locked before each flight.
Reference(s)
(o) Refer to OpsProc 52-07-06A Avionics Compartment Access Door Indication on the
DOOR/OXY SD page
(m) Refer to AMM 52-70-00-040-004

LAN COLOMBIA FLEET MI-52-07 P 6/6

MEL E to F 10 OCT 14
 MEL ITEMS
52 - DOORS
52-10 - Passenger/Crew Door
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-10-01 Cabin Passenger Door

Ident.: MI-52-10-00008689.0001001 / 10 OCT 14
Applicable to: ALL

52-10-01A
Repair interval Nbr installed Nbr required Placard
B 4 3 No
Only one may be inoperative provided:
1) The total number of passengers on board should not exceed of 114, and
2) All other main entry doors and overwing emergency exit are fully operational, and
3) Affected door is not used for passenger load, and
4) A conspicuous barrier strap or rope and a placard stating that the door is inoperative
shall be placed across the inoperative door, and
5) Emergency exit sign and proximity lights associated with the inoperative exit must be
covered to obscure the sign and lights, and
6) Passenger must be briefed not to use the affected door, and
7) All passenger seats in excess of 114 must be blocked for take off and landing, and
8) The following number of passenger seats must be blocked for takeoff and landing:
a) For aircraft with 156 passenger seats 42 seats immediately adjacent to the
inoperative door across the entire width of the airplane must be blocked for take off and
landing.
b) For aircraft with 168 passenger seats : 54 seats immediately adjacent to the
inoperative door across the entire width of the airplane must be blocked for take off and
landing, and
c) For aircraft with 174 passenger seats : 60 seats immediately adjacent to the
inoperative door across the entire width of the airplane must be blocked for take off and
landing, and
9) All passenger seats affected shall be blocked with a conspicuous tapes or ropes that
contrast with the interior prior to passenger loading. Only the seats in these areas shall
be blocked. Main passenger aisles, cross aisles and exits areas must not be blocked,
and
10) Conspicuous signs and placard shall be placed in appropriate locations indicating these
seats are not to be occupied by passengers for take off and landing.
Note: Weight and balance manifest must be revised.
Note: Cabin attendants may be stationed in vicinity of each door within blocked area
Continued on the following page

LAN COLOMBIA FLEET MI-52-10 P 1/6

MEL A 10 OCT 14
 MEL ITEMS
52 - DOORS
52-10 - Passenger/Crew Door
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Note: The maintenance procedure for load adjustment of the control handle is applied
before the first flight under this item, if the emergency escape slide is removed.

LAN COLOMBIA FLEET MI-52-10 P 2/6

MEL A 10 OCT 14
 MEL ITEMS
52 - DOORS
52-10 - Passenger/Crew Door
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-10-02 Overwing Emergency Exit

Ident.: MI-52-10-00008690.0001001 / 10 OCT 14
Applicable to: ALL

52-10-02A
Repair interval Nbr installed Nbr required Placard
B 4 3 No
Only one may be inoperative provided :
1) Both overwing emergency exits on the same side are considered inoperative.
2) The total number of passengers on board shall not exceed of 90, and
3) All other main entry doors and operative overwing emergency exit are fully operational,
and
4) A conspicuous barrier strap or rope and a placard stating that the overwing emergency
exit is inoperative shall be place across the inoperative exit, and
5) Emergency exit sign and floor proximity lights associated with the inoperative exit must
be covered to obscure the signs and lights, and
6) Passenger must be briefed not to use the affected emergency exit, and
7) All passenger seats in excess of 90 must be blocked for take off and landing, and
8) The following passenger seats rows must be blocked for takeoff and landing:
a) For aircraft with 156 passenger seats: - Two passenger seats rows forward and nine
passenger seats rows aft of the inoperative overwing emergency exit across the entire
width of the airplane must be blocked for take off and landing.
b) For aircraft with 168 passenger seats: - Two passenger seats rows forward and
eleven passenger seats rows aft of the inoperative overwing emergency exit across the
entire width of the airplane must be blocked for take off and landing, and
c) For aircraft with 174 passenger seats: - Two passenger seats rows forward and
twelve passenger seats rows aft of the inoperative overwing emergency exit across the
entire width of the airplane must be blocked for take off and landing, and
9) All passenger seats affected shall be blocked off with a conspicuous tapes of ropes that
contrast with the interior prior to passenger loading. Only the seats in these areas shall
be blocked. Main aisles and exits areas must not be blocked, and
10) Conspicuous signs and placard shall be placed in appropriate locations indicating these
seats are not to be occupied by passengers for take off and landing.
Note: Weight and balance manifest must be revised.
Note: Attendants may be stationed in vicinity of each exit within blocked areas.
Continued on the following page

LAN COLOMBIA FLEET MI-52-10 P 3/6

MEL B 10 OCT 14
 MEL ITEMS
52 - DOORS
52-10 - Passenger/Crew Door
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Note: When an overwing emergency exit is inoperative, both emergency exits on the
same side are considered inoperative.

52-10-03 Passenger Exit Stop Fitting

Ident.: MI-52-10-00008691.0001001 / 23 MAR 11
Applicable to: ALL

52-10-03A
Repair interval Nbr installed Nbr required Placard
C 56 52 No
A maximum of one per exit may be inoperative provided that the flight is not pressurized.

52-10-04 Door Damper Function

Ident.: MI-52-10-00008692.0001001 / 10 OCT 14
Applicable to: ALL

52-10-04A
Repair interval Nbr installed Nbr required Placard
D 4 0 No
One or more may be inoperative.

52-10-05 Door Emergency Opening Function

Ident.: MI-52-10-00008693.0001001 / 10 OCT 14
Applicable to: ALL

52-10-05A
Repair interval Nbr installed Nbr required Placard
B 4 3 No
One may be inoperative provided that the affected door is considered inoperative.
Refer to Item 52-10-01 Cabin Passenger Door

LAN COLOMBIA FLEET MI-52-10 P 4/6

MEL B to E 10 OCT 14
 MEL ITEMS
52 - DOORS
52-10 - Passenger/Crew Door
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-10-06 CHECK DOOR PRESSURE Message

on the Flight Attendant Panel (FAP)
Ident.: MI-52-10-00008694.0004001 / 10 OCT 14
Applicable to: ALL

52-10-06A
Repair interval Nbr installed Nbr required Placard
D 4 0 No
(m) One or more messages may be displayed provided that the door bottle pressure is checked
on the associated bottle pressure gauge before the first MEL dispatch and then every 8
days.
Reference(s)
(m) Refer to AMM 52-00-00-040-003

52-10-07 Passenger Door Stay Mechanism

Ident.: MI-52-10-00008695.0001001 / 10 OCT 14
Applicable to: ALL

52-10-07A
Repair interval Nbr installed Nbr required Placard
B 4 3 No
One may be inoperative provided that the affected door is considered inoperative.
Refer to Item 52-10-01 Cabin Passenger Door

52-10-08 CABIN PRESSURE light (on Doors)

Ident.: MI-52-10-00008696.0001001 / 10 OCT 14
Applicable to: ALL

52-10-08A
Repair interval Nbr installed Nbr required Placard
C 4 0 No
One or more may be inoperative.

LAN COLOMBIA FLEET MI-52-10 P 5/6

MEL F to H 10 OCT 14
 MEL ITEMS
52 - DOORS
52-10 - Passenger/Crew Door
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-52-10 P 6/6

MEL 10 OCT 14
 MEL ITEMS
52 - DOORS
52-30 - Cargo Door
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-30-01 Cargo Door (FWD, AFT and BULK)

Ident.: MI-52-30-00008733.0001001 / 12 SEP 11
Applicable to: ALL

52-30-01A Cargo door indicated locked on the DOOR/OXY SD page

Repair interval Nbr installed Nbr required Placard
C 3 0 No
One or more may be inoperative in the closed and locked position provided that they are
indicated locked on the DOOR/OXY SD page.

52-30-01B Visual check of the cargo door

Repair interval Nbr installed Nbr required Placard
C 3 0 No
(m) One or more may be inoperative in the closed and locked position provided that the
associated cargo door is visually checked to be closed and locked before each flight.
Reference(s)
(m) Refer to AMM 52-30-00-040-001

52-30-02 Cargo Door Actuator

Ident.: MI-52-30-00008734.0002001 / 12 SEP 11
Applicable to: ALL

52-30-02A A maximum of one actuator inoperative per cargo door

Repair interval Nbr installed Nbr required Placard
C 4 2 No
A maximum of one per cargo door may be inoperative provided that:
1) The integrity of the yellow hydraulic system is not affected, and
2) The wind velocity during loading and unloading operations is below 30 kt, and
3) The operation of the door with a single actuator is limited to 100 open/close cycles.
Continued on the following page

LAN COLOMBIA FLEET MI-52-30 P 1/4

MEL A to B 05 NOV 13
 MEL ITEMS
52 - DOORS
52-30 - Cargo Door
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

52-30-02B One or more actuator inoperative
Repair interval Nbr installed Nbr required Placard
C 4 0 No
(m) One or more may be inoperative provided that:
1) The integrity of the yellow hydraulic system is not affected, and
2) The associated cargo door is manually closed and locked.
Reference(s)
(m) Refer to AMM 52-36-00-040-001

52-30-03 Cargo Door Electrical Control

Ident.: MI-52-30-00008737.0001001 / 12 SEP 11
Applicable to: ALL

52-30-03A Cargo door operated using hand pump

Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or more may be inoperative provided that the associated cargo doors can be operated
using the hand pump.

52-30-03B Cargo door considered inoperative

Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or more may be inoperative provided that the associated cargo doors are considered
inoperative.
Refer to Item 52-30-01 Cargo Door (FWD, AFT and BULK)

LAN COLOMBIA FLEET MI-52-30 P 2/4

MEL B to C 05 NOV 13
 MEL ITEMS
52 - DOORS
52-30 - Cargo Door
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-30-04 Cargo Door Locking Hooks and Spools (Rollers)

Ident.: MI-52-30-00008739.0001001 / 18 MAY 11
Applicable to: ALL

52-30-04A
Repair interval Nbr installed Nbr required Placard
C 24 22 No
A maximum of one locking hook or one spool per cargo door may be inoperative provided
that:
1) All the others have no damage, and
2) The flight is not pressurized.

52-30-05 Cargo Door Hand Pump

Ident.: MI-52-30-00008741.0001001 / 21 MAR 10
Applicable to: ALL

52-30-05A
Repair interval Nbr installed Nbr required Placard
C 1 0 No
May be inoperative provided that the integrity of the yellow hydraulic system is not affected.

52-30-06 Cargo Door Drift Pin

Ident.: MI-52-30-00008742.0001001 / 21 MAR 10
Applicable to: ALL

52-30-06A
Repair interval Nbr installed Nbr required Placard
A 4 0 No
One or both on each cargo door may be inoperative for one flight.

LAN COLOMBIA FLEET MI-52-30 P 3/4

MEL D to F 05 NOV 13
 MEL ITEMS
52 - DOORS
52-30 - Cargo Door
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-30-07 Cargo Doors Open/Locked Indicator light

Ident.: MI-52-30-00008743.0001001 / 21 MAR 10
Applicable to: ALL

52-30-07A
Repair interval Nbr installed Nbr required Placard
D 2 0 No
(o) One or both may be inoperative provided that the associated cargo door is in the fully open
position during loading and unloading operations.
Reference(s)
(o) Refer to OpsProc 52-30-07A Cargo Door Open/Locked Indicator light

LAN COLOMBIA FLEET MI-52-30 P 4/4

MEL G 05 NOV 13
 MEL ITEMS
52 - DOORS
52-33 - Bulk Cargo Compartment Door
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-33-01 Cargo Door Balance Mechanism

Ident.: MI-52-33-00008746.0001001 / 27 FEB 15
Applicable to: ALL

52-33-01A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(m) May be inoperative or damaged provided that:
1) A safety hold device is used to maintain the cargo door in the open position during
loading and unloading operations, and
2) The associated cargo door is visually checked to be closed and locked.
Reference(s)
(m) Refer to AMM 52-33-00-040-001

LAN COLOMBIA FLEET MI-52-33 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
52 - DOORS
52-33 - Bulk Cargo Compartment Door
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-52-33 P 2/2

MEL 27 FEB 15
 MEL ITEMS
52 - DOORS
52-51 - Reinforced Cockpit Door (CDLS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-51-01 CDLS Normal System (Normal Control Unit, Toggle Switch and
Lights on Cockpit Door Panel, Buzzer, Keypad, Door Strike Release).
Ident.: MI-52-51-00008750.0001001 / 10 OCT 14
Applicable to: ALL

52-51-01B
Repair interval Nbr installed Nbr required Placard
A 1 0 Yes
(o) Any part of the Normal System may be inoperative provided:
1) Normal System is deactivated in unlocked position, and
2) Deadbolt is operative and used for locking and unlocking the cockpit door, and
3) Interphone between the cabin and cockpit is operative, and
4) Two persons must be permanently present in the cockpit throughout the flight, and
5) Repairs are made within two flight days.
Reference(s)
(o) Refer to OpsProc 52-51-01B Normal System

52-51-03 CDLS Buzzer

Ident.: MI-52-51-00008754.0001001 / 27 NOV 12
Applicable to: ALL

52-51-03A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided :
1) The interphone system between the cabin and the cockpit is operative, and
2) A protocol of routine access via the cabin/cockpit interphone system is established by
captain in-command before each flight, and
3) Flight attendant must be informed of the protocol of routine access that will be used by
captain in-command.

LAN COLOMBIA FLEET MI-52-51 P 1/4

MEL A to B 27 FEB 15
 MEL ITEMS
52 - DOORS
52-51 - Reinforced Cockpit Door (CDLS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-51-04 CDLS Keypad

Ident.: MI-52-51-00008759.0001001 / 18 MAY 11
Applicable to: ALL

52-51-04A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) (m) May be inoperative provided that:
1) The interphone system between the cabin and the cockpit is operative, and
2) The CDLS keypad is deactivated.
Reference(s)
(o) Refer to OpsProc 52-51-04A CDLS Keypad
(m) Refer to AMM 52-51-00-040-007

52-51-05 CDLS Keypad LED

Ident.: MI-52-51-00008762.0001001 / 10 OCT 14
Applicable to: ALL

52-51-05A
Repair interval Nbr installed Nbr required Placard
C 3 0 Yes
(o) May be inoperative
Reference(s)
(o) Refer to OpsProc 52-51-05A LEDS

LAN COLOMBIA FLEET MI-52-51 P 2/4

MEL C to D 27 FEB 15
 MEL ITEMS
52 - DOORS
52-51 - Reinforced Cockpit Door (CDLS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-51-06 CDLS Door Release Strike (Catch, Spring, Solenoid, Bolt)

Ident.: MI-52-51-00008764.0001001 / 27 NOV 12
Applicable to: ALL

52-51-06A
Repair interval Nbr installed Nbr required Placard
D 3 2 No
(m) One may be inoperative for overflight USA territory
Note: Apply the maintenance procedure only when the inoperative door release strike is
failed in the locked position.
Reference(s)
(m) Refer to AMM 52-51-00-040-010

52-51-06B
Repair interval Nbr installed Nbr required Placard
C 3 1 No
(m) Except for overflight USA territory, one or two may be inoperative.
Note: Apply the maintenance procedure only when the inoperative door release strike is
failed in the locked position.
Reference(s)
(m) Refer to AMM 52-51-00-040-010

52-51-07 CDLS Deadbolt

Ident.: MI-52-51-00008766.0001001 / 27 FEB 15
Applicable to: ALL

52-51-07A
Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
May be inoperative provided automatic lock function operate normally.

LAN COLOMBIA FLEET MI-52-51 P 3/4

MEL E to F 27 FEB 15
 MEL ITEMS
52 - DOORS
52-51 - Reinforced Cockpit Door (CDLS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-52-51 P 4/4

MEL 27 FEB 15
 MEL ITEMS
52 - DOORS
52-53 - COCKPIT DOOR Panel on the Center Pedestal
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-53-01 COCKPIT DOOR FAULT light

Ident.: MI-52-53-00008768.0001001 / 18 OCT 11
Applicable to: ALL

52-53-01A On COCKPIT DOOR Panel

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative
Reference(s)
(o) Refer to OpsProc 52-53-01A Fault light

52-53-02 COCKPIT DOOR OPEN light

Ident.: MI-52-53-00008770.0001001 / 18 OCT 11
Applicable to: ALL

52-53-02A On COCKPIT DOOR Panel

Repair interval Nbr installed Nbr required Placard
C 1 0 Yes
(o) May be inoperative or fixed on provided that CDLS system operates normally.
Reference(s)
(o) Refer to OpsProc 52-53-02A Open Light

LAN COLOMBIA FLEET MI-52-53 P 1/2

MEL A to B 10 OCT 14
 MEL ITEMS
52 - DOORS
52-53 - COCKPIT DOOR Panel on the Center Pedestal
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-53-03 LOCK Function of the COCKPIT DOOR sw

Ident.: MI-52-53-00008772.0001001 / 10 OCT 14
Applicable to: ALL

52-53-03A
Repair interval Nbr installed Nbr required Placard
A 1 0 Yes
(o) (m) May be inoperative provided:
1) The interphone system between the cabin and the cockpit is operative, and
2) The keypad is deactivated, and
3) At least two people must be permanently present in the cockpit throughout the entire
flight, and
4) Repairs are made within two flight days.
Reference(s)
(o) Refer to OpsProc 52-53-03A Toggle Switch on Cockpit Door Panel. Lock Function
(m) Refer to AMM 52-51-00-040-007

52-53-04 UNLOCK Function of the COCKPIT DOOR sw

Ident.: MI-52-53-00008774.0001001 / 10 OCT 14
Applicable to: ALL

52-53-04A
Repair interval Nbr installed Nbr required Placard
A 1 0 Yes
(o) May be inoperative provided :
1) The interphone system between the cabin and the cockpit is operative, and
2) The LOCK function must not be used, and
3) At least two people must be permanently present in the cockpit throughout the entire
flight., and
4) Repairs are made within two flight days.
Reference(s)
(o) Refer to OpsProc 52-53-04A Toggle Switch on Cockpit Door Panel. Unlock Function

LAN COLOMBIA FLEET MI-52-53 P 2/2

MEL C to D 10 OCT 14
 MEL ITEMS
56 - WINDOWS
56-10 - Cockpit
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

56-10-01 Front Windshield

Ident.: MI-56-10-00008671.0001001 / 21 MAR 10
Applicable to: ALL

Note: A cockpit window with minor damages (as described in the associated maintenance
procedure) is considered operative, but the vision through this cockpit window must be
acceptable to the flight crew.

56-10-01A For SPS Windshields (Except P/N STA320-1-3-1 and STA320-2-3-1) and for
PPG Windshields and for PAL Windshields (Only P/N PAL 06282 & 06283)
Repair interval Nbr installed Nbr required Placard
A 2 2 No
(o) (m) One front windshield external ply may be cracked for ten flights provided that:
1) The other front windshield is not damaged, and
2) The associated windshield heating is deactivated, and
3) The visibility through the associated front windshield is acceptable to the flight crew, and
4) The aircraft is not operated in known or forecast icing conditions.
Reference(s)
(o) Refer to OpsProc 56-10-01A Front Windshield
(m) Refer to AMM 56-10-00-040-001

56-10-01B For SPS Windshields (Except P/N STA320-1-3-1 and STA320-2-3-1) and for
PPG Windshields and for PAL Windshields (Only P/N PAL 06282 & 06283)
Repair interval Nbr installed Nbr required Placard
C 2 2 No
(o) (m) One front windshield may have burn spots in the bus bar area beyond the limits provided
that:
1) The other front windshield is not damaged, and
2) The associated windshield heating is deactivated, and
3) The visibility through the associated front windshield is acceptable to the flight crew, and
4) The aircraft is not operated in known or forecast icing conditions.
Continued on the following page

LAN COLOMBIA FLEET MI-56-10 P 1/4

MEL A 27 FEB 15
 MEL ITEMS
56 - WINDOWS
56-10 - Cockpit
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Reference(s)
(o) Refer to OpsProc 56-10-01B Front Windshield
(m) Refer to AMM 56-10-00-040-001

56-10-01C For SPS Windshields (only P/N STA320-1-3-1 and STA320-2-3-1)

Repair interval Nbr installed Nbr required Placard
A 2 2 No
(o) (m) One front windshield external ply may be cracked for one flight provided that:
1) The other front windshield is not damaged, and
2) The associated windshield heating is deactivated, and
3) The visibility through the associated front windshield is acceptable to the flight crew, and
4) The aircraft is not operated in known or forecast icing conditions.
Reference(s)
(o) Refer to OpsProc 56-10-01C Front Windshield
(m) Refer to AMM 56-10-00-040-001

56-10-01D For SPS Windshields (only P/N STA320-1-3-1 and STA320-2-3-1)

Repair interval Nbr installed Nbr required Placard
C 2 2 No
(o) (m) One front windshield may have burn spots in the bus bar area beyond the limits provided
that:
1) The other front windshield is not damaged, and
2) The associated windshield heating is deactivated, and
3) The visibility through the associated front windshield is acceptable to the flight crew, and
4) The aircraft is not operated in known or forecast icing conditions.
Reference(s)
(o) Refer to OpsProc 56-10-01D Front Windshield
(m) Refer to AMM 56-10-00-040-001

LAN COLOMBIA FLEET MI-56-10 P 2/4

MEL A 27 FEB 15
 MEL ITEMS
56 - WINDOWS
56-10 - Cockpit
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

56-10-02 Lateral Fixed/Sliding Window

Ident.: MI-56-10-00008673.0001001 / 27 FEB 15
Applicable to: ALL

Note: A cockpit window with minor damages (as described in the associated inspection
procedure) is considered operative, but the vision through this cockpit window must be
acceptable to the flight crew.

56-10-02A For Acrylic Window (LUCAS/ACT Supplier, P/N starting with NH)
Repair interval Nbr installed Nbr required Placard
C 4 4 No
(m) One or more lateral windows may have burn spots in the bus bar area provided that:
1) The diameter of the mark is less than 10 mm, and
2) The associated lateral window heating is deactivated, and
3) The visibility through the affected lateral window is acceptable to the flight crew.
Reference(s)
(m) Refer to AMM Task 56-10-00-040-002

56-10-02B For Glass Window (SPS Supplier (P/N starting with SPS) and PPG Supplier
(P/N starting with NP))
Repair interval Nbr installed Nbr required Placard
A 4 4 No
External ply may be cracked for one flight provided that:
1) The other lateral windows are not damaged, and
2) The visibility through the affected lateral window is acceptable to the flight crew.
Continued on the following page

LAN COLOMBIA FLEET MI-56-10 P 3/4

MEL B 27 FEB 15
 MEL ITEMS
56 - WINDOWS
56-10 - Cockpit
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

56-10-02C For Glass Window (SPS Supplier (P/N starting with SPS) and PPG Supplier
(P/N starting with NP))
Repair interval Nbr installed Nbr required Placard
C 4 4 No
One or more lateral windows may have burn spots in the bus bar area provided that:
1) The diameter of the mark is less than 10 mm, and
2) The visibility through the affected lateral window is acceptable to the flight crew.

56-10-03 Sliding Window Opening/Closing Mechanism

Ident.: MI-56-10-00008675.0001001 / 21 MAR 10
Applicable to: ALL

56-10-03A
Repair interval Nbr installed Nbr required Placard
2 2 No
Both must be operative.

LAN COLOMBIA FLEET MI-56-10 P 4/4

MEL B to C 27 FEB 15
 MEL ITEMS
56 - WINDOWS
56-20 - Cabin
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

56-20-01 Cabin Window

Ident.: MI-56-20-00008676.0001001 / 23 MAR 11
Applicable to: ALL

56-20-01A
Repair interval Nbr installed Nbr required Placard
C 80 0 No
One or more may be cracked provided that the flight is not pressurized.

LAN COLOMBIA FLEET MI-56-20 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
56 - WINDOWS
56-20 - Cabin
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-56-20 P 2/2

MEL 05 NOV 13
 MEL ITEMS
70 - ENGINE
70-00 - MAINTENANCE Messages on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

70-00-01 ENG FADEC MAINTENANCE Message

Ident.: MI-70-00-00008668.0002001 / 10 OCT 14
Applicable to: MSN 4758-4972

70-00-01A For Engines Not Affected by CFM VSB 73-0241

Repair interval Nbr installed Nbr required Placard
C No
ENG FADEC MAINTENANCE message may be displayed on the STATUS SD page

70-00-01B For Engines Affected by CFM VSB 73-0241

Repair interval Nbr installed Nbr required Placard
A No
ENG FADEC MAINTENANCE message may be displayed on the STATUS SD page for 25
flight hours or 3 days, whichever occurs first.

70-00-01C For Engines Affected by CFM VSB 73-0241

Repair interval Nbr installed Nbr required Placard
C No
(m) ENG FADEC MAINTENANCE message may be displayed on the STATUS SD page
provided it is checked before the first flight of each day that the CFDS does not report any
fault on a T12 sensor.
Reference(s)
(m) Refer to AMM Task 73-29-00-040-001

LAN COLOMBIA FLEET MI-70-00 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
70 - ENGINE
70-00 - MAINTENANCE Messages on the STATUS SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

70-00-01 ENG FADEC MAINTENANCE Message

Ident.: MI-70-00-00008668.0001001 / 27 FEB 15
Applicable to: MSN 4516-4546, 5178-5453

70-00-01A
Repair interval Nbr installed Nbr required Placard
C No
ENG FADEC MAINTENANCE message may be displayed on the STATUS SD page.

70-00-02 ENG EIU MAINTENANCE Message

Ident.: MI-70-00-00008669.0001001 / 21 MAR 10
Applicable to: ALL

70-00-02A
Repair interval Nbr installed Nbr required Placard
C No
ENG EIU MAINTENANCE message may be displayed on the STATUS SD page.

70-00-03 ENG EVMU MAINTENANCE Message

Ident.: MI-70-00-00008670.0001001 / 21 MAR 10
Applicable to: ALL

70-00-03A
Repair interval Nbr installed Nbr required Placard
C No
ENG EVMU MAINTENANCE message may be displayed on the STATUS SD page.

LAN COLOMBIA FLEET MI-70-00 P 2/2

MEL A to C 27 FEB 15
 MEL ITEMS
73 - ENGINE FUEL AND CONTROL
73-07 - Indications on the ENGINE SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

73-07-01 Fuel Used Indication on the ENGINE SD page

Ident.: MI-73-07-00008664.0002001 / 27 FEB 15
Applicable to: ALL

73-07-01A One indication inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative provided that:
1) The fuel quantity indication on the associated tanks are operative on the FUEL SD page
, and
2) The Fuel Used 1+2 Indication is considered inoperative.
Refer to Item 28-07-06-02 Fuel Used 1+2 Indication on the FUEL SD page

73-07-01B Both indicationS inoperative

Repair interval Nbr installed Nbr required Placard
C 2 0 No
Both may be inoperative provided that:
1) ETOPS is not conducted, and
2) The fuel quantity indications of the associated tanks are operative on the FUEL SD page
, and
3) The Fuel Used 1+2 Indication is considered inoperative.
Refer to Item 28-07-06-02 Fuel Used 1+2 Indication on the FUEL SD page

73-07-02 Fuel Filter Clog Indication on the ENGINE SD page

Ident.: MI-73-07-00008665.0001001 / 21 MAR 10
Applicable to: ALL

73-07-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

LAN COLOMBIA FLEET MI-73-07 P 1/2

MEL A to B 27 FEB 15
 MEL ITEMS
73 - ENGINE FUEL AND CONTROL
73-07 - Indications on the ENGINE SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-73-07 P 2/2

MEL 27 FEB 15
 MEL ITEMS
73 - ENGINE FUEL AND CONTROL
73-08 - Indications on the EWD
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

73-08-01 Fuel Flow Indication on the EWD

Ident.: MI-73-08-00008666.0002001 / 27 FEB 15
Applicable to: ALL

73-08-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative provided that the Fuel Flow 1+2 Indication on the FUEL SD page is
considered inoperative.
Refer to Item 28-07-05-01 Fuel Flow 1+2 Indication on the FUEL SD Page

LAN COLOMBIA FLEET MI-73-08 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
73 - ENGINE FUEL AND CONTROL
73-08 - Indications on the EWD
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-73-08 P 2/2

MEL 27 FEB 15
 MEL ITEMS
73 - ENGINE FUEL AND CONTROL
73-09 - ECAM Alert
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

73-09-01 ENG 1(2) FUEL FILTER CLOG Alert

Ident.: MI-73-09-00008667.0001001 / 27 FEB 15
Applicable to: ALL

73-09-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(m) One may be displayed provided that:
1) The alert is confirmed to be false by troubleshooting, and
2) The associated filter is replaced every day.
Reference(s)
(m) Refer to AMM

LAN COLOMBIA FLEET MI-73-09 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
73 - ENGINE FUEL AND CONTROL
73-09 - ECAM Alert
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-73-09 P 2/2

MEL 27 FEB 15
 MEL ITEMS
73 - ENGINE FUEL AND CONTROL
73-10 - Distribution
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

73-10-01 Fuel Return Valve

Ident.: MI-73-10-00008653.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

73-10-01A Inoperative in closed position

Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative in the closed position on one engine provided that the APU and the
AC auxiliary generation are operative.

73-10-01B Inoperative in open position

Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative in the open position provided that the four wing tank pumps
are operative.

73-10-03 Fuel Metering Valve

Ident.: MI-73-10-00008655.0001001 / 12 SEP 12
Applicable to: ALL

73-10-03A
Repair interval Nbr installed Nbr required Placard
2 2 No
Both must be operative.

LAN COLOMBIA FLEET MI-73-10 P 1/2

MEL A to B 27 FEB 15
 MEL ITEMS
73 - ENGINE FUEL AND CONTROL
73-10 - Distribution
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

73-10-04 Engine HP Fuel Valve

Ident.: MI-73-10-00008656.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

73-10-04A
Repair interval Nbr installed Nbr required Placard
2 2 No
Both must be operative.

LAN COLOMBIA FLEET MI-73-10 P 2/2

MEL C 27 FEB 15
 MEL ITEMS
73 - ENGINE FUEL AND CONTROL
73-20 - Controlling
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

73-20-01 Flex Takeoff Mode

Ident.: MI-73-20-00008657.0001001 / 21 MAR 10
Applicable to: ALL

73-20-01A
Repair interval Nbr installed Nbr required Placard
D 2 0 No
May be inoperative on one or both engines provided that the maximum thrust is used for
takeoff.

73-20-04 EPR Control Mode

Ident.: MI-73-20-00008660.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

73-20-04A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) The EPR control mode may be inoperative on one or both engines provided that:
1) ETOPS is not conducted, and
2) The rated N1 control mode is operative on both engines ( ENG 1(2) N1 DEGRADED
MODE message is not displayed on the STATUS SD page ), and
3) The Flight Manual performance penalties are applied.
Note: When the EPR Control Mode is inoperative, the Autothrust is inoperative.
Refer to Item 22-30-01 Autothrust (A/THR)
Reference(s)
(o) Refer to OpsProc 73-20-04A EPR Control Mode

LAN COLOMBIA FLEET MI-73-20 P 1/2

MEL A to B 10 OCT 14
 MEL ITEMS
73 - ENGINE FUEL AND CONTROL
73-20 - Controlling
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

73-20-05 Minimum Idle on Ground

Ident.: MI-73-20-00008661.0001001 / 21 MAR 10
Applicable to: ALL

73-20-05A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) One or both may be inoperative provided that the Flight Manual performance penalties are
applied.
Reference(s)
(o) Refer to OpsProc 73-20-05A Minimum Idle on Ground

73-20-06 EEC ACFT 28V Power Supply

Ident.: MI-73-20-00008662.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

73-20-06A
Repair interval Nbr installed Nbr required Placard
C 4 2 No
The channel B power supply may be inoperative on one or both engines.

LAN COLOMBIA FLEET MI-73-20 P 2/2

MEL C to D 10 OCT 14
 MEL ITEMS
74 - IGNITION
74-07 - Indications on the ENGINE SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

74-07-01 Selected Igniter Indication on the ENGINE SD page

Ident.: MI-74-07-00008651.0001001 / 27 FEB 15
Applicable to: ALL

74-07-01A
Repair interval Nbr installed Nbr required Placard
C 4 0 No
(o) One or more may be inoperative provided that the associated ENG 1(2) IGN A(B)(A+B)
FAULT alert is checked operative.
Reference(s)
(o) Refer to OpsProc 74-07-01A Selected Igniter Indication on the ENGINE SD page

LAN COLOMBIA FLEET MI-74-07 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
74 - IGNITION
74-07 - Indications on the ENGINE SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-74-07 P 2/2

MEL 27 FEB 15
 MEL ITEMS
74 - IGNITION
74-09 - ECAM Alert
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

74-09-01 ENG 1(2) IGN A(B)(A+B) FAULT Alert

Ident.: MI-74-09-00008652.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

74-09-01B One displayed

Repair interval Nbr installed Nbr required Placard
C 4 3 No
(m) One may be displayed provided that the associated engine ignition system is checked
operative every day.
Reference(s)
(m) Refer to AMM

74-09-01C Two displayed

Repair interval Nbr installed Nbr required Placard
C 4 2 No
(m) Two may be displayed provided that the associated engine ignition systems are checked
operative before each flight.
Reference(s)
(m) Refer to AMM

74-09-01 ENG 1(2) IGN A(B)(A+B) FAULT Alert

Ident.: MI-74-09-00008652.0002001 / 10 OCT 14
Applicable to: MSN 4516-4546

74-09-01A
Repair interval Nbr installed Nbr required Placard
C 4 2 No
One or two may be displayed.

LAN COLOMBIA FLEET MI-74-09 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
74 - IGNITION
74-09 - ECAM Alert
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-74-09 P 2/2

MEL 27 FEB 15
 MEL ITEMS
74 - IGNITION
74-31 - Ignition Starting and Continuous Relight
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

74-31-01 Ignition System A

Ident.: MI-74-31-00008649.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

74-31-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) One may be inoperative provided that:
1) ETOPS is not conducted, and
2) The associated engine ignition system B is operative.
Reference(s)
(o) Refer to OpsProc 74-31-01A Ignition System A

74-31-01 Ignition System A

Ident.: MI-74-31-00008649.0002001 / 10 OCT 14
Applicable to: MSN 4516-4546

74-31-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) One may be inoperative provided that:
1) ETOPS is not conducted, and
2) The associated engine ignition system B is operative.
Note: System A is considered inoperative on both engines (NO DISPATCH) when the
common power supply line from 401XP 115VAC ESS BUS is inoperative as a
result of either a loss of electrical continuity or a short circuit ( ENGINE/1 AND 2
IGN/SYS A (49VUA03) C/B tripped).
Reference(s)
(o) Refer to OpsProc 74-31-01A Ignition System A

LAN COLOMBIA FLEET MI-74-31 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
74 - IGNITION
74-31 - Ignition Starting and Continuous Relight
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

74-31-02 Ignition System B

Ident.: MI-74-31-00008650.0001001 / 21 MAR 10
Applicable to: ALL

74-31-02A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) One or both may be inoperative.
Reference(s)
(o) Refer to OpsProc 74-31-02A Ignition System B

LAN COLOMBIA FLEET MI-74-31 P 2/2

MEL B 27 FEB 15
 MEL ITEMS
76 - ENGINE CONTROLS
76-11 - Throttle Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

76-11-01 Thrust lever Position Sensor

Ident.: MI-76-11-00008646.0001001 / 21 MAR 10
Applicable to: ALL

76-11-01A
Repair interval Nbr installed Nbr required Placard
A 4 3 No
One may be inoperative on one engine for three days provided that:
1) The A/THR is operative, and
2) Both LGCIUs are operative, and
3) The L/G shock absorbers proximity detectors are operative.

LAN COLOMBIA FLEET MI-76-11 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
76 - ENGINE CONTROLS
76-11 - Throttle Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-76-11 P 2/2

MEL 05 NOV 13
 MEL ITEMS
77 - ENGINE INDICATING
77-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES 77-07-01 - Indications on the CRUISE SD page
MINIMUM EQUIPMENT LIST

77-07-01-01 N1 Vibration Indication on the CRUISE SD page

Ident.: MI-77-07-01-00008609.0001001 / 21 MAR 10
Applicable to: ALL

77-07-01-01A
Repair interval Nbr installed Nbr required Placard

Refer to Item 77-07-02-05 N1 Vibration Indication on the ENGINE SD page

77-07-01-02 N2 Vibration Indication on the CRUISE SD page

Ident.: MI-77-07-01-00008610.0001001 / 21 MAR 10
Applicable to: ALL

77-07-01-02A
Repair interval Nbr installed Nbr required Placard

Refer to Item 77-07-02-06 N2 Vibration Indication on the ENGINE SD page

77-07-01-03 F. USED (Fuel Used) Indication on the CRUISE SD page

Ident.: MI-77-07-01-00008611.0001001 / 21 MAR 10
Applicable to: ALL

77-07-01-03A
Repair interval Nbr installed Nbr required Placard

Refer to Item 73-07-01 Fuel Used Indication on the ENGINE SD page

LAN COLOMBIA FLEET MI-77-07-01 P 1/2

MEL A to C 05 NOV 13
 MEL ITEMS
77 - ENGINE INDICATING
77-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES 77-07-01 - Indications on the CRUISE SD page
MINIMUM EQUIPMENT LIST

77-07-01-04 OIL QT (Oil Quantity) Indication on the CRUISE SD page

Ident.: MI-77-07-01-00008612.0001001 / 21 MAR 10
Applicable to: ALL

77-07-01-04A
Repair interval Nbr installed Nbr required Placard

Refer to Item 79-07-03 Oil Quantity Indication on the ENGINE SD page

LAN COLOMBIA FLEET MI-77-07-01 P 2/2

MEL D 05 NOV 13
 MEL ITEMS
77 - ENGINE INDICATING
77-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES 77-07-02 - Indications on the ENGINE SD page
MINIMUM EQUIPMENT LIST

77-07-02-01 Engine Bleed Pressure Indication on the ENGINE SD page

Ident.: MI-77-07-02-00008629.0001001 / 21 MAR 10
Applicable to: ALL

77-07-02-01A
Repair interval Nbr installed Nbr required Placard

Refer to Item 36-07-04 Engine Bleed Precooler Inlet Pressure Indication on the BLEED SD
page

77-07-02-02 Fuel Filter Clog Indication on the ENGINE SD page

Ident.: MI-77-07-02-00008630.0001001 / 21 MAR 10
Applicable to: ALL

77-07-02-02A
Repair interval Nbr installed Nbr required Placard

Refer to Item 73-07-02 Fuel Filter CLOG Indication on the ENGINE SD page

77-07-02-03 Fuel Used Indication on the ENGINE SD page

Ident.: MI-77-07-02-00008631.0001001 / 21 MAR 10
Applicable to: ALL

77-07-02-03A
Repair interval Nbr installed Nbr required Placard

Refer to Item 73-07-01 Fuel Used Indication on the ENGINE SD page

LAN COLOMBIA FLEET MI-77-07-02 P 1/6

MEL A to C 27 FEB 15
 MEL ITEMS
77 - ENGINE INDICATING
77-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES 77-07-02 - Indications on the ENGINE SD page
MINIMUM EQUIPMENT LIST

77-07-02-04 Nacelle Temperature Indication on the ENGINE SD page

Ident.: MI-77-07-02-00008632.0001001 / 21 MAR 10
Applicable to: ALL

77-07-02-04A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

77-07-02-05 N1 Vibration Indication on the ENGINE SD page

Ident.: MI-77-07-02-00008633.0001001 / 12 SEP 11
Applicable to: ALL

77-07-02-05A One indication inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative.

77-07-02-05B Both indications inoperative

Repair interval Nbr installed Nbr required Placard
A 2 0 No
Both may be inoperative for three flights provided that:
1) ETOPS is not conducted, and
2) No vibration advisory was displayed during the previous flight.

77-07-02-06 N2 Vibration Indication on the ENGINE SD page

Ident.: MI-77-07-02-00008634.0001001 / 12 SEP 11
Applicable to: ALL

77-07-02-06A One indication inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative.
Continued on the following page

LAN COLOMBIA FLEET MI-77-07-02 P 2/6

MEL D to F 27 FEB 15
 MEL ITEMS
77 - ENGINE INDICATING
77-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES 77-07-02 - Indications on the ENGINE SD page
MINIMUM EQUIPMENT LIST

Continued from the previous page

77-07-02-06B Both indications inoperative
Repair interval Nbr installed Nbr required Placard
A 2 0 No
Both may be inoperative for three flights provided that:
1) ETOPS is not conducted, and
2) No vibration advisory was displayed during the previous flight.

77-07-02-07 Oil Filter Clog Indication on the ENGINE SD page

Ident.: MI-77-07-02-00008635.0001001 / 21 MAR 10
Applicable to: ALL

77-07-02-07A
Repair interval Nbr installed Nbr required Placard

Refer to Item 79-07-01 CLOG Indication on the ENGINE SD page

77-07-02-08 Oil Pressure Indication on the ENGINE SD page

Ident.: MI-77-07-02-00008636.0001001 / 21 MAR 10
Applicable to: ALL

77-07-02-08A
Repair interval Nbr installed Nbr required Placard

Refer to Item 79-07-02 Oil Pressure Indication and Advisory on the ENGINE SD page

LAN COLOMBIA FLEET MI-77-07-02 P 3/6

MEL F to H 27 FEB 15
 MEL ITEMS
77 - ENGINE INDICATING
77-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES 77-07-02 - Indications on the ENGINE SD page
MINIMUM EQUIPMENT LIST

77-07-02-09 Oil Quantity Indication on the ENGINE SD page

Ident.: MI-77-07-02-00008637.0001001 / 21 MAR 10
Applicable to: ALL

77-07-02-09A
Repair interval Nbr installed Nbr required Placard

Refer to Item 79-07-03 Oil Quantity Indication on the ENGINE SD page

77-07-02-10 Oil Temperature Indication on the ENGINE SD page

Ident.: MI-77-07-02-00008638.0001001 / 21 MAR 10
Applicable to: ALL

77-07-02-10A
Repair interval Nbr installed Nbr required Placard

Refer to Item 79-07-04 Oil Temperature Indication on the ENGINE SD page

77-07-02-11 Selected Igniter Indication on the ENGINE SD page

Ident.: MI-77-07-02-00008639.0001001 / 27 FEB 15
Applicable to: ALL

77-07-02-11A
Repair interval Nbr installed Nbr required Placard

Refer to Item 74-07-01 Selected Igniter Indication on the ENGINE SD page

LAN COLOMBIA FLEET MI-77-07-02 P 4/6

MEL I to K 27 FEB 15
 MEL ITEMS
77 - ENGINE INDICATING
77-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES 77-07-02 - Indications on the ENGINE SD page
MINIMUM EQUIPMENT LIST

77-07-02-12 Start Valve Position Indication on the ENGINE SD page

Ident.: MI-77-07-02-00008640.0001001 / 21 MAR 10
Applicable to: ALL

77-07-02-12A
Repair interval Nbr installed Nbr required Placard

Refer to Item 80-07-01 Start Valve Position Indication on the ENGINE SD page

LAN COLOMBIA FLEET MI-77-07-02 P 5/6

MEL L 27 FEB 15
 MEL ITEMS
77 - ENGINE INDICATING
77-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES 77-07-02 - Indications on the ENGINE SD page
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-77-07-02 P 6/6

MEL 27 FEB 15
 MEL ITEMS
77 - ENGINE INDICATING
77-08 - Indications on the EWD
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

77-08-01 EGT Indication on the EWD

Ident.: MI-77-08-00008641.0001001 / 21 MAR 10
Applicable to: ALL

77-08-01A
Repair interval Nbr installed Nbr required Placard
2 2 No
Must be operative.

77-08-02 EPR Indication on the EWD

Ident.: MI-77-08-00008642.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

77-08-02A
Repair interval Nbr installed Nbr required Placard

Refer to Item 73-20-04 EPR Control Mode

77-08-03 Fuel Flow Indication on the EWD

Ident.: MI-77-08-00008643.0001001 / 02 NOV 11
Applicable to: ALL

77-08-03A
Repair interval Nbr installed Nbr required Placard

Refer to Item 73-08-01 Fuel Flow Indication on the EWD

LAN COLOMBIA FLEET MI-77-08 P 1/2

MEL A to C 10 OCT 14
 MEL ITEMS
77 - ENGINE INDICATING
77-08 - Indications on the EWD
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

77-08-04 N1 Indication on the EWD

Ident.: MI-77-08-00008644.0001001 / 21 MAR 10
Applicable to: ALL

77-08-04A
Repair interval Nbr installed Nbr required Placard
2 2 No
Must be operative.

77-08-05 N2 Indication on the EWD

Ident.: MI-77-08-00008645.0001001 / 21 MAR 10
Applicable to: ALL

77-08-05A
Repair interval Nbr installed Nbr required Placard
2 2 No
Must be operative.

LAN COLOMBIA FLEET MI-77-08 P 2/2

MEL D to E 10 OCT 14
 MEL ITEMS
78 - EXHAUST
78-08 - Indications on the EWD
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

78-08-01 REV Indication on the EWD

Ident.: MI-78-08-00008608.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

78-08-01A
Repair interval Nbr installed Nbr required Placard
2 2 No
Both must be operative.

78-08-01 REV Indication on the EWD

Ident.: MI-78-08-00008608.0002001 / 10 OCT 14
Applicable to: MSN 4516-4546

78-08-01B
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative provided that the associated thrust reverser is considered
inoperative.
Refer to Item 78-30-01 Thrust Reverser

LAN COLOMBIA FLEET MI-78-08 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
78 - EXHAUST
78-08 - Indications on the EWD
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-78-08 P 2/2

MEL 27 FEB 15
 MEL ITEMS
78 - EXHAUST
78-30 - Thrust Reversers
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

78-30-01 Thrust Reverser

Ident.: MI-78-30-00008603.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

78-30-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(o) (m) One or both may be inoperative provided that:
1) The inoperative thrust reverser is deactivated and secured in the stowed position, and
2) All stow and deploy switches circuits on the inoperative thrust reverser are checked
operative, and
3) The ENG 1(2) REV PRESSURIZED alert is not displayed on the EWD after deactivation,
and
4) The appropriate performance adjustments are applied, and
5) Do not dispatch to runways less than 1900 mts length.
Note: Check aircraft performance on takeoff and landing at departure, alternate and
destination aerodromes.
Reference(s)
(o) Refer to OpsProc 78-30-01A Thrust Reverser
(m) Refer to AMM 78-30-00-040-040

LAN COLOMBIA FLEET MI-78-30 P 1/4

MEL A 27 FEB 15
 MEL ITEMS
78 - EXHAUST
78-30 - Thrust Reversers
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

78-30-01 Thrust Reverser

Ident.: MI-78-30-00008603.0002001 / 10 OCT 14
Applicable to: MSN 4516-4546

78-30-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
(o) (m) One or both may be inoperative provided that:
1) The inoperative reverser is deactivated and secured in the stowed position, and
2) Both LVDT s on the inoperative reverser are checked operative, and
3) The ENG 1(2) REV PRESSURIZED alert is not displayed on the EWD after deactivation,
and
4) The appropriate performance adjustments are applied.
5) Do not dispatch to runways less than 1900 mts length.
Note: Check aircraft performance on takeoff and landing at departure, alternate and
destination aerodromes.
Reference(s)
(o) Refer to OpsProc 78-30-01A Thrust Reverser
(m) Refer to AMM 78-30-00-040-013

78-30-02 Thrust Reverser Inhibition Relay sw

Ident.: MI-78-30-00008604.0001001 / 27 FEB 15
Applicable to: ALL

78-30-02A
Repair interval Nbr installed Nbr required Placard
C 4 0 No
One or more may be inoperative provided that the associated thrust reverser is considered
inoperative.
Refer to Item 78-30-01 Thrust Reverser

LAN COLOMBIA FLEET MI-78-30 P 2/4

MEL A to B 27 FEB 15
 MEL ITEMS
78 - EXHAUST
78-30 - Thrust Reversers
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

78-30-03 Thrust Reverser Shutoff Valve

Ident.: MI-78-30-00008605.0001001 / 27 FEB 15
Applicable to: ALL

78-30-03A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative in the open position.

LAN COLOMBIA FLEET MI-78-30 P 3/4

MEL C 27 FEB 15
 MEL ITEMS
78 - EXHAUST
78-30 - Thrust Reversers
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-78-30 P 4/4

MEL 27 FEB 15
 MEL ITEMS
79 - OIL
79-07 - Indications on the ENGINE SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

79-07-01 CLOG Indication on the ENGINE SD page

Ident.: MI-79-07-00008596.0001001 / 21 MAR 10
Applicable to: ALL

79-07-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
One or both may be inoperative.

79-07-02 Oil Pressure Indication and Advisory on the ENGINE SD page

Ident.: MI-79-07-00008597.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

Note: Simultaneous illumination of the BLUE ELEC PUMP pb-sw FAULT light and the ENG 1(2)
PUMP pb-sw FAULT light with engines off may be due to a failed engine oil low pressure
switch. In this case, the ENG 1(2) OIL LO PR alert is inoperative.
Refer to Item 79-09-01 ENG 1(2) OIL LO PR Alert

79-07-02C
Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative provided that:
1) ETOPS is not conducted, and
2) The associated ENG 1(2) OIL LO PR alert is operative, and
3) The associated oil quantity indication is operative on the ENGINE SD page .

LAN COLOMBIA FLEET MI-79-07 P 1/4

MEL A to B 27 FEB 15
 MEL ITEMS
79 - OIL
79-07 - Indications on the ENGINE SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

79-07-02 Oil Pressure Indication and Advisory on the ENGINE SD page

Ident.: MI-79-07-00008597.0002001 / 27 FEB 15
Applicable to: MSN 4758-5453

Note: Simultaneous illumination of the BLUE ELEC PUMP pb-sw FAULT light and the ENG 1(2)
PUMP pb-sw FAULT light with engines off may be due to a failed engine oil low pressure
switch. In this case, the ENG 1(2) OIL LO PR alert is inoperative.
Refer to Item 79-09-01 ENG 1(2) OIL LO PR Alert

79-07-02A Associated thrust reverser checked operative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
(m) One may be inoperative provided that:
1) ETOPS is not conducted, and
2) The associated ENG 1(2) OIL LO PR alert is operative, and
3) The associated oil quantity indication is operative on the ENGINE SD page , and
4) The associated thrust reverser is checked operative.
Reference(s)
(m) Refer to AMM

79-07-02B Associated thrust reverser considered inoperative

Repair interval Nbr installed Nbr required Placard
C 2 1 No
One may be inoperative provided that:
1) ETOPS is not conducted, and
2) The associated ENG 1(2) OIL LO PR alert is operative, and
3) The associated oil quantity indication is operative on the ENGINE SD page , and
4) The associated thrust reverser is considered inoperative.
Refer to Item 78-30-01 Thrust Reverser

LAN COLOMBIA FLEET MI-79-07 P 2/4

MEL B 27 FEB 15
 MEL ITEMS
79 - OIL
79-07 - Indications on the ENGINE SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

79-07-03 Oil Quantity Indication on the ENGINE SD page

Ident.: MI-79-07-00008598.0001001 / 21 MAR 10
Applicable to: ALL

79-07-03A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(m) One may be inoperative provided that the associated oil quantity is checked before each
flight.
Reference(s)
(m) Refer to AMM

79-07-04 Oil Temperature Indication on the ENGINE SD page

Ident.: MI-79-07-00008599.0001001 / 21 MAR 10
Applicable to: ALL

79-07-04A
Repair interval Nbr installed Nbr required Placard
2 2 No
Must be operative.

LAN COLOMBIA FLEET MI-79-07 P 3/4

MEL C to D 27 FEB 15
 MEL ITEMS
79 - OIL
79-07 - Indications on the ENGINE SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-79-07 P 4/4

MEL 27 FEB 15
 MEL ITEMS
79 - OIL
79-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

79-09-01 ENG 1(2) OIL LO PR Alert

Ident.: MI-79-09-00008600.0001001 / 27 FEB 15
Applicable to: ALL

79-09-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) One or both may be displayed.
Reference(s)
(o) Refer to OpsProc 79-09-01A ENG 1(2) OIL LO PR Alert

79-09-02 ENG 1(2) OIL FILTER CLOG Alert

Ident.: MI-79-09-00008601.0002001 / 27 FEB 15
Applicable to: MSN 4758-5453

79-09-02B Inspection of the visual indicator (pop-out) of the electrical master chip
detector
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(m) One may be displayed provided that:
1) The associated filter is replaced every day, and
2) The visual indicator (pop-out) of the electrical master chip detector is checked operative
before the first MEL dispatch, and
3) The visual indicator (pop-out) of theelectrical master chip detector is inspected when the
filter is replaced and does not reveal the presence of chips.
Reference(s)
(m) Refer to AMM 79-35-00-040-042
Continued on the following page

LAN COLOMBIA FLEET MI-79-09 P 1/2

MEL A to B 27 FEB 15
 MEL ITEMS
79 - OIL
79-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

79-09-02C Inspection of the electrical master chip detector
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(m) One may be displayed provided that:
1) The associated filter is replaced every day, and
2) The electrical master chip detector is inspected when the filter is replaced and does not
reveal the presence of chips.
Reference(s)
(m) Refer to AMM 79-35-00-040-044

79-09-03 ENG 1(2) BEARING 4 OIL SYS Alert

Ident.: MI-79-09-00008602.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

79-09-03A
Repair interval Nbr installed Nbr required Placard
A 2 0 No
One or both may be displayed for 3 days provided that the ENG 1(2) BEARING 4 OIL SYS
alert is not associated with the HI PRESS message.

LAN COLOMBIA FLEET MI-79-09 P 2/2

MEL B to C 27 FEB 15
 MEL ITEMS
79 - OIL
79-20 - Distribution
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

79-20-01 Air Cooled Oil Cooler ( ACOC ) Modulating Valve

Ident.: MI-79-20-00008592.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

79-20-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(o) One or both may be inoperative in the open position provided that the fuel temperature in
the inner tank is checked to be above -20 C .
Reference(s)
(o) Refer to OpsProc 79-20-01A Air Cooled Oil Cooler (ACOC) Modulating Valve

79-20-02 EMCD Visual Pop-Out Indicator

Ident.: MI-79-20-00008593.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

79-20-02A
Repair interval Nbr installed Nbr required Placard
D 2 0 No
One or both may be inoperative.

LAN COLOMBIA FLEET MI-79-20 P 1/2

MEL A to B 27 FEB 15
 MEL ITEMS
79 - OIL
79-20 - Distribution
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-79-20 P 2/2

MEL 27 FEB 15
 MEL ITEMS
79 - OIL
79-40 - IDG Oil Cooling System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

79-40-01 Fuel Return Valve

Ident.: MI-79-40-00008595.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

79-40-01A
Repair interval Nbr installed Nbr required Placard

Refer to Item 73-10-01 Fuel Return Valve

LAN COLOMBIA FLEET MI-79-40 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
79 - OIL
79-40 - IDG Oil Cooling System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-79-40 P 2/2

MEL 27 FEB 15
 MEL ITEMS
80 - STARTING
80-01 - ENG MAN START Overhead Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

80-01-31 ENG MAN START pb-sw

Ident.: MI-80-01-00008588.0001001 / 21 MAR 10
Applicable to: ALL

80-01-31A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

LAN COLOMBIA FLEET MI-80-01 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
80 - STARTING
80-01 - ENG MAN START Overhead Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-80-01 P 2/2

MEL 05 NOV 13
 MEL ITEMS
80 - STARTING
80-07 - Indication on the ENGINE SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

80-07-01 Start Valve Position Indication on the ENGINE SD page

Ident.: MI-80-07-00008591.0001001 / 21 MAR 10
Applicable to: ALL

80-07-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 No
(m) One or both may be inoperative provided that the associated start valve is checked closed
after the start of the affected engine.
Reference(s)
(m) Refer to AMM

LAN COLOMBIA FLEET MI-80-07 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
80 - STARTING
80-07 - Indication on the ENGINE SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-80-07 P 2/2

MEL 05 NOV 13
 MEL ITEMS
80 - STARTING
80-11 - Pneumatic Starter and Valve System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

80-11-01 Start Valve

Ident.: MI-80-11-00008589.0001001 / 27 FEB 15
Applicable to: ALL

80-11-01A
Repair interval Nbr installed Nbr required Placard
C 2 1 No
(o) (m) One may be inoperative provided that the start valve is manually closed after the start of the
affected engine.
Reference(s)
(o) Refer to OpsProc 80-11-01A Start Valve
(m) Refer to AMM 80-11-00-040-043

LAN COLOMBIA FLEET MI-80-11 P 1/2

MEL A 27 FEB 15
 MEL ITEMS
80 - STARTING
80-11 - Pneumatic Starter and Valve System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-80-11 P 2/2

MEL 27 FEB 15
 MEL ITEMS
80 - STARTING
80-12 - ENG MASTER Panel on the Center Pedestal
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

80-12-01 FAULT light on the ENG MASTER Panel

Ident.: MI-80-12-00008590.0001001 / 21 MAR 10
Applicable to: ALL

80-12-01A
Repair interval Nbr installed Nbr required Placard
C 2 0 Yes
One or both may be inoperative.

LAN COLOMBIA FLEET MI-80-12 P 1/2

MEL A 05 NOV 13
 MEL ITEMS
80 - STARTING
80-12 - ENG MASTER Panel on the Center Pedestal
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MI-80-12 P 2/2

MEL 05 NOV 13


MEL OPERATIONAL
PROCEDURES
Intentionally left blank
 MEL OPERATIONAL PROCEDURES
PRELIMINARY PAGES - TABLE OF CONTENTS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

MO-21 Air Conditioning

MO-21-09 ECAM Alerts
21-09-01A VENT BLOWER FAULT Alert............................................................................................................... A
21-09-02A VENT EXTRACT FAULT Alert.............................................................................................................. B

MO-21-23 Lavatory And Galley Ventilation

21-23-01B Lavatory and Galley Extraction Fan...................................................................................................... A

MO-21-26 Avionics Equipment Ventilation

21-26-01A Avionics Blower Fan ( VENT AVNCS SYS FAULT Alert not displayed) .............................................. A
21-26-01B Avionics Blower Fan (Air conditioning inlet valve checked open before each flight)............................. B
21-26-01C Avionics Blower Fan (Avionics ventilation system checked before each flight).................................... C
21-26-02A Avionics Extract Fan (VENT AVNCS SYS FAULT Alert not displayed)................................................D
21-26-02B Avionics Extract Fan (Air conditioning inlet valve checked open before each flight)............................. E
21-26-02C Avionics Extract Fan (Avionics ventilation system checked before each flight).....................................F
21-26-03A Avionics Skin Exchanger Inlet Bypass Valve........................................................................................G
21-26-04A Avionics Skin Air Outlet Valve...............................................................................................................H
21-26-05A Avionics Skin Air Inlet Valve (Air conditioning inlet valve open on the ground)...................................... I
21-26-05B Avionics Skin Air Inlet Valve (Air conditioning inlet valve secured in the open position)........................ J
21-26-06A(B) Avionics Skin Exchanger Isolation Valve..........................................................................................K
21-26-08A Avionics Air Conditioning Inlet Valve..................................................................................................... L
21-26-09A Avionics Ventilation Filter (VENT AVNCS SYS FAULT Alert not displayed)........................................ M
21-26-09B Avionics Ventilation Filter (Air conditioning inlet valve checked open before each flight)......................N
21-26-09C Avionics Ventilation Filter (Avionics ventilation system checked before each flight).............................O
21-26-10A Avionics Equipment Ventilation Computer (AEVC)............................................................................... P

MO-21-28 Cargo Compartment Ventilation

21-28-03A AFT Cargo Extraction Fan.....................................................................................................................A
21-28-04A AFT Cargo Isolation Valve (Valves checked closed)............................................................................ B
21-28-04B AFT Cargo Isolation Valve (Valves secured closed).............................................................................C

MO-21-31 Pressure Control and Monitoring

21-31-01A(B) Automatic Cabin Pressure Control System (CPC, Outflow Valve AUTO Channel).......................... A
21-31-04A Landing Elevation Selection AUTO Function........................................................................................ B
21-31-05A Landing Elevation Selection MAN Function.......................................................................................... C

MO-21-51 Flow Control and Indicating

21-51-03A Pack Flow Sensor..................................................................................................................................A

MO-21-52 Air Cooling System

21-52-01D(E) Air Conditioning Pack (One Air Conditioning Pack Inoperative for C Repair Interval)...................... A
21-52-01G Air Conditioning Pack (One Air Conditioning Pack in Heat Exchanger Cooling Mode only)................. B
Continued on the following page

LAN COLOMBIA FLEET MO-PLP-TOC P 1/14

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
PRELIMINARY PAGES - TABLE OF CONTENTS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

MO-21-63 Cockpit and Cabin Temperature Control
21-63-02A Cockpit and Cabin Trim Air Valve (Affected valve checked closed)......................................................A
21-63-02B Cockpit and Cabin Trim Air Valve (Hot air pressure regulating valve checked operative).....................B
21-63-03A Hot Air Pressure Regulating Valve (Hot air pressure valve checked closed)........................................C
21-63-03B Hot Air Pressure Regulating Valve (Trim air valve checked closed).....................................................D
21-63-03C Hot Air Pressure Regulating Valve (Affected valve secured in the closed position)..............................E

MO-22 Auto Flight

MO-22-05 FMA Indications on the PFD
22-05-01B AP Related Indications on the FMA .....................................................................................................A
22-05-03A Approach and Landing Capabilities on the FMA ..................................................................................B

MO-22-10 Autopilot/Flight Director (AP/FD)

22-10-01A(B) Autopilot (AP)....................................................................................................................................A
22-10-02A Flight Director (FD)................................................................................................................................ B
22-10-04A Take-over pb AP Disconnection Function (One inoperative)................................................................ C
22-10-04B Take-over pb AP Disconnection Function (Both inoperative)................................................................D
22-10-05A AUTO LAND light ................................................................................................................................. E
22-10-06A AP Disengagement Warning..................................................................................................................F
22-10-07A Sticks and Rudder Pedals Locking Solenoid in AP Mode.................................................................... G

MO-22-30 Autothrust
22-30-01A Autothrust (A/THR)................................................................................................................................ A
22-30-02A Autothrust Instinctive Disconnect pb .................................................................................................... B

MO-22-60 Flight Augmentation (FAC)

22-60-02A FAC 2.....................................................................................................................................................A
22-60-04A Yaw Damper System.............................................................................................................................B

MO-22-70 Flight Management System (FMS)

22-70-01A(B) Flight Management System (FMS)................................................................................................... A

MO-22-83 Flight Management and Guidance Computer (FMGC)

22-83-01A(B) Flight Management and Guidance Computer (FMGC).....................................................................A

MO-23 Communications
MO-23-01 Overhead Panels
MO-23-01-01 RCDR Overhead Panel
23-01-01-31A RCDR-GND CTL pb-sw (Inoperative in the AUTO position)............................................................A
23-01-01-31B RCDR-GND CTL pb-sw (Inoperative in the ON position)................................................................ B
Continued on the following page

LAN COLOMBIA FLEET MO-PLP-TOC P 2/14

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
PRELIMINARY PAGES - TABLE OF CONTENTS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

MO-23-09 ECAM Alerts
23-09-01A COM HF 1(2) EMITTING Alert.............................................................................................................. A
23-09-02A COM VHF 1(2)(3) EMITTING Alert....................................................................................................... B

MO-23-40 Interphone
23-40-01A Ground External Horn............................................................................................................................A
23-40-03A Flight Crew to Ground Communication System.................................................................................... B
23-40-04A Service Interphone Jack........................................................................................................................C

MO-23-51 Audio Management

23-51-05A Cockpit Loudspeaker Volume Control................................................................................................... A

MO-23-52 Audio Control Panel (ACP)

23-52-01A CAPT and F/O ACP ............................................................................................................................. A

MO-23-73 Cabin Intercommunication Data System

MO-23-73-02 DEU A
23-73-02-01A Cabin DEU A.................................................................................................................................... A

MO-23-73-03 DEU B
23-73-03-01B Cabin DEU B.................................................................................................................................... A

MO-23-73-05 Cabin Loudspeaker

23-73-05-02A Lavatory Loudspeaker...................................................................................................................... A

MO-23-73-06 Handset
23-73-06-02A Cabin Handset.................................................................................................................................. A

MO-23-73-07 Prerecorded Announcement and Music Reproducer (PRAM)

Prerecorded Announcement and Music Reproducer (PRAM)................................................................................ A

MO-23-74 Cabin Crew Panel

23-74-01A FAP Display Unit................................................................................................................................... A

MO-24 Electrical Power

MO-24-01 Overhead Panels
MO-24-01-01 ELEC Overhead Panel
24-01-01-07A EXT PWR pb-sw AVAIL light .......................................................................................................... A
24-01-01-09A GALY & CAB pb-sw FAULT light ....................................................................................................B

MO-24-07 Indications on the ELEC SD page

24-07-01A AC Generation Indications on the ELEC SD page .............................................................................. A
Continued on the following page

LAN COLOMBIA FLEET MO-PLP-TOC P 3/14

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
PRELIMINARY PAGES - TABLE OF CONTENTS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

MO-24-09 ECAM Alerts
24-09-01A ELEC AC ESS BUS SHED Alert...........................................................................................................A

MO-24-22 AC Main Generation

24-22-01A AC Main Generation (IDG, GCU, Line Contactor)................................................................................ A

MO-24-25 AC Essential Generation Switching

24-25-01A Manual Transfer to the AC BUS 2 (ALTN Function).............................................................................A
24-25-02A Automatic Transfer to the AC BUS 2.................................................................................................... B

MO-24-26 Galley and Commercial Supply System

24-26-02B GALY & CAB Manual Load Shed System (GALY & CAB pb-sw)......................................................... A
24-26-03A Commercial Supply System...................................................................................................................B

MO-24-32 DC Main Generation (TR 1, TR 2)

24-32-01A DC Main Generation (TR 1 inoperative)................................................................................................A
24-32-01B DC Main Generation (TR 2 inoperative)................................................................................................B

MO-24-38 DC Battery Generation

24-38-02A Battery Charge Limiter (BCL)................................................................................................................ A

MO-25 Equipment/Furnishings
MO-25-07 Indications on the DOOR/OXY SD page
25-07-01A Passenger Door Slide Permanently Indicated Armed........................................................................... A
25-07-02A Passenger Door Slide Permanently Indicated Not Armed.................................................................... B

MO-25-11 Pilot Seats

25-11-07A Pilot Seat Fifth Strap............................................................................................................................. A

MO-25-12 Third and Fourth Occupant Seats

25-12-04A Third Occupant Seat Fifth Strap............................................................................................................A
25-12-08A Fourth Occupant Seat Fifth Strap......................................................................................................... B

MO-25-20 Cabin Seats

25-20-03A(B) Cabin Attendant Seat........................................................................................................................A

MO-25-35 Galley equipment

25-35-01A Galley Waste Compartment Flapper Door............................................................................................ A

MO-25-40 Lavatories
25-40-01A(B) Toilet Waste Compartment Flapper Door.........................................................................................A
Continued on the following page

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MO-25-63 Evacuation Signaling Equipment
25-63-01A Emergency Evacuation Signaling System (COMMAND pb-sw, HORN SHUT OFF pb, CAPT&PURS and
CAPT sw).................................................................................................................................................................A

MO-26 Fire Protection

MO-26-12 Engine Fire and Overheat Detection
26-12-01A & 26-12-02A & 26-12-03A & 26-12-04A Engine Fire Detection Loop................................................... A

MO-26-13 APU Fire and Overheat Detection

26-13-01A(B) APU Fire Detection Loop..................................................................................................................A

MO-26-15 Avionics Compartment Smoke Detection

26-15-01A Avionics Smoke Detection System........................................................................................................A

MO-26-16 Cargo Compartment Smoke Detection

26-16-02C(E) Smoke Detector in the AFT and the BULK Cargo Compartments................................................... A

MO-26-17 Lavatory Smoke Detection

26-17-01A(B) & 26-25-01B(C) Lavatory Smoke Detection System........................................................................ A

MO-27 Flight Controls

MO-27-07 Indications on SD pages
27-07-02A Aileron Position Indication on the F/CTL SD page .............................................................................. A
27-07-04A Elevator Position Indication on the F/CTL SD page ............................................................................ B
27-07-05A Pitch Trim Position Indication on the F/CTL SD page ......................................................................... C
27-07-06A Rudder Position Indication on the F/CTL SD page ..............................................................................D
27-07-11A Spoilers/Speedbrakes Indication on the F/CTL SD page .....................................................................E
27-07-12A Spoilers/Speedbrakes Indication on the WHEEL SD page .................................................................. F

MO-27-14 Aileron and Hydraulic Actuation

27-14-01A Left Aileron Blue Servo-Control (Controlled by ELAC 1).......................................................................A
27-14-03A Right Aileron Green Servo-Control (Controlled by ELAC 1)..................................................................B

MO-27-21 Rudder Mechanical Control

27-21-01A Rudder Pedal Adjustment System.........................................................................................................A

MO-27-22 Rudder Trim Actuation

27-22-01A(B) Rudder Trim System.........................................................................................................................A

MO-27-51 Flaps Electrical Control and Monitoring

27-51-01A SFCC Flap Channel.............................................................................................................................. A
27-51-02A SFCC Slat Channel............................................................................................................................... B
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MO-27-64 Spoiler Hydraulic Actuation
27-64-01A Spoiler 5.................................................................................................................................................A
27-64-02A Spoiler 1 or 3.........................................................................................................................................B
27-64-03A Spoiler 2 or 4.........................................................................................................................................C
27-64-04A Spoilers 1 and 2.................................................................................................................................... D
27-64-05A Spoiler 3 and 4...................................................................................................................................... E

MO-27-92 Electrical Flight Control System (EFCS) Control Inputs and Power Supply
27-92-01A Speedbrake Control System (speedbrake control system inoperative).................................................A
27-92-01B Speedbrake Control System (speedbrake 2 or speedbrakes 3 and 4 inoperative)............................... B
27-92-02A Ground Spoiler Control System (Ground spoiler control system inoperative)....................................... C
27-92-02A Ground Spoiler Control System (ground spoiler control system inoperative)........................................D
27-92-02B Ground Spoiler Control System (Pair of spoilers 5 inoperative)............................................................E
27-92-02C Ground Spoiler Control System (Pairs of spoilers 1 and 2 or pairs of spoilers 3 and 4 inoperative)...... F

MO-27-93 ELAC (Elevator Aileron Computer) System

27-93-01A ELAC 1.................................................................................................................................................. A

MO-27-94 SEC (Spoiler and Elevator Computer) System

27-94-01A SEC 1 ................................................................................................................................................... A
27-94-02A SEC 2.................................................................................................................................................... B
27-94-03A SEC 3 ...................................................................................................................................................C

MO-27-95 FCDC (Flight Control Data Concentrator) System

27-95-02A FCDC 2..................................................................................................................................................A

MO-28 Fuel
MO-28-01 Overhead Panels
MO-28-01-01 FUEL Overhead Panel
28-01-01-07A FUEL MODE SEL pb-sw FAULT light ............................................................................................ A

MO-28-07 Indications on the FUEL SD page

MO-28-07-01 Fuel Quantity Indications on the FUEL SD page
28-07-01-01A Fuel On Board (FOB) Indication on the FUEL SD page .................................................................A
28-07-01-02A Fuel Quantity Indication in Degraded Mode on the FUEL SD page ............................................... B
28-07-01-03A(C) Outer Tank Fuel Quantity Indication on the FUEL SD page ......................................................C
28-07-01-04A Inner Tank Fuel Quantity Indication on the FUEL SD page ........................................................... D
28-07-01-05A Center Tank Fuel Quantity Indication on the FUEL SD page ......................................................... E

MO-28-07-04 Valve Indications on the FUEL SD page

28-07-04-04A Wing Transfer Valve Indication on the FUEL SD page ...................................................................A
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MO-28-09 ECAM Alerts
28-09-01A(B) FUEL L(R) INNER(OUTER) TK HI TEMP Alert............................................................................... A
28-09-02A(B) FUEL L(R) INNER(OUTER) TK LO TEMP Alert.............................................................................. B

MO-28-12 Tank Venting System

28-12-01A Overpressure Protector Between the Inner and the Outer Tank (Inner tank fuel temperature monitored) A
28-12-01B Overpressure Protector Between the Inner and the Outer Tank (Transfer valves opened)...................B
28-12-02A Overpressure Protector in the Vent Surge Tank...................................................................................C

MO-28-15 Intercell Transfer System

28-15-01A(C) LH Wing Transfer Valve (At least one transfer valve open).............................................................A
28-15-01B LH Wing Transfer Valve (At least one transfer valve failed closed)...................................................... B
28-15-02A(C) RH Wing Transfer Valve (At least one transfer valve open)............................................................ C
28-15-02B RH Wing Transfer Valve (At least one transfer valve failed closed)..................................................... D

MO-28-20 Distribution
28-20-01A Automatic Fuel Feed System................................................................................................................ A

MO-28-21 Main Fuel Pump System

28-21-02A Center Tank Pump (One inoperative)................................................................................................... A
28-21-02D Center Tank Pump (Both inoperative)...................................................................................................B

MO-28-22 APU Fuel Pump System

28-22-01A(B) APU Fuel Pump................................................................................................................................ A

MO-28-29 APU LP Fuel Shutoff

28-29-01A APU LP Fuel Valve............................................................................................................................... A

MO-28-50 Fuel Management

28-50-01A Fuel Quantity Indicating Computer (FQIC) Channel............................................................................. A

MO-29 Hydraulic Power

MO-29-07 Indications on the HYD SD page
29-07-07A System Label Indication on the HYD SD page ....................................................................................A
29-07-08A System Pressure Indication on the HYD SD page .............................................................................. B

MO-29-09 ECAM Alerts

29-09-03A HYD G(Y) ENG 1(2) PUMP LO PR Alert..............................................................................................A
29-09-07A HYD PTU FAULT Alert..........................................................................................................................B
29-09-09A HYD G(B)(Y)(B+G)(G+Y)(B+Y) SYS LO PR Alert...............................................................................C

MO-29-10 Main Hydraulic Power

29-10-03A Blue System Electric Pump................................................................................................................... A
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MO-29-23 Power Transfer
29-23-01A Power Transfer Unit (PTU)....................................................................................................................A

MO-29-24 Yellow Auxiliary Hydraulic Power

29-24-01A Yellow System Electric Pump................................................................................................................A

MO-30 Ice and Rain Protection

MO-30-01 Overhead Panels
MO-30-01-01 ANTI ICE Overhead Panel
30-01-01-03A ANTI ICE WING pb-sw FAULT light ............................................................................................... A

MO-30-11 Wing Ice Protection

30-11-01A Wing Anti-Ice Control Valve.................................................................................................................. A

MO-30-21 Engine Air Intake Ice Protection

30-21-01B(C) Engine Anti-Ice Valve....................................................................................................................... A

MO-30-31 Probe Ice Protection

30-31-01B Probe Heat Computer (PHC)................................................................................................................ A
30-31-02A Pitot Heater............................................................................................................................................B
30-31-03C F/O Static Ports Heater.........................................................................................................................C
CAPT Static Ports Heater....................................................................................................................................... D
30-31-04A Angle of Attack (AOA) Probes Heating (F/O inoperative)..................................................................... E
30-31-04B(C) Angle of Attack (AOA) Probes Heating (CAPT or STBY inoperative)...............................................F

MO-30-42 Windshield Anti-Icing and Defogging

30-42-01A Window Heat Computer........................................................................................................................ A
30-42-03A Windshield Heating................................................................................................................................ B

MO-30-45 Windshield Rain Protection

30-45-01B Windshield Wiper...................................................................................................................................A

MO-30-81 Ice Detection

30-81-01A Ice Detection System.............................................................................................................................A
30-81-03A Lighting of External Visual Icing Indicator............................................................................................. B

MO-31 Indicating/Recording Systems

MO-31-07 Indications on the System Display (SD)
31-07-02A Permanent Data (TAT, SAT, ISA, GLOAD - ALT SEL, UTC, GW) Indications on the SD ....................A

MO-31-20 Independent Instruments

31-20-01A Electrical Clock Indicator....................................................................................................................... A
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MO-31-53 Flight Warning Computer (FWC)
31-53-01A FLIGHT WARNING COMPUTER (FWC).............................................................................................. A
31-53-06A Altitude Alert.......................................................................................................................................... B

MO-31-56 ECAM Control Panel (ECP)

31-56-07A T.O CONFIG pb on the ECP ............................................................................................................... A

MO-31-62 Display Management Computer (DMC)

31-62-01B DMC 1....................................................................................................................................................A
31-62-02A DMC 2....................................................................................................................................................B
31-62-03B DMC 3................................................................................................................................................... C

MO-31-63 Display Unit (DU)

31-63-02A PFDU 2.................................................................................................................................................. A
31-63-03A NDU 1.................................................................................................................................................... B
31-63-04A NDU 2....................................................................................................................................................C
31-63-05A SDU ...................................................................................................................................................... D

MO-31-68 Switching Panel

31-68-05A PFD/ND XFR pb on the Lateral Instrument Panel................................................................................ A

MO-32 Landing Gear

MO-32-07 Indications on the WHEEL SD page
32-07-01A(B) Brakes Temperature Indication on the WHEEL SD page ............................................................... A
32-07-03A L/G Doors Position Indication on the WHEEL SD page ...................................................................... B

MO-32-09 ECAM Alerts

32-09-01C BRAKES-N/WS MINOR FAULT Alert (Alternate braking checked operative)....................................... A

MO-32-31 Normal Extension and Retraction

32-31-01A Landing Gear Control and Interface Unit ( LGCIU ) ............................................................................ A
32-31-02A Landing Gear Retracting System.......................................................................................................... B

MO-32-32 Proximity Detector System

32-32-02A LGCIU 2 RH L/G Shock Absorber Proximity Detector ......................................................................... A
32-32-03A LGCIU 2 LH L/G Shock Absorber Proximity Detector ..........................................................................B
32-32-04A LGCIU 2 Nose L/G Shock Absorber Proximity Detector ......................................................................C
32-32-05A LGCIU 2 RH L/G Down Lock Proximity Detector..................................................................................D
32-32-06A LGCIU 2 LH L/G Down Lock Proximity Detector.................................................................................. E
32-32-07A LGCIU 2 Nose L/G Down Lock Proximity Detector ..............................................................................F
32-32-08A LGCIU 2 RH L/G Up Lock Proximity Detector .....................................................................................G
32-32-09A LGCIU 2 LH L/G Up Lock Proximity Detector ..................................................................................... H
32-32-10A LGCIU 2 Nose L/G Up Lock Proximity Detector ................................................................................... I
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32-32-11A LGCIU 2 RH L/G Doors Open Proximity Detector ................................................................................J
32-32-12A LGCIU 2 LH L/G Doors Open Proximity Detector ................................................................................K
32-32-13A LGCIU 2 Nose L/G Doors Open Proximity Detector ............................................................................ L
32-32-14A LGCIU 2 RH L/G Doors Closed Proximity Detector ............................................................................ M
32-32-15A LGCIU 2 LH L/G Doors Closed Proximity Detector ............................................................................. N
32-32-16A LGCIU 2 Nose L/G Doors Closed Proximity Detector ......................................................................... O

MO-32-33 Free Fall Extension

32-33-01A Landing Gear Gravity Extension System.............................................................................................. A

MO-32-42 Normal Braking

32-42-01A Main Wheel Brake................................................................................................................................. A
32-42-02A Green System Brake............................................................................................................................. B
32-42-05A AUTO/BRK Function..............................................................................................................................C

MO-32-47 Brake Temperature System

32-47-01A Brake Temperature Monitoring Unit ( BTMU ) ..................................................................................... A

MO-32-51 Steering
32-51-01A Nose Wheel Steering Control System...................................................................................................A
32-51-02A Rudder PEDALS DISC pb ................................................................................................................... B
32-51-03A NWS Electrical Deactivation Box (towing mode is not available when the lever is in the TOWING
position)....................................................................................................................................................................C
32-51-03B NWS Electrical Deactivation Box (NWS Electrical Deactivation Box deactivated)................................ D
32-51-04A PARKING BRAKE light on the NWS Electrical Deactivation Box......................................................... E

MO-33 Lights
MO-33-01 Overhead Panels
MO-33-01-02 SIGNS Overhead Panel
33-01-02-02A AUTO Function of SEAT BELTS SIGNS selector............................................................................A
33-01-02-03A AUTO Function of NO SMOKING SIGNS selector ......................................................................... B

MO-33-20 Cabin Lighting

33-20-03A Lavatory Sign (Return to seat).............................................................................................................. A

MO-33-40 Exterior Lighting

33-40-04A Landing light Extension/Retraction System........................................................................................... A
33-40-08A(B) Beacon light ..................................................................................................................................... B
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MO-34 Navigation
MO-34-01 Overhead Panels
MO-34-01-01 ADIRS Overhead Panel
34-01-01-31A ADR pb-sw ...................................................................................................................................... A
34-01-01-32A IR pb-sw .......................................................................................................................................... B

MO-34-05 Indications on the Primary Flight Display (PFD)

34-05-07A Other Air Data Related Indications on the PFD ...................................................................................A
34-05-08A Attitude Indication on the PFD ............................................................................................................. B

MO-34-10 Air Data/Inertial Reference System (ADIRS)

34-10-02B ADR 2.................................................................................................................................................... A
34-10-03A ADR 3.................................................................................................................................................... B
34-10-04B(C) IR 1 (only NAV mode of IR 1 inoperative)....................................................................................... C
34-10-05B IR 2 (IR 2 totally inoperative)................................................................................................................ D
34-10-05C IR 2 (only NAV mode of IR 2 inoperative)............................................................................................ E
34-10-06A IR 3 ADIRU with IR 3 totally inoperative).............................................................................................F
34-10-06B IR 3 (ADIRU with only NAV mode of IR 3 inoperative)........................................................................ G

MO-34-11 Sensors
34-11-02A CAPT Total Air Temperature ( TAT ) Sensor Element Connected to ADR 1 ....................................... A
34-11-03A CAPT Total Air Temperature (TAT) Sensor Element Connected to ADR 3.......................................... B
34-11-04A F/O Total Air Temperature ( TAT ) Sensor Element Connected to ADR 2 .......................................... C

MO-34-22 Attitude and Heading Standby Data

34-22-01B Standby Compass Indicator...................................................................................................................A

MO-34-23 Integrated Standby Instrument System (ISIS)

ISIS Attitude Indication............................................................................................................................................ A

MO-34-30 Landing and Taxiing Aid

34-30-04A Instrument Landing System (ILS)..........................................................................................................A

MO-34-40 GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar

34-40-02A Radio Altimeter Automatic Callout.........................................................................................................A
34-40-03A Radio Altimeter System......................................................................................................................... B
34-40-07A PULL UP-GPWS pb-sw ....................................................................................................................... C

MO-34-50 ATC and Radio/GPS Navigation Systems

34-50-01A ATC .......................................................................................................................................................A
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MO-35 Oxygen
MO-35-01 Overhead Panels
MO-35-01-01 OXYGEN Overhead Panel
35-01-01-31B MANUAL Control of the MASK MAN ON pb .................................................................................. A
35-01-01-33A HI ALT LANDING pb-sw ................................................................................................................. B

MO-35-07 Indications on the DOOR/OXY SD page

35-07-01A Crew OXY High Pressure Indication on the DOOR/OXY SD page ......................................................A
35-07-02A Crew Oxygen REGUL LO PR Indication on the DOOR/OXY SD page ............................................... B

MO-35-10 Crew Oxygen

35-10-03A Exterior Crew Oxygen Overpressure Indicator Disc (Green Disc)........................................................ A

MO-35-20 Passenger Oxygen

35-20-01B Passenger Oxygen Unit.........................................................................................................................A
35-20-02B Cabin Attendant Oxygen Unit................................................................................................................B
35-20-04A Galley Oxygen Unit (cabin attendant oxygen unit available near the galley)........................................ C
35-20-04B Galley Oxygen Unit (cabin attendant portable oxygen device available near the galley)...................... D

MO-36 Pneumatic
MO-36-11 Engine Bleed Air Supply System
36-11-01A(E) Engine Bleed Air Supply System (non-ETOPS flights).....................................................................A
Engine Bleed Air Supply System (ETOPS flights).................................................................................................. B
36-11-06B Engine Bleed IP Check Valve............................................................................................................... C
36-11-07B Engine Bleed HP Valve ....................................................................................................................... D

MO-36-12 APU Bleed Air Supply and Crossbleed Systems

36-12-02B APU Bleed Valve................................................................................................................................... A
36-12-04A Automatic control of the X Bleed Valve................................................................................................ B
36-12-05A Manual Control of the X Bleed Valve....................................................................................................C

MO-36-22 Leak Detection Loop

36-22-03B(C) APU Leak Detection Loop................................................................................................................ A

MO-49 Airborne Power Unit

MO-49-10 Power Plant
49-10-01A(B)(C) Power Plant (APU).......................................................................................................................A
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MO-52 Doors
MO-52-07 Indications on the DOOR/OXY SD page
52-07-01A Passenger Door Permanently Indicated Open on the DOOR/OXY SD page (SLIDE ARMED light
operative)................................................................................................................................................................. A
52-07-01B(C)(D) Passenger Door Permanently Indicated Open on the DOOR/OXY SD page (SLIDE ARMED light
may be permanently illuminated)............................................................................................................................ B
52-07-02A(B) Passenger Door Permanently Indicated Closed on the DOOR/OXY SD page ............................... C
52-07-03A(B)(C)(D) Overwing Emergency Exit Permanently Indicated Open on the DOOR/OXY SD page ......... D
52-07-04A(B) Overwing Emergency Exit Permanently Indicated Closed on the DOOR/OXY SD page .................E
52-07-05A Cargo Door Indication on the DOOR/OXY SD page ............................................................................F
52-07-06A Avionics Compartment Access Door Indication on the DOOR/OXY SD page .....................................G

MO-52-30 Cargo Door

52-30-07A Cargo Door Open/Locked Indicator light ..............................................................................................A

MO-52-51 Reinforced Cockpit Door (CDLS)

52-51-01B Normal System...................................................................................................................................... A
52-51-04A CDLSKeypad......................................................................................................................................... B
52-51-05A LEDS......................................................................................................................................................C

MO-52-53 Cockpit Door Panel on the Center Pedestal

52-53-01A Fault light............................................................................................................................................... A
52-53-02A Open Light............................................................................................................................................. B
52-53-03A Toggle Switch on Cockpit Door Panel.................................................................................................. C
52-53-04A Toggle Switch on Cockpit Door Panel. ................................................................................................ D

MO-56 Windows
MO-56-10 Cockpit
56-10-01A(B)(C)(D) Front Windshield..................................................................................................................... A

MO-73 Engine Fuel and Control

MO-73-20 Controlling
73-20-04A EPR Control Mode.................................................................................................................................A
73-20-05A Minimum Idle on Ground....................................................................................................................... B

MO-74 Ignition
MO-74-07 Indications on the ENGINE SD page
74-07-01A Selected Igniter Indication on the ENGINE SD page ...........................................................................A
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MO-74-31 Ignition Starting and Continuous Relight
74-31-01A Ignition System A...................................................................................................................................A
74-31-02A Ignition System B...................................................................................................................................B

MO-78 Exhaust
MO-78-30 Thrust Reversers
78-30-01A Thrust Reverser..................................................................................................................................... A

MO-79 Oil
MO-79-09 ECAM Alerts
79-09-01A ENG 1(2) OIL LO PR Alert....................................................................................................................A

MO-79-20 Distribution
79-20-01A Air Cooled Oil Cooler (ACOC) Modulating Valve.................................................................................. A

MO-80 Starting
MO-80-11 Pneumatic Starter and Valve System
80-11-01A Start Valve............................................................................................................................................. A

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Localization Toc ID Reason

Title Index
MO-34-10 D 1 Addition of information to clarify the impact on ADS-B OUT
34-10-05B IR 2 (IR 2 totally function.
inoperative) Procedure update to specify the case of simultaneous ADR
and IR failure.
MO-34-10 F 2 Procedure update to specify the case of simultaneous ADR and IR
34-10-06A IR 3 ADIRU with IR 3 failure.
totally inoperative)
MO-35-01-01 A 1 Update of the reference to the European Regulation for
35-01-01-31B MANUAL Control of Supplemental Oxygen.
the MASK MAN ON pb
MO-35-20 A 1 Update of the reference to the European Regulation for
35-20-01B Passenger Oxygen Unit Supplemental Oxygen.
MO-35-20 B 2 Update of the reference to the European Regulation for
35-20-02B Cabin Attendant Oxygen Supplemental Oxygen
Unit
MO-36-11 A 2 In the case of a live animal transportation, with a cargo heating
36-11-01A(E) Engine Bleed Air switched off, the reference to the Live Animal Transportation
Supply System (non-ETOPS flights) Calculation Tool is added.
MO-36-11 A 4 In the case of a live animal transportation, with a cargo heating
36-11-01A(E) Engine Bleed Air switched off, the reference to the Live Animal Transportation
Supply System (non-ETOPS flights) Calculation Tool is added.
MO-36-11 B 6 In the case of a live animal transportation, with a cargo heating
Engine Bleed Air Supply System switched off, the reference to the Live Animal Transportation
(ETOPS flights) Calculation Tool is added.
MO-36-11 B 8 In the case of a live animal transportation, with a cargo heating
Engine Bleed Air Supply System switched off, the reference to the Live Animal Transportation
(ETOPS flights) Calculation Tool is added.
MO-36-11 C 9 Documentation update: Information "N.00008870.0001001.019"
36-11-06B Engine Bleed IP Check moved from "N.00008870.0001001.018" to
Valve "N.00008870.0001001.038"
Documentation update: Information "N.00008870.0001001.020"
moved from "N.00008870.0001001.018" to
"N.00008870.0001001.038"
Documentation update: Deletion of information.
MO-78-30 A 2 Documentation update: Addition of "Thrust Reverser"
78-30-01A Thrust Reverser documentary unit
MO-36-11 A 1 Effectivity update: The information now also applies to MSN 4516,
36-11-01A(E) Engine Bleed Air 4767, 4972, 5178, 5234.
Supply System (non-ETOPS flights)
MO-36-11 A 3 Effectivity update: The information no longer applies to MSN 4516,
4767, 4972, 5178, 5234.
Continued on the following page

LAN COLOMBIA FLEET MO-PLP-SOH P 1/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
PRELIMINARY PAGES - SUMMARY OF HIGHLIGHTS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Localization Toc ID Reason
Title Index
36-11-01A(E) Engine Bleed Air
Supply System (non-ETOPS flights)
MO-36-11 B 5 Effectivity update: The information no longer applies to MSN 4516,
Engine Bleed Air Supply System 4767, 4972, 5178, 5234.
(ETOPS flights)
MO-36-11 B 7 Effectivity update: The information now also applies to MSN 4516,
Engine Bleed Air Supply System 4767, 4972, 5178, 5234.
(ETOPS flights)
MO-78-30 A 1 Effectivity update: The information no longer applies to MSN 5178,
78-30-01A Thrust Reverser 5234.

LAN COLOMBIA FLEET MO-PLP-SOH P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-09-01A VENT BLOWER FAULT Alert

Ident.: MO-21-09-00008895.0001001 / 17 SEP 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Disregard the VENT BLOWER FAULT alert displayed on the EWD.
Disregard the BLOWER pb-sw FAULT light illuminated on the VENTILATION Overhead .
Note: If the ground horn sounds:
EIS/HORN/SPLY (121VU P09) C/B ............................................................................. Pull
The C/B must be closed again after first engine start
If the ground horn sounds after landing when engines are off, it can be silenced again. In
this case, the ADIRS must be set to OFF before leaving the aircraft.

21-09-02A VENT EXTRACT FAULT Alert

Ident.: MO-21-09-00008896.0001001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Disregard the VENT EXTRACT FAULT alert displayed on the EWD.

LAN COLOMBIA FLEET MO-21-09 P 1/2

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-21-09 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-23 - Lavatory And Galley Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-23-01B Lavatory and Galley Extraction Fan

Ident.: MO-21-23-00008830.0005001 / 27 FEB 15
Applicable to: ALL

GENERAL INFORMATION
Two amber crosses replace the cabin zone temperature indications on the COND SD page .
Refer to Item 21-07-03-01 Indications on the COND SD page
The INOP SYS column on the STATUS SD page may display the LAV DET message.
The cabin zone temperature regulation is lost.
The Air Conditioning System Controller commands FWD and AFT cabin ducts temperature using
the position of the FWD CABIN selector and the AFT CABIN selector on the AIR COND overhead
panel.
Slight effect on cabin comfort may occur.
The cockpit temperature regulation is still operative.

LAN COLOMBIA FLEET MO-21-23 P 1/2

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-23 - Lavatory And Galley Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-21-23 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-26-01A Avionics Blower Fan ( VENT AVNCS SYS FAULT Alert not displayed)
Ident.: MO-21-26-00008831.0001001 / 10 OCT 14
Applicable to: ALL

DURING COCKPIT PREPARATION

Supply the aircraft electrical network.
Check that the air conditioning correctly operates with both air conditioning packs set to on.
BLOWER pb-sw ..................................................................................................................OVRD
AVNCS VENT/BLOWER/FAN (123VU AD10) C/B .................................................................Pull
Check that the VENT AVNCS SYS FAULT and VENT EXTRACT FAULT alerts are not
displayed on the EWD .
If the VENT EXTRACT FAULT alert is displayed on the EWD , the blower fan may be
seized. In that case:
Contact the maintenance personnel to exchange the blower fan and the extract fan.
Only the VENT EXTRACT FAULT alert must then be displayed on the EWD .
When the blower and extract fans are exchanged, Refer to Item 21-26-02 Avionics Extract
Fan

Avionics Blower Fan (Air conditioning inlet

21-26-01B
valve checked open before each flight)
Ident.: MO-21-26-00009179.0001001 / 10 OCT 14
Applicable to: ALL

DURING COCKPIT PREPARATION

Supply the aircraft electrical network.
Check that the air conditioning correctly operates with both air conditioning packs set to on.
BLOWER pb-sw ..................................................................................................................OVRD
AVNCS VENT/BLOWER/FAN (123VU AD10) C/B .................................................................Pull
Check that the VENT EXTRACT FAULT alert is not displayed on the EWD
If the VENT EXTRACT FAULT alert is displayed on the EWD , the blower fan may be
seized. In that case:
Contact the maintenance personnel to exchange the blower fan and the extract fan.
Only the VENT EXTRACT FAULT alert must then be displayed on the EWD .
When the blower and extract fans are exchanged, Refer to Item 21-26-02 Avionics Extract
Fan

LAN COLOMBIA FLEET MO-21-26 P 1/8

MEL A to B 10 OCT 14
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Avionics Blower Fan (Avionics ventilation

21-26-01C
system checked before each flight)
Ident.: MO-21-26-00009180.0001001 / 10 OCT 14
Applicable to: ALL

DURING COCKPIT PREPARATION

Supply the aircraft electrical network.
Check that air the conditioning correctly operates with both air conditioning packs set to on.
BLOWER pb-sw ..................................................................................................................OVRD
AVNCS VENT/BLOWER/FAN (123VU AD10) C/B .................................................................Pull
Check that the VENT EXTRACT FAULT alert is not displayed on the EWD
After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert using the CLR pb .
The VENT AVNCS SYS FAULT alert will be displayed after landing
If the VENT EXTRACT FAULT alert is displayed on the EWD , the blower fan may be
seized. In that case:
Contact the maintenance personnel to exchange the blower fan and the extract fan.
Only the VENT EXTRACT FAULT alert must then be displayed on the EWD .
When the blower and extract fans are exchanged, Refer to Item 21-26-02 Avionics Extract
Fan

21-26-02A Avionics Extract Fan (VENT AVNCS SYS FAULT Alert not displayed)
Ident.: MO-21-26-00009184.0001001 / 10 OCT 14
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Time limitation on ground with electrical network supplied:
OAT (C) 38 45 55
Max time No limit 3h 35 min

DURING COCKPIT PREPARATION

Supply the aircraft electrical network.
Check that the air conditioning correctly operates with both air conditioning packs set to on.
EXTRACT pb-sw ................................................................................................................ OVRD
Clear the VENT EXTRACT FAULT alert using the CLR pb.
AVNCS VENT/EXTC/FAN (123VU AE2) C/B .........................................................................Pull
Check that the VENT AVNCS SYS FAULT alert is not displayed on the EWD.
Continued on the following page

LAN COLOMBIA FLEET MO-21-26 P 2/8

MEL C to D 10 OCT 14
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Note: If the ground horn sounds:

EIS/HORN/SPLY (121VU P09) C/B ............................................................................. Pull
The C/B must be closed again after first engine start
If the ground horn sounds after landing when engines are off, it can be silenced again. In
this case, the ADIRS must be set to OFF before leaving the aircraft.

Avionics Extract Fan (Air conditioning inlet

21-26-02B
valve checked open before each flight)
Ident.: MO-21-26-00009185.0001001 / 10 OCT 14
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Time limitation on ground with electrical network supplied:
OAT (C) 38 45 55
Max time No limit 3h 35 min

DURING COCKPIT PREPARATION

Supply the aircraft electrical network.
Check that the air conditioning correctly operates with both air conditioning packs set to on.
EXTRACT pb-sw ................................................................................................................ OVRD
Clear the VENT EXTRACT FAULT alert using the CLR pb.
AVNCS VENT/EXTC/FAN (123VU AE2) C/B .........................................................................Pull
Note: If the ground horn sounds:
EIS/HORN/SPLY (121VU P09) C/B ............................................................................. Pull
The C/B must be closed again after first engine start
If the ground horn sounds after landing when engines are off, it can be silenced again. In
this case, the ADIRS must be set to OFF before leaving the aircraft.

LAN COLOMBIA FLEET MO-21-26 P 3/8

MEL D to E 10 OCT 14
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Avionics Extract Fan (Avionics ventilation

21-26-02C
system checked before each flight)
Ident.: MO-21-26-00008853.0001001 / 10 OCT 14
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Time limitation on ground with electrical network supplied:
OAT (C) 38 45 55
Max time No limit 3h 35 min

DURING COCKPIT PREPARATION

Supply the aircraft electrical network.
Check that the air conditioning correctly operates with both air conditioning packs set to on.
EXTRACT pb-sw ................................................................................................................ OVRD
Clear the VENT EXTRACT FAULT alert using the CLR pb.
AVNCS VENT/EXTC/FAN (123VU AE2) C/B .........................................................................Pull
After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert using the CLR pb.
The VENT AVNCS SYS FAULT alert will be displayed after landing.
Note: If the ground horn sounds:
EIS/HORN/SPLY (121VU P09) C/B ............................................................................. Pull
The C/B must be closed again after first engine start
If the ground horn sounds after landing when engines are off, it can be silenced again. In
this case, the ADIRS must be set to OFF before leaving the aircraft.

21-26-03A Avionics Skin Exchanger Inlet Bypass Valve

Ident.: MO-21-26-00008855.0001001 / 11 MAR 10
Applicable to: ALL

ON GROUND
After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb.
The VENT AVNCS SYS FAULT alert will be displayed after landing.

LAN COLOMBIA FLEET MO-21-26 P 4/8

MEL F to G 10 OCT 14
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-26-04A Avionics Skin Air Outlet Valve

Ident.: MO-21-26-00008856.0001001 / 10 OCT 14
Applicable to: ALL

ON GROUND
After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb.
The VENT AVNCS SYS FAULT alert will be displayed after landing.
Note: Avionics smoke may be not perceptible from the cockpit due to the opening of the
internal flap of the valve.
In the case of AVIONICS SMOKE alert:
Apply the ECAM procedure even if the smoke is not perceptible.

Avionics Skin Air Inlet Valve (Air

21-26-05A
conditioning inlet valve open on the ground)
Ident.: MO-21-26-00009186.0001001 / 10 OCT 14
Applicable to: ALL

DURING COCKPIT PREPARATION

Supply the aircraft electrical network.
Check that the air conditioning is operating with one or two air conditioning packs set to on.
EXTRACT pb-sw ................................................................................................................ OVRD
Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb.
Note: With only one air conditioning pack operative, operating time on ground is limited to 1 h.
AFTER TAKEOFF
EXTRACT pb-sw ..................................................................................................................... AUTO
AFTER LANDING
EXTRACT pb-sw ..................................................................................................................... OVRD

LAN COLOMBIA FLEET MO-21-26 P 5/8

MEL H to I 10 OCT 14
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Avionics Skin Air Inlet Valve (Air conditioning

21-26-05B
inlet valve secured in the open position)
Ident.: MO-21-26-00008857.0001001 / 10 OCT 14
Applicable to: ALL

DURING COCKPIT PREPARATION

Supply the aircraft electrical network.
Check that the air conditioning is operating with one or two air conditioning packs set to on.
EXTRACT pb-sw ................................................................................................................ OVRD
After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb.
The VENT AVNCS SYS FAULT alert will be displayed after landing.
Note: With only one air conditioning pack operative, operating time on ground is limited to 1 h.
AFTER TAKEOFF
EXTRACT pb-sw ..................................................................................................................... AUTO
AFTER LANDING
EXTRACT pb-sw ..................................................................................................................... OVRD

21-26-06A
Avionics Skin Exchanger Isolation Valve
21-26-06B
Ident.: MO-21-26-00008859.0001001 / 11 MAR 10
Applicable to: ALL

ON GROUND
After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb.

21-26-08A Avionics Air Conditioning Inlet Valve

Ident.: MO-21-26-00008860.0001001 / 11 MAR 10
Applicable to: ALL

ON GROUND
After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb.

LAN COLOMBIA FLEET MO-21-26 P 6/8

MEL J to L 10 OCT 14
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Avionics Ventilation Filter (VENT

21-26-09A
AVNCS SYS FAULT Alert not displayed)
Ident.: MO-21-26-00008861.0001001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Supply the aircraft electrical network.
Check that the air conditioning is operating with both air conditioning packs set to on.
EXTRACT pb-sw ................................................................................................................ OVRD
Check that the VENT AVNCS SYS FAULT alert is not displayed on the EWD.

Avionics Ventilation Filter (Air conditioning

21-26-09B
inlet valve checked open before each flight)
Ident.: MO-21-26-00009187.0001001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Supply the aircraft electrical network.
Check that the air conditioning is operating with both air conditioning packs set to on.
EXTRACT pb-sw ................................................................................................................ OVRD

Avionics Ventilation Filter (Avionics

21-26-09C
ventilation system checked before each flight)
Ident.: MO-21-26-00009188.0001001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Supply the aircraft electrical network.
Check that the air conditioning is operating with both air conditioning packs set to on.
EXTRACT pb-sw ................................................................................................................ OVRD
After application of the maintenance procedure:
Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb.
The VENT AVNCS SYS FAULT alert will be displayed after landing.

LAN COLOMBIA FLEET MO-21-26 P 7/8

MEL M to O 10 OCT 14
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-26 - Avionics Equipment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-26-10A Avionics Equipment Ventilation Computer (AEVC)

Ident.: MO-21-26-00008862.0001001 / 17 SEP 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Supply the aircraft electrical network.
Check that the conditioning is operating with both air conditioning packs set to on.
BLOWER pb-sw ..................................................................................................................OVRD
EXTRACT pb-sw ................................................................................................................ OVRD
Note: If the ground horn sounds:
EIS/HORN/SPLY (121VU P09) C/B ............................................................................. Pull
The C/B must be closed again after first engine start
If the ground horn sounds after landing when engines are off, it can be silenced again. In
this case, the ADIRS must be set to OFF before leaving the aircraft.

Note: In the case of a low pressure in the avionics compartment ventilation ducts, the weather
radar image may not be displayed on the ND on ground.

Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb
IN FLIGHT
In the case of an air conditioning pack failure:
The cabin altitude may reach about 9 700 ft (3 000 m), and
The CAB PR EXCESS CAB ALT alert may be displayed on the EWD.

LAN COLOMBIA FLEET MO-21-26 P 8/8

MEL P 10 OCT 14
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-28 - Cargo Compartment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-28-03A AFT Cargo Extraction Fan

Ident.: MO-21-28-00008871.0001001 / 27 FEB 15
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
For live animal transportation, use the Live Animal Transportation Calculation Tool.

21-28-04A AFT Cargo Isolation Valve (Valves checked closed)

Ident.: MO-21-28-00008874.0001001 / 27 FEB 15
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
For live animal transportation, use the Live Animal Transportation Calculation Tool.
DURING COCKPIT PREPARATION
ANN LT selector .................................................................................................................. TEST
Check that the AFT ISOL VALVE pb-sw FAULT light comes on
ANN LT selector ........................................................................................................BRT or DIM
AFT ISOL VALVE pb-sw ....................................................................................................... OFF
Check that the AFT ISOL VALVE pb-sw FAULT light does not come on.
Note: If the AFT ISOL VALVE pb-sw FAULT light comes on:
The AFT cargo isolation valve must be secured in the closed position. Refer to Item
21-28-04B AFT Cargo Isolation Valve

21-28-04B AFT Cargo Isolation Valve (Valves secured closed)

Ident.: MO-21-28-00012797.0001001 / 27 FEB 15
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
For live animal transportation, use the Live Animal Transportation Calculation Tool.

LAN COLOMBIA FLEET MO-21-28 P 1/2

MEL A to C 27 FEB 15
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-28 - Cargo Compartment Ventilation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-21-28 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-31 - Pressure Control and Monitoring
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-31-01A Automatic Cabin Pressure Control System

21-31-01B (CPC, Outflow Valve AUTO Channel)
Ident.: MO-21-31-00008875.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

DURING COCKPIT PREPARATION

If CPC 1 is affected:
AIR COND/CAB/PRESS/CTL 1 (49VU D09) C/B .................................................................Pull
If CPC 2 is affected:
AIR COND/CAB/PRESS/CTL 2 (122VU Y22) C/B ............................................................... Pull
MODE SEL pb-sw .................................................................................................................MAN
On the CAB PRESS SD page, check that the cabin differential pressure, the cabin vertical
speed, the cabin altitude, and the outflow valve position are available.
MAN V/S CTL sw .................................................................................................................... DN
On the CAB PRESS SD page, check outflow valve movement.
MODE SEL pb-sw ...............................................................................................................AUTO

21-31-01A Automatic Cabin Pressure Control System

21-31-01B (CPC, Outflow Valve AUTO Channel)
Ident.: MO-21-31-00008875.0002001 / 27 FEB 15
Applicable to: MSN 4758-5453

DURING COCKPIT PREPARATION

If CPC 1 is affected:
AIR COND/CAB/PRESS/CTL 1 (49VU D09) C/B .................................................................Pull
If CPC 2 is affected:
AIR COND/CAB/PRESS/CTL 2 (122VU Y22) C/B ............................................................... Pull
RPCU (122VU X23) C/B .........................................................................................................Pull
MODE SEL pb-sw .................................................................................................................MAN
On the CAB PRESS SD page, check that the cabin differential pressure, the cabin vertical
speed, the cabin altitude, and the outflow valve position are available.
MAN V/S CTL sw .................................................................................................................... DN
On the CAB PRESS SD page, check outflow valve movement.
RPCU (122VU X23) C/B ...................................................................................................... Push
MODE SEL pb-sw ...............................................................................................................AUTO

LAN COLOMBIA FLEET MO-21-31 P 1/2

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-31 - Pressure Control and Monitoring
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-31-04A Landing Elevation Selection AUTO Function

Ident.: MO-21-31-00008876.0001001 / 11 MAR 10
Applicable to: ALL

BEFORE TAKEOFF
Set the LDG ELEV selector on the CABIN PRESS panel at the destination airport altitude.
On the CAB PRESS SD page, check that the LDG ELEV MAN message is displayed .

21-31-05A Landing Elevation Selection MAN Function

Ident.: MO-21-31-00008877.0001001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

On the CAB PRESS SD page, check that the LDG ELEV AUTO message is displayed to confirm
correct position of the LDG ELEV selector.
Note: The landing field elevation of the destination airport may not be correctly displayed on the
CAB PRESS SD page. It is automatically corrected after first engine start.

LAN COLOMBIA FLEET MO-21-31 P 2/2

MEL B to C 27 FEB 15
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-51 - Flow Control and Indicating
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-51-03A Pack Flow Sensor

Ident.: MO-21-51-00008886.0001001 / 27 FEB 15
Applicable to: ALL

GENERAL INFORMATION
The hot air pressure regulating valve automatically closes.
The Flow Control Valve on the affected side operates in pneumatic backup mode.
FLIGHT PREPARATION/LIMITATIONS
If the FWD cargo heating is installed:
For live animal transportation, use the Live Animal Transportation Calculation Tool.
DURING COCKPIT PREPARATION
AIR COND HOT AIR pb-sw ....................................................................................................... OFF
Note: Unequal passengers distribution may cause high temperature in the rear cabin when
the hot air pressure regulating valve is closed.
The temperature in the cockpit may be low when the hot air pressure regulating valve
is closed combined with single pack operation.

LAN COLOMBIA FLEET MO-21-51 P 1/2

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-51 - Flow Control and Indicating
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-21-51 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-52 - Air Cooling System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-52-01D Air Conditioning Pack (One Air Conditioning

21-52-01E Pack Inoperative for C Repair Interval)
Ident.: MO-21-52-00008889.0005001 / 10 OCT 14
Applicable to: ALL

DURING COCKPIT PREPARATION

PACK FLOW pb-sw ....................................................................................................................... HI
IN FLIGHT
If BLOWER pb-sw and EXTRACT pb-sw are set to OVRD:
The cabin altitude may reach about 9 700 ft, and
The CAB PR EXCESS CAB ALT alert may be displayed on the EWD
Observe the MOCA or Grid MORA altitudes.

Air Conditioning Pack (One Air Conditioning

21-52-01G
Pack in Heat Exchanger Cooling Mode only)
Ident.: MO-21-52-00009193.0001001 / 27 NOV 12
Applicable to: ALL

DURING COCKPIT PREPARATION

PACK 1(2) pb-sw in "heat exchanger cooling only"....................................................................OFF
IN FLIGHT
When the TAT is equal to or less than 12C:
PACK 1(2) pb-sw in "heat exchanger cooling only"................................................................On
If the non affected air conditioning pack fails:
Maximum flight altitude................................................................................ 31 500 ft (9 600 m)
Observe the MOCA or Grid MORA altitudes.

DURING DESCENT
If the TAT is above 12C:
PACK 1(2) pb-sw in "heat exchanger cooling only"............................................................. OFF
AT THE END OF THE DESCENT, BEFORE LANDING
PACK 1(2) pb-sw in "heat exchanger cooling only"....................................................................OFF

LAN COLOMBIA FLEET MO-21-52 P 1/2

MEL A to B 10 OCT 14
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-52 - Air Cooling System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-21-52 P 2/2

MEL 10 OCT 14
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-63 - Cockpit and Cabin Temperature Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-63-02A Cockpit and Cabin Trim Air Valve (Affected valve checked closed)
Ident.: MO-21-63-00008893.0002001 / 27 FEB 15
Applicable to: ALL

DURING COCKPIT PREPARATION

On the COND SD page , check that the affected trim air valve is closed.
IN FLIGHT
If the affected zone temperature becomes uncomfortable:
HOT AIR pb-sw ................................................................................................................... OFF

Cockpit and Cabin Trim Air Valve (Hot air

21-63-02B
pressure regulating valve checked operative)
Ident.: MO-21-63-00009194.0003001 / 27 FEB 15
Applicable to: ALL

DURING COCKPIT PREPARATION

HOT AIR pb-sw ........................................................................................................OFF then on
On the COND SD page, check that the hot air pressure regulating valve follows the HOT AIR
pb-sw command.
IN FLIGHT
If affected zone temperature becomes uncomfortable:
HOT AIR pb-sw ................................................................................................................... OFF

Hot Air Pressure Regulating Valve (Hot

21-63-03A
air pressure valve checked closed)
Ident.: MO-21-63-00009195.0001001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

HOT AIR pb-sw ..................................................................................................................... OFF
On the COND SD page page, check that the hot air pressure regulating valve is closed amber.

LAN COLOMBIA FLEET MO-21-63 P 1/2

MEL A to C 27 FEB 15
 MEL OPERATIONAL PROCEDURES
21 - AIR CONDITIONING
21-63 - Cockpit and Cabin Temperature Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

21-63-03B Hot Air Pressure Regulating Valve (Trim air valve checked closed)
Ident.: MO-21-63-00009196.0002001 / 27 FEB 15
Applicable to: ALL

GENERAL INFORMATION
On the COND SD page, the hot air pressure regulating valve is displayed amber open.
DURING COCKPIT PREPARATION
HOT AIR pb-sw ..................................................................................................................... OFF
On the COND SD page, check that all the trim air valves are closed.

Hot Air Pressure Regulating Valve (Affected

21-63-03C
valve secured in the closed position)
Ident.: MO-21-63-00008894.0001001 / 14 FEB 13
Applicable to: ALL

DURING COCKPIT PREPARATION

HOT AIR pb-sw .......................................................................................................................... OFF

LAN COLOMBIA FLEET MO-21-63 P 2/2

MEL D to E 27 FEB 15
 MEL OPERATIONAL PROCEDURES
22 - AUTO FLIGHT
22-05 - FMA Indications on the PFD
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-05-01B AP Related Indications on the FMA

Ident.: MO-22-05-00008922.0001001 / 12 SEP 11
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
RVSM operations are not permitted.
Maximum landing capability is CAT 1.

22-05-03A Approach and Landing Capabilities on the FMA

Ident.: MO-22-05-00008923.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
When one FMA is affected:
Maximum landing capability is CAT 2.
When both FMAs are affected:
Maximum landing capability is CAT 1.

LAN COLOMBIA FLEET MO-22-05 P 1/2

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
22 - AUTO FLIGHT
22-05 - FMA Indications on the PFD
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-22-05 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
22 - AUTO FLIGHT
22-10 - Autopilot/Flight Director (AP/FD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-10-01A
Autopilot (AP)
22-10-01B
Ident.: MO-22-10-00008897.0001001 / 18 MAY 11
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
When one AP is inoperative:
Maximum landing capability is CAT 3 SINGLE.
When both APs are inoperative:
RVSM operations are not permitted.
Maximum landing capability is CAT 1.

22-10-02A Flight Director (FD)

Ident.: MO-22-10-00008898.0001001 / 12 SEP 11
Applicable to: ALL

FOR TAKEOFF
For a takeoff without FDs:
Refer to FCOM/ No Flight Director Takeoff.

22-10-04A Take-over pb AP Disconnection Function (One inoperative)

Ident.: MO-22-10-00008899.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 1.
BEFORE ENGINE START
AP 1...........................................................................................................................................On
Operative take-over pb......................................................................................................... Press
Check that the red AP OFF message is displayed on the EWD.
AP 2...........................................................................................................................................On
Operative take-over pb......................................................................................................... Press
Check that the red AP OFF message is displayed on the EWD.
Continued on the following page

LAN COLOMBIA FLEET MO-22-10 P 1/2

MEL A to C 20 JUN 14
 MEL OPERATIONAL PROCEDURES
22 - AUTO FLIGHT
22-10 - Autopilot/Flight Director (AP/FD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

BEFORE APPROACH
If the AP is used for approach:
The operative AP disconnect pb must be assigned to the PF.

22-10-04B Take-over pb AP Disconnection Function (Both inoperative)

Ident.: MO-22-10-00008900.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 1.

22-10-05A AUTO LAND light

Ident.: MO-22-10-00008901.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
When both lights are inoperative:
Maximum landing capability is CAT 1.

22-10-06A AP Disengagement Warning

Ident.: MO-22-10-00008902.0001001 / 18 MAY 11
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
RVSM operations are not permitted.
Maximum landing capability is CAT 1.

22-10-07A Sticks and Rudder Pedals Locking Solenoid in AP Mode

Ident.: MO-22-10-00008903.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 2 without autoland.

LAN COLOMBIA FLEET MO-22-10 P 2/2

MEL C to G 20 JUN 14
 MEL OPERATIONAL PROCEDURES
22 - AUTO FLIGHT
22-30 - Autothrust
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-30-01A Autothrust (A/THR)

Ident.: MO-22-30-00008904.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 2.
AFTER ENGINE START
Press and hold either autothrust instinctive disconnect pb for at least 15 s.
The A/THR system is permanently disconnected for the entire flight.
Check that A/THR INOP SYS is displayed on the STATUS SD page.
All A/THR functions including ALPHA FLOOR protection are lost.

22-30-02A Autothrust Instinctive Disconnect pb

Ident.: MO-22-30-00008905.0002001 / 12 MAR 10
Applicable to: ALL

The purpose of the procedure is to check the A/THR disconnection via the remaining Instinctive
Disconnect pb and via the A/THR pb on the FCU.
AFTER IRS ALIGNMENT
Note: Disregard alerts during the test. Use the EMER CANCEL pb on the ECAM control panel
as necessary.
Aircraft configuration for the check via the FMS 1:
ENG/FADEC GND PWR 1 and 2.............................................................................................ON
Both thrust levers................................................................................................................... MCT
FD.............................................................................................................................................. Off
AUTO FLT/FMGC/2 (121 VU M17) C/B ................................................................................. Pull
A/THR........................................................................................................................................ On
Check that green SPEED and white A/THR indications appear on the PFD.
Check that A/THR pb light bars are ON.
Continued on the following page

LAN COLOMBIA FLEET MO-22-30 P 1/4

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
22 - AUTO FLIGHT
22-30 - Autothrust
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Check of the A/THR disconnection via the remaining Instinctive Disconnect pb:
A/THR instinctive disconnect pb (non affected autothrust)....................................................Push
Check that the A/THR pb light bars are OFF.
Check that green SPEED and white A/THR indications are no more displayed on the PFD.
A/THR........................................................................................................................................ On
Check that the A/THR pb light bars are ON.
Check that green SPEED and white A/THR indications are displayed on the PFD.
Check of the A/THR disconnection via the A/THR pb on the FCU:
A/THR pb (on the FCU)............................................................................................................ Off
Check that the A/THR pb light bars are ON.
Check that green SPEED and white A/THR indications are no more displayed on the PFD.
A/THR........................................................................................................................................ On
Aircraft configuration for the check via the FMS 2:
AUTO FLT/FMGC/2 (121VU M17) C/B ................................................................................ Push
AUTO FLT/FMGC/1 (49VU B02) C/B .....................................................................................Pull
Wait 2 min.
Check of the A/THR disconnection via the remaining Instinctive Disconnect pb:
A/THR instinctive disconnect pb (non affected autothrust)....................................................Push
Check that the A/THR pb light bars are OFF.
Check that green SPEED and white A/THR indications are no more displayed on the PFD.
A/THR........................................................................................................................................ On
Check that the A/THR pb light bars are ON.
Check that green SPEED and white A/THR indications are displayed on the PFD.
Check of the A/THR disconnection via the A/THR pb on the FCU:
A/THR pb (on the FCU)............................................................................................................ Off
Check that the A/THR pb light bars are ON.
Check that green SPEED and white A/THR indications are no more displayed on the PFD.
A/THR........................................................................................................................................ On
Continued on the following page

LAN COLOMBIA FLEET MO-22-30 P 2/4

MEL B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
22 - AUTO FLIGHT
22-30 - Autothrust
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Restore normal aircraft configuration:
A/THR........................................................................................................................................ Off
AUTO FLT/FMGC/1 (49VU B02) C/B ...................................................................................Push
ENG/FADEC GND PWR 1 and 2............................................................................................. Off
Both thrust levers................................................................................................................... IDLE
RCL pb (on the ECAM control panel)....................................................................................Push
Wait 2 min before using the MCDU and the FD.

LAN COLOMBIA FLEET MO-22-30 P 3/4

MEL B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
22 - AUTO FLIGHT
22-30 - Autothrust
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-22-30 P 4/4

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
22 - AUTO FLIGHT
22-60 - Flight Augmentation (FAC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-60-02A FAC 2
Ident.: MO-22-60-00008906.0001001 / 27 FEB 15
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 SINGLE.
ON GROUND
If the AUTO FLT FAC 2 FAULT alert is displayed on the EWD
or
If erroneous speeds are displayed:
AUTO FLT/FAC 2/28VDC (121VU M19) C/B ...................................................................Pull
FAC 2 pb-sw ................................................................................................................... OFF

22-60-04A Yaw Damper System

Ident.: MO-22-60-00008907.0001001 / 27 FEB 15
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 SINGLE.

LAN COLOMBIA FLEET MO-22-60 P 1/2

MEL A to B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
22 - AUTO FLIGHT
22-60 - Flight Augmentation (FAC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-22-60 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
22 - AUTO FLIGHT
22-70 - Flight Management System (FMS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-70-01A
Flight Management System (FMS)
22-70-01B
Ident.: MO-22-70-00008913.0001001 / 27 FEB 15
Applicable to: ALL

IN FLIGHT
In the case of FMS 1+2 failure:
MCDU NAV B/UP .................................................................................................................Use
Refer to FCOM/DSC-22_20-60-130 MCDU Back Up Navigation.

LAN COLOMBIA FLEET MO-22-70 P 1/2

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
22 - AUTO FLIGHT
22-70 - Flight Management System (FMS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-22-70 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
22 - AUTO FLIGHT
22-83 - Flight Management and Guidance Computer (FMGC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

22-83-01A
Flight Management and Guidance Computer (FMGC)
22-83-01B
Ident.: MO-22-83-00008919.0001001 / 20 JUN 14
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 SINGLE.
DURING COCKPIT PREPARATION
If FMGC 1 is affected:
AUTO FLT/FMGC/1 (49VU B02 or 121VU M16) C/B ...........................................................Pull
If ADS-B or EHS is required for the intended flight:
ATC selector .......................................................................................................................2
If FMGC 2 is affected:
AUTO FLT/FMGC/2 (121VU M17) C/B ................................................................................ Pull
Note: During IR alignment, when the FMGC 2 is deactivated, IRS IN ALIGN memo cannot
be displayed until the FD 1 is engaged.
If ADS-B or EHS is required for the intended flight:
ATC selector .......................................................................................................................1

LAN COLOMBIA FLEET MO-22-83 P 1/2

MEL A 20 JUN 14
 MEL OPERATIONAL PROCEDURES
22 - AUTO FLIGHT
22-83 - Flight Management and Guidance Computer (FMGC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-22-83 P 2/2

MEL 20 JUN 14
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 23-01-01 - RCDR Overhead Panel
MINIMUM EQUIPMENT LIST

23-01-01-31A RCDR-GND CTL pb-sw (Inoperative in the AUTO position)

Ident.: MO-23-01-01-00008925.0001001 / 11 MAR 10
Applicable to: ALL

ON GROUND
CVR can only be tested through the CVR test pb-sw during the first 5 minutes after supply of the
aircraft electrical network.

23-01-01-31B RCDR-GND CTL pb-sw (Inoperative in the ON position)

Ident.: MO-23-01-01-00009178.0001001 / 11 MAR 10
Applicable to: ALL

AFTER LANDING
To stop CVR recording, if needed:
COM/CVR/SPLY (49 VU E14) C/B ....................................................................................PULL

LAN COLOMBIA FLEET MO-23-01-01 P 1/2

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 23-01-01 - RCDR Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-23-01-01 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-09-01A COM HF 1(2) EMITTING Alert

Ident.: MO-23-09-00008969.0001001 / 31 AUG 11
Applicable to: ALL

GENERAL INFORMATION
To make troubleshooting easier, Refer to FCOM/ COM VHF 1(2)(3)/HF 1(2) EMITTING (If
Installed).
DURING COCKPIT PREPARATION
To deactivate the HF1 system, apply:
COM HF1 (49 VU HA14) C/B ............................................................................................PULL
or
COM NAV/HF1 (121 VU L10) C/B .................................................................................... PULL
To deactivate the HF2 system, apply:
COM NAV/HF2 (121 VU L13) C/B .................................................................................... PULL

23-09-02A COM VHF 1(2)(3) EMITTING Alert

Ident.: MO-23-09-00008970.0001001 / 15 SEP 11
Applicable to: ALL

GENERAL INFORMATION
To make troubleshooting easier, Refer to FCOM/ COM VHF 1(2)(3)/HF 1(2) EMITTING (If
Installed).
DURING COCKPIT PREPARATION
To deactivate the VHF1 system, apply:
COM/VHF/1 (49 VU G09) C/B ...........................................................................................PULL
To deactivate the VHF2 system, apply:
COM NAV/VHF/2 (121 VU L04) C/B ................................................................................. PULL
To deactivate the VHF3 system, apply:
COM NAV/VHF/3 (121 VU L05) C/B ................................................................................. PULL

LAN COLOMBIA FLEET MO-23-09 P 1/2

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-23-09 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-40 - Interphone
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-40-01A Ground External Horn

Ident.: MO-23-40-00008960.0001001 / 02 NOV 11
Applicable to: ALL

ON GROUND
When the aircraft electrical network is supplied:
Monitor the avionics equipment ventilation in the cockpit.
BEFORE LEAVING THE AIRCRAFT
Set the three ADIRS Mode selectors to OFF.

23-40-03A Flight Crew to Ground Communication System

Ident.: MO-23-40-00008961.0001001 / 02 NOV 11
Applicable to: ALL

PROCEDURE
Hand signal must be use.

23-40-04A Service Interphone Jack

Ident.: MO-23-40-00008962.0001001 / 02 NOV 11
Applicable to: ALL

PROCEDURE
Use any jack available. If the system is completed inoperative, use hand signal or portable radio
communications.

LAN COLOMBIA FLEET MO-23-40 P 1/2

MEL A to C 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-40 - Interphone
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-23-40 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-51 - Audio Management
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-51-05A Cockpit Loudspeaker Volume Control

Ident.: MO-23-51-00008963.0001001 / 02 NOV 11
Applicable to: ALL

PROCEDURE
Affected crew member may be use a boom set compatible for use with quick donning oxygen
mask.

LAN COLOMBIA FLEET MO-23-51 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-51 - Audio Management
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-23-51 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-52 - Audio Control Panel (ACP)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-52-01A CAPT and F/O ACP

Ident.: MO-23-52-00008964.0001001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

To recover the audio channel on the affected side:
AUDIO SWITCHING selector .................................................................................. CAPT 3 (F/O 3)

LAN COLOMBIA FLEET MO-23-52 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-52 - Audio Control Panel (ACP)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-23-52 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-02 - DEU A
MINIMUM EQUIPMENT LIST

23-73-02-01A Cabin DEU A

Ident.: MO-23-73-02-00009538.0001001 / 11 MAR 10
Applicable to: ALL

GENERAL INFORMATION
On the affected cabin area:
general cabin illumination is set to full brightness,
Passenger Call is not available,
The (No Smoking/Fasten Seat Belt/No Portable Electric Device) Signs are not available.
IN FLIGHT
When return to seat is requested,
or
When seat belts should be fasten,
or
When smoking is prohibited,
or
When portable electric device use is prohibited,
Use the passenger address system to alert cabin attendants and passengers.

LAN COLOMBIA FLEET MO-23-73-02 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-02 - DEU A
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-23-73-02 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-03 - DEU B
MINIMUM EQUIPMENT LIST

23-73-03-01B Cabin DEU B

Ident.: MO-23-73-03-00009539.0001001 / 02 NOV 11
Applicable to: ALL

PROCEDURE
The following alternate normal procedures and emergency procedures have to be established
before departure:
As alternate normal procedure use the operative handset.
Note: All cabin attendant must take knowledge of the operative handset.
As emergency procedure (fail of the operative handset) use direct verbal communication
between Flight Attendants.

LAN COLOMBIA FLEET MO-23-73-03 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-03 - DEU B
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-23-73-03 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-05 - Cabin Loudspeaker
MINIMUM EQUIPMENT LIST

23-73-05-02A Lavatory Loudspeaker

Ident.: MO-23-73-05-00008965.0001001 / 02 NOV 11
Applicable to: ALL

PROCEDURE
The following alternate normal procedures and emergency procedures have to be established
before departure to alert the passenger in the lavatory, if needed:
After each PA announcement, Flight Attendant must verify that the passenger in the affected
lavatories take knowledge of the announcement that was made (if necessary).
Note: Use this procedure as alternate normal and emergency procedure.

LAN COLOMBIA FLEET MO-23-73-05 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-05 - Cabin Loudspeaker
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-23-73-05 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-06 - Handset
MINIMUM EQUIPMENT LIST

23-73-06-02A Cabin Handset

Ident.: MO-23-73-06-00008966.0001001 / 02 NOV 11
Applicable to: ALL

PROCEDURE
The following alternate normal procedures and emergency procedures have to be established
before departure:
As alternate normal procedure use the operative handset.
Note: All cabin attendant must take knowledge of the operative handset.
As emergency procedure (fail of the operative handset) use direct verbal communication
between Flight Attendants.

LAN COLOMBIA FLEET MO-23-73-06 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-06 - Handset
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-23-73-06 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-07 - Prerecorded Announcement and Music Reproducer (PRAM)
MINIMUM EQUIPMENT LIST

Prerecorded Announcement and Music Reproducer (PRAM)

Ident.: MO-23-73-07-00008967.0002001 / 18 MAY 11
Applicable to: ALL

PROCEDURE TO BE DEVELOPED IN THE OPERATOR'S MEL

Each airline must establish the procedure to replace the prerecorded announcement. Required
demonstration equipment must be provided onboard.

LAN COLOMBIA FLEET MO-23-73-07 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-73 - Cabin Intercommunication Data System
COLOMBIA
LAN COLOMBIA AIRLINES 23-73-07 - Prerecorded Announcement and Music Reproducer (PRAM)
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-23-73-07 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-74 - Cabin Crew Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

23-74-01A FAP Display Unit

Ident.: MO-23-74-00008968.0001001 / 27 FEB 15
Applicable to: ALL

GENERAL INFORMATION
The cabin lighting may be dimmed through the Additional Attendant Panel (AAP) (If available).

LAN COLOMBIA FLEET MO-23-74 P 1/2

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
23 - COMMUNICATIONS
23-74 - Cabin Crew Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-23-74 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
24 - ELECTRICAL POWER
24-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 24-01-01 - ELEC Overhead Panel
MINIMUM EQUIPMENT LIST

24-01-01-07A EXT PWR pb-sw AVAIL light

Ident.: MO-24-01-01-00008971.0001001 / 13 MAR 10
Applicable to: ALL

BEFORE PUSHBACK
Confirm the external power disconnection either on the ELEC SD page or with the ground crew.
PARKING
If the APU is not available:
EXT PWR pb-sw ...............................................................................................................ON
Confirm the external power connection either on the ELEC SD page or with the ground
crew before engine shutdown.

24-01-01-09A GALY & CAB pb-sw FAULT light

Ident.: MO-24-01-01-00008972.0002001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Check of the galley automatic load shed system:
Supply the electrical network from the APU or the external power.
GALY & CAB pb-sw ............................................................................................................AUTO
ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24) C/B .......................................................Pull
Check that a part of the operative galley equipment does not operate.
ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24) C/B .....................................................Push
Note: Disregard this procedure if main galleys are not connected.

LAN COLOMBIA FLEET MO-24-01-01 P 1/2

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
24 - ELECTRICAL POWER
24-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 24-01-01 - ELEC Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-24-01-01 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
24 - ELECTRICAL POWER
24-07 - Indications on the ELEC SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-07-01A AC Generation Indications on the ELEC SD page

Ident.: MO-24-07-00008983.0002001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Check that GEN 1(2) pb-sw FAULT light is on (with the GEN 1(2) pb-sw in the on position).
Check of the galley automatic load shed system:
Supply the electrical network from the APU or the external power.
GALY & CAB pb-sw ............................................................................................................AUTO
ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24) C/B .......................................................Pull
Check that a part of the operative galley equipment does not operate.
ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24) C/B .....................................................Push
Note: Disregard this procedure if main galleys are not connected.

LAN COLOMBIA FLEET MO-24-07 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
24 - ELECTRICAL POWER
24-07 - Indications on the ELEC SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-24-07 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
24 - ELECTRICAL POWER
24-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-09-01A ELEC AC ESS BUS SHED Alert

Ident.: MO-24-09-00008984.0003001 / 18 MAR 10
Applicable to: ALL

GENERAL INFORMATION
When the ELEC AC ESS BUS SHED alert is displayed on the EWD:
The AC ESS BUS SHED message may appear on the ELEC SD page,
The CAPT AOA message may be displayed in the INOP SYS column on the STATUS SD page,
The ELEC/AC BUS/8XP/MONG (49VU H11) C/B may trip.
DURING COCKPIT PREPARATION
COM/HF1 (49VU HA14) C/B .......................................................................................................Pull
Check of the AC ESS BUS SHED:
Supply the electrical network from the APU or the external power.
Check that the CAPT right DU is operative.
IN FLIGHT
If either the ANTI ICE F/O AOA alert or the ANTI ICE F/O PROBES alert is displayed on
the EWD, and icing conditions cannot be avoided:
ADR 2 pb-sw ...................................................................................................................OFF
AIR DATA sw ................................................................................................................F/O 3
Note: If the ADR 2 pb-sw is set to OFF, takeoff in CONF 1+F is not permitted.
If either the ANTI ICE STBY AOA alert or the ANTI ICE STBY PROBES alert is displayed
on the EWD, and icing conditions cannot be avoided:
ADR 3 pb-sw ....................................................................................................................... OFF

LAN COLOMBIA FLEET MO-24-09 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
24 - ELECTRICAL POWER
24-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-24-09 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
24 - ELECTRICAL POWER
24-22 - AC Main Generation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-22-01A AC Main Generation (IDG, GCU, Line Contactor)

Ident.: MO-24-22-00008973.0048001 / 27 FEB 15
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 SINGLE.
APU fuel consumption with APU GEN pb-sw On:
FL GND 200 250 300 335 390
KG/H 100 63 57 54 49 42
LB/H 220 139 126 119 108 93

Note: When the External Power is disconnected, the IFE is lost until the APU supplies the
electrical network.
DURING COCKPIT PREPARATION
Check of the galley automatic load shed system:
Supply the electrical network from the APU or the external power.
GALY & CAB pb-sw ............................................................................................................AUTO
ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24) C/B .......................................................Pull
Check that a part of the operative galley equipment does not operate.
ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24) C/B .....................................................Push
Note: Disregard this procedure if main galleys are not connected.
BEFORE ENGINE START
If the IDG 1(2) associated with the inoperative AC main generation 1(2) has been
disconnected:
Check that the DISC message is displayed on the ELEC SD page.
CAUTION For economical reason, the IDG should not operate for more than 50 flight hours
in the disconnected mode.
Continued on the following page

LAN COLOMBIA FLEET MO-24-22 P 1/2

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
24 - ELECTRICAL POWER
24-22 - AC Main Generation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

AFTER ENGINE START
Check that the electrical busses have power:
APU MASTER SW pb-sw ....................................................................................................... ON
APU GEN pb-sw ...................................................................................................................... On
GEN 1 pb-sw ......................................................................................................................... OFF
GEN 2 pb-sw ......................................................................................................................... OFF
On the ELEC SD page, check that all AC busses have power.
GEN pb-sw (operative)..............................................................................................................On
APU GEN pb-sw ....................................................................................................................OFF
On the ELEC SD page, check that all AC busses have power.
APU GEN pb-sw ...................................................................................................................... On

LAN COLOMBIA FLEET MO-24-22 P 2/2

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
24 - ELECTRICAL POWER
24-25 - AC Essential Generation Switching
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-25-01A Manual Transfer to the AC BUS 2 (ALTN Function)

Ident.: MO-24-25-00008974.0001001 / 11 MAR 10
Applicable to: ALL

DURING PRELIMINARY COCKPIT PREPARATION

On the ELEC SD page, check that the AC BUS 1 supplies the AC ESS BUS.

24-25-02A Automatic Transfer to the AC BUS 2

Ident.: MO-24-25-00008976.0001001 / 01 AUG 13
Applicable to: ALL

DURING PRELIMINARY COCKPIT PREPARATION

On the ELEC SD page, check that the AC BUS 1 supplies the AC ESS BUS.

LAN COLOMBIA FLEET MO-24-25 P 1/2

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
24 - ELECTRICAL POWER
24-25 - AC Essential Generation Switching
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-24-25 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
24 - ELECTRICAL POWER
24-26 - Galley and Commercial Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-26-02B GALY & CAB Manual Load Shed System (GALY & CAB pb-sw)
Ident.: MO-24-26-00008979.0002001 / 27 FEB 15
Applicable to: ALL

ON GROUND OR IN FLIGHT
If the AVNCS SMOKE emergency procedure is applied or if the AVIONICS SMOKE alert
is displayed on the EWD replace the action to set the GALY & CAB pb-sw to OFF by the
following actions:
EMER EXIT LT selector ...................................................................................... As required
COMMERCIAL pb-sw ......................................................................................................OFF
Note: When the COMMERCIAL pb-sw is set to OFF, the normal cabin lighting goes off.
Minimum cabin lighting is recovered when the EMER EXIT LT selector is set to ON.

24-26-03A Commercial Supply System

Ident.: MO-24-26-00008980.0001001 / 27 FEB 15
Applicable to: ALL

ON GROUND OR IN FLIGHT
If the AVNCS SMOKE emergency procedure is applied or if the AVIONICS SMOKE alert
is displayed on the EWD replace the action to set the COMMERCIAL pb-sw to OFF by
the following actions:
BUS TIE pb ..................................................................................................................... OFF
GEN 2 pb-sw ...................................................................................................................OFF
The F/O PFDU, the F/O NDU, and the ECAM lower display are lost.
If the smoke persists:
GEN 2 pb-sw .............................................................................................................. On
When the GEN 2 pb-sw is set to on, all the electrical busses are recovered but the TR 2
remains inoperative
BUS TIE pb ............................................................................................................AUTO
Before the landing gear extension:
GEN 2 pb-sw ..................................................................................................................... On
When the GEN 2 pb-sw is set to on, all the electrical busses are recovered but the TR 2
remains inoperative
BUS TIE pb .................................................................................................................. AUTO

LAN COLOMBIA FLEET MO-24-26 P 1/2

MEL A to B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
24 - ELECTRICAL POWER
24-26 - Galley and Commercial Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-24-26 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
24 - ELECTRICAL POWER
24-32 - DC Main Generation (TR 1, TR 2)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-32-01A DC Main Generation (TR 1 inoperative)

Ident.: MO-24-32-00008981.0001001 / 20 JUN 14
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 SINGLE.
DURING PRELIMINARY COCKPIT PREPARATION
TR 1/CNTOR/SPLY (125VU CF01) C/B ..................................................................................... Pull
On the ELEC SD page, disregard the indications related to the deactivated TR 1.
On the ELEC SD page, check that the TR 2 and the ESS TR voltages are both equal to or above
27 V.
The batteries must be set to OFF for the following check: On the battery voltage indicator, check
that the BAT 1 and the BAT 2 voltages are both equal to or above 25.5 V.

24-32-01B DC Main Generation (TR 2 inoperative)

Ident.: MO-24-32-00009495.0001001 / 10 OCT 14
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 SINGLE.
DURING PRELIMINARY COCKPIT PREPARATION
TR 2/CNTOR/SPLY (124VU BC01) C/B ..................................................................................... Pull
On the ELEC SD page, disregard the indications related to the deactivated TR 2.
On the ELEC SD page, check that the TR 1and the ESS TR voltages are both equal to or above
27 V.
The batteries must be set to OFF for the following check: On the battery voltage indicator, check
that the BAT 1 and the BAT 2 voltages are both equal to or above 25.5 V.
AC ESS FEED pb-sw ...............................................................................................................ALTN
IN FLIGHT
In the case of failure of the AC BUS 2, all DUs are lost. In this case:
AC ESS FEED pb-sw ........................................................................................................ Norm
In the case of failure of the AC BUS 1:
RAT MAN ON pb-sw (on HYD overhead panel).................................................................... Set

LAN COLOMBIA FLEET MO-24-32 P 1/2

MEL A to B 20 JUN 14
 MEL OPERATIONAL PROCEDURES
24 - ELECTRICAL POWER
24-32 - DC Main Generation (TR 1, TR 2)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-24-32 P 2/2

MEL 20 JUN 14
 MEL OPERATIONAL PROCEDURES
24 - ELECTRICAL POWER
24-38 - DC Battery Generation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

24-38-02A Battery Charge Limiter (BCL)

Ident.: MO-24-38-00008982.0001001 / 10 OCT 14
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Do not start the APU.
Use a ground power unit to start the engines on ground.
DURING PRELIMINARY COCKPIT PREPARATION
If BAT 1 is affected:
BAT 1 pb-sw ........................................................................................................................ OFF
If BAT 2 is affected:
BAT 2 pb-sw ........................................................................................................................ OFF

LAN COLOMBIA FLEET MO-24-38 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
24 - ELECTRICAL POWER
24-38 - DC Battery Generation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-24-38 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
25 - EQUIPMENT/FURNISHINGS
25-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-07-01A Passenger Door Slide Permanently Indicated Armed

Ident.: MO-25-07-00009021.0001001 / 10 OCT 14
Applicable to: ALL

ON GROUND
Cabin crew must confirm before each flight that the associated slide is armed.

25-07-02A Passenger Door Slide Permanently Indicated Not Armed

Ident.: MO-25-07-00009022.0001001 / 10 OCT 14
Applicable to: ALL

ON GROUND
Cabin crew must confirm before each flight that the associated slide is armed.

LAN COLOMBIA FLEET MO-25-07 P 1/2

MEL A to B 10 OCT 14
 MEL OPERATIONAL PROCEDURES
25 - EQUIPMENT/FURNISHINGS
25-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-25-07 P 2/2

MEL 10 OCT 14
 MEL OPERATIONAL PROCEDURES
25 - EQUIPMENT/FURNISHINGS
25-11 - Pilot Seats
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-11-07A Pilot Seat Fifth Strap

Ident.: MO-25-11-00008986.0001001 / 11 MAR 10
Applicable to: ALL

DURING FLIGHT
To cope with any potential turbulence situation:
The crewmember of the affected seat must tightly fasten the operative harness straps.

LAN COLOMBIA FLEET MO-25-11 P 1/2

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
25 - EQUIPMENT/FURNISHINGS
25-11 - Pilot Seats
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-25-11 P 2/2

MEL 10 OCT 14
 MEL OPERATIONAL PROCEDURES
25 - EQUIPMENT/FURNISHINGS
25-12 - Third and Fourth Occupant Seats
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-12-04A Third Occupant Seat Fifth Strap

Ident.: MO-25-12-00008987.0001001 / 11 MAR 10
Applicable to: ALL

DURING FLIGHT
To cope with any potential turbulence situation:
The third occupant must tightly fasten the operative harness straps.

25-12-08A Fourth Occupant Seat Fifth Strap

Ident.: MO-25-12-00009015.0002001 / 11 MAR 10
Applicable to: ALL

DURING FLIGHT
To cope with any potential turbulence situation:
The fourth occupant must tightly fasten the operative harness straps.

LAN COLOMBIA FLEET MO-25-12 P 1/2

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
25 - EQUIPMENT/FURNISHINGS
25-12 - Third and Fourth Occupant Seats
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-25-12 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
25 - EQUIPMENT/FURNISHINGS
25-20 - Cabin Seats
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-20-03A
Cabin Attendant Seat
25-20-03B
Ident.: MO-25-20-00009017.0001001 / 02 NOV 11
Applicable to: ALL

PROCEDURE
Cabin attendant seat may be inoperative if Cabin Attendant assigned to affected seat occupies
a passenger seat as close to or closer than nearest seated passenger to associated exit. Cabin
attendant can reach assigned exit and emergency equipment in nearly the same time as from
normally assigned seat. The cabin attendant must be able to reach the assigned emergency exit in
essentially the same time as from the normally assigned seat.

LAN COLOMBIA FLEET MO-25-20 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
25 - EQUIPMENT/FURNISHINGS
25-20 - Cabin Seats
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-25-20 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
25 - EQUIPMENT/FURNISHINGS
25-35 - Galley equipment
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-35-01A Galley Waste Compartment Flapper Door

Ident.: MO-25-35-00009018.0001001 / 02 NOV 11
Applicable to: ALL

PROCEDURE
Ensure that the sufficient galley waste receptacles are available to accommodate all waste,
including affected galley, that may be generated on a flight.

LAN COLOMBIA FLEET MO-25-35 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
25 - EQUIPMENT/FURNISHINGS
25-35 - Galley equipment
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-25-35 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
25 - EQUIPMENT/FURNISHINGS
25-40 - Lavatories
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

25-40-01A
Toilet Waste Compartment Flapper Door
25-40-01B
Ident.: MO-25-40-00009019.0001001 / 19 OCT 11
Applicable to: ALL

PROCEDURE
Inform Flight Attendants that associated lavatories must be checked periodically to verify that the
waste compartment flapper door remain secured closed at intervals not exceeding 30 minutes. If
found that is not secured closed verify that there are not waste inside of the compartment.

LAN COLOMBIA FLEET MO-25-40 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
25 - EQUIPMENT/FURNISHINGS
25-40 - Lavatories
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-25-40 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
25 - EQUIPMENT/FURNISHINGS
25-63 - Evacuation Signaling Equipment
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Emergency Evacuation Signaling System (COMMAND

25-63-01A
pb-sw, HORN SHUT OFF pb, CAPT&PURS and CAPT sw)
Ident.: MO-25-63-00009020.0001001 / 18 MAY 11
Applicable to: ALL

GENERAL INFORMATION
If necessary, the information will be given through the passenger address system or the cabin
interphone system.

LAN COLOMBIA FLEET MO-25-63 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
25 - EQUIPMENT/FURNISHINGS
25-63 - Evacuation Signaling Equipment
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-25-63 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
26 - FIRE PROTECTION
26-12 - Engine Fire and Overheat Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-12-01A
26-12-02A
Engine Fire Detection Loop
26-12-03A
26-12-04A
Ident.: MO-26-12-00015645.0001001 / 27 FEB 15
Applicable to: ALL

COCKPIT PREPARATION
The engine fire test is made before each flight.

LAN COLOMBIA FLEET MO-26-12 P 1/2

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
26 - FIRE PROTECTION
26-12 - Engine Fire and Overheat Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-26-12 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
26 - FIRE PROTECTION
26-13 - APU Fire and Overheat Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-13-01A
APU Fire Detection Loop
26-13-01B
Ident.: MO-26-13-00015646.0001001 / 27 FEB 15
Applicable to: ALL

ON GROUND
The APU fire test is made before each APU start.

LAN COLOMBIA FLEET MO-26-13 P 1/2

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
26 - FIRE PROTECTION
26-13 - APU Fire and Overheat Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-26-13 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
26 - FIRE PROTECTION
26-15 - Avionics Compartment Smoke Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-15-01A Avionics Smoke Detection System

Ident.: MO-26-15-00009025.0001001 / 10 OCT 14
Applicable to: ALL

ON GROUND OR IN FLIGHT
Disregard:
on the VENTILATION overhead panel: the BLOWER pb-sw FAULT light and the EXTRACT
pb-sw FAULT light
on the EMER ELEC PWR overhead panel: the GEN 1 LINE pb-sw SMOKE light
IN FLIGHT
In the case of an electrical smoke:
Apply the AVNCS SMOKE emergency procedure. Refer to QRH/ABN-26-Fire
Protection-A.SMOKE/FUMES/AVNCS SMOKE.

LAN COLOMBIA FLEET MO-26-15 P 1/2

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
26 - FIRE PROTECTION
26-15 - Avionics Compartment Smoke Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-26-15 P 2/2

MEL 10 OCT 14
 MEL OPERATIONAL PROCEDURES
26 - FIRE PROTECTION
26-16 - Cargo Compartment Smoke Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-16-02C
Smoke Detector in the AFT and the BULK Cargo Compartments
26-16-02E
Ident.: MO-26-16-00009027.0004001 / 10 OCT 14
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
For live animal transportation, use the Live Animal Transportation Calculation Tool.
DURING COCKPIT PREPARATION
AFT ISOL VALVE pb-sw ............................................................................................................OFF

LAN COLOMBIA FLEET MO-26-16 P 1/2

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
26 - FIRE PROTECTION
26-16 - Cargo Compartment Smoke Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-26-16 P 2/2

MEL 10 OCT 14
 MEL OPERATIONAL PROCEDURES
26 - FIRE PROTECTION
26-17 - Lavatory Smoke Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

26-17-01A
26-17-01B
Lavatory Smoke Detection System
26-25-01B
26-25-01C
Ident.: MO-26-17-00009028.0001001 / 02 NOV 11
Applicable to: ALL

PROCEDURE
Inform Flight Attendants that associated lavatories must be checked periodically for absence of
smoke at intervals not exceeding 30 minutes.

LAN COLOMBIA FLEET MO-26-17 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
26 - FIRE PROTECTION
26-17 - Lavatory Smoke Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-26-17 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-07-02A Aileron Position Indication on the F/CTL SD page

Ident.: MO-27-07-00009073.0001001 / 17 SEP 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Note: If the Yellow Electric Pump is not available:
Pressurize the Yellow Hydraulic System with:
A Ground cart, or with
The Yellow Engine 2 Pump with the Engine 2 running.
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
Check of the aileron control through the ELACs:
Put the aircraft in the test configuration:
YELLOW ELEC PUMP pb-sw ....................................................................................ON
PTU pb-sw ............................................................................................................. AUTO
BLUE ELEC PUMP pb-sw .....................................................................................AUTO
BLUE PUMP OVRD pb ..............................................................................................ON
ELAC 1 pb-sw .............................................................................................................On
ELAC 2 pb-sw .............................................................................................................On
Check of the aileron control through the ELAC 1:
Move the CAPT stick from right stop to left stop.
Visually check the full travel of the ailerons.
CAUTION If the expected aileron movement does not occur, do not attempt any
reset.
Contact the maintenance.
Check of the aileron control through the ELAC 2:
ELAC 1 pb-sw ...........................................................................................................OFF
Move the CAPT stick from right stop to left stop, then from forward stop to aft stop.
Visually check the full travel of the ailerons.
CAUTION If the expected aileron movement does not occur, do not attempt any
reset.
Contact the maintenance.
Return to normal configuration:
Continued on the following page

LAN COLOMBIA FLEET MO-27-07 P 1/6

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

YELLOW ELEC PUMP pb-sw .................................................................................... Off
BLUE PUMP OVRD pb-sw ......................................................................................... Off
ELAC 1 pb-sw .............................................................................................................On

27-07-04A Elevator Position Indication on the F/CTL SD page

Ident.: MO-27-07-00009074.0001001 / 17 SEP 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Note: If the Yellow Electric Pump is not available:
Pressurize the Yellow Hydraulic System with:
A Ground cart, or with
The Yellow Engine 2 Pump with the Engine 2 running.
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
Check of the elevator control:
YELLOW ELEC PUMP pb-sw .................................................................................................ON
PTU pb-sw .......................................................................................................................... AUTO
BLUE ELEC PUMP pb-sw ..................................................................................................AUTO
BLUE PUMP OVRD pb ........................................................................................................... ON
Establish communication with the ground crew.
Move the CAPT or the F/O stick to the maximum nose down position.
Visually check that both elevators move down.
Move the CAPT or the F/O stick to the maximum nose up position.
Visually check that both elevators move up.
Move the CAPT or the F/O stick to the neutral position.
Visually check that both elevators go back to the neutral position.
YELLOW ELEC PUMP pb-sw ................................................................................................. Off
BLUE PUMP OVRD pb-sw ...................................................................................................... Off

LAN COLOMBIA FLEET MO-27-07 P 2/6

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-07-05A Pitch Trim Position Indication on the F/CTL SD page

Ident.: MO-27-07-00009075.0001001 / 17 SEP 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Note: If the Yellow Electric Pump is not available:
Pressurize the Yellow Hydraulic System with:
A Ground cart, or with
The Yellow Engine 2 Pump with the Engine 2 running.
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
Check of the stabilizer control:
YELLOW ELEC PUMP pb-sw .................................................................................................ON
Establish communication with the ground crew.
Move the pitch trim handwheel to the full DN position.
Visually check that the stabilizer moves to the full down position.
Move the pitch trim handwheel to the full UP position.
Visually check that the stabilizer moves to the full up position.
Move the pitch trim handwheel to the required position.
YELLOW ELEC PUMP pb-sw ................................................................................................. Off

27-07-06A Rudder Position Indication on the F/CTL SD page

Ident.: MO-27-07-00009076.0001001 / 17 SEP 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Note: If the Yellow Electric Pump is not available:
Pressurize the Yellow Hydraulic System with:
A Ground cart, or with
The Yellow Engine 2 Pump with the Engine 2 running.
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
Continued on the following page

LAN COLOMBIA FLEET MO-27-07 P 3/6

MEL C to D 05 NOV 13
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Check of the rudder control:
YELLOW ELEC PUMP pb-sw .................................................................................................ON
Establish communication with the ground crew.
On the CAPT or the F/O side, apply left rudder.
Visually check that the rudder moves to the left.
On the CAPT or the F/O side, apply right rudder.
Visually check that the rudder moves to the right.
On the CAPT or the F/O side, release the pedals.
Visually check that the rudder moves to the neutral position.
YELLOW ELEC PUMP pb-sw ................................................................................................. Off

27-07-11A Spoilers/Speedbrakes Indication on the F/CTL SD page

Ident.: MO-27-07-00009077.0001001 / 17 SEP 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Note: If the Yellow Electric Pump is not available:
Pressurize the Yellow Hydraulic System with:
A Ground cart, or with
The Yellow Engine 2 Pump with the Engine 2 running.
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
If surface 1 indication is inoperative:
CAUTION The aircraft must be stopped during the check.

YELLOW ELEC PUMP pb-sw .......................................................................................... ON

PTU pb-sw ....................................................................................................................AUTO
SPEEDBRAKES lever ................................................................................................... FULL
Visually check that surface 1 slightly extends (approximately 6).
YELLOW ELEC PUMP pb-sw ........................................................................................... Off
If surface 3 indication is inoperative:
BLUE ELEC PUMP pb-sw ........................................................................................... AUTO
BLUE PUMP OVRD pb-sw ...............................................................................................ON
Move the stick from left stop to right stop.
Visually check the correct movement of surface 3.
BLUE PUMP OVRD pb-sw ................................................................................................Off
Continued on the following page

LAN COLOMBIA FLEET MO-27-07 P 4/6

MEL D to E 05 NOV 13
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

If surface 2, 4, or 5 indication is inoperative:
YELLOW ELEC PUMP pb-sw .......................................................................................... ON
PTU pb-sw ....................................................................................................................AUTO
Move the stick from left stop to right stop and visually check the correct movement of
surfaces 2, 4 and 5.
YELLOW ELEC PUMP pb-sw ........................................................................................... Off

27-07-12A Spoilers/Speedbrakes Indication on the WHEEL SD page

Ident.: MO-27-07-00009078.0001001 / 17 SEP 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Note: If the Yellow Electric Pump is not available:
Pressurize the Yellow Hydraulic System with:
A Ground cart, or with
The Yellow Engine 2 Pump with the Engine 2 running.
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
If surface 1 indication is inoperative:
CAUTION The aircraft must be stopped during the check.

YELLOW ELEC PUMP pb-sw .......................................................................................... ON

PTU pb-sw ....................................................................................................................AUTO
SPEEDBRAKES lever ................................................................................................... FULL
Visually check that surface 1 slightly extends (approximately 6).
YELLOW ELEC PUMP pb-sw ........................................................................................... Off
If surface 3 indication is inoperative:
BLUE ELEC PUMP pb-sw ........................................................................................... AUTO
BLUE PUMP OVRD pb-sw ...............................................................................................ON
Move the stick from left stop to right stop.
Visually check the correct movement of surface 3.
BLUE PUMP OVRD pb-sw ................................................................................................Off
Continued on the following page

LAN COLOMBIA FLEET MO-27-07 P 5/6

MEL E to F 05 NOV 13
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-07 - Indications on SD pages
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

If surface 2, 4, or 5 indication is inoperative:
YELLOW ELEC PUMP pb-sw .......................................................................................... ON
PTU pb-sw ....................................................................................................................AUTO
Move the stick from left stop to right stop and visually check the correct movement of
surfaces 2, 4 and 5.
YELLOW ELEC PUMP pb-sw ........................................................................................... Off

LAN COLOMBIA FLEET MO-27-07 P 6/6

MEL F 05 NOV 13
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-14 - Aileron and Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-14-01A Left Aileron Blue Servo-Control (Controlled by ELAC 1)

Ident.: MO-27-14-00009029.0001001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Check that DC TIE contactor 1 is closed:
Supply the electrical network from the APU or the external power.
On the ELEC SD page, check the link between the DC BUS 1 and the DC BAT BUS.

27-14-03A Right Aileron Green Servo-Control (Controlled by ELAC 1)

Ident.: MO-27-14-00009030.0001001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Check that DC TIE contactor 1 is closed:
Supply the electrical network from the APU or the external power.
On the ELEC SD page, check the link between the DC BUS 1 and the DC BAT BUS.

LAN COLOMBIA FLEET MO-27-14 P 1/2

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-14 - Aileron and Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-27-14 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-21 - Rudder Mechanical Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-21-01A Rudder Pedal Adjustment System

Ident.: MO-27-21-00009040.0001001 / 20 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Simultaneously apply loads on both pedals (in rudder control movement direction) to make sure
that the secured position is reached. For that purpose, the effort shall be equivalent to a full rudder
deflection.

LAN COLOMBIA FLEET MO-27-21 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-21 - Rudder Mechanical Control
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-27-21 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-22 - Rudder Trim Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-22-01A
Rudder Trim System
27-22-01B
Ident.: MO-27-22-00009043.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 SINGLE.

LAN COLOMBIA FLEET MO-27-22 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-22 - Rudder Trim Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-27-22 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-51 - Flaps Electrical Control and Monitoring
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-51-01A SFCC Flap Channel

Ident.: MO-27-51-00009044.0001001 / 11 MAR 10
Applicable to: ALL

GENERAL INFORMATION
ENG 2 APPR IDLE ONLY message is displayed on the STATUS SD page.
FLAPS SLOW message is displayed on the STATUS SD page.
DURING COCKPIT PREPARATION
Disregard and clear the F/CTL FLAP SYS 2 FAULT alert displayed on the EWD.

27-51-02A SFCC Slat Channel

Ident.: MO-27-51-00009045.0001001 / 11 MAR 10
Applicable to: ALL

GENERAL INFORMATION
SLATS SLOW message is displayed on the STATUS SD page.
DURING COCKPIT PREPARATION
Disregard and clear the F/CTL SLAT SYS 2 FAULT alert displayed on the EWD.

LAN COLOMBIA FLEET MO-27-51 P 1/2

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-51 - Flaps Electrical Control and Monitoring
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-27-51 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-64 - Spoiler Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-64-01A Spoiler 5
Ident.: MO-27-64-00009046.0001001 / 12 MAR 10
Applicable to: ALL

AFTER ENGINE START

On the HYD SD page, check the absence of amber data.
Note: No performance penalty applies when the pair of spoilers 5 is inoperative.

27-64-02A Spoiler 1 or 3
Ident.: MO-27-64-00009048.0013001 / 10 OCT 14
Applicable to: MSN 4516-5364

FLIGHT PREPARATION/LIMITATIONS
The following penalties may be used for takeoff and landing performance determination if no
takeoff and landing data (predetermined by using OCTOPUS program or other equivalent program
with present failure case) is available.
Takeoff performance computation:
WARNING Do not use this method for takeoff on wet or contaminated runways.

Determine the Maximum Takeoff Weight and associated speeds in normal conditions on dry
runway.
Decrease the Maximum Takeoff Weight by 800 kg (1 770 lb).
Decrease V1 by 1 kt. Keep VR and V2 unchanged.
If the actual TOW is lower than the MTOW calculated using above method:
The speeds determined without failure and associated with the actual TOW may be
retained provided they are all lower than the speeds calculated using above method.
Check that the corrected V1 is equal to or above the minimum V1 value shown on the RTOW
chart (due to VMCG limitation).
If the corrected V1 is lower than the minimum V1:
Take this last value as V1
Further decrease the weight by 3 000 kg (6 600 lb) per kt difference between both values.
Landing performance computation:
Multiply the landing distances by 1.05.
Continued on the following page

LAN COLOMBIA FLEET MO-27-64 P 1/8

MEL A to B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-64 - Spoiler Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

AFTER ENGINE START
On the HYD SD page, check the absence of amber data.
FOR TAKEOFF
If the above method was used for takeoff performance determination:
Perform the takeoff using full thrust (TOGA).

27-64-02A Spoiler 1 or 3
Ident.: MO-27-64-00009048.0045001 / 27 FEB 15
Applicable to: MSN 5443-5453

FLIGHT PREPARATION/LIMITATIONS
Takeoff and landing performance computation:
The takeoff performance must be determined by using OCTOPUS program or other equivalent
program with present failure case taken into account.

Launch PEP.
Landing performance computation
Multiply the landing distances by 1.05.
AFTER ENGINE START
On the HYD SD page, check the absence of amber data.

27-64-03A Spoiler 2 or 4
Ident.: MO-27-64-00009051.0001001 / 12 SEP 11
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
For performance penalties, Refer to OpsProc 27-64-02A Spoiler 1 or 3
AFTER ENGINE START
On the HYD SD page , check the absence of amber data.

LAN COLOMBIA FLEET MO-27-64 P 2/8

MEL B to C 27 FEB 15
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-64 - Spoiler Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-64-04A Spoilers 1 and 2

Ident.: MO-27-64-00009055.0068001 / 18 JUL 14
Applicable to: MSN 4758-5364

FLIGHT PREPARATION/LIMITATIONS
The following penalties may be used for takeoff and landing performance determination if no
takeoff and landing data (predetermined by using OCTOPUS program or other equivalent program
with present failure case) is available.
Takeoff performance computation:
The method explained hereafter allows the determination of the MTOW and associated
speeds (V1, VR, V2), by applying decrements on the MTOW and associated speeds
computed in normal conditions (i.e. all systems operative). The method is based on the use of
RTOW charts established at optimum V2/VS, optimum V1/VR, minimum V1.
WARNING Do not use this method with takeoff charts computed with other conditions.
Do not use this method for takeoff with tailwind.
Do not use this method for takeoff on wet or contaminated runways.
How to proceed ?
Read, in 0 kt wind column of the takeoff chart computed in normal condition, the MTOW
and associated speeds (V1, VR, V2) corresponding to the actual temperature, even in the
case of headwind (the method does not take into account the headwind benefit on takeoff
performance).
Apply the QNH and/or bleed corrections, if any, to determine the MTOW.
Enter the following table to determine the MTOW and speed decrements.
Applying these decrements, calculate the MTOW and associated speeds corresponding to
the actual temperature.
CAUTION Do not extrapolate below the shortest runway length provided by the table.
DECREMENTS (W, V1, VR, V2) WHEN TWO PAIRS OF SPOILERS ARE INOPERATIVE
CONFIGURATION
RUNWAY 1+F 2 3
LENGTH (m) W (kg/lb) V1 VR V2 W (kg/lb) V1 VR V2 W (kg/lb) V1 VR V2
(kt) (kt) (kt) (kt) (kt) (kt) (kt) (kt) (kt)
1 500 1 400/3 000 3 1 1 1 300/2 800 3 1 1 1 300/2 800 2 1 1
2 000 1 900/4 100 2 0 0 1 300/2 800 1 0 0 1 000/2 200 1 0 0
2 500 1 000/2 200 2 1 1 1 200/2 600 2 1 1 1 100/2 400 2 1 1
3 000 1 300/2 800 4 4 4 1 300/2 800 4 3 3 1 000/2 200 4 3 3
Continued on the following page

LAN COLOMBIA FLEET MO-27-64 P 3/8

MEL D 27 FEB 15
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-64 - Spoiler Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

DECREMENTS (W, V1, VR, V2) WHEN TWO PAIRS OF SPOILERS ARE INOPERATIVE
CONFIGURATION
RUNWAY 1+F 2 3
LENGTH (m) W (kg/lb) V1 VR V2 W (kg/lb) V1 VR V2 W (kg/lb) V1 VR V2
(kt) (kt) (kt) (kt) (kt) (kt) (kt) (kt) (kt)
3 500 1 700/3 700 7 6 6 1 000/2 200 4 3 3 900/1 900 5 3 3
4 000 and
900/1 900 4 2 2 900/1 900 4 3 3 800/1 700 5 3 3
above
If the actual TOW is lower than the MTOW calculated using above method:
The speeds determined without failure and associated with the actual TOW may be
retained provided that they are all lower than the speeds calculated using above method.
Check that the corrected V1 is equal to or above the minimum V1 value shown on the RTOW
chart (due to VMCG limitation).
If the corrected V1 is lower than the minimum V1:
Take this last value as V1.
Further decrease the weight by 3 000 kg (6 600 lb) per kt difference between both values.
Check that the corrected VR is equal to or above the minimum VR value shown on the RTOW
chart (due to VMCA limitation).
If the corrected VR is lower than the minimum VR:
Takeoff cannot be performed using this method.
Check that the corrected V2 is equal to or above the minimum V2 value shown on the RTOW
chart (due to VMCA limitation).
If the corrected V2 is lower than the minimum V2:
Takeoff cannot be performed using this method.
Check that the corrected V2 is equal to or above the minimum V2 due to VMU limitation (Refer
to FCOM/ MINIMUM V2 LIMITED BY VMU/VMCA (KT IAS)).
If the corrected V2 is lower than the minimum V2:
Takeoff cannot be performed using this method.
Landing performance computation:
Multiply the landing distances by 1.10.
Continued on the following page

LAN COLOMBIA FLEET MO-27-64 P 4/8

MEL D 27 FEB 15
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-64 - Spoiler Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

DURING COCKPIT PREPARATION
SEC 3 pb-sw ..........................................................................................................................OFF
FLIGHT CONTROLS/SEC3/SPLY (121VU Q19) C/B ............................................................ Pull
TAKEOFF
If the above method was used for takeoff performance computation:
Perform the takeoff using full thrust (TOGA).
IN FLIGHT
In the case of further failure of SEC 1 and SEC 2:
Autoland is not permitted.
Disengage the AP at 500 ft RA before landing in direct law. As soon as the AP is
disengaged when the three SECs are failed, it cannot be engaged again.
Maximum landing capability is CAT 1

27-64-04A Spoilers 1 and 2

Ident.: MO-27-64-00009055.0024001 / 27 NOV 12
Applicable to: MSN 4516-4546

FLIGHT PREPARATION/LIMITATIONS
The following penalties may be used for takeoff and landing performance determination if no
takeoff and landing data (predetermined by using OCTOPUS program or other equivalent program
with present failure case) is available.
Takeoff performance computation:
The method explained hereafter allows the determination of the MTOW and associated
speeds (V1, VR, V2), by applying decrements on the MTOW and associated speeds
computed in normal conditions (i.e. all systems operative). The method is based on the use of
RTOW charts established at optimum V2/VS, optimum V1/VR, minimum V1.
WARNING Do not use this method with takeoff charts computed with other conditions.
Do not use this method for takeoff with tailwind.
Do not use this method for takeoff on wet or contaminated runways.
Continued on the following page

LAN COLOMBIA FLEET MO-27-64 P 5/8

MEL D 27 FEB 15
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-64 - Spoiler Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

How to proceed ?
Read, in 0 kt wind column of the takeoff chart computed in normal condition, the MTOW
and associated speeds (V1, VR, V2) corresponding to the actual temperature, even in the
case of headwind (the method does not take into account the headwind benefit on takeoff
performance).
Apply the QNH and/or bleed corrections, if any, to determine the MTOW.
Enter the following table to determine the MTOW and speed decrements.
Applying these decrements, calculate the MTOW and associated speeds corresponding to
the actual temperature.
CAUTION Do not extrapolate below the shortest runway length provided by the table.
DECREMENTS (W, V1, VR, V2) WHEN TWO PAIRS OF SPOILERS ARE INOPERATIVE
CONFIGURATION
RUNWAY 1+F 2 3
LENGTH (m) W (kg/lb) V1 VR V2 W (kg/lb) V1 VR V2 W (kg/lb) V1 VR V2
(kt) (kt) (kt) (kt) (kt) (kt) (kt) (kt) (kt)
1 500 1 400/3 100 3 1 1 1 600/3 600 3 1 1 1 400/3 100 3 1 1
2 000 1 600/3 600 3 1 1 1 400/3 100 1 0 0 1 200/2 700 1 0 0
2 500 1 600/3 600 3 1 1 1 600/3 600 3 1 1 2 000/4 500 3 1 1
3 000 1 600/3 600 3 1 1 1 800/4 000 3 2 2 1 200/2 700 4 3 3
3 500 1 200/2 700 3 1 1 1 200/2 700 4 3 3 1 400/3 100 6 4 4
4 000 and
1 400/3 100 3 1 1 1 200/2 700 4 3 3 1 000/2 300 5 3 3
above
If the actual TOW is lower than the MTOW calculated using above method:
The speeds determined without failure and associated with the actual TOW may be
retained provided that they are all lower than the speeds calculated using above method.
Check that the corrected V1 is equal to or above the minimum V1 value shown on the RTOW
chart (due to VMCG limitation).
If the corrected V1 is lower than the minimum V1:
Take this last value as V1.
Further decrease the weight by 3 000 kg (6 600 lb) per kt difference between both values.
Check that the corrected VR is equal to or above the minimum VR value shown on the RTOW
chart (due to VMCA limitation).
Continued on the following page

LAN COLOMBIA FLEET MO-27-64 P 6/8

MEL D 27 FEB 15
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-64 - Spoiler Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

If the corrected VR is lower than the minimum VR:
Takeoff cannot be performed using this method.
Check that the corrected V2 is equal to or above the minimum V2 value shown on the RTOW
chart (due to VMCA limitation).
If the corrected V2 is lower than the minimum V2:
Takeoff cannot be performed using this method.
Check that the corrected V2 is equal to or above the minimum V2 due to VMU limitation (Refer
to FCOM/ MINIMUM V2 LIMITED BY VMU/VMCA (KT IAS)).
If the corrected V2 is lower than the minimum V2:
Takeoff cannot be performed using this method.
Landing performance computation:
Multiply the landing distances by 1.10.
DURING COCKPIT PREPARATION
SEC 3 pb-sw ..........................................................................................................................OFF
FLIGHT CONTROLS/SEC3/SPLY (121VU Q19) C/B ............................................................ Pull
TAKEOFF
If the above method was used for takeoff performance computation:
Perform the takeoff using full thrust (TOGA).
IN FLIGHT
In the case of further failure of SEC 1 and SEC 2:
Autoland is not permitted.
Disengage the AP at 500 ft RA before landing in direct law. As soon as the AP is
disengaged when the three SECs are failed, it cannot be engaged again.
Maximum landing capability is CAT 1

27-64-04A Spoilers 1 and 2

Ident.: MO-27-64-00009055.0234001 / 10 OCT 14
Applicable to: MSN 5443-5453

FLIGHT PREPARATION/LIMITATIONS
Takeoff and landing performance computation:
Continued on the following page

LAN COLOMBIA FLEET MO-27-64 P 7/8

MEL D 27 FEB 15
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-64 - Spoiler Hydraulic Actuation
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

The takeoff performance must be determined by using OCTOPUS program or other equivalent
program with present failure case taken into account.

Launch PEP.
Landing performance computation
Multiply the landing distances by 1.10.
DURING COCKPIT PREPARATION
SEC 3 pb-sw ..........................................................................................................................OFF
FLIGHT CONTROLS/SEC3/SPLY (121VU Q19) C/B ............................................................ Pull
IN FLIGHT
In the case of further failure of SEC 1 and SEC 2:
Autoland is not permitted.
Disengage the AP at 500 ft RA before landing in direct law. As soon as the AP is
disengaged when the three SECs are failed, it cannot be engaged again.
Maximum landing capability is CAT 1

27-64-05A Spoiler 3 and 4

Ident.: MO-27-64-00009058.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
For performance penalties Refer to OpsProc 27-64-04A Spoilers 1 and 2
DURING COCKPIT PREPARATION
Check that the DC TIE contactor 1 is closed:
Supply the electrical network from the APU or the external power.
On the ELEC SD page , check the link between the DC BUS 1 and the DC BAT BUS.
IN FLIGHT
Do not use the speedbrakes.

LAN COLOMBIA FLEET MO-27-64 P 8/8

MEL D to E 27 FEB 15
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-92 - Electrical Flight Control System
COLOMBIA
LAN COLOMBIA AIRLINES (EFCS) Control Inputs and Power Supply
MINIMUM EQUIPMENT LIST

27-92-01A Speedbrake Control System (speedbrake control system inoperative)

Ident.: MO-27-92-00009063.0001001 / 11 MAR 10
Applicable to: ALL

Refer to OpsProc 27-92-02A Ground Spoiler Control System (ground spoiler control system
inoperative)

Speedbrake Control System (speedbrake

27-92-01B
2 or speedbrakes 3 and 4 inoperative)
Ident.: MO-27-92-00009064.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
If speedbrake n2 is inoperative:
Apply performance penalties associated with the pair of spoilers 2 inoperative. Refer to
OpsProc 27-64-03A Spoiler 2 or 4
If speedbrakes n3 and n4 are inoperative:
Apply performance penalties associated with two pairs of spoilers inoperative. Refer to
OpsProc 27-64-04A Spoilers 1 and 2
IN FLIGHT
If speedbrakes n3 and n4 are inoperative:
Do not use the speedbrakes.

Ground Spoiler Control System (Ground

27-92-02A
spoiler control system inoperative)
Ident.: MO-27-92-00009065.0016001 / 18 JUL 14
Applicable to: MSN 4758-5364

GENERAL INFORMATION
The autobrake function is not available. Refer to OpsProc 32-42-05A AUTO/BRK Function
CAUTION One or both thrust reversers may not deploy at landing. Consequently, for
performance determination, do not take into account the credit of the thrust
reversers.
Continued on the following page

LAN COLOMBIA FLEET MO-27-92 P 1/8

MEL A to C 10 OCT 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-92 - Electrical Flight Control System
COLOMBIA
LAN COLOMBIA AIRLINES (EFCS) Control Inputs and Power Supply
MINIMUM EQUIPMENT LIST

Continued from the previous page

FLIGHT PREPARATION/LIMITATIONS
The following penalties may be used for takeoff and landing performance determination if no
takeoff and landing data (predetermined by using OCTOPUS program or other equivalent program
with present failure case) is available.
Takeoff performance computation:
The method explained hereafter allows the determination of the MTOW and associated
speeds ( V1 , VR , V2 ), by applying decrements on the MTOW and associated speeds
computed in normal conditions (i.e. all systems operative).
WARNING Do not use this method with takeoff charts computed with other conditions
or by using TLC program.
Do not use this method for takeoff with tailwind.
Do not use this method for takeoff on wet or contaminated runways.
How to proceed ?
Read, in 0 kt wind column of the takeoff chart computed in normal condition, the MTOW and
associated speeds ( V1 , VR , V2 ) corresponding to the actual temperature, even in the
case of headwind (the method does not take into account the headwind benefit on takeoff
performance).
Apply the QNH and/or bleed corrections, if any, to determine the MTOW .
Enter the following table to determine the MTOW and speed decrements.
Applying these decrements, calculate the MTOW and associated speeds corresponding to
the actual temperature.
DECREMENTS (W, V1 , VR , V2 ) WHEN GROUND SPOILER CONTROL SYSTEM IS INOPERATIVE
CONFIGURATION
1+F 2 3
RUNWAY
LENGTH (m) W (kg/lb) V2 W (kg/lb) V2 W (kg/lb) V2
V1 VR (kt) V1 VR (kt) V1 VR (kt)
(kt) (kt) (kt) (kt) (kt) (kt)
2 000 2 400 / 5 200 6 2 2 2 200 / 4 800 4 1 1 2 200 / 4 800 6 2 2
2 500 1 500 / 3 300 3 1 1 1 700 / 3 700 3 1 1 2 000 / 4 400 5 2 2
3 000 2 500 / 5 500 10 9 9 2 200 / 4 800 7 7 7 1 600 / 3 500 8 5 5
3 500 1 700 / 3 700 7 6 6 1 800 / 3 900 7 6 6 1 500 / 3 300 9 5 5
4 000 and
1 400 / 3 000 7 4 4 1 500 / 3 300 8 5 5 1 300 / 2 800 9 5 5
above
Continued on the following page

LAN COLOMBIA FLEET MO-27-92 P 2/8

MEL C 10 OCT 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-92 - Electrical Flight Control System
COLOMBIA
LAN COLOMBIA AIRLINES (EFCS) Control Inputs and Power Supply
MINIMUM EQUIPMENT LIST

Continued from the previous page

If the actual TOW is lower than the MTOW calculated using above method:
The speeds determined without failure and associated with the actual TOW may be
retained provided that they are all lower than the speeds calculated using above method.
Check that the corrected V1 is equal to or above the minimum V1 value shown on the RTOW
chart (due to VMCG limitation).
If the corrected V1 is lower than the minimum V1 :
Take this last value as V1 .
Further decrease the weight by 3 000 kg ( 6 600 lb ) per kt difference between both
values.
Check that the corrected VR is equal to or above the minimum VR value shown on the RTOW
chart (due to VMCA limitation).
If the corrected VR is lower than the minimum VR :
Takeoff cannot be performed using this method.
Check that the corrected V2 is equal to or above the minimum V2 value shown on the RTOW
chart (due to VMCA limitation).
If the corrected V2 is lower than the minimum V2 :
Takeoff cannot be performed using this method.
Check that the corrected V2 is equal to or above the minimum V2 due to VMU limitation (
Refer to FCOM/ MINIMUM V2 LIMITED BY VMU/VMCA (KT IAS) ).
If the corrected V2 is lower than the minimum V2 :
Takeoff cannot be performed using this method.
Landing performance computation:
Multiply the landing distances by 1.35.
TAKEOFF
If the above method was used for takeoff performance computation:
Perform the takeoff using full thrust ( TOGA ).

LAN COLOMBIA FLEET MO-27-92 P 3/8

MEL C 10 OCT 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-92 - Electrical Flight Control System
COLOMBIA
LAN COLOMBIA AIRLINES (EFCS) Control Inputs and Power Supply
MINIMUM EQUIPMENT LIST

Ground Spoiler Control System (Ground

27-92-02A
spoiler control system inoperative)
Ident.: MO-27-92-00009065.0026001 / 27 NOV 12
Applicable to: MSN 4516-4546

GENERAL INFORMATION
The autobrake function is not available. Refer to OpsProc 32-42-05A AUTO/BRK Function
CAUTION One or both thrust reversers may not deploy at landing. Consequently, for
performance determination, do not take into account the credit of the thrust
reversers.
FLIGHT PREPARATION/LIMITATIONS
The following penalties may be used for takeoff and landing performance determination if no
takeoff and landing data (predetermined by using OCTOPUS program or other equivalent program
with present failure case) is available.
Takeoff performance computation:
The method explained hereafter allows the determination of the MTOW and associated
speeds ( V1 , VR , V2 ), by applying decrements on the MTOW and associated speeds
computed in normal conditions (i.e. all systems operative).
WARNING Do not use this method with takeoff charts computed with other conditions
or by using TLC program.
Do not use this method for takeoff with tailwind.
Do not use this method for takeoff on wet or contaminated runways.
How to proceed ?
Read, in 0 kt wind column of the takeoff chart computed in normal condition, the MTOW and
associated speeds ( V1 , VR , V2 ) corresponding to the actual temperature, even in the
case of headwind (the method does not take into account the headwind benefit on takeoff
performance).
Apply the QNH and/or bleed corrections, if any, to determine the MTOW .
Enter the following table to determine the MTOW and speed decrements.
Applying these decrements, calculate the MTOW and associated speeds corresponding to
the actual temperature.
Continued on the following page

LAN COLOMBIA FLEET MO-27-92 P 4/8

MEL C 10 OCT 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-92 - Electrical Flight Control System
COLOMBIA
LAN COLOMBIA AIRLINES (EFCS) Control Inputs and Power Supply
MINIMUM EQUIPMENT LIST

Continued from the previous page

DECREMENTS (W, V1 , VR , V2 ) WHEN GROUND SPOILER CONTROL SYSTEM IS INOPERATIVE
CONFIGURATION
1+F 2 3
RUNWAY
LENGTH (m) W (kg/lb) V2 W V2 W (kg/lb) V2
V1 VR (kt) (kg/lb) V1 VR (kt) V1 VR (kt)
(kt) (kt) (kt) (kt) (kt) (kt)
2 400 /
2 000 2 600 / 5 800 6 2 2 5 300 4 1 1 2 400 / 5 300 6 2 2
1 600 /
2 500 1 600 / 3 600 3 1 1 3 600 3 1 1 2 600 / 5 800 5 2 2
2 600 /
3 000 2 400 / 5 300 5 2 2 5 800 6 2 2 2 000 / 4 500 8 5 5
2 000 /
3 500 2 800 / 6 200 5 3 3 4 500 7 5 5 2 400 / 5 300 8 7 7
4 000 and 2 200 /
3 400 / 7 500 5 3 3 7 6 6 2 200 / 4 900 8 6 6
above 4 900

If the actual TOW is lower than the MTOW calculated using above method:
The speeds determined without failure and associated with the actual TOW may be
retained provided that they are all lower than the speeds calculated using above method.
Check that the corrected V1 is equal to or above the minimum V1 value shown on the RTOW
chart (due to VMCG limitation).
If the corrected V1 is lower than the minimum V1 :
Take this last value as V1 .
Further decrease the weight by 3 000 kg ( 6 600 lb ) per kt difference between both
values.
Check that the corrected VR is equal to or above the minimum VR value shown on the RTOW
chart (due to VMCA limitation).
If the corrected VR is lower than the minimum VR :
Takeoff cannot be performed using this method.
Check that the corrected V2 is equal to or above the minimum V2 value shown on the RTOW
chart (due to VMCA limitation).
If the corrected V2 is lower than the minimum V2 :
Takeoff cannot be performed using this method.
Continued on the following page

LAN COLOMBIA FLEET MO-27-92 P 5/8

MEL C 10 OCT 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-92 - Electrical Flight Control System
COLOMBIA
LAN COLOMBIA AIRLINES (EFCS) Control Inputs and Power Supply
MINIMUM EQUIPMENT LIST

Continued from the previous page

Check that the corrected V2 is equal to or above the minimum V2 due to VMU limitation (
Refer to FCOM/ MINIMUM V2 LIMITED BY VMU/VMCA (KT IAS) ).
If the corrected V2 is lower than the minimum V2 :
Takeoff cannot be performed using this method.
Landing performance computation:
Multiply the landing distances by 1.15.
TAKEOFF
If the above method was used for takeoff performance computation:
Perform the takeoff using full thrust ( TOGA ).

Ground Spoiler Control System (ground

27-92-02A
spoiler control system inoperative)
Ident.: MO-27-92-00009065.0229001 / 10 OCT 14
Applicable to: MSN 5443-5453

GENERAL INFORMATION
The autobrake function is not available. Refer to OpsProc 32-42-05A AUTO/BRK Function
CAUTION One or both thrust reversers may not deploy at landing. Consequently, for
performance determination, do not take into account the credit of the thrust
reversers.
FLIGHT PREPARATION/LIMITATIONS
The takeoff performance must be determined by using OCTOPUS program or other equivalent
program with present failure case taken into account.

Launch PEP.
Landing performance computation
Multiply the landing distances by 1.35.

LAN COLOMBIA FLEET MO-27-92 P 6/8

MEL C to D 10 OCT 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-92 - Electrical Flight Control System
COLOMBIA
LAN COLOMBIA AIRLINES (EFCS) Control Inputs and Power Supply
MINIMUM EQUIPMENT LIST

27-92-02B Ground Spoiler Control System (Pair of spoilers 5 inoperative)

Ident.: MO-27-92-00009066.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
For performance penalties, Refer to OpsProc 27-64-01A Spoiler 5

Ground Spoiler Control System (Pairs of spoilers

27-92-02C
1 and 2 or pairs of spoilers 3 and 4 inoperative)
Ident.: MO-27-92-00009067.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
If the pairs of spoilers 1 and 2 are inoperative:
For performance penalties, Refer to OpsProc 27-64-04A Spoilers 1 and 2
If the pairs of spoilers 3 and 4 are inoperative:
For performance penalties, Refer to OpsProc 27-64-05A Spoilers 3 and 4

LAN COLOMBIA FLEET MO-27-92 P 7/8

MEL E to F 10 OCT 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-92 - Electrical Flight Control System
COLOMBIA
LAN COLOMBIA AIRLINES (EFCS) Control Inputs and Power Supply
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-27-92 P 8/8

MEL 10 OCT 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-93 - ELAC (Elevator Aileron Computer) System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-93-01A ELAC 1
Ident.: MO-27-93-00009068.0002001 / 10 OCT 14
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
If the AP 1 is engaged for landing:
Maximum landing capability is CAT 1.
If the AP 2 is engaged for landing:
Maximum landing capability is CAT 3 SINGLE.
DURING COCKPIT PREPARATION
Note: If the Yellow Electric Pump is not available:
Pressurize the Yellow Hydraulic System with:
A Ground cart, or with
The Yellow Engine 2 Pump with the Engine 2 running.
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
If the F/CTL ELAC 1 FAULT alert is displayed on the EWD:
Note: 1. After application of the maintenance procedure, the following ECAM alerts remain
displayed on the EWD :
C/B TRIPPED R ELEC BAY alert , and
C/B TRIPPED ON OVHD PNL alert, and
F/CTL ELAC 1 FAULT alert.
2. After first engine start, the F/CTL ALTN LAW alert may be spuriously displayed. It
normally disappears after second engine start.
Check of the elevator and the roll spoilers control through the SECs:
Put the aircraft in the test configuration:
Continued on the following page

LAN COLOMBIA FLEET MO-27-93 P 1/6

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-93 - ELAC (Elevator Aileron Computer) System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

YELLOW ELEC PUMP pb-sw ............................................................................. ON
Note: If the Yellow Electric Pump is not available, pressurize the Yellow
Hydraulic System with a Ground Cart or with the Yellow Engine 2 Pump
with the Engine 2 running.
PTU pb-sw .......................................................................................................AUTO
BLUE ELEC PUMP pb-sw .............................................................................. AUTO
BLUE PUMP OVRD pb ....................................................................................... ON
ELAC 2 pb-sw ...................................................................................................... On
SEC 1 pb-sw ........................................................................................................ On
SEC 2 pb-sw ........................................................................................................ On
SEC 3 pb-sw ........................................................................................................ On
Wait 5 s
Check of the elevator control through the SEC 1 and the spoilers control through the SEC
1 and the SEC 3:
BLUE PUMP OVRD pb-sw .................................................................................. Off
Wait for hydraulic circuit depressurization.
On the F/CTL SD page, check that blue elevator actuator symbol becomes amber.
Wait 5 s
BLUE PUMP OVRD pb-sw ..................................................................................ON
ELAC 2 pb-sw .................................................................................................... OFF
SEC 2 pb-sw ...................................................................................................... OFF
Move the CAPT stick from right stop to left stop, then from forward stop to aft stop.
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2, 3,
and 4 and the full travel of both elevators.
Move the F/O stick from right stop to left stop, then from forward stop to aft stop.
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2, 3,
and 4 and the full travel of both elevators.
CAUTION If an expected spoiler or elevator movement does not occur, do not
attempt any reset.
Contact the maintenance.
Check of the elevator control through the SEC 2 and of the spoilers control through the
SEC 2 and the SEC 3:
Continued on the following page

LAN COLOMBIA FLEET MO-27-93 P 2/6

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-93 - ELAC (Elevator Aileron Computer) System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

ELAC 2 pb-sw ...................................................................................................... On
SEC 2 pb-sw ........................................................................................................ On
Wait 5 s
YELLOW ELEC PUMP pb-sw .............................................................................. Off
Wait for hydraulic circuits depressurization.
On the F/CTL SD page, check that the yellow and the green elevator actuators
symbols become amber.
Wait 5 s
YELLOW ELEC PUMP pb-sw ............................................................................. ON
ELAC 2 pb-sw .................................................................................................... OFF
SEC 1 pb-sw ...................................................................................................... OFF
Move the CAPT stick from right stop to left stop, then from forward stop to aft stop.
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2 and
5 and the full travel of both elevators.
Move the F/O stick from right stop to left stop, then from forward stop to aft stop.
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2 and
5 and the full travel of both elevators.
CAUTION If an expected spoiler or elevator movement does not occur, do not
attempt any reset.
Contact the maintenance.
Return to normal configuration:
YELLOW ELEC PUMP pb-sw .............................................................................. Off
BLUE PUMP OVRD pb-sw .................................................................................. Off
ELAC 1 pb-sw .................................................................................................... OFF
ELAC 2 pb-sw ...................................................................................................... On
SEC 1 pb-sw ........................................................................................................ On
Check that the DC TIE contactor 1 is closed:
Supply the electrical network from the APU or the external power.
On the ELEC SD page, check the link between the DC BUS 1 and the DC BAT BUS.
If the F/CTL ELAC 1 PITCH FAULT alert is displayed on the EWD:
Note: After first engine start, the F/CTL ALTN LAW alert may be spuriously displayed on
the EWD. It normally disappears after second engine start.
Check of the elevator and the roll spoilers control through the SECs:
Put the aircraft in the test configuration:
Continued on the following page

LAN COLOMBIA FLEET MO-27-93 P 3/6

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-93 - ELAC (Elevator Aileron Computer) System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

YELLOW ELEC PUMP pb-sw ............................................................................. ON
PTU pb-sw .......................................................................................................AUTO
BLUE ELEC PUMP pb-sw .............................................................................. AUTO
BLUE PUMP OVRD pb ....................................................................................... ON
ELAC 1 pb-sw ...................................................................................................... On
ELAC 2 pb-sw ...................................................................................................... On
SEC 1 pb-sw ........................................................................................................ On
SEC 2 pb-sw ........................................................................................................ On
SEC 3 pb-sw ........................................................................................................ On
Wait 5 s
Check of the elevator control through the SEC 1 and of the spoilers control through the
SEC 1 and the SEC 3:
BLUE PUMP OVRD pb-sw .................................................................................. Off
Wait for hydraulic circuit depressurization.
On the F/CTL SD page, check that blue elevator actuator symbol becomes amber.
Wait 5 s
BLUE PUMP OVRD pb-sw ..................................................................................ON
ELAC 1 pb-sw .................................................................................................... OFF
ELAC 2 pb-sw .................................................................................................... OFF
SEC 2 pb-sw ...................................................................................................... OFF
Move the CAPT stick from right stop to left stop, then from forward stop to aft stop.
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2, 3,
and 4 and the full travel of both elevators.
Move the F/O stick from right stop to left stop, then from forward stop to aft stop.
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2, 3,
and 4 and the full travel of both elevators.
CAUTION If an expected spoiler or elevator movement does not occur, do not
attempt any reset.
Contact the maintenance.
Check of the elevator control through the SEC 2 and of the spoilers control through the
SEC 2 and the SEC 3:
Continued on the following page

LAN COLOMBIA FLEET MO-27-93 P 4/6

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-93 - ELAC (Elevator Aileron Computer) System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

ELAC 1 pb-sw ...................................................................................................... On
ELAC 2 pb-sw ...................................................................................................... On
SEC 2 pb-sw ........................................................................................................ On
Wait 5 s
YELLOW ELEC PUMP pb-sw .............................................................................. Off
Wait for hydraulic circuits depressurization.
On the F/CTL SD page, check that the yellow and the green elevator actuators
symbols become amber.
Wait 5 s
YELLOW ELEC PUMP pb-sw ............................................................................. ON
ELAC 1 pb-sw .................................................................................................... OFF
ELAC 2 pb-sw .................................................................................................... OFF
SEC 1 pb-sw ...................................................................................................... OFF
Move the CAPT stick from right stop to left stop, then from forward stop to aft stop.
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2 and
5 and the full travel of both elevators.
Move the F/O stick from right stop to left stop, then from forward stop to aft stop.
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2 and
5 and the full travel of both elevators.
CAUTION If an expected spoiler or elevator movement does not occur, do not
attempt any reset.
Contact the maintenance.
Return to normal configuration:
YELLOW ELEC PUMP pb-sw .............................................................................. Off
BLUE PUMP OVRD pb-sw .................................................................................. Off
ELAC 1 pb-sw ...................................................................................................... On
ELAC 2 pb-sw ...................................................................................................... On
SEC 1 pb-sw ........................................................................................................ On
Check that the DC TIE contactor 1 is closed:
Supply the electrical network from the APU or the external power.
On the ELEC SD page, check the link between the DC BUS 1 and the DC BAT BUS.
APPROACH
If the AP 1 is used for the approach:
The captain must be the PF.
Continued on the following page

LAN COLOMBIA FLEET MO-27-93 P 5/6

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-93 - ELAC (Elevator Aileron Computer) System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Note: Due to the fact that the ELAC 1 is not electrically supplied, the F/O take-over pb cannot
disengage the AP 1.

LAN COLOMBIA FLEET MO-27-93 P 6/6

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-94 - SEC (Spoiler and Elevator Computer) System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-94-01A SEC 1
Ident.: MO-27-94-00009069.0001001 / 20 JUN 14
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
For performance penalties, Refer to OpsProc 27-64-05A Spoilers 3 and 4
DURING COCKPIT PREPARATION
Note: If the Yellow Electric Pump is not available:
Pressurize the Yellow Hydraulic System with:
A Ground cart, or with
The Yellow Engine 2 Pump with the Engine 2 running.
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
Note: After application of the maintenance procedure, the C/B TRIPPED R ELEC BAY and the
C/B TRIPPED ON OVHD PNL alerts are displayed on the EWD .
Check of the elevator control and roll spoilers control through the operative computers:
Put the aircraft in the test configuration:
YELLOW ELEC PUMP pb-sw ....................................................................................ON
PTU pb-sw ............................................................................................................. AUTO
BLUE ELEC PUMP pb-sw .....................................................................................AUTO
BLUE PUMP OVRD pb ..............................................................................................ON
ELAC 1 pb-sw .............................................................................................................On
ELAC 2 pb-sw .............................................................................................................On
SEC 2 pb-sw ...............................................................................................................On
SEC 3 pb-sw ...............................................................................................................On
Wait 5 s
Check of the elevator control through the ELAC 1:
Continued on the following page

LAN COLOMBIA FLEET MO-27-94 P 1/6

MEL A 20 JUN 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-94 - SEC (Spoiler and Elevator Computer) System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

BLUE PUMP OVRD pb-sw ......................................................................................... Off
Wait for hydraulic circuit depressurization.
On the F/CTL SD page , check that blue elevator actuator symbol becomes amber.
Wait 5 s
BLUE PUMP OVRD pb-sw ........................................................................................ ON
ELAC 2 pb-sw ...........................................................................................................OFF
SEC 2 pb-sw ............................................................................................................ OFF
Move the CAPT stick from forward stop to aft stop.
On the F/CTL SD page , check the full travel of both elevators.
CAUTION If an expected elevator movement does not occur, do not attempt any
reset.
Contact the maintenance.
Check of the elevator control through the SEC 2:
ELAC 2 pb-sw .............................................................................................................On
SEC 2 pb-sw ...............................................................................................................On
Wait 5 s
YELLOW ELEC PUMP pb-sw .................................................................................... Off
Wait for hydraulic circuits depressurization.
On the F/CTL SD page , check that the yellow and the green elevator actuators
symbols become amber.
Wait 5 s
YELLOW ELEC PUMP pb-sw ....................................................................................ON
ELAC 1 pb-sw ...........................................................................................................OFF
ELAC 2 pb-sw ...........................................................................................................OFF
Move the CAPT stick from right stop to left stop, then from forward stop to aft stop.
Each stop must be applied during 3 s
On the F/CTL SD page , check the correct movement of the pairs of spoilers 2 and 5
and the full travel of both elevators.
Move the F/O stick from right stop to left stop, then from forward stop to aft stop.
Each stop must be applied during 3 s
On the F/CTL SD page , check the correct movement of the pairs of spoilers 2 and 5
and the full travel of both elevators.
CAUTION If an expected spoiler or elevator movement does not occur, do not
attempt any reset.
Contact the maintenance.
Continued on the following page

LAN COLOMBIA FLEET MO-27-94 P 2/6

MEL A 20 JUN 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-94 - SEC (Spoiler and Elevator Computer) System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Return to normal configuration:
YELLOW ELEC PUMP pb-sw .................................................................................... Off
BLUE PUMP OVRD pb-sw ......................................................................................... Off
ELAC 1 pb-sw .............................................................................................................On
ELAC 2 pb-sw .............................................................................................................On
Check that the DC TIE contactor 1 is closed:
Supply the electrical network from the APU or the external power.
On the ELEC SD page , check the link between the DC BUS 1 and the DC BAT BUS.
IN FLIGHT
Do not use the speedbrakes.
If the SEC 2 and the SEC 3 fail during the flight:
Autoland is not permitted.
Maximum landing capability is CAT 1
Disengage the AP at 500 ft RA before landing in direct law.
When the AP is disengaged with the three SEC s failed, it cannot be engaged again.

27-94-02A SEC 2
Ident.: MO-27-94-00009070.0001001 / 20 JUN 14
Applicable to: ALL

DURING COCKPIT PREPARATION

Note: If the Yellow Electric Pump is not available:
Pressurize the Yellow Hydraulic System with:
A Ground cart, or with
The Yellow Engine 2 Pump with the Engine 2 running.
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
Note: After application of the maintenance procedure, the C/B TRIPPED REAR PNL N-R alert
is displayed on the EWD.
Check of the elevator control and roll spoilers control through the operative computers:
Put the aircraft in the test configuration:
Continued on the following page

LAN COLOMBIA FLEET MO-27-94 P 3/6

MEL A to B 20 JUN 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-94 - SEC (Spoiler and Elevator Computer) System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

YELLOW ELEC PUMP pb-sw ....................................................................................ON
PTU pb-sw ............................................................................................................. AUTO
BLUE ELEC PUMP pb-sw .....................................................................................AUTO
BLUE PUMP OVRD pb ..............................................................................................ON
ELAC 1 pb-sw .............................................................................................................On
ELAC 2 pb-sw .............................................................................................................On
SEC 1 pb-sw ...............................................................................................................On
SEC 3 pb-sw ...............................................................................................................On
Wait 5 s
Check of the elevator control through the ELAC 1:
BLUE PUMP OVRD pb-sw ......................................................................................... Off
Wait for hydraulic circuit depressurization.
On the F/CTL SD page, check that blue elevator actuator symbol becomes amber.
Wait 5 s
BLUE PUMP OVRD pb-sw ........................................................................................ ON
ELAC 2 pb-sw ...........................................................................................................OFF
SEC 1 pb-sw ............................................................................................................ OFF
Move the CAPT stick from forward stop to aft stop.
On the F/CTL SD page, check the full travel of both elevators.
CAUTION If an expected elevator movement does not occur, do not attempt any
reset.
Contact the maintenance.
Check of the elevator control through the SEC 1:
Continued on the following page

LAN COLOMBIA FLEET MO-27-94 P 4/6

MEL B 20 JUN 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-94 - SEC (Spoiler and Elevator Computer) System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

ELAC 2 pb-sw .............................................................................................................On
SEC 1 pb-sw ...............................................................................................................On
Wait 5 s
BLUE PUMP OVRD pb-sw ......................................................................................... Off
Wait for hydraulic circuits depressurization.
On the F/CTL SD page, check that the blue elevator actuator symbols becomes amber.
Wait 5 s
BLUE PUMP OVRD pb-sw ........................................................................................ ON
ELAC 1 pb-sw ...........................................................................................................OFF
ELAC 2 pb-sw ...........................................................................................................OFF
Move the CAPT stick from right stop to left stop, then from forward stop to aft stop.
Each stop must be applied during 3 s
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2, 3, and 4
and the full travel of both elevators.
Move the F/O stick from right stop to left stop, then from forward stop to aft stop.
Each stop must be applied during 3 s
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2, 3, and 4
and the full travel of both elevators.
CAUTION If an expected spoiler or elevator movement does not occur, do not
attempt any reset.
Contact the maintenance.
Return to normal configuration:
YELLOW ELEC PUMP pb-sw .................................................................................... Off
BLUE PUMP OVRD pb-sw ......................................................................................... Off
ELAC 1 pb-sw .............................................................................................................On
ELAC 2 pb-sw .............................................................................................................On
AFTER ENGINE START
Note: The F/CTL ELEV SERVO FAULT alert may be displayed on the EWD if the PTU is
inhibited and only one engine is operating. This alert must disappear when the PTU or
the second engine is started.
IN FLIGHT
If the SEC 1 and the SEC 3 fail during the flight:
Autoland is not permitted.
Maximum landing capability is CAT 1
Continued on the following page

LAN COLOMBIA FLEET MO-27-94 P 5/6

MEL B 20 JUN 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-94 - SEC (Spoiler and Elevator Computer) System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Disengage the AP at 500 ft RA before landing in direct law.
When the AP is disengaged with the three SECs failed, it cannot be engaged again.

27-94-03A SEC 3
Ident.: MO-27-94-00009071.0001001 / 17 SEP 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
For performance penalties, Refer to OpsProc 27-64-04A Spoilers 1 and 2
DURING COCKPIT PREPARATION
Deactivation of the SEC 3:
SEC 3 pb-sw ..........................................................................................................................OFF
FLIGHT CONTROLS/SEC 3/SPLY (121VU Q19) C/B ........................................................... Pull
IN FLIGHT
If the SEC 1 and the SEC 2 fail during the flight:
Autoland is not permitted.
Maximum landing capability is CAT 1
Disengage the AP at 500 ft RA before landing in direct law.
When the AP is disengaged with the three SEC s failed, it cannot be engaged again.

LAN COLOMBIA FLEET MO-27-94 P 6/6

MEL B to C 20 JUN 14
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-95 - FCDC (Flight Control Data Concentrator) System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

27-95-02A FCDC 2
Ident.: MO-27-95-00009072.0001001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

FLIGHT CONTROLS/FCDC2/SPLY (121VU Q20) C/B .............................................................. Pull

LAN COLOMBIA FLEET MO-27-95 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
27 - FLIGHT CONTROLS
27-95 - FCDC (Flight Control Data Concentrator) System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-27-95 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 28-01-01 - FUEL Overhead Panel
MINIMUM EQUIPMENT LIST

28-01-01-07A FUEL MODE SEL pb-sw FAULT light

Ident.: MO-28-01-01-00009079.0003001 / 10 OCT 14
Applicable to: ALL

AFTER ENGINE START

If there is fuel in the center tank and with the slats retracted:
On the FUEL SD page, check that the center tank pumps indications are in line.
With the slats extended:
On the FUEL SD page, check that the center tank pumps indications are cross line.
AFTER TAKEOFF
If there is fuel in the center tank and with the slats retracted:
On the FUEL SD page, check that the center tank pumps indications are in line.

LAN COLOMBIA FLEET MO-28-01-01 P 1/2

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 28-01-01 - FUEL Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-28-01-01 P 2/2

MEL 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-01 - Fuel Quantity Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

28-07-01-01A Fuel On Board (FOB) Indication on the FUEL SD page

Ident.: MO-28-07-01-00009109.0001001 / 28 JUN 11
Applicable to: ALL

AFTER ENGINE START

Check that /FF is selected on the MCDU FUEL PRED page.
If /FF is not selected on the MCDU FUEL PRED page:
Insert the FOB.
The FOB may be calculated either using the indications on the refuel control
panel (if available) or by using the Manual Magnetic Indicators (MMIs):Refer to
FCOM/PER-LOD-FUL-FUEL-C.USE OF MANUAL MAGNETIC INDICATORS (MMI).

28-07-01-02A Fuel Quantity Indication in Degraded Mode on the FUEL SD page

Ident.: MO-28-07-01-00009110.0001001 / 10 OCT 14
Applicable to: ALL

ON GROUND
The FQI is in degraded mode when the FOB indication is displayed with two dashes across the
two last digits on the EWD.
When the FQI is in degraded mode:
On the FUEL SD page, determine which tank is affected.
The resulting loss of accuracy must be taken into account by using the two following
parameters:
1. Fq : The extra fuel quantity to be loaded.
2. W: The weight to be added to the total fuel weight for TOW calculation only.
Fq and W parameters are given as follows :
LOSS OF ACCURACY DUE TO THE FUEL QUANTITY INDICATION IN DEGRADED MODE
(Values in kg)
Fq (kg) W (kg)
OUTER TANK 20 200
INNER TANK 110 110
CENTER TANK 130 130
ALL TANKS 390 750
Continued on the following page

LAN COLOMBIA FLEET MO-28-07-01 P 1/4

MEL A to B 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-01 - Fuel Quantity Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

Continued from the previous page

LOSS OF ACCURACY DUE TO THE FUEL QUANTITY INDICATION IN DEGRADED MODE
(Values in lb - If applicable)
Fq (lb) W (lb)
OUTER TANK 45 450
INNER TANK 240 240
CENTER TANK 290 290
ALL TANKS 860 1 670

When the auto refuel stops:

Preselect the fuel quantity required for the mission : Fm
Enter the table and determine Fq and W values for the affected tank.
Start again the auto refuel with the new preselected quantity which corresponds to the
total FOB : Fm+Fq
Note: If all tanks reach high level before having loaded the complete Fq value, this
shows that all tanks are volumetrically full but the necessary fuel mass for the
mission is not guaranteed since the fuel quantity indication varies with the fuel
density. Therefore the mission or the aircraft load must be amended to match
the minimum fuel quantity known to be onboard.

When the auto refuel stops again:

The FOB value to be considered for TOW calculation is: FOB = Fm+Fq+W
If all tanks reach high level before having loaded Fq value:
The extra fuel quantity known to be onboard is Fq* with: Fq* < Fq
The FOB value to be considered for TOW calculation is: FOB = Fm+Fq *+W
If the resulting TOW is higher than the MTOW:
The aircraft load must be reduced.

28-07-01-03A
Outer Tank Fuel Quantity Indication on the FUEL SD page
28-07-01-03C
Ident.: MO-28-07-01-00009111.0001001 / 10 OCT 14
Applicable to: ALL

AFTER REFUELING
To check the fuel quantity in the associated tank: Refer to
FCOM/PER-LOD-FUL-FUEL-A.GENERAL INFORMATION - USABLE FUEL VOLUME..

LAN COLOMBIA FLEET MO-28-07-01 P 2/4

MEL B to C 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-01 - Fuel Quantity Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

28-07-01-04A Inner Tank Fuel Quantity Indication on the FUEL SD page

Ident.: MO-28-07-01-00009112.0001001 / 10 OCT 14
Applicable to: ALL

AFTER ENGINE START

Check that /FF is selected on the MCDU FUEL PRED page.
If /FF is not selected on the MCDU FUEL PRED page:
Insert the FOB.
The FOB may be calculated either using the indications on the refuel control
panel (if available) or by using the Manual Magnetic Indicators (MMIs): Refer to
FCOM/PER-LOD-FUL-FUEL-C.USE OF MANUAL MAGNETIC INDICATORS (MMI).

28-07-01-05A Center Tank Fuel Quantity Indication on the FUEL SD page

Ident.: MO-28-07-01-00009113.0002001 / 20 JUN 14
Applicable to: ALL

AFTER REFUELING
To check the fuel quantity in the associated tank: Refer to
FCOM/PER-LOD-FUL-FUEL-A.GENERAL INFORMATION - USABLE FUEL VOLUME..

LAN COLOMBIA FLEET MO-28-07-01 P 3/4

MEL D to E 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-01 - Fuel Quantity Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-28-07-01 P 4/4

MEL 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-04 - Valve Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

28-07-04-04A Wing Transfer Valve Indication on the FUEL SD page

Ident.: MO-28-07-04-00009115.0001001 / 10 OCT 14
Applicable to: ALL

IN FLIGHT
When any inner tank fuel quantity reaches 750 kg (1 650 lb) of fuel:
On the FUEL SD page, check the associated outer tank transfer.

LAN COLOMBIA FLEET MO-28-07-04 P 1/2

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-07 - Indications on the FUEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES 28-07-04 - Valve Indications on the FUEL SD page
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-28-07-04 P 2/2

MEL 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-09-01A
FUEL L(R) INNER(OUTER) TK HI TEMP Alert
28-09-01B
Ident.: MO-28-09-00009116.0001001 / 10 OCT 14
Applicable to: ALL

ON GROUND OR IN FLIGHT
On the FUEL SD page, monitor the fuel temperature before takeoff and periodically during the
flight.
Note: For fuel temperature limits, Refer to AFM/LIM-28 Fuel Temperature Limits.
If fuel temperature reaches limits:
Before takeoff:
Delay takeoff and shut down the engine on the affected side.
In flight:
Increase the engine fuel flow on the affected side.
If necessary use the APU GEN and switch off the IDG on the affected side (if the
opposite GEN is available).

28-09-02A
FUEL L(R) INNER(OUTER) TK LO TEMP Alert
28-09-02B
Ident.: MO-28-09-00009117.0001001 / 10 OCT 14
Applicable to: ALL

ON GROUND OR IN FLIGHT
On the FUEL SD page, monitor the fuel temperature before takeoff and periodically during the
flight.
Note: For fuel temperature limits, Refer to AFM/LIM-28 Fuel Temperature Limits.
If fuel temperature reaches limits:
Before takeoff:
Delay takeoff.
In flight:
Consider descending to a lower altitude and/or increasing the mach to increase the TAT.

LAN COLOMBIA FLEET MO-28-09 P 1/2

MEL A to B 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-28-09 P 2/2

MEL 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-12 - Tank Venting System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Overpressure Protector Between the Inner and the

28-12-01A
Outer Tank (Inner tank fuel temperature monitored)
Ident.: MO-28-12-00009085.0001001 / 10 OCT 14
Applicable to: ALL

GENERAL INFORMATION
The dispatch condition results in an unusual distribution of the fuel quantity: the outer tank of the
affected wing will be partially empty with the transfer valves normally closed.
FLIGHT PREPARATION/LIMITATIONS
Fuel management should be performed with care.
ON GROUND AND IN FLIGHT
After a long taxi or if the outside air temperature is high, with the outer tank of the
affected wing empty:
The FUEL L(R) OUTER TK HI TEMP alert may be displayed on the EWD .
If the FUEL L(R) OUTER TK HI TEMP alert is displayed on the EWD :
Disregard the FUEL L(R) OUTER TK HI TEMP alert.
Monitor the inner tank fuel temperature during taxi and in flight to ensure that it
decreases and remains within the temperature limitations.
Note: For fuel temperature limitations, Refer to AFM/LIM-28 Fuel Temperature
Limits .
If the inner tank fuel temperature exceeds the temperature limitations, apply the FUEL
L(R) INNER TK HI TEMP procedure: Refer to OpsProc 28-09-01A(B) FUEL L(R)
INNER(OUTER)/WING TK HI TEMP Alert .

Overpressure Protector Between the Inner

28-12-01B
and the Outer Tank (Transfer valves opened)
Ident.: MO-28-12-00009086.0001001 / 10 OCT 14
Applicable to: ALL

GENERAL INFORMATION
The dispatch condition results in an unusual distribution of the fuel quantity: the fuel in both outer
tanks will transfer to the inner tanks even when the inner tanks are not empty.
ON GROUND
Check that the associated wing transfer valves are indicated open on the FUEL SD page.

LAN COLOMBIA FLEET MO-28-12 P 1/2

MEL A to B 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-12 - Tank Venting System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-12-02A Overpressure Protector in the Vent Surge Tank

Ident.: MO-28-12-00009087.0001001 / 11 MAR 10
Applicable to: ALL

ON GROUND AND IN FLIGHT

Avoid lateral accelerations in order to reduce the possibility of fuel spill during taxi and climb
out.
In cruise check that no fuel spillage occurred.
Check that the FOB is sufficient to reach the destination with the adequate reserve.

LAN COLOMBIA FLEET MO-28-12 P 2/2

MEL C 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-15 - Intercell Transfer System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-15-01A
LH Wing Transfer Valve (At least one transfer valve open)
28-15-01C
Ident.: MO-28-15-00009088.0001001 / 10 OCT 14
Applicable to: ALL

GENERAL INFORMATION
If one or both wing transfer valves are inoperative in the open position:
The dispatch condition results in an unusual distribution of the fuel quantity: the fuel in the
outer tank on the affected side will transfer to the inner tank even when the inner tank is not
empty.
If one wing transfer valve is secured in the open position:
The dispatch condition results in an unusual distribution of the fuel quantity: the fuel in both
outer tanks will transfer to the inner tanks even when the inner tanks are not empty.
ON GROUND
If one wing transfer valve is secured in the open position:
Check that the wing transfer valve is indicated open on the FUEL SD page.

28-15-01B LH Wing Transfer Valve (At least one transfer valve failed closed)
Ident.: MO-28-15-00009089.0001001 / 10 OCT 14
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
The fuel in the affected outer tank should be considered as not usable for the flight planning.

28-15-02A
RH Wing Transfer Valve (At least one transfer valve open)
28-15-02C
Ident.: MO-28-15-00009090.0001001 / 10 OCT 14
Applicable to: ALL

GENERAL INFORMATION
If one or both wing transfer valves are inoperative in the open position:
The dispatch condition results in an unusual distribution of the fuel quantity: the fuel in the
outer tank on the affected side will transfer to the inner tank even when the inner tank is not
empty.
Continued on the following page

LAN COLOMBIA FLEET MO-28-15 P 1/2

MEL A to C 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-15 - Intercell Transfer System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

If one wing transfer valve is secured in the open position:
The dispatch condition results in an unusual distribution of the fuel quantity: the fuel in both
outer tanks will transfer to the inner tanks even when the inner tanks are not empty.
ON GROUND
If one wing transfer valve is secured in the open position:
Check that the wing transfer valve is indicated open on the FUEL SD page.

28-15-02B RH Wing Transfer Valve (At least one transfer valve failed closed)
Ident.: MO-28-15-00009091.0001001 / 10 OCT 14
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
The fuel in the affected outer tank should be considered as not usable for the flight planning.

LAN COLOMBIA FLEET MO-28-15 P 2/2

MEL C to D 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-20 - Distribution
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-20-01A Automatic Fuel Feed System

Ident.: MO-28-20-00009092.0003001 / 10 OCT 14
Applicable to: MSN 4516-4546

ON GROUND
If the center tank is empty for the flight:
MODE SEL pb-sw .......................................................................................................... MAN
CTR TK PUMP 1 and 2 pb-sw ....................................................................................... OFF
If the center tank is not empty for the flight:
Before engine start:
MODE SEL pb-sw ........................................................................................................ MAN
3 min after engine start:
CTR TK PUMP 1 and 2 pb-sw ..................................................................................... OFF
IN FLIGHT
If the center tank is not empty for the flight:
After slat retraction and when the fuel in one wing is less than 5 000 kg (11 000 lb) :
CTR TK PUMP 1 and 2 pb-sw ........................................................................................On
When the FUEL CTR TK PUMPS LO PR alert is displayed on the EWD:
CTR TK PUMP 1 and 2 pb-sw ..................................................................................... OFF

28-20-01A Automatic Fuel Feed System

Ident.: MO-28-20-00009092.0004001 / 10 OCT 14
Applicable to: MSN 4758-5453

ON GROUND
If the center tank is empty for the flight:
MODE SEL pb-sw ...............................................................................................................MAN
CTR TK PUMP 1 and 2 pb-sw ............................................................................................OFF
If the center tank is not empty for the flight:
Before engine start:
MODE SEL pb-sw ........................................................................................................ MAN
3 min after engine start:
CTR TK PUMP 1 and 2 pb-sw ..................................................................................... OFF
Continued on the following page

LAN COLOMBIA FLEET MO-28-20 P 1/2

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-20 - Distribution
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

IN FLIGHT
If the center tank is not empty for the flight:
After slat retraction and when the fuel in one wing is less than 5 000 kg (11 000 lb):
CTR TK PUMP 1 and 2 pb-sw ....................................................................................... ON
If the FUEL CTR TK PUMPS LO PR alert is displayed on the EWD, or if the center
tank is not empty at slat extension:
CTR TK PUMP 1 and 2 pb-sw ..................................................................................... OFF

LAN COLOMBIA FLEET MO-28-20 P 2/2

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-21 - Main Fuel Pump System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-21-02A Center Tank Pump (One inoperative)

Ident.: MO-28-21-00009096.0003001 / 10 OCT 14
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
In the case of dispatch with fuel in the center tank, the remaining center tank pump failure must be
considered for the flight planning. Operator has to ensure that, from any point of the first part of the
route where the center tank is not empty the aircraft may reach a suitable airport considering the
fuel quantity (FQ) contained in the center tank as definitely not usable for the flight planning (as a
consequence of the failure of the remaining center tank pump).
DURING COCKPIT PREPARATION
X FEED pb-sw ............................................................................................................CHECK Off
Affected CTR TK PUMP pb-sw ............................................................................................. OFF
Operative CTR TK PUMP pb-sw ...........................................................................................OFF
IN FLIGHT
If the fuel quantity in the center tank is less than 200 kg (440 lb):
Operative CTR TK PUMP pb-sw .......................................................................... Maintain OFF
If the fuel quantity in the center tank is more than 200 kg (440 lb):
The fuel in the center tank can be completely used if the operative center tank pump does not
fail before the center tank is empty. If the operative center tank pump fails before the center
tank is empty, consider the fuel quantity remaining and the time to destination to decide either
to continue the flight or to divert.
When the fuel quantity in one wing inner tank is less than 4 500 kg (10 000 lb):
Operative CTR TK PUMP pb-sw .....................................................................................On
X FEED pb-sw ................................................................................................................ ON
When the fuel quantity in one wing inner tank increases above 5 500 kg (12 000 lb):
X FEED pb-sw .................................................................................................................Off
Operative CTR TK PUMP pb-sw .................................................................................. OFF
Note: Repeat the previous two steps as many times as necessary until the center tank is
empty.The operative center tank pump will switch off automatically
When the fuel quantity in the center tank is less than 250 kg (550 lb):
X FEED pb-sw .................................................................................................................Off

LAN COLOMBIA FLEET MO-28-21 P 1/2

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-21 - Main Fuel Pump System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-21-02D Center Tank Pump (Both inoperative)

Ident.: MO-28-21-00009095.0003001 / 10 OCT 14
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
CTR TK PUMP 1 and 2 pb-sw .................................................................................................. OFF

LAN COLOMBIA FLEET MO-28-21 P 2/2

MEL B 10 OCT 14
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-22 - APU Fuel Pump System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-22-01A
APU Fuel Pump
28-22-01B
Ident.: MO-28-22-00009097.0001001 / 11 MAR 10
Applicable to: ALL

FOR APU START OPERATION

Pressurize the LH fuel manifold with at least one fuel tank pump.

LAN COLOMBIA FLEET MO-28-22 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-22 - APU Fuel Pump System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-28-22 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-29 - APU LP Fuel Shutoff
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-29-01A APU LP Fuel Valve

Ident.: MO-28-29-00009107.0001001 / 12 SEP 11
Applicable to: ALL

BEFORE ENGINE START

The APU is not available.
APU MASTER SW pb-sw .............................................................................................................Off
Note: 1. No APU bleed air will be available for the Main Engine Start (MES) or the air
conditioning.
2. No electrical power will be available from the APU generator.
On the FUEL SD page, check that the APU LP valve is indicated closed: Refer to FCOM/ ECAM
Fuel Page.

LAN COLOMBIA FLEET MO-28-29 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-29 - APU LP Fuel Shutoff
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-28-29 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-50 - Fuel Management
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

28-50-01A Fuel Quantity Indicating Computer (FQIC) Channel

Ident.: MO-28-50-00009108.0003001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
1. Ensure that correct weights are entered in the FMGC associated with the affected FQIC
channel.
2. In the case of failure in-flight of the remaining FQIC channel, all fuel quantities indications on the
EWD are lost.

LAN COLOMBIA FLEET MO-28-50 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
28 - FUEL
28-50 - Fuel Management
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-28-50 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
29 - HYDRAULIC POWER
29-07 - Indications on the HYD SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-07-07A System Label Indication on the HYD SD page

Ident.: MO-29-07-00009122.0001001 / 17 SEP 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Note: If the Yellow Electric Pump is not available:
Pressurize the Yellow Hydraulic System with:
A Ground cart, or with
The Yellow Engine 2 Pump with the Engine 2 running.
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
YELLOW ELEC PUMP pb-sw .................................................................................................ON
BLUE ELEC PUMP pb-sw ..................................................................................................AUTO
BLUE PUMP OVRD pb-sw ..................................................................................................... ON
PTU pb-sw .......................................................................................................................... AUTO
Move the CAPT stick left or right.
On the F/CTL SD page, check the pairs of spoilers movement.
YELLOW ELEC PUMP pb-sw ................................................................................................. Off
BLUE PUMP OVRD pb-sw ....................................................................................................OFF

29-07-08A System Pressure Indication on the HYD SD page

Ident.: MO-29-07-00009123.0001001 / 17 SEP 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Note: If the Yellow Electric Pump is not available:
Pressurize the Yellow Hydraulic System with:
A Ground cart, or with
The Yellow Engine 2 Pump with the Engine 2 running.
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
Continued on the following page

LAN COLOMBIA FLEET MO-29-07 P 1/2

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
29 - HYDRAULIC POWER
29-07 - Indications on the HYD SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

If the blue system pressure indication is inoperative:
Check of the system label:
On the HYD SD page, check that the BLUE system label is amber.
BLUE ELEC PUMP pb-sw ........................................................................................... AUTO
BLUE PUMP OVRD pb-sw ...............................................................................................ON
On the HYD SD page, check that the BLUE system label is white and that the arrow is
green.
BLUE PUMP OVRD pb-sw ................................................................................................Off
If the yellow system pressure indication is inoperative:
Check of the system label:
YELLOW ELEC PUMP pb-sw ........................................................................................... Off
On the HYD SD page, check that the YELLOW system label is amber.
YELLOW ELEC PUMP pb-sw .......................................................................................... ON
On the HYD SD page, check that the YELLOW system label is white and that the arrow is
green.
YELLOW ELEC PUMP pb-sw ........................................................................................... Off
If the green system pressure indication is inoperative:
Check of the system label:
On the HYD SD page, check that the GREEN system label is amber.
YELLOW ELEC PUMP pb-sw .......................................................................................... ON
PTU pb-sw ....................................................................................................................AUTO
On the HYD SD page, check that the GREEN system label is white and that the arrow is
green.
YELLOW ELEC PUMP pb-sw ........................................................................................... Off

LAN COLOMBIA FLEET MO-29-07 P 2/2

MEL B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
29 - HYDRAULIC POWER
29-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-09-03A HYD G(Y) ENG 1(2) PUMP LO PR Alert

Ident.: MO-29-09-00009124.0002001 / 27 FEB 15
Applicable to: ALL

AFTER ENGINE START

Check of the engines pumps:
PTU pb-sw ............................................................................................................................. OFF
On the HYD SD page, check that the green and the yellow hydraulic systems pressures are
correct.
A correct pressure is 3 000 PSI ( 200 PSI).
PTU pb-sw .......................................................................................................................... AUTO
Note: On the HYD SD page, the PTU remains indicated running .

TAXI
Note: Due to a false HYD G(Y) ENG 1(2) PUMP LO PR alert displayed on the EWD, the "T.O
CONFIG NORMAL line will not replace the "T.O CONFIG . . TEST" line in the T.O
MEMO.
Consider normal configuration for takeoff provided that no alert was displayed during the
T.O CONFIG TEST except a false HYD G(Y) ENG 1(2) PUMP LO PR alert.
CAUTION The T.O CONFIG TEST pb must be maintained pressed to check that there is no
alert except a false HYD G(Y) ENG 1(2) PUMP LO PR alert.

29-09-07A HYD PTU FAULT Alert

Ident.: MO-29-09-00009125.0001001 / 17 SEP 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Note: If the Yellow Electric Pump is not available:
Pressurize the Yellow Hydraulic System with:
A Ground cart, or with
The Yellow Engine 2 Pump with the Engine 2 running.
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
Continued on the following page

LAN COLOMBIA FLEET MO-29-09 P 1/4

MEL A to B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
29 - HYDRAULIC POWER
29-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Check of the PTU:
YELLOW ELEC PUMP pb-sw .................................................................................................ON
PTU pb-sw .......................................................................................................................... AUTO
On the HYD SD page, check that the green hydraulic system pressure indication is green.
If the green hydraulic system pressure indication is not available, check on the HYD SD page
that the GREEN system label is white and the arrow is green.
YELLOW ELEC PUMP pb-sw ................................................................................................. Off

29-09-09A HYD G(B)(Y)(B+G)(G+Y)(B+Y) SYS LO PR Alert

Ident.: MO-29-09-00009126.0002001 / 27 FEB 15
Applicable to: ALL

DURING COCKPIT PREPARATION

Note: If the Yellow Electric Pump is not available:
Pressurize the Yellow Hydraulic System with:
A Ground cart, or with
The Yellow Engine 2 Pump with the Engine 2 running.
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the
Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
YELLOW ELEC PUMP pb-sw .................................................................................................ON
BLUE ELEC PUMP pb-sw ..................................................................................................AUTO
BLUE PUMP OVRD pb-sw ..................................................................................................... ON
PTU pb-sw .......................................................................................................................... AUTO
On the CAPT or the F/O side, move the stick left or right.
On the F/CTL SD page, check the pairs of spoilers movement.
YELLOW ELEC PUMP pb-sw ................................................................................................. Off
BLUE PUMP OVRD pb-sw ...................................................................................................... Off
TAXI
Note: Due to a false HYD G(B)(Y)(G+B)(G+Y)(B+Y) SYS LO PR alert displayed on the EWD,
the "T.O CONFIG NORMAL line will not replace the "T.O CONFIG . . TEST" line in the
T.O MEMO.
Consider normal configuration for takeoff provided that no alert was displayed during the
T.O CONFIG TEST except a false HYD G(B)(Y)(G+B)(G+Y)(B+Y) SYS LO PR alert.
Continued on the following page

LAN COLOMBIA FLEET MO-29-09 P 2/4

MEL B to C 27 FEB 15
 MEL OPERATIONAL PROCEDURES
29 - HYDRAULIC POWER
29-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

CAUTION The T.O CONFIG TEST pb must be maintained pressed to check that there is no
alert except a false HYD G(B)(Y)(G+B)(G+Y)(B+Y) SYS LO PR alert.

LAN COLOMBIA FLEET MO-29-09 P 3/4

MEL C 27 FEB 15
 MEL OPERATIONAL PROCEDURES
29 - HYDRAULIC POWER
29-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-29-09 P 4/4

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
29 - HYDRAULIC POWER
29-10 - Main Hydraulic Power
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-10-03A Blue System Electric Pump

Ident.: MO-29-10-00009119.0001001 / 20 MAR 10
Applicable to: ALL

DURING PRELIMINARY COCKPIT PREPARATION

If the blue electric pump continuously runs:
At electrical power supply application:
BLUE ELEC PUMP pb-sw ...................................................................................................OFF
AFTER ENGINE START
BLUE ELEC PUMP pb-sw ...................................................................................................... AUTO
If the blue electric pump does not automatically start:
BLUE PUMP OVRD pb-sw ...............................................................................................ON
On the HYD SD page, check that the blue hydraulic circuit pressure is available.
AFTER ENGINE SHUTDOWN
BLUE ELEC PUMP pb-sw ......................................................................................................... OFF

LAN COLOMBIA FLEET MO-29-10 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
29 - HYDRAULIC POWER
29-10 - Main Hydraulic Power
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-29-10 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
29 - HYDRAULIC POWER
29-23 - Power Transfer
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-23-01A Power Transfer Unit (PTU)

Ident.: MO-29-23-00009120.0001001 / 12 SEP 12
Applicable to: ALL

AFTER ENGINE START

Check of the PTU operation:
GREEN ENG 1 PUMP pb-sw ................................................................................................OFF
On the HYD SD page, check that the green system pressure is correct.
A correct pressure is 3 000 PSI ( 200 PSI).
Check the PTU arrow indication.
GREEN ENG 1 PUMP pb-sw .................................................................................................. On
PTU pb-sw ............................................................................................................................. OFF
YELLOW ENG 2 PUMP pb-sw ............................................................................................. OFF
YELLOW ELEC PUMP pb-sw ................................................................................................. Off
Let the pressure in the yellow hydraulic system decrease to 200 PSI or less.
If the pressure is not below 200 PSI, the indications on the HYD SD page will not be displayed.
PTU pb-sw .......................................................................................................................... AUTO
On the HYD SD page, check that the yellow system pressure is correct.
A correct pressure is 3 000 PSI ( 200 PSI).
Check the PTU arrow indication.
YELLOW ENG 2 PUMP pb-sw ................................................................................................On
Note: 1. The PTU pressurizes the system to a nominal value of 3 000 PSI ( 200 PSI), but if
no consumers are operated the pressure is not constant. The PTU operates in a cycle
which keeps the pressure in the hydraulic systems between 2 100 PSI and 3 200 PSI.
2. For passengers comfort, the PTU may be set to OFF during the taxi after landing
provided that both engines hydraulic pumps are operative and running. The PTU must
be set back to AUTO before leaving the aircraft.

LAN COLOMBIA FLEET MO-29-23 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
29 - HYDRAULIC POWER
29-23 - Power Transfer
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-29-23 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
29 - HYDRAULIC POWER
29-24 - Yellow Auxiliary Hydraulic Power
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

29-24-01A Yellow System Electric Pump

Ident.: MO-29-24-00009121.0001001 / 20 MAR 10
Applicable to: ALL

ON GROUND
If the pump continuously runs and does not stop when set to off:
DOORS/CARGO (T12 on 122 VU) C/B ............................................................................... Pull
If unsuccessful:
Y HYD/ELEC PUMP/NORM (AB 03 on 123 VU) C/B ............................................... Pull
Y HYD/ELEC/PUMP (AB 06 on 123 VU) C/B ........................................................... Pull
Note: 1. If the pump continuously runs on the ground, there is a potential overheat
situation.
2. The reset of the C/Bs must be limited to the time required to open or close the
cargo doors.

LAN COLOMBIA FLEET MO-29-24 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
29 - HYDRAULIC POWER
29-24 - Yellow Auxiliary Hydraulic Power
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-29-24 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 30-01-01 - ANTI ICE Overhead Panel
MINIMUM EQUIPMENT LIST

30-01-01-03A ANTI ICE WING pb-sw FAULT light

Ident.: MO-30-01-01-00009042.0001001 / 10 OCT 14
Applicable to: ALL

DURING COCKPIT PREPARATION

Check of the anti-ice "arrow" symbol:
Make sure that the APU bleed air supply system is available.
ANTI ICE WING pb-sw ............................................................................................................ON
On the BLEED SD page, check that the anti-ice "arrow" symbols are displayed amber and
disappear after 30 s.
ANTI ICE WING pb-sw ............................................................................................................ Off

LAN COLOMBIA FLEET MO-30-01-01 P 1/2

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 30-01-01 - ANTI ICE Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-30-01-01 P 2/2

MEL 10 OCT 14
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-11 - Wing Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-11-01A Wing Anti-Ice Control Valve

Ident.: MO-30-11-00009047.0008001 / 10 OCT 14
Applicable to: MSN 4516-4546

FLIGHT PREPARATION/LIMITATIONS
Flight planning:
Increase fuel consumption by:
Zp (ft) 5 000 10 000 15 000 20 000 25 000 30 000 35 000 40 000
Fuel penalties 3.0 % 3.0 % 3.0 % 3.0 % 3.5 % 3.5 % 3.5 % 3.5 %

Single engine cruise:

Decrease drift down ceilings by:
1 200 ft when OAT ISA + 15 C
4 200 ft when OAT>ISA + 15 C
Approach climb performance:
When the engine bleed air supply system is closed:
No penalty.
When the engine bleed air supply system is open:
Decrease maximum climb limiting weight by:
2 200 kg (4 900 lb)
DURING COCKPIT PREPARATION
After application of the maintenance procedure:
On the BLEED SD page, check that the anti-ice arrow symbol is displayed.
The anti-ice arrow symbol may be displayed amber or green.
The WING ANTI ICE L(R) HI PR alert must not be displayed on the EWD.
BEFORE ENGINE START
Maintain the X BLEED selector at SHUT before engine start when the APU bleed is used.
Start the engine 1.
Maintain the X BLEED selector at SHUT during the start of engine 1.
Use the CROSS BLEED ENGINE START (Refer to FCOM/ Crossbleed Engine Start)
procedure to start the engine 2.
Apply the procedure associated with the WING ANTI ICE R VALVE OPEN alert displayed on
the EWD.
Continued on the following page

LAN COLOMBIA FLEET MO-30-11 P 1/6

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-11 - Wing Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

AFTER TAKEOFF
When above 1 500 ft:
Apply the automatic recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the
EWD.
IN FLIGHT
If the wing anti ice is operated in flight, WING ANTI ICE R HI PR alert may be displayed on the
EWD.
In the case of failure of a Bleed Air Supply System:
PACK (affected side) pb-sw ................................................................................................ OFF
AFTER LANDING
Apply the automatic recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the
EWD.

30-11-01A Wing Anti-Ice Control Valve

Ident.: MO-30-11-00009047.0018001 / 10 OCT 14
Applicable to: MSN 4758-5364

FLIGHT PREPARATION/LIMITATIONS
Flight planning:
Increase fuel consumption by:
Zp (ft) 5 000 10 000 15 000 20 000 25 000 30 000 35 000 40 000
Fuel penalties 4.5 % 4.5 % 6.0 % 4.5 % 3.5 % 2.5 % 2.5 % 2.5 %

Single engine cruise:

Decrease drift down ceilings by:
1 100 ft when OAT ISA
4 500 ft when OAT>ISA
Approach climb performance:
When the engine bleed air supply system is closed:
No penalty.
When the engine bleed air supply system is open:
Decrease maximum climb limiting weight by:
Continued on the following page

LAN COLOMBIA FLEET MO-30-11 P 2/6

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-11 - Wing Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

800 kg (1 800 lb) when OAT ISA + 5 C
4 900 kg (10 900 lb) when OAT>ISA + 5 C
DURING COCKPIT PREPARATION
After application of the maintenance procedure:
On the BLEED SD page, check that the anti-ice arrow symbol is displayed.
The anti-ice arrow symbol may be displayed amber or green.
The WING ANTI ICE L(R) HI PR alert must not be displayed on the EWD.
BEFORE ENGINE START
Maintain the X BLEED selector at SHUT before engine start when the APU bleed is used.
Start the engine 1.
Maintain the X BLEED selector at SHUT during the start of engine 1.
Use the CROSS BLEED ENGINE START (Refer to FCOM/ Crossbleed Engine Start)
procedure to start the engine 2.
Apply the procedure associated with the WING ANTI ICE R VALVE OPEN alert displayed on
the EWD.
AFTER TAKEOFF
When above 1 500 ft:
Apply the automatic recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the
EWD.
IN FLIGHT
If the wing anti ice is operated in flight, WING ANTI ICE R HI PR alert may be displayed on the
EWD.
In the case of failure of a Bleed Air Supply System:
PACK (affected side) pb-sw ................................................................................................ OFF
AFTER LANDING
Apply the automatic recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the
EWD.

LAN COLOMBIA FLEET MO-30-11 P 3/6

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-11 - Wing Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-11-01A Wing Anti-Ice Control Valve

Ident.: MO-30-11-00009047.0024001 / 10 OCT 14
Applicable to: MSN 5443-5453

FLIGHT PREPARATION/LIMITATIONS
Flight planning:
Increase fuel consumption by:
Zp (ft) 5 000 10 000 15 000 20 000 25 000 30 000 35 000 40 000
Fuel penalties 7% 6.5 % 5.5 % 4% 4% 2.5 % 2.5 % 2.5 %

Single engine cruise:

Decrease drift down ceilings by:
1 400 ft when OAT ISA
4 600 ft when OAT>ISA
Approach climb performance:
When the engine bleed air supply system is closed:
No penalty.
When the engine bleed air supply system is open:
Decrease maximum climb limiting weight by:
800 kg (1 800 lb) when OAT ISA + 5 C
4 900 kg (10 900 lb) when OAT>ISA + 5 C
DURING COCKPIT PREPARATION
After application of the maintenance procedure:
On the BLEED SD page, check that the anti-ice arrow symbol is displayed.
The anti-ice arrow symbol may be displayed amber or green.
The WING ANTI ICE L(R) HI PR alert must not be displayed on the EWD.
Continued on the following page

LAN COLOMBIA FLEET MO-30-11 P 4/6

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-11 - Wing Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

BEFORE ENGINE START
Maintain the X BLEED selector at SHUT before engine start when the APU bleed is used.
Start the engine 1.
Maintain the X BLEED selector at SHUT during the start of engine 1.
Use the CROSS BLEED ENGINE START (Refer to FCOM/ Crossbleed Engine Start)
procedure to start the engine 2.
Apply the procedure associated with the WING ANTI ICE R VALVE OPEN alert displayed on
the EWD.
AFTER TAKEOFF
When above 1 500 ft:
Apply the automatic recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the
EWD.
IN FLIGHT
If the wing anti ice is operated in flight, WING ANTI ICE R HI PR alert may be displayed on the
EWD.
In the case of failure of a Bleed Air Supply System:
PACK (affected side) pb-sw ................................................................................................ OFF
AFTER LANDING
Apply the automatic recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the
EWD.

LAN COLOMBIA FLEET MO-30-11 P 5/6

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-11 - Wing Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-30-11 P 6/6

MEL 10 OCT 14
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-21 - Engine Air Intake Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-21-01B
Engine Anti-Ice Valve
30-21-01C
Ident.: MO-30-21-00009049.0015001 / 18 JUL 14
Applicable to: MSN 4758-5364

GENERAL INFORMATION
An higher idle speed is set on both engines when an engine anti-ice valve is inoperative in the
open position.
FLIGHT PREPARATION/LIMITATIONS
Note: 1. The following decrements may be used for takeoff performance determination only for
dry runways if no takeoff data (predetermined by using OCTOPUS program or other
equivalent program with present failure case taken into account) is available.
2. Performance penalties apply whatever one or both valves are inoperative.
Takeoff performance:
Perform the takeoff using full thrust.
Apply the following reductions on the MTOW and the speeds :
OAT (C) ISA +10 C ISA +10 C < OAT ISA +20 C > ISA +20 C
Weight decrement (kg/lb) 1 100/2 500 2 000/4 500 3 200/7 100
V1, VR and V2 1 1 2
decrement (kt IAS)
Flight planning:
Increase fuel consumption by:
Zp (ft) 2 Valves blocked OPEN 1 Valve blocked OPEN
5 000 5.5 % 3.0 %
10 000 4.5 % 2.5 %
15 000 4.0 % 2.0 %
20 000 3.0 % 1.5 %
25 000 3.0 % 1.5 %
30 000 2.0 % 1.0 %
35 000 2.0 % 1.0 %
40 000 2.0 % 1.0 %

Single engine cruise:

Decrease drift down ceilings by:
400 ft when OAT ISA + 5 C
Continued on the following page

LAN COLOMBIA FLEET MO-30-21 P 1/4

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-21 - Engine Air Intake Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

3 700 ft when OAT > ISA + 5 C
Approach climb performance:
Decrease maximum climb limiting weight by:
300 kg (700 lb) when OAT ISA + 10 C
4 400 kg (9 700 lb) when OAT > ISA + 10 C
DURING COCKPIT PREPARATION
ANTI ICE ENG (affected) pb-sw ..................................................................................................ON
AFTER ENGINE START
The FADEC commands the continuous ignition on the affected engine.

30-21-01B
Engine Anti-Ice Valve
30-21-01C
Ident.: MO-30-21-00009049.0005001 / 17 SEP 10
Applicable to: MSN 4516-4546

GENERAL INFORMATION
An higher idle speed is set on both engines when an engine anti-ice valve is inoperative in the
open position.
FLIGHT PREPARATION/LIMITATIONS
Note: 1. The following decrements may be used for takeoff performance determination only for
dry runways if no takeoff data (predetermined by using OCTOPUS program or other
equivalent program with present failure case taken into account) is available.
2. Performance penalties apply whatever one or both valves are inoperative.
Takeoff performance:
Perform the takeoff using full thrust.
Apply the following reductions on the MTOW and the speeds :
OAT (C) ISA +20 C > ISA +20 C
Weight decrement (kg/lb) 500/1 200 2 800/6 200
V1, VR and V2 decrement (kt IAS) 1 2

Flight planning:
Increase fuel consumption by:
Continued on the following page

LAN COLOMBIA FLEET MO-30-21 P 2/4

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-21 - Engine Air Intake Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Zp (ft) 2 Valves blocked OPEN 1 Valve blocked OPEN
5 000 3.5 % 2.0 %
10 000 3.5 % 2.0 %
15 000 3.5 % 2.0 %
20 000 3.5 % 2.0 %
25 000 3.5 % 2.0 %
30 000 3.5 % 2.0 %
35 000 3.5 % 2.0 %
40 000 3.0 % 1.5 %

Single engine cruise:

Decrease drift down ceilings by:
900 ft when OAT ISA + 15 C
4 000 ft when OAT > ISA + 15 C
Approach climb performance:
Decrease maximum climb limiting weight by:
No penalty when OAT ISA + 20 C
4 300 kg (9 500 lb) when OAT > ISA + 20 C
DURING COCKPIT PREPARATION
ANTI ICE ENG (affected) pb-sw ..................................................................................................ON
AFTER ENGINE START
The FADEC commands the continuous ignition on the affected engine.

30-21-01B
Engine Anti-Ice Valve
30-21-01C
Ident.: MO-30-21-00009049.0026001 / 10 OCT 14
Applicable to: MSN 5443-5453

GENERAL INFORMATION
An higher idle speed is set on both engines when an engine anti-ice valve is inoperative in the
open position.
FLIGHT PREPARATION/LIMITATIONS
Same performance penalties apply with one or two valves inoperative.
Continued on the following page

LAN COLOMBIA FLEET MO-30-21 P 3/4

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-21 - Engine Air Intake Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Takeoff performance:
The takeoff performance must be determined by using OCTOPUS program or other equivalent
program with present failure case taken into account.

Launch PEP.
Flight planning:
Increase fuel consumption by:
Zp (ft) 2 Valves blocked OPEN 1 Valve blocked OPEN
5 000 15.0 % 8.0 %
10 000 12.0 % 6.0 %
15 000 7.0 % 3.5 %
20 000 5.0 % 2.5 %
25 000 4.0 % 2.0 %
30 000 2.5 % 1.5 %
35 000 2.5 % 1.5 %
40 000 2.0 % 1.0 %

Single engine cruise:

Decrease drift down ceilings by:
600 ft when OAT ISA + 5 C
4 200 ft when OAT > ISA + 5 C
Approach climb performance:
Decrease maximum climb limiting weight by:
300 kg (700 lb) when OAT ISA + 10 C
4 500 kg (9 900 lb) when OAT > ISA + 10 C
DURING COCKPIT PREPARATION
ANTI ICE ENG (affected) pb-sw ..................................................................................................ON
AFTER ENGINE START
The FADEC commands the continuous ignition on the affected engine.

LAN COLOMBIA FLEET MO-30-21 P 4/4

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-31 - Probe Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-31-01B Probe Heat Computer (PHC)

Ident.: MO-30-31-00009050.0002001 / 27 FEB 15
Applicable to: ALL

DURING COCKPIT PREPARATION

AIR DATA selector ...................................................................................................................F/O 3
IN FLIGHT
If icing conditions are encountered:
ADR 2 pb-sw ....................................................................................................................... OFF
CAUTION When ADR 2 is set to OFF,
takeoff in CONF 1+F is not permitted, and
maximum landing capability is CAT 3 SINGLE.
The ADR 2 pb-sw must remain set to OFF for the remainder of the flight.

30-31-02A Pitot Heater

Ident.: MO-30-31-00009052.0001001 / 11 MAR 10
Applicable to: ALL

Refer to OpsProc 30-31-01B Probe Heat Computer

30-31-03C F/O Static Ports Heater

Ident.: MO-30-31-00009053.0001001 / 27 FEB 15
Applicable to: ALL

Refer to OpsProc 30-31-01B Probe Heat Computer

CAPT Static Ports Heater

Ident.: MO-30-31-00015607.0001001 / 27 FEB 15
Applicable to: ALL

ON GROUND OR IN FLIGHT
Disregard and clear the ANTI ICE CAPT L(R) STAT alert associated with the CAPT static ports
heater(s) inoperative for the dispatch.

LAN COLOMBIA FLEET MO-30-31 P 1/2

MEL A to D 27 FEB 15
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-31 - Probe Ice Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-31-04A Angle of Attack (AOA) Probes Heating (F/O inoperative)

Ident.: MO-30-31-00009054.0002001 / 27 FEB 15
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
If icing conditions are encountered during the flight:
Maximum landing capability may be downgraded to CAT 3 SINGLE.
DURING COCKPIT PREPARATION
AIR DATA selector ...................................................................................................................F/O 3

30-31-04B
Angle of Attack (AOA) Probes Heating (CAPT or STBY inoperative)
30-31-04C
Ident.: MO-30-31-00009198.0001001 / 12 SEP 11
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
If icing conditions are encountered during the flight:
Maximum landing capability may be downgraded to CAT 3 SINGLE.

LAN COLOMBIA FLEET MO-30-31 P 2/2

MEL E to F 27 FEB 15
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-42 - Windshield Anti-Icing and Defogging
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-42-01A Window Heat Computer

Ident.: MO-30-42-00009056.0001001 / 27 NOV 12
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
When the PF side is inoperative:
Maximum landing capability is CAT 1.
When the PNF side is inoperative:
Maximum landing capability is CAT 3 DUAL.

30-42-03A Windshield Heating

Ident.: MO-30-42-00009057.0001001 / 12 SEP 11
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
When the PF side is inoperative:
Maximum landing capability is CAT 1.
When the PNF side is inoperative:
Maximum landing capability is CAT 3 DUAL.

LAN COLOMBIA FLEET MO-30-42 P 1/2

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-42 - Windshield Anti-Icing and Defogging
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-30-42 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-45 - Windshield Rain Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-45-01B Windshield Wiper

Ident.: MO-30-45-00009059.0001001 / 12 SEP 11
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
When the wiper and the rain repellent are inoperative or deactivated on the PF side:
Maximum landing capability is CAT 1.

LAN COLOMBIA FLEET MO-30-45 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-45 - Windshield Rain Protection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-30-45 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-81 - Ice Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

30-81-01A Ice Detection System

Ident.: MO-30-81-00009060.0002001 / 27 FEB 15
Applicable to: ALL

IN FLIGHT
The presence of ice in the vicinity of the windshield and on the wipers is periodically checked.

30-81-03A Lighting of External Visual Icing Indicator

Ident.: MO-30-81-00009062.0001001 / 11 MAR 10
Applicable to: ALL

IN FLIGHT
If icing conditions are expected during night operations:
Refer to AFM/LIM-70 Operations in Icing Conditions

LAN COLOMBIA FLEET MO-30-81 P 1/2

MEL A to B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
30 - ICE AND RAIN PROTECTION
30-81 - Ice Detection
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-30-81 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
31 - INDICATING/RECORDING SYSTEMS
31-07 - Indications on the System Display (SD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Permanent Data (TAT, SAT, ISA, GLOAD -

31-07-02A
ALT SEL, UTC, GW) Indications on the SD
Ident.: MO-31-07-00009041.0003001 / 27 FEB 15
Applicable to: ALL

DURING COCKPIT PREPARATION

Check that the TAT value is operative on the SD permanent data.
If the TAT value is not operative:
Check that the TAT value is available through the ADR 3.
Note: Use the AIR DATA SWITCHING selector to display temporarily the TAT value on the
SD.
IN FLIGHT
If needed:
The TAT value may be displayed through the same action on the AIR DATA SWITCHING
selector.

LAN COLOMBIA FLEET MO-31-07 P 1/2

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
31 - INDICATING/RECORDING SYSTEMS
31-07 - Indications on the System Display (SD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-31-07 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
31 - INDICATING/RECORDING SYSTEMS
31-20 - Independent Instruments
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-20-01A Electrical Clock Indicator

Ident.: MO-31-20-00009031.0001001 / 12 SEP 11
Applicable to: ALL

ON GROUND OR IN FLIGHT
After any electrical power interruption resulting in the loss of the UTC on the SD:
Initialize the UTC and the date using the MCDU: Refer to FCOM/ GMT/Date Initialization.

LAN COLOMBIA FLEET MO-31-20 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
31 - INDICATING/RECORDING SYSTEMS
31-20 - Independent Instruments
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-31-20 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
31 - INDICATING/RECORDING SYSTEMS
31-53 - Flight Warning Computer (FWC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-53-01A FLIGHT WARNING COMPUTER (FWC)

Ident.: MO-31-53-00009032.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 SINGLE.

31-53-06A Altitude Alert

Ident.: MO-31-53-00009462.0001001 / 18 MAY 11
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
When both altitude alert functions are inoperative:
RVSM operations are not permitted.

LAN COLOMBIA FLEET MO-31-53 P 1/2

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
31 - INDICATING/RECORDING SYSTEMS
31-53 - Flight Warning Computer (FWC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-31-53 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
31 - INDICATING/RECORDING SYSTEMS
31-56 - ECAM Control Panel (ECP)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-56-07A T.O CONFIG pb on the ECP

Ident.: MO-31-56-00009033.0001001 / 12 SEP 12
Applicable to: ALL

BEFORE TAKEOFF
Check that the aircraft is in the correct takeoff configuration:
FLAPS/SLATS....................................................................................................................CHECK
On EWD, check that the FLAPS position corresponds to the position inserted in the MCDU
PERF TAKE OFF Page.
PITCH TRIM...................................................................................................................... CHECK
Check that the selected pitch trim is in the green band of the pitch trim wheel and corresponds
to the value inserted in the MCDU PERF TAKE OFF Page.
RUDDER TRIM.......................................................................................................CHECK ZERO
GROUND SPOILERS..........................................................................................CHECK ARMED
SIDESTICK PRIORITY light ..............................................................................CHECK NO RED
On the WHEEL SD page, check that the brakes temperature is below 300 C.
DOORS.............................................................................................................................. CHECK
On the DOOR/OXY SD page, check that all doors are indicated closed.
Deselect the DOOR/OXY SD page after the check.

LAN COLOMBIA FLEET MO-31-56 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
31 - INDICATING/RECORDING SYSTEMS
31-56 - ECAM Control Panel (ECP)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-31-56 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
31 - INDICATING/RECORDING SYSTEMS
31-62 - Display Management Computer (DMC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-62-01B DMC 1
Ident.: MO-31-62-00010598.0002001 / 27 FEB 15
Applicable to: ALL

ON GROUND OR IN FLIGHT
In the case of multiple undue ECAM alerts concerning ENG 1(2) N1(N2) (EGT)(FF) OVER
LIMIT
or
ENG 1(2) N1(N2)(EGT)(EPR)(FF) DISCREPANCY
or
NAV ATT(ALT1)(HDG) DISCREPANCY
or
NAV FM/GPS POS DISAGREE
or
FUEL F.USED/FOB DISAGREE
or
MINIMUM or HUNDRED ABOVE callouts, possibly associated with EFIS red flags, apply
the below procedure:
Crosscheck the affected parameters on the EWD, PFD, ND, or on the related SD page to
confirm that the alerts are undue.
EIS DMC SWITCHING selector .................................................................................. NORM
Note: CAPT PFD and ND ae lost when EIS DMC SWITCHING selector is set to NORM.

If the undue ECAM alerts stop:

Pull EIS/DMC3/SPLY (121 VU Q09) C/B and EIS/DMC3/STBY/SPLY (49 VU E10) C/B
for more than 5 s and push them back.
EIS DMC SWITCHING selector ..........................................................................CAPT 3
If the undue ECAM alerts continue:
EIS DMC SWITCHING selector ..........................................................................CAPT 3
Wait for CAPT PFD and ND recovery.
Pull EIS/DMC2/SPLY (121 VU Q08) C/B for more than 5 s and push it back.

LAN COLOMBIA FLEET MO-31-62 P 1/4

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
31 - INDICATING/RECORDING SYSTEMS
31-62 - Display Management Computer (DMC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-62-02A DMC 2
Ident.: MO-31-62-00009034.0004001 / 27 FEB 15
Applicable to: ALL

ON GROUND OR IN FLIGHT
In the case of multiple undue ECAM alerts concerning ENG 1(2) N1(N2) (EGT)(FF) OVER
LIMIT
or
ENG 1(2) N1(N2)(EGT)(EPR)(FF) DISCREPANCY
or
NAV ATT(ALT1)(HDG) DISCREPANCY
or
NAV FM/GPS POS DISAGREE
or
FUEL F.USED/FOB DISAGREE
or
MINIMUM or HUNDRED ABOVE callouts, possibly associated with EFIS red flags, apply
the below procedure:
Crosscheck the affected parameters on the EWD, PFD, ND, or on the related SD page to
confirm that the alerts are undue.
EIS DMC SWITCHING selector .................................................................................. NORM
Note: F/O PFD and ND are lost when EIS DMC SWITCHING selector is set to NORM.

If the undue ECAM alerts stop:

Pull EIS/DMC3/SPLY (121 VU Q09) C/B and EIS/DMC3/STBY/SPLY (49 VU E10) C/B
for more than 5 s and push them back.
EIS DMC SWITCHING selector ............................................................................. F/O 3
If the undue ECAM alerts continue:
EIS DMC SWITCHING selector ............................................................................. F/O 3
Wait for F/O PFD and ND recovery.
Pull EIS/DMC1/SPLY (49 VU E11) C/B for more than 5 s and push it back.

LAN COLOMBIA FLEET MO-31-62 P 2/4

MEL B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
31 - INDICATING/RECORDING SYSTEMS
31-62 - Display Management Computer (DMC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-62-03B DMC 3
Ident.: MO-31-62-00010599.0001001 / 27 FEB 15
Applicable to: ALL

ON GROUND OR IN FLIGHT
In the case of multiple undue ECAM alerts concerning ENG 1(2) N1(N2) (EGT)(FF) OVER
LIMIT
or
ENG 1(2) N1(N2)(EGT)(EPR)(FF) DISCREPANCY
or
NAV ATT(ALT1)(HDG) DISCREPANCY
or
NAV FM/GPS POS DISAGREE
or
FUEL F.USED/FOB DISAGREE
or
MINIMUM or HUNDRED ABOVE callouts, possibly associated with EFIS red flags, apply
the below procedure:
Crosscheck the affected parameters on the EWD, PFD, ND, or on the related SD page to
confirm that the alerts are undue.
EIS DMC SWITCHING selector ................................................................................ CAPT 3
Note: CAPT PFD and ND are lost when EIS DMC SWITCHING selector is set to CAPT
3.

If the undue ECAM alerts stop:

Pull EIS/DMC1/SPLY (49 VU E11) C/B a for more than 5 s and push it back.
EIS DMC SWITCHING selector ............................................................................NORM
If the undue ECAM alerts continue:
EIS DMC SWITCHING selector ............................................................................NORM
Wait for CAPT PFD and ND recovery.
Pull EIS/DMC2/SPLY (121 VU Q08) C/B for more than 5 s and push it back.

LAN COLOMBIA FLEET MO-31-62 P 3/4

MEL C 27 FEB 15
 MEL OPERATIONAL PROCEDURES
31 - INDICATING/RECORDING SYSTEMS
31-62 - Display Management Computer (DMC)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-31-62 P 4/4

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
31 - INDICATING/RECORDING SYSTEMS
31-63 - Display Unit (DU)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-63-02A PFDU 2
Ident.: MO-31-63-00009035.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 2.
ON GROUND OR IN FLIGHT
PFDU 2 knob ..............................................................................................................................OFF

31-63-03A NDU 1
Ident.: MO-31-63-00009036.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 2.
ON GROUND OR IN FLIGHT
NDU 1 knob ................................................................................................................................OFF

31-63-04A NDU 2
Ident.: MO-31-63-00009037.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 2.
ON GROUND OR IN FLIGHT
NDU 2 knob ................................................................................................................................OFF

31-63-05A SDU
Ident.: MO-31-63-00009038.0001001 / 12 SEP 11
Applicable to: ALL

ON GROUND OR IN FLIGHT
SDU knob ................................................................................................................................... OFF
In the case of alerts being displayed on the EWD:
Use the ECAM/ND SWITCHING selector to display the system page on the selected NDU.
Continued on the following page

LAN COLOMBIA FLEET MO-31-63 P 1/2

MEL A to D 05 NOV 13
 MEL OPERATIONAL PROCEDURES
31 - INDICATING/RECORDING SYSTEMS
31-63 - Display Unit (DU)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

In the case of failure of the AC BUS 1:
If all the Display Units are lost:
Apply the ELEC AC ESS BUS FAULT alert procedure: Refer to
FCOM/PRO-ABN-24-ELECTRICAL-ELEC AC ESS BUS FAULT.
Note: The AC ESS BUS is recovered when the AC ESS FEED pb-sw is set to ALTN.

LAN COLOMBIA FLEET MO-31-63 P 2/2

MEL D 05 NOV 13
 MEL OPERATIONAL PROCEDURES
31 - INDICATING/RECORDING SYSTEMS
31-68 - Switching Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

31-68-05A PFD/ND XFR pb on the Lateral Instrument Panel

Ident.: MO-31-68-00009039.0001001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

On the side where the PFD/ND XFR pb is inoperative:
PFD brightness control knob ...........................................................................................OFF
Check that the PFD image is automatically displayed on the NDU.
PFD brightness control knob .............................................................................................On
If the PFD image is not automatically displayed on the NDU:
The affected side cannot be used by the Pilot Flying.
On the side where the PFD to ND automatic switching is inoperative:
PFD brightness control knob ...........................................................................................OFF
EIS DMC SWITCHING selector (Affected side).............................................CAPT 3 (F/O 3)
Check that the PFD image is displayed on the associated NDU.
PFD brightness control knob .............................................................................................On
EIS DMC SWITCHING knob (Affected side)................................................................NORM
IN FLIGHT
If a PFDU fails with no automatic transfer to the associated NDU:
PFD brightness control knob ...........................................................................................OFF
EIS DMC SWITCHING selector (Affected side).............................................CAPT 3 (F/O 3)
Check that the PFD image is displayed on the associated NDU.

LAN COLOMBIA FLEET MO-31-68 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
31 - INDICATING/RECORDING SYSTEMS
31-68 - Switching Panel
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-31-68 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-07 - Indications on the WHEEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-07-01A
Brakes Temperature Indication on the WHEEL SD page
32-07-01B
Ident.: MO-32-07-00009012.0003001 / 10 OCT 14
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
The brake energy graph and the brake cooling time table given hereafter permit to determine the
ground brake cooling time.
BRAKE ENERGY GRAPH
If MAX reverser thrust was selected for all reversers during the braking phase:
Enter the brake energy graph: WITH THRUST REVERSERS USE.
If MAX reverser thrust was NOT selected for all reversers during the braking phase:
Enter the brake energy graph: WITHOUT THRUST REVERSERS USE.
Determination of the brake energy accumulated during a REJECTED TAKEOFF ( RTO ) :
Enter with the aircraft takeoff weight ( TOW ) and with the rejected takeoff speed in kt IAS ).
Apply airport pressure altitude, temperature, wind and runway slope corrections.
Determination of the brake energy accumulated during a LANDING :
Enter with the aircraft landing weight, and
Enter with the touch down speed in kt IAS if the autobrake was selected and applied or with the
manual braking speed in kt IAS in the other cases.
Apply airport pressure altitude, temperature, wind and runway slope corrections.
Correct for brake setting with a preselected autobrake setting (LO, MED) or with MAX PEDAL
braking in the other cases.
Note: In the case of a dispatch with one brake inoperative ( Refer to Item 32-42-01 Main
Wheel Brake or Refer to Item 32-42-02 Green System Brake ), the brake energy
accumulated is increased by 34 % .

Continued on the following page

LAN COLOMBIA FLEET MO-32-07 P 1/6

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-07 - Indications on the WHEEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Brake Energy with Thrust Reverser Use

Continued on the following page

LAN COLOMBIA FLEET MO-32-07 P 2/6

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-07 - Indications on the WHEEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Brake Energy without Thrust Reverser Use

Continued on the following page

LAN COLOMBIA FLEET MO-32-07 P 3/6

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-07 - Indications on the WHEEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

BRAKE COOLING TIME TABLE
Determination of the brake cooling time:
EXAMPLE:
55 152 153 154 155 155 ====> TIME (min) WITHOUT BRAKE COOLING FAN
46 46 46 46 47 ====> TIME (min) WITH BRAKE COOLING FAN

If the Energy and the OAT are not given in the table, use the values given in the next adjacent
column/row.
For Example, with Energy = 78 MJ , and OAT = 15 C , entering the next adjacent column/row
(Energy = 80 MJ , OAT = 20 C ) gives the following results:
Without brake cooling fan: 189 min
With brake cooling fan: 57 min
Enter the following table with the energy and the OAT to determine the ground brake cooling time.
GROUND BRAKE COOLING TIME (min)
ENERGY OAT (C)
(MJ) -50 -40 -30 -20 -10 0 10 20 30 40 50 55
0 0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
5 0 0 0 0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0 0 0 0
10 0 0 0 4 9 14 19 23 27 31 35 37
0 0 0 1 3 4 6 7 8 9 10 11
15 31 35 38 42 45 48 51 54 57 60 62 64
9 10 11 12 13 14 15 16 17 18 19 19
20 59 62 65 67 70 72 74 77 79 81 83 84
18 19 19 20 21 22 22 23 24 24 25 25
25 81 83 85 87 89 91 92 94 96 98 99 100
24 25 25 26 27 27 28 28 29 29 30 30
30 98 99 101 103 104 106 107 109 110 112 113 114
29 30 30 31 31 32 32 33 33 34 34 34
35 112 113 115 116 117 119 120 121 123 124 125 126
34 34 34 35 35 36 36 36 37 37 38 38
40 124 125 126 127 129 130 131 132 133 134 135 136
37 37 38 38 39 39 39 40 40 40 41 41
45 134 135 136 137 139 140 141 142 143 144 145 145
40 41 41 41 42 42 42 42 43 43 43 44
50 144 145 146 146 147 148 149 150 151 152 153 153
43 43 44 44 44 45 45 45 45 46 46 46
Continued on the following page

LAN COLOMBIA FLEET MO-32-07 P 4/6

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-07 - Indications on the WHEEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

GROUND BRAKE COOLING TIME (min)
ENERGY OAT (C)
(MJ) -50 -40 -30 -20 -10 0 10 20 30 40 50 55
55 152 153 154 155 155 156 157 158 159 160 160 161
46 46 46 46 47 47 47 47 48 48 48 48
60 160 160 161 162 163 164 164 165 166 167 167 168
48 48 48 49 49 49 49 50 50 50 50 50
65 167 167 168 169 170 170 171 172 172 173 174 174
50 50 50 51 51 51 51 52 52 52 52 52
70 173 174 174 175 176 176 177 178 178 179 180 180
52 52 52 53 53 53 53 53 54 54 54 54
75 179 180 180 181 182 182 183 183 184 185 185 186
54 54 54 54 54 55 55 55 55 55 56 56
80 185 185 186 186 187 188 188 189 189 190 190 191
55 56 56 56 56 56 56 57 57 57 57 57
85 190 190 191 191 192 193 193 194 194 195 195 196
57 57 57 57 58 58 58 58 58 58 59 59
90 195 195 196 196 197 197 198 198 199 199 200 200
58 59 59 59 59 59 59 60 60 60 60 60
95 199 200 200 201 201 202 202 203 203 204 204 205
60 60 60 60 60 61 61 61 61 61 61 61
100 204 204 205 205 206 206 207 207 208 208 208 209
61 61 61 62 62 62 62 62 62 62 63 63
105 208 208 209 209 210 210 211 211 212 212 212 213
62 63 63 63 63 63 63 63 63 64 64 64
110 212 212 213 213 214 214 215 215 215 216 216 216
64 64 64 64 64 64 64 64 65 65 65 65
115 216 216 217 217 217 218 218 219 219 219 220 220
65 65 65 65 65 65 65 66 66 66 66 66
120 219 220 220 221 221 221 222 222 222 223 223 223
66 66 66 66 66 66 67 67 67 67 67 67
A320 Messier/Goodrich - 03.01.05 - F476021.txt

AFTER ENGINE START

In the case of a false BRAKES HOT alert displayed on the EWD :
EMER CANC pb ................................................................................................................ Press
Note: In the case of a false BRAKES HOT alert due to a faulty BTMU or a faulty BSCU ,
the "T.O CONFIG NORMAL line will not replace the "T.O CONFIG . . TEST" line in
the T.O MEMO. Consider normal configuration for takeoff provided that no alert was
displayed during the T.O CONFIG TEST.
Continued on the following page

LAN COLOMBIA FLEET MO-32-07 P 5/6

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-07 - Indications on the WHEEL SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

CAUTION The T.O CONFIG TEST pb must be maintained pressed to check that there is
no alert.

32-07-03A L/G Doors Position Indication on the WHEEL SD page

Ident.: MO-32-07-00009013.0001001 / 18 MAR 10
Applicable to: ALL

IN FLIGHT
MAX SPEED............................................................................................................... 250 kt M 0.60

LAN COLOMBIA FLEET MO-32-07 P 6/6

MEL A to B 10 OCT 14
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

BRAKES-N/WS MINOR FAULT Alert

32-09-01C
(Alternate braking checked operative)
Ident.: MO-32-09-00009197.0001001 / 27 FEB 15
Applicable to: ALL

DURING COCKPIT PREPARATION

The ACCU PRESS indication must be in the green band.
If ACCU PRESS indication not in the green band:
Y ELEC PUMP pb-sw ...........................................................................................ON then OFF
CHOCKS..........................................................................................................CHECK IN PLACE
PARKING BRAKE handle.......................................................................................................OFF
PARKING PEDALS............................................................................................................ PRESS
Apply maximum pressure on both pedals.
BRAKE PRESSURE (on BRAKES pressure indicators)................................................... CHECK
Pressure must increase without delay symmetrically on left and right sides for the same
application simultaneously applied on left and right pedals. With full pedal deflection, the
pressure must be between 900 and 1100 psi.
BRAKES PEDALS......................................................................................................... RELEASE
Check that no residual pressure in the brakes remains.
PARKING BRAKE handle.........................................................................................................ON

LAN COLOMBIA FLEET MO-32-09 P 1/2

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-32-09 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-31 - Normal Extension and Retraction
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-31-01A Landing Gear Control and Interface Unit ( LGCIU )

Ident.: MO-32-31-00008975.0002001 / 10 OCT 14
Applicable to: ALL

DURING COCKPIT PREPARATION

HYDRAULIC/LGCIU/SYS2 (121VU Q35) C/B ..........................................................................PULL
The following table gives the consequences on the systems affected when the LGCIU 2 is
inoperative and above mentioned C/B is pulled.
SYSTEMS CONSEQUENCES PROCEDURE
The system remains in closed circuit Time limitations on ground for ELEC PWR
configuration. supply:
The ground cooling system is
OAT 43 C : No Limitation
AVNCS VENT inoperative. 44 C OAT 52 C : 3 h
(on ground) OAT 53 C : 30 min
Check that the air conditioning system is
operative.
The PTU runs after the first engine start until
the second engine is started.
HYD
The BLUE ELEC PUMP FAULT light and the
(on ground) YELLOW ENG 2 PUMP FAULT light come on
when engines are off.
TPIS The WHEEL TYRE LO PR alert threshold is
set to flight level.
ATC 2 The ATC 2 is not inhibited. On ground, set the ATC selector to SYS 1.
(on ground)
The strobe lights are not inhibited on On ground, set the STROBE sw to OFF.
ground when set to AUTO.
On ground, with flaps retracted, logo lights do
LIGHTS not come on.
The taxi light , the runway turn-off light , and
the takeoff light are inoperative on ground and
in flight.
When only the APU generator or the GPU
ELEC
supplies the aircraft, the main galleys are not
(on ground) supplied.
Continued on the following page

LAN COLOMBIA FLEET MO-32-31 P 1/4

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-31 - Normal Extension and Retraction
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

SYSTEMS CONSEQUENCES PROCEDURE
The FADEC supply is continuously on.
The automatic start abort is inoperative. Use the MAN START procedure. Refer to
FCOM/PRO-SUP-70 Manual Engine Start -
Manual Engine Start Procedure
ENG 2 The minimum idle is inoperative when Refer to OpsProc 73-20-05A Minimum Idle on
(on ground) slats/flaps are extended. Ground
When FLX TO is selected, MCT thrust is set. Use the TOGA for takeoff.
The thrust reverser is inoperative. Refer to OpsProc 78-30-01A Thrust Reverser
The BUMP function is inoperative. Do not use the BUMP function.
SLATS The slats are slow from 1 to 0.
(on ground)
AIR COND Both air conditioning packs ram air inlet do not
(on ground) close.
On ground, when set to ON, the WING A
ICE valve do not close at the end of the test
WING A ICE
sequence ( 30 s ).
(on ground) The WING A.ICE OPEN ON GND alert will be
displayed on the EWD .
ADIRU and The horn and the light are inoperative.
AVNCS VENTalert
WATER The preselect water servicing is inoperative.
SERVICING
(on ground)
CARGO DOOR Only the manual control is operative.
( FWD and AFT)
The CVR test and the CVR erase functions are
RECORDERS inoperative.
(on ground) The CVR and the DFDR do not stop after
engine shutdown.
BRAKES The brakes cooling is inoperative.
(on ground)
AIRSTAIRS The airstairs cannot be extended.
Continued on the following page

LAN COLOMBIA FLEET MO-32-31 P 2/4

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-31 - Normal Extension and Retraction
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

SYSTEMS CONSEQUENCES PROCEDURE
WEIGHT AND The WBS is inoperative.
BALANCE
SYSTEM
ECAM On the WHEEL SD page , the landing gear
(in flight and on position indications associated with the
ground) LGCIU 2 are displayed XX .
The L/G LGCIU 2 FAULT alert is diplayed
on the EWD .

IN FLIGHT
In the case of loss of the LGCIU 1:
AP and FD are lost.
Maximum landing capability is CAT 1.

32-31-02A Landing Gear Retracting System

Ident.: MO-32-31-00008977.0001001 / 12 SEP 11
Applicable to: ALL

Refer to FCOM/PRO-SPO-25-FLIGHT WITH GEAR DOWN.

LAN COLOMBIA FLEET MO-32-31 P 3/4

MEL A to B 10 OCT 14
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-31 - Normal Extension and Retraction
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-32-31 P 4/4

MEL 10 OCT 14
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-32-02A LGCIU 2 RH L/G Shock Absorber Proximity Detector

Ident.: MO-32-32-00008978.0002001 / 10 OCT 14
Applicable to: ALL

GENERAL INFORMATION
SYSTEMS CONSEQUENCES PROCEDURES
PITOTS The F/O pitot is set to high heating level when Keep the EXT PWR pb-sw set to ON until the
(on ground) the EXT PWR pb-sw is set to OFF. engine start.

The system remains in the closed circuit Time limitations on ground for ELEC PWR
configuration. supply:
The ground cooling system is
OAT 43 C : No limitation
AVNCS VENT inoperative. OAT = 52 C : 3 h
(on ground) OAT = 61 C : 30 min
Check that the air conditioning system is
operative.

ADIRU and The horn and the light are inoperative.

AVNCS VENT alert
(on ground)
The BLUE ELEC PUMP FAULT light and the
HYD alerts
YELLOW ENG 2 PUMP FAULT light come on
(on ground) when engines are off.
The wing anti-ice is not inhibited. On ground, do not set the WING ANTI ICE
WING A/ICE
pb-sw to ON for more that 30 s . If required, set
(on ground) it to ON just before takeoff.
TPIS The WHEEL TYRE LO PR alert threshold is set
(on ground) to flight level.
ATC 2 The ATC 2 is not inhibited. On ground, set the ATC selector to SYS 1.
(on ground)
The strobe lights are not inhibited. On ground, set the STROBE sw to OFF.
LIGHTS
On ground, with flaps retracted, the logo lights
(on ground) do not come on.
ELEC When only the APU generator or GPU supplies
(on ground) the aircraft, the main galleys are not supplied.
Continued on the following page

LAN COLOMBIA FLEET MO-32-32 P 1/8

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

SYSTEMS CONSEQUENCES PROCEDURES
The FADEC supply is continuously on.
The automatic start abort is inoperative. Use the MAN START procedure. Refer to
FCOM/PRO-SUP-70 Manual Engine Start -
Manual Engine Start Procedure
ENG 2 The minimum idle is inoperative. Refer to OpsProc 73-20-05A Minimum Idle on
(on ground) Ground
When FLX TO is selected, MCT thrust is set. Use the TOGA for takeoff.
The thrust Reverser is inoperative. Refer to OpsProc 78-30-01A Thrust Reverser
The BUMP function is inoperative. Do not use the BUMP function.
SLATS The slats are slow from 1 to 0.
(on ground)
CARGO DOOR Only the manual control is operative.
(on ground)
AIR COND The air conditioning pack 2 ram air inlet does
(on ground) not close.
WATER The preselect water servicing is inoperative.
SERVICING
(on ground)
AIRSTAIRS The airstairs cannot be extended.
(on ground)
The CVR test and the CVR erase functions are
RECORDERS inoperative.
(on ground) The CVR and the DFDR do not stop after
engine shutdown.
On the WHEEL SD page , the landing gear
ECAM position indications associated with the
(in flight and LGCIU 2 are displayed XX .
on ground) The L/G LGCIU 2 FAULT alert is displayed
on the EWD .

LAN COLOMBIA FLEET MO-32-32 P 2/8

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-32-03A LGCIU 2 LH L/G Shock Absorber Proximity Detector

Ident.: MO-32-32-00008988.0016001 / 27 FEB 15
Applicable to: ALL

GENERAL INFORMATION
SYSTEMS CONSEQUENCES PROCEDURES
PITOTS The CAPT pitot is set to the high heating level Keep the EXT PWR pb-sw set to ON until
(on ground) when the EXT PWR pb-sw is set to OFF. engine start.

The system remains in the closed circuit Time limitations on ground for ELEC PWR
configuration supply:
The ground cooling system is
OAT 42 C : No limitation
AVNCS VENT inoperative. OAT = 53 C : 3 h
(on ground) OAT = 61 C : 30 min
Check that the air conditioning system is
operative.

ADIRU and The horn and the light are inoperative.

AVNCS VENT alert
(on ground)
HYD alerts The BLUE ELEC PUMP FAULT light and the
(on ground) YELLOW ENG 2 PUMP FAULT light come on
when engines are off.
TPIS The WHEEL TYRE LO PR alert threshold is set
(on ground) to flight level.
LIGHTS The strobe lights are not inhibited. On ground, set the STROBE sw to OFF.
(on ground) On ground, with flaps retracted, the logo lights
do not come on.
ELEC When only the APU generator or GPU supplies
(on ground) the aircraft, the main galleys are not supplied.
The FADEC supply is continuously on.
The automatic start abort is inoperative. Use the MAN START procedure. Refer to
FCOM/PRO-SUP-70 Manual Engine Start -
Manual Engine Start Procedure
ENG 2 The minimum idle is inoperative. Refer to OpsProc 73-20-05A Minimum Idle on
(on ground) Ground
When FLX TO selected, MCT thrust is set. Use the TOGA for takeoff.
The thrust reverser is inoperative. Refer to OpsProc 78-30-01A Thrust Reverser
The BUMP function is inoperative. Do not use the BUMP function.
SLATS The slats are slow from 1 to 0.
(on ground)
Continued on the following page

LAN COLOMBIA FLEET MO-32-32 P 3/8

MEL B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

SYSTEMS CONSEQUENCES PROCEDURES
AIR COND The air conditioning pack 1 ram air inlet does not
(on ground) close.
CARGO DOOR Only the manual control is operative.
WATER The preselect water servicing is inoperative.
SERVICING
(on ground)
RECORDERS The CVR test and the CVR erase functions are
(on ground) inoperative.
The CVR and the DFDR do not stop after engine
shutdown.
ECAM On the WHEEL SD page , the landing gear
(in flight and position indications associated with the
on ground) LGCIU 2 are displayed XX .
The L/G LGCIU 2 FAULT alert is displayed on
the EWD .

32-32-04A LGCIU 2 Nose L/G Shock Absorber Proximity Detector

Ident.: MO-32-32-00008989.0001001 / 12 MAR 10
Applicable to: ALL

GENERAL INFORMATION
SYSTEMS CONSEQUENCES PROCEDURES
The STBY pitot is set to the high heating level Keep the EXT PWR pb-sw set to ON until the
when the EXT PWR pb-sw is set to OFF. engine start.
PITOTS
If displayed, disregard the ANTI ICE CAPT(F/O)
(on ground) PITOT alert on the EWD when EXT PWR pb-sw
is set to OFF.
HYD The PTU runs after the first engine start until the
(on ground) second engine is started.
ENG 2 The minimum idle is inoperative when
(on ground) slats/flaps are extended.
ECAM For WHEEL SD page and ECAM alert Refer to OpsProc 32-32-03A LGCIU 2 LH L/G Shock
(in flight and Absorber Proximity Detector " ECAM " line.
on ground)

LAN COLOMBIA FLEET MO-32-32 P 4/8

MEL B to C 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-32-05A LGCIU 2 RH L/G Down Lock Proximity Detector

Ident.: MO-32-32-00008990.0004001 / 10 OCT 14
Applicable to: ALL

GENERAL INFORMATION
SYSTEMS CONSEQUENCES PROCEDURES
REVERSER 2 is displayed in the INOP SYS The REVERSER 2 is still operative.
ENG 2 column on the STATUS SD page.
(on ground) The minimum idle is inoperative when
slats/flaps are extended.
ECAM On the WHEEL SD page, the landing gear position indications associated with the LGCIU 2
(in flight and are displayed XX.
on ground) The L/G LGCIU 2 FAULT alert is displayed on the EWD.

32-32-06A LGCIU 2 LH L/G Down Lock Proximity Detector

Ident.: MO-32-32-00008991.0010001 / 10 OCT 14
Applicable to: ALL

GENERAL INFORMATION
SYSTEMS CONSEQUENCES PROCEDURES
BRAKES The brakes cooling is inoperative.
REVERSER 2 is displayed in the INOP SYS The REVERSER 2 is still operative.
ENG 2 column on the STATUS SD page.
(on ground) The minimum idle is inoperative when
slats/flaps are extended.
ECAM On the WHEEL SD page, the landing gear position indications associated with the LGCIU 2
(in flight and are displayed XX.
on ground) The L/G LGCIU 2 FAULT alert is displayed on the EWD.

LAN COLOMBIA FLEET MO-32-32 P 5/8

MEL D to E 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-32-07A LGCIU 2 Nose L/G Down Lock Proximity Detector

Ident.: MO-32-32-00008992.0001001 / 02 NOV 11
Applicable to: ALL

GENERAL INFORMATION
SYSTEMS CONSEQUENCES
LIGHTS The Taxi light and the takeoff light are inoperative.
(in flight and on ground)
ECAM For WHEEL SD page and ECAM alert Refer to Item 32-31-01 Landing Gear
(in flight and on ground) Control and Interface Unit (LGCIU) " ECAM " line.

32-32-08A LGCIU 2 RH L/G Up Lock Proximity Detector

Ident.: MO-32-32-00008993.0004001 / 05 OCT 10
Applicable to: ALL

GENERAL INFORMATION
SYSTEMS CONSEQUENCES PROCEDURES
REVERSER 2 is displayed in the INOP SYS The thrust Reverser 2 is still operative.
ENG 2 column on the STATUS SD page .
(on ground) The minimum idle on ground is inoperative
when slats/flaps are extended.
ECAM For WHEEL SD page and ECAM alert Refer to Item 32-31-01 Landing Gear Control and
(in flight and Interface Unit (LGCIU) " ECAM " line.
on ground)

LAN COLOMBIA FLEET MO-32-32 P 6/8

MEL F to G 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-32-09A LGCIU 2 LH L/G Up Lock Proximity Detector

Ident.: MO-32-32-00008994.0004001 / 17 SEP 10
Applicable to: ALL

GENERAL INFORMATION
SYSTEMS CONSEQUENCES PROCEDURES
REVERSER 2 is displayed in the INOP SYS The thrust Reverser 2 is still operative.
ENG 2 column on the STATUS SD page .
(on ground) The minimum idle on ground is inoperative
when slats/flaps are extended.
ECAM For WHEEL SD page and ECAM alert Refer to Item 32-31-01 Landing Gear Control and
(in flight and Interface Unit (LGCIU) " ECAM " line.
on ground)

32-32-10A LGCIU 2 Nose L/G Up Lock Proximity Detector

Ident.: MO-32-32-00009002.0004001 / 12 SEP 11
Applicable to: ALL

GENERAL INFORMATION
SYSTEMS CONSEQUENCES PROCEDURES
REVERSER 2 is displayed in the INOP SYS The thrust Reverser 2 is still operative.
ENG 2 column on the STATUS SD page .
(on ground) The minimum idle on ground is inoperative
when slats/flaps are extended.
ECAM For WHEEL SD page and ECAM alert Refer to Item 32-31-01 Landing Gear Control and
(in flight and Interface Unit (LGCIU) " ECAM " line.
on ground)

32-32-11A LGCIU 2 RH L/G Doors Open Proximity Detector

Ident.: MO-32-32-00008995.0001001 / 11 MAR 10
Applicable to: ALL

Refer to OpsProc 32-32-08A LGCIU 2 RH L/G Up Lock Proximity Detector

LAN COLOMBIA FLEET MO-32-32 P 7/8

MEL H to J 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-32 - Proximity Detector System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-32-12A LGCIU 2 LH L/G Doors Open Proximity Detector

Ident.: MO-32-32-00008996.0001001 / 11 MAR 10
Applicable to: ALL

Refer to OpsProc 32-32-09A LGCIU 2 LH L/G Up Lock Proximity Detector

32-32-13A LGCIU 2 Nose L/G Doors Open Proximity Detector

Ident.: MO-32-32-00008997.0001001 / 11 MAR 10
Applicable to: ALL

Refer to OpsProc 32-32-10A LGCIU 2 Nose L/G Up Lock Proximity Detector

32-32-14A LGCIU 2 RH L/G Doors Closed Proximity Detector

Ident.: MO-32-32-00008998.0001001 / 11 MAR 10
Applicable to: ALL

Refer to OpsProc 32-32-08A LGCIU 2 RH L/G Up Lock Proximity Detector

32-32-15A LGCIU 2 LH L/G Doors Closed Proximity Detector

Ident.: MO-32-32-00008999.0001001 / 11 MAR 10
Applicable to: ALL

Refer to OpsProc 32-32-09A LGCIU 2 LH L/G Up Lock Proximity Detector

32-32-16A LGCIU 2 Nose L/G Doors Closed Proximity Detector

Ident.: MO-32-32-00009000.0001001 / 11 MAR 10
Applicable to: ALL

Refer to OpsProc 32-32-10A LGCIU 2 Nose L/G Up Lock Proximity Detector

LAN COLOMBIA FLEET MO-32-32 P 8/8

MEL K to O 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-33 - Free Fall Extension
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-33-01A Landing Gear Gravity Extension System

Ident.: MO-32-33-00009003.0001001 / 12 SEP 11
Applicable to: ALL

Refer to FCOM/PRO-SPO-25-FLIGHT WITH GEAR DOWN.

LAN COLOMBIA FLEET MO-32-33 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-33 - Free Fall Extension
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-32-33 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-42 - Normal Braking
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-42-01A Main Wheel Brake

Ident.: MO-32-42-00009004.0024001 / 18 JUL 14
Applicable to: MSN 4758-5364

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 Single.
The following penalties may be used for takeoff and landing performance determination if no
takeoff and landing data (predetermined by using OCTOPUS program or other equivalent program
with present failure case) is available.
Takeoff performance computation:
The method explained hereafter allows the determination of the MTOW and associated
speeds (V1, VR, V2), by applying decrements on the MTOW and associated speeds
computed in normal conditions (i.e. all systems operative). The method is based on the use of
RTOW charts established at optimum V2/VS, optimum V1/VR, minimum V1.
WARNING Do not use this method with takeoff charts computed with other conditions.
Do not use this method for takeoff with tailwind.
Do not use this method for takeoff on wet or contaminated runways.
How to proceed ?
Read, in 0 kt wind column of the takeoff chart computed in normal condition, the MTOW
and associated speeds (V1, VR, V2) corresponding to the actual temperature, even in the
case of headwind (the method does not take into account the headwind benefit on takeoff
performance).
Apply the QNH and/or bleed corrections, if any, to determine the MTOW.
Enter the following table to determine the MTOW and speed decrements.
Applying these decrements, calculate the MTOW and associated speeds corresponding to
the actual temperature.
CAUTION Do not extrapolate below the shortest runway length provided by the table.
DECREMENTS (W, V1, VR, V2) WHEN ONE BRAKE IS INOPERATIVE
CONFIGURATION
RUNWAY 1+F 2 3
LENGTH (m) W (kg/lb) V1 VR V2 W (kg/lb) V1 VR V2 W (kg/lb) V1 VR V2
(kt) (kt) (kt) (kt) (kt) (kt) (kt) (kt) (kt)
1 500 2 700/5 900 7 2 2 3 200/7 000 8 3 3 3 000/6 600 8 2 2
2 000 3 600/7 900 8 2 2 3 800/8 300 8 3 3 3 100/6 800 8 3 3
2 500 5 600/12 300 16 5 5 5 100/11 200 15 5 5 4 800/10 500 16 5 5
Continued on the following page

LAN COLOMBIA FLEET MO-32-42 P 1/8

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-42 - Normal Braking
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

DECREMENTS (W, V1, VR, V2) WHEN ONE BRAKE IS INOPERATIVE
CONFIGURATION
RUNWAY 1+F 2 3
LENGTH (m) W (kg/lb) V1 VR V2 W (kg/lb) V1 VR V2 W (kg/lb) V1 VR V2
(kt) (kt) (kt) (kt) (kt) (kt) (kt) (kt) (kt)
3 000 9 900/21 800 16 10 10 7 200/15 800 17 7 7 5 100/11 200 21 8 8
3 500 9 300/20 500 17 15 15 7 400/16 300 19 19 19 6 800/14 900 20 14 14
4 000 and
9 800/21 600 15 13 13 7 200/15 800 20 21 21 6 500/14 300 19 17 17
above
If the actual TOW is lower than the MTOW calculated using above method:
The speeds determined without failure and associated with the actual TOW may be
retained provided that they are all lower than the speeds calculated using above method.
Check that the corrected V1 is equal to or above the minimum V1 value shown on the RTOW
chart (due to VMCG limitation).
If the corrected V1 is lower than the minimum V1:
Take this last value as V1.
Further decrease the weight by 3 000 kg (6 600 lb) per kt difference between both values.
Check that the corrected VR is equal to or above the minimum VR value shown on the RTOW
chart (due to VMCA limitation).
If the corrected VR is lower than the minimum VR:
Takeoff cannot be performed using this method.
Check that the corrected V2 is equal to or above the minimum V2 value shown on the RTOW
chart (due to VMCA limitation).
If the corrected V2 is lower than the minimum V2:
Takeoff cannot be performed using this method.
Check that the corrected V2 is equal to or above the minimum V2 due to VMU limitation (see
Refer to FCOM/ MINIMUM V2 LIMITED BY VMU/VMCA (KT IAS)).
If the corrected V2 is lower than the minimum V2:
Takeoff cannot be performed using this method.
Landing performance computation:
Multiply the landing distances by 1.20.
Continued on the following page

LAN COLOMBIA FLEET MO-32-42 P 2/8

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-42 - Normal Braking
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

FOR TAKEOFF
The autobrake function, even if available, must not be used.
If the above method was used for takeoff performance computation:
Perform the takeoff using full thrust (TOGA).
In the case of engine failure at takeoff:
Retract the landing gear when positive climb.
Vibrations may occur during 1 or 2 min after the retraction of the landing gear.
If both engines are operative:
Keep the landing gear down for 1 min.
FOR LANDING
The autobrake function, even if available, must not be used.

32-42-01A Main Wheel Brake

Ident.: MO-32-42-00009004.0170001 / 27 NOV 12
Applicable to: MSN 4516-4546

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 Single.
The following penalties may be used for takeoff and landing performance determination if no
takeoff and landing data (predetermined by using OCTOPUS program or other equivalent program
with present failure case) is available.
Takeoff performance computation:
The method explained hereafter allows the determination of the MTOW and associated
speeds (V1, VR, V2), by applying decrements on the MTOW and associated speeds
computed in normal conditions (i.e. all systems operative). The method is based on the use of
RTOW charts established at optimum V2/VS, optimum V1/VR, minimum V1.
WARNING Do not use this method with takeoff charts computed with other conditions.
Do not use this method for takeoff with tailwind.
Do not use this method for takeoff on wet or contaminated runways.
Continued on the following page

LAN COLOMBIA FLEET MO-32-42 P 3/8

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-42 - Normal Braking
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

How to proceed ?
Read, in 0 kt wind column of the takeoff chart computed in normal condition, the MTOW
and associated speeds (V1, VR, V2) corresponding to the actual temperature, even in the
case of headwind (the method does not take into account the headwind benefit on takeoff
performance).
Apply the QNH and/or bleed corrections, if any, to determine the MTOW.
Enter the following table to determine the MTOW and speed decrements.
Applying these decrements, calculate the MTOW and associated speeds corresponding to
the actual temperature.
CAUTION Do not extrapolate below the shortest runway length provided by the table.
DECREMENTS (W, V1, VR, V2) WHEN ONE BRAKE IS INOPERATIVE
CONFIGURATION
RUNWAY 1+F 2 3
LENGTH (m) W V1 VR V2 W V1 VR V2 W V1 VR V2
kg (lb) (kt) (kt) (kt) kg (lb) (kt) (kt) (kt) kg (lb) (kt) (kt) (kt)
3 000 3 000 2 600
1 500 (6 700) 7 2 2 (6 700) 7 2 2 (5 800) 7 2 2
3 200 3 200 3 000
2 000 (7 100) 7 2 2 (7 100) 7 2 2 (6 700) 7 2 2
5 000 4 200 4 600
2 500 (11 100) 14 5 5 (9 300) 12 4 4 (10 200) 12 4 4
9 600 8 400 6 800
3 000 (21 200) 15 10 10 (18 600) 16 9 9 (15 000) 19 12 12
13 000 9 400 6 800
3 500 (28 700) 11 9 9 (20 800) 15 14 14 (15 000) 19 17 17
4 000 11 600 9 600 6 100
13 12 12 17 14 14 19 17 17
and above (25 600) (21 200) (13 500)

If the actual TOW is lower than the MTOW calculated using above method:
The speeds determined without failure and associated with the actual TOW may be
retained provided that they are all lower than the speeds calculated using above method.
Check that the corrected V1 is equal to or above the minimum V1 value shown on the RTOW
chart (due to VMCG limitation).
If the corrected V1 is lower than the minimum V1:
Take this last value as V1.
Further decrease the weight by 3 000 kg (6 600 lb) per kt difference between both values.
Continued on the following page

LAN COLOMBIA FLEET MO-32-42 P 4/8

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-42 - Normal Braking
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Check that the corrected VR is equal to or above the minimum VR value shown on the RTOW
chart (due to VMCA limitation).
If the corrected VR is lower than the minimum VR:
Takeoff cannot be performed using this method.
Check that the corrected V2 is equal to or above the minimum V2 value shown on the RTOW
chart (due to VMCA limitation).
If the corrected V2 is lower than the minimum V2:
Takeoff cannot be performed using this method.
Check that the corrected V2 is equal to or above the minimum V2 due to VMU limitation (see
Refer to FCOM/ MINIMUM V2 LIMITED BY VMU/VMCA (KT IAS)).
If the corrected V2 is lower than the minimum V2:
Takeoff cannot be performed using this method.
Landing performance computation:
Multiply the landing distances by 1.20.
FOR TAKEOFF
The autobrake function, even if available, must not be used.
If the above method was used for takeoff performance computation:
Perform the takeoff using full thrust (TOGA).
In the case of engine failure at takeoff:
Retract the landing gear when positive climb.
Vibrations may occur during 1 or 2 min after the retraction of the landing gear.
If both engines are operative:
Keep the landing gear down for 1 min.
FOR LANDING
The autobrake function, even if available, must not be used.

LAN COLOMBIA FLEET MO-32-42 P 5/8

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-42 - Normal Braking
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-42-01A Main Wheel Brake

Ident.: MO-32-42-00009004.0236001 / 27 FEB 15
Applicable to: MSN 5443-5453

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 Single.
Takeoff performance computation:
The takeoff and landing performance must be determined by using OCTOPUS program or
other equivalent program with present failure case taken into account.

Launch PEP.
Landing performance computation
Multiply the landing distances by 1.20.
FOR TAKEOFF
The autobrake function, even if available, must not be used.
In the case of engine failure at takeoff:
Retract the landing gear when positive climb.
Vibrations may occur during 1 or 2 min after the retraction of the landing gear.
If both engines are operative:
Keep the landing gear down for 1 min.
FOR LANDING
The autobrake function, even if available, must not be used.

32-42-02A Green System Brake

Ident.: MO-32-42-00009005.0001001 / 11 MAR 10
Applicable to: ALL

Refer to OpsProc 32-42-01A Main Wheel Brake

LAN COLOMBIA FLEET MO-32-42 P 6/8

MEL A to B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-42 - Normal Braking
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-42-05A AUTO/BRK Function

Ident.: MO-32-42-00009006.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 SINGLE.
BEFORE TAKEOFF
When T.O MEMO is displayed on the EWD, disregard the line:
AUTO BRK....................................................................................................................... MAX (blue)

LAN COLOMBIA FLEET MO-32-42 P 7/8

MEL C 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-42 - Normal Braking
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-32-42 P 8/8

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-47 - Brake Temperature System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-47-01A Brake Temperature Monitoring Unit ( BTMU )

Ident.: MO-32-47-00009008.0001001 / 12 SEP 11
Applicable to: ALL

DURING PRELIMINARY COCKPIT PREPARATION

HYDRAULIC/BRK/TEMP/DET/UNIT (121VU M26 or M37) C/B .............................................. PULL
Determine brake cooling time ( Refer to OpsProc 32-07-01A(B) Brakes Temperature Indication on
the WHEEL SD page ).

LAN COLOMBIA FLEET MO-32-47 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-47 - Brake Temperature System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-32-47 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-51 - Steering
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-51-01A Nose Wheel Steering Control System

Ident.: MO-32-51-00009009.0006001 / 27 FEB 15
Applicable to: MSN 4758-5453

GENERAL INFORMATION
The electrical and hydraulic control of NWS is inoperative. Do not reset the WHEEL N/W STRG
FAULT alert with A/SKID & N/W STRG selector . The WHEEL N/W STRG FAULTalert indicates
that no hydraulic pressure is applied on the NWS actuator.
FLIGHT PREPARATION/LIMITATIONS
Dispatch is not permitted from (or to) contaminated runways.
Maximum crosswind component for takeoff and landing: 20 kt.
Maximum landing capability is CAT 3 SINGLE.
Note: the automatic roll out is not permitted (Refer to QRH/ Required Equipment for CAT2 and
CAT3).
For operations with crosswind component above 5 kt:
Reduce maximum takeoff performance limiting weight by 1 000 kg (2 200 lb)
DURING TAXI
Taxiing Procedure:
Avoid high thrust settings, taxi speed limited to 20 kt .
Check brakes temperature (if available) before takeoff.
If necessary, set the BRAKES FAN pb-sw to ON.
Minimum speed of 5 kt is required to initiate a turn.
Apply asymmetrical thrust in straight taxi to compensate crosswind and differential braking for
taxi and line up as required.
Avoid sharp turns and use maximum width of the runway.
Do not apply too high asymmetrical thrust to avoid that nose landing gear get stuck to full travel
(90 ) (in that case release the aircraft by towing).
FOR TAKEOFF
In the case of crosswind component above 5 kt:
Set full nose down elevator till 80 kt regardless of the aircraft loading.
Apply N1 = 50 % on the brakes
Release the brakes, and smoothly apply takeoff power
Use asymmetric braking, if required, to keep on runway center-line until directional control
is available by use of rudder.
Release stick progressively to reach neutral at about 100 kt.
Continued on the following page

LAN COLOMBIA FLEET MO-32-51 P 1/6

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-51 - Steering
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

FOR LANDING
Do not use autobrake for landing.
In the case of crosswing component above 5 kt:
Aircraft lateral control is achieved with the rudder until slowing to approximately 50 kt IAS.
Upon reaching 50 kt IAS use differential braking to achieve taxi speed as required.
AFTER LANDING
Disengage AP at touchdown when autoland is performed.

32-51-01A Nose Wheel Steering Control System

Ident.: MO-32-51-00009009.0005001 / 10 OCT 14
Applicable to: MSN 4516-4546

GENERAL INFORMATION
The electrical and hydraulic control of NWS is inoperative. Do not reset the WHEEL N/W STRG
FAULT alert with A/SKID & N/W STRG selector . The WHEEL N/W STRG FAULTalert indicates
that no hydraulic pressure is applied on the NWS actuator.
FLIGHT PREPARATION/LIMITATIONS
Dispatch is not permitted from (or to) contaminated runways.
Maximum crosswind component for takeoff and landing: 20 kt.
Maximum landing capability is CAT 3 SINGLE.
Note: the automatic roll out is not permitted (Refer to QRH/ Required Equipment for CAT2 and
CAT3).
For operations with crosswind component above 5 kt:
Reduce maximum takeoff performance limiting weight by 1 000 kg (2 200 lb)
Continued on the following page

LAN COLOMBIA FLEET MO-32-51 P 2/6

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-51 - Steering
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

DURING TAXI
Taxiing Procedure:
Avoid high thrust settings, taxi speed limited to 20 kt .
Check brakes temperature (if available) before takeoff.
If necessary, set the BRAKES FAN pb-sw to ON.
Minimum speed of 5 kt is required to initiate a turn.
Apply asymmetrical thrust in straight taxi to compensate crosswind and differential braking for
taxi and line up as required.
Avoid sharp turns and use maximum width of the runway.
Do not apply too high asymmetrical thrust to avoid that nose landing gear get stuck to full travel
(90 ) (in that case release the aircraft by towing).
FOR TAKEOFF
In the case of crosswind component above 5 kt:
Set full nose down elevator till 80 kt regardless of the aircraft loading.
Apply EPR = 1.05 on the brakes
Release the brakes, and smoothly apply takeoff power
Use asymmetric braking, if required, to keep on runway center-line until directional control
is available by use of rudder.
Release stick progressively to reach neutral at about 100 kt.
FOR LANDING
Do not use autobrake for landing.
In the case of crosswing component above 5 kt:
Aircraft lateral control is achieved with the rudder until slowing to approximately 50 kt IAS.
Upon reaching 50 kt IAS use differential braking to achieve taxi speed as required.
AFTER LANDING
Disengage AP at touchdown when autoland is performed.

32-51-02A Rudder PEDALS DISC pb

Ident.: MO-32-51-00012799.0001001 / 17 SEP 10
Applicable to: ALL

The purpose of the procedure is to explain how to perform the flight control check with one or both
PEDALS DISC pb failed in the released position.
Continued on the following page

LAN COLOMBIA FLEET MO-32-51 P 3/6

MEL A to B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-51 - Steering
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

GENERAL INFORMATION
When the disconnection is not possible on one side:
The flight control check can be performed on the operative side.
When the disconnection is not possible on both sides:
The flight control check must be performed while aircraft is stopped.
Note: it is not necessary to set the A/SKID & N/W STRG sw to OFF.

NWS Electrical Deactivation Box (towing mode is not

32-51-03A
available when the lever is in the TOWING position)
Ident.: MO-32-51-00009010.0001001 / 17 SEP 10
Applicable to: ALL

BEFORE CONVENTIONAL OR TOWLESS PUSHBACK

A/SKID & N/W STRG selector ................................................................................................... OFF
AFTER PUSHBACK
A/SKID & N/W STRG selector .....................................................................................................ON

NWS Electrical Deactivation Box (NWS

32-51-03B
Electrical Deactivation Box deactivated)
Ident.: MO-32-51-00012592.0001001 / 17 SEP 10
Applicable to: ALL

BEFORE CONVENTIONAL OR TOWLESS PUSHBACK

A/SKID & N/W STRG selector ................................................................................................... OFF
As a result of the NWS electrical box deactivation, the parking brake light on that box will not be
available.
The parking brake setting must be verbally confirmed between the flight crew and the ground
personnel before pushback.
AFTER PUSHBACK
A/SKID & N/W STRG selector .....................................................................................................ON

LAN COLOMBIA FLEET MO-32-51 P 4/6

MEL B to D 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-51 - Steering
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

32-51-04A PARKING BRAKE light on the NWS Electrical Deactivation Box

Ident.: MO-32-51-00009011.0001001 / 17 SEP 10
Applicable to: ALL

BEFORE PUSHBACK
The parking brake setting must be verbally confirmed between the flight crew and the ground
personnel.

LAN COLOMBIA FLEET MO-32-51 P 5/6

MEL E 27 FEB 15
 MEL OPERATIONAL PROCEDURES
32 - LANDING GEAR
32-51 - Steering
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-32-51 P 6/6

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
33 - LIGHTS
33-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 33-01-02 - SIGNS Overhead Panel
MINIMUM EQUIPMENT LIST

33-01-02-02A AUTO Function of SEAT BELTS SIGNS selector

Ident.: MO-33-01-02-00008954.0001001 / 18 MAY 11
Applicable to: ALL

DURING COCKPIT PREPARATION

SEAT BELTS selector ..................................................................................................................ON
AFTER TAKEOFF
SEAT BELTS selector .................................................................................................... As required
DURING APPROACH
SEAT BELTS selector ..................................................................................................................ON

33-01-02-03A AUTO Function of NO SMOKING SIGNS selector

Ident.: MO-33-01-02-00008955.0001001 / 11 MAR 10
Applicable to: ALL

ON GROUND OR IN FLIGHT
Set the NO SMOKING selector ON as required.

LAN COLOMBIA FLEET MO-33-01-02 P 1/2

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
33 - LIGHTS
33-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 33-01-02 - SIGNS Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-33-01-02 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
33 - LIGHTS
33-20 - Cabin Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

33-20-03A Lavatory Sign (Return to seat)

Ident.: MO-33-20-00008956.0001001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Check that the passenger address function is operative in the affected lavatory with the door
closed.

LAN COLOMBIA FLEET MO-33-20 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
33 - LIGHTS
33-20 - Cabin Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-33-20 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
33 - LIGHTS
33-40 - Exterior Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

33-40-04A Landing light Extension/Retraction System

Ident.: MO-33-40-00008957.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
The fuel consumption is increased by 1 % per landing light extended.

33-40-08A
Beacon light
33-40-08B
Ident.: MO-33-40-00008958.0001001 / 11 MAR 10
Applicable to: ALL

BEFORE ENGINE START

If the bottom light is inoperative:
If this light is used to alert the ground crew of the engine start, an alternate procedure must be
established by each airline to alert the ground crew of the engine start.

LAN COLOMBIA FLEET MO-33-40 P 1/2

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
33 - LIGHTS
33-40 - Exterior Lighting
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-33-40 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 34-01-01 - ADIRS Overhead Panel
MINIMUM EQUIPMENT LIST

34-01-01-31A ADR pb-sw

Ident.: MO-34-01-01-00008926.0001001 / 17 SEP 10
Applicable to: ALL

IN FLIGHT
If needed, the associated ADR can be set to OFF through the associated mode selector.
Note: If the ADR is set to OFF:
The associated IR is also set to OFF.
The F/CTL MAINTENANCE message is displayed on the STATUS SD page.

34-01-01-32A IR pb-sw
Ident.: MO-34-01-01-00008927.0001001 / 27 FEB 15
Applicable to: ALL

IN FLIGHT
If needed, the associated IR can be set to OFF through the associated mode selector.
Note: If the IR is set to OFF:
The associated ADR is also set to OFF.
The F/CTL MAINTENANCE message is displayed on the STATUS SD page.

LAN COLOMBIA FLEET MO-34-01-01 P 1/2

MEL A to B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 34-01-01 - ADIRS Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-34-01-01 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-05 - Indications on the Primary Flight Display (PFD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-05-07A Other Air Data Related Indications on the PFD

Ident.: MO-34-05-00008951.0001001 / 18 JUL 14
Applicable to: ALL

GENERAL INFORMATION
For F, S, Green Dot determination, Refer to QRH/PER-A Speeds.
For VAPP determination, Refer to QRH/PER-C VAPP Determination without Failure and Refer to
QRH/PER-C VAPP Determination with Failure.
For VFE or VLE determination, refer to the corresponding placard in the cockpit.

34-05-08A Attitude Indication on the PFD

Ident.: MO-34-05-00008953.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 1.

LAN COLOMBIA FLEET MO-34-05 P 1/2

MEL A to B 20 JUN 14
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-05 - Indications on the Primary Flight Display (PFD)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-34-05 P 2/2

MEL 20 JUN 14
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-10 - Air Data/Inertial Reference System (ADIRS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-10-02B ADR 2
Ident.: MO-34-10-00008928.0003001 / 27 FEB 15
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 SINGLE.
DURING COCKPIT PREPARATION
ADR 2 pb-sw ......................................................................................................................... OFF
The F/CTL MAINTENANCE message is displayed on the STATUS SD page.
AIR DATA SWITCHING selector .........................................................................................F/O 3
ADIRS/ADIRU/2/26VAC AND AOA (location 121VU N08 or N09) C/B .................................. Pull
AFTER ENGINE START
Use the RCL pb-sw on the ECAM control panel, in order to recall the NAV ADR 2 FAULT alert.
On the EWD, check that the ADR 2...OFF procedure is not displayed.
FOR TAKEOFF
Takeoff in CONF 1+F is not permitted.
Note: When the ADR 2 pb-sw is set to OFF, and if the aircraft is in CONF 1+F, the SFCS
n2 Flap channel is unable to crosscheck the airspeed coming from the ADR 1 with
the ADR 2 airspeed coming from the SFCS n2 Slat channel. This may lead to an
uncommanded flap retraction during the takeoff. As a consequence, takeoff in CONF 1+F
is not permitted when the ADR 2 pb-sw is set to OFF.

34-10-03A ADR 3
Ident.: MO-34-10-00008929.0001001 / 17 SEP 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 SINGLE.
DURING COCKPIT PREPARATION
ADR 3 pb-sw ......................................................................................................................... OFF
The F/CTL MAINTENANCE message is displayed on the STATUS SD page.
ADIRS/ADIRU/3/26VAC AND AOA (location 121VU N07 or N08) C/B .................................. Pull
Continued on the following page

LAN COLOMBIA FLEET MO-34-10 P 1/4

MEL A to B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-10 - Air Data/Inertial Reference System (ADIRS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

AFTER ENGINE START
Use the RCL pb-sw on the ECAM control panel, in order to recall the NAV ADR 3 FAULT alert.
On the EWD, check that the ADR 3...OFF procedure is not displayed.

34-10-04B
IR 1 (only NAV mode of IR 1 inoperative)
34-10-04C
Ident.: MO-34-10-00008930.0002001 / 27 FEB 15
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 SINGLE.
DURING COCKPIT PREPARATION
ATT HDG SWITCHING selector ...................................................................................... CAPT 3
IR 1 mode selector ................................................................................................................ ATT
The heading must be entered through the MCDU for the IR 1 and has to be frequently reset
(Refer to FCOM/ IR ALIGNMENT IN ATT MODE).

34-10-05B IR 2 (IR 2 totally inoperative)

Ident.: MO-34-10-00008931.0004001 / 27 FEB 15
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 SINGLE.
1
DURING COCKPIT PREPARATION
IR 2 pb-sw ............................................................................................................................. OFF
The F/CTL MAINTENANCE message is displayed on the STATUS SD page.
ATT HDG SWITCHING selector ..........................................................................................F/O 3
AIR DATA SWITCHING selector .........................................................................................F/O 3
Note: When the ADR 2 is inoperative and if the IR 2 pb-sw OFF light does not come on:
Set the IR 2 mode selector to OFF.

If the ADS-B OUT function is required for the intended route:

ATC selector ............................................................................................................................. 1

LAN COLOMBIA FLEET MO-34-10 P 2/4

MEL B to D 27 FEB 15
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-10 - Air Data/Inertial Reference System (ADIRS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-10-05C IR 2 (only NAV mode of IR 2 inoperative)

Ident.: MO-34-10-00008932.0002001 / 27 FEB 15
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 SINGLE.
DURING COCKPIT PREPARATION
ATT HDG SWITCHING selector ..........................................................................................F/O 3
IR 2 mode selector ................................................................................................................ ATT
The heading must be entered through the MCDU keyboard for the IR 2 and has to be frequently
reset (Refer to FCOM/ IR ALIGNMENT IN ATT MODE).

34-10-06A IR 3 ADIRU with IR 3 totally inoperative)

Ident.: MO-34-10-00008933.0002001 / 27 FEB 15
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 SINGLE.
2
DURING COCKPIT PREPARATION
IR 3 pb-sw ..................................................................................................................................OFF
The F/CTL MAINTENANCE is displayed on the STATUS SD page.
Note: When the ADR 3 is inoperative and if the IR 3 pb-sw OFF light does not come on:
Set the IR 3 mode selector to OFF.

34-10-06B IR 3 (ADIRU with only NAV mode of IR 3 inoperative)

Ident.: MO-34-10-00008934.0002001 / 27 FEB 15
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 3 SINGLE.
Continued on the following page

LAN COLOMBIA FLEET MO-34-10 P 3/4

MEL E to G 27 FEB 15
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-10 - Air Data/Inertial Reference System (ADIRS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

DURING COCKPIT PREPARATION
IR 3 mode selector ................................................................................................................ ATT
The heading must be entered through the MCDU for the IR 3 and has to be frequently reset
(Refer to FCOM/ IR ALIGNMENT IN ATT MODE).

LAN COLOMBIA FLEET MO-34-10 P 4/4

MEL G 27 FEB 15
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-11 - Sensors
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

CAPT Total Air Temperature ( TAT )

34-11-02A
Sensor Element Connected to ADR 1
Ident.: MO-34-11-00008937.0001001 / 11 MAR 10
Applicable to: ALL

Refer to OpsProc 31-07-02A Permanent Data Indications on the SD

CAPT Total Air Temperature (TAT)

34-11-03A
Sensor Element Connected to ADR 3
Ident.: MO-34-11-00008938.0001001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Check that the TAT is displayed on the SD permanent data.

34-11-04A F/O Total Air Temperature ( TAT ) Sensor Element Connected to ADR 2
Ident.: MO-34-11-00008939.0001001 / 11 MAR 10
Applicable to: ALL

Refer to OpsProc 31-07-02A Permanent Data Indications on the SD

LAN COLOMBIA FLEET MO-34-11 P 1/2

MEL A to C 05 NOV 13
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-11 - Sensors
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-34-11 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-22 - Attitude and Heading Standby Data
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-22-01B Standby Compass Indicator

Ident.: MO-34-22-00008941.0001001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Check of the ATT HDG, PFD/ND, and EIS DMC switching:
ATT HDG SWITCHING selector ...................................................................................... CAPT 3
Check that the display is normal on the CAPT PFD, the CAPT ND, and the RMI VOR.
ATT HDG SWITCHING selector ..........................................................................................F/O 3
Check that the display is normal on the F/O PFD and the F/O ND.
ATT HDG SWITCHING selector ........................................................................................NORM
EIS DMC SWITCHING selector .......................................................................................CAPT 3
Check that the display is normal on the CAPT PFD and the CAPT ND.
EIS DMC SWITCHING selector .......................................................................................... F/O 3
Check that the display is normal on the F/O PFD and the F/O ND.
EIS DMC SWITCHING selector .........................................................................................NORM
CAPT PFD/ND XFR pb ....................................................................................................... Press
Check that the CAPT PFD and the CAPT ND images are exchanged.
CAPT PFD/ND XFR pb ....................................................................................................... Press
F/O PFD/ND XFR pb ...........................................................................................................Press
Check that the F/O PFD and the F/O ND images are exchanged.
F/O PFD/ND XFR pb ...........................................................................................................Press

LAN COLOMBIA FLEET MO-34-22 P 1/2

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-22 - Attitude and Heading Standby Data
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-34-22 P 2/2

MEL 10 OCT 14
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-23 - Integrated Standby Instrument System (ISIS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

ISIS Attitude Indication

Ident.: MO-34-23-00008943.0002001 / 27 FEB 15
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 1.

LAN COLOMBIA FLEET MO-34-23 P 1/2

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-23 - Integrated Standby Instrument System (ISIS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-34-23 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-30 - Landing and Taxiing Aid
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-30-04A Instrument Landing System (ILS)

Ident.: MO-34-30-00008944.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
When one ILS is inoperative:
Maximum landing capability is ILS CAT 1.
When both ILS are inoperative:
CAT 1 ILS approaches are not permitted.

LAN COLOMBIA FLEET MO-34-30 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-30 - Landing and Taxiing Aid
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-34-30 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-40 - GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-40-02A Radio Altimeter Automatic Callout

Ident.: MO-34-40-00008946.0001001 / 17 SEP 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 2 without autoland.

34-40-03A Radio Altimeter System

Ident.: MO-34-40-00008947.0001001 / 10 OCT 14
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Maximum landing capability is CAT 2.
The F/CTL MAINTENANCE message is displayed on the STATUS SD page.
DURING COCKPIT PREPARATION
If RA 1 is inoperative:
COM NAV/RAD ALTM/1 (121VU K11) C/B ..........................................................................Pull
If RA 2 is inoperative:
COM NAV/RAD ALTM/2 (121VU K12) C/B ..........................................................................Pull
DURING APPROACH
During an ILS (or MLS, or GLS) approach with AP engaged, the flight crew must closely monitor
all primary flight parameters and FMA indications. An early/untimely FLARE and THR IDLE mode
engagement may occur in the case of an erroneous RA height indication from the remaining RA.
In the event of an early/untimely FLARE and THR IDLE mode engagement:
Immediately perform an automatic go-around (thrust levers set to TOGA),
OR
Immediately disconnect AP and set both FDs to OFF. If external visual references are
sufficient, the approach may be continued manually.
Note: If the flight crew does not immediately react, the angle-of-attack will increase and may
reach the stall value,
In CONF FULL, the auto-trim function is inhibited. In manual flight, a significant
longitudinal sidestick input may be required.

LAN COLOMBIA FLEET MO-34-40 P 1/2

MEL A to B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-40 - GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-40-07A PULL UP-GPWS pb-sw

Ident.: MO-34-40-00008949.0002001 / 27 FEB 15
Applicable to: ALL

DURING COCKPIT PREPARATION

Check of the GPWS (or TAWS) aural and visual warnings:
PULL UP GPWS pb-sw (operative)...................................................................................Press
Check that the GPWS (or the TAWS) aural and visual warnings are operative. Refer to
FCOM/DSC-34-70 GPWS.

LAN COLOMBIA FLEET MO-34-40 P 2/2

MEL C 27 FEB 15
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-50 - ATC and Radio/GPS Navigation Systems
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

34-50-01A ATC
Ident.: MO-34-50-00008950.0001001 / 11 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
When both ATCs are inoperative, RVSM operations are not permitted.

LAN COLOMBIA FLEET MO-34-50 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
34 - NAVIGATION
34-50 - ATC and Radio/GPS Navigation Systems
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-34-50 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
35 - OXYGEN
35-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 35-01-01 - OXYGEN Overhead Panel
MINIMUM EQUIPMENT LIST

35-01-01-31B MANUAL Control of the MASK MAN ON pb

Ident.: MO-35-01-01-00008882.0001001 / 27 FEB 15
Applicable to: ALL
1
FLIGHT PREPARATION/LIMITATIONS
The flight crew shall brief the cabin crew on the alternate emergency procedures that will be
used.
The affected occupants are briefed appropriately.
The quantity of oxygen needed for the intended flight is in accordance with PART
CAT.IDE.A.235.

35-01-01-33A HI ALT LANDING pb-sw

Ident.: MO-35-01-01-00008884.0001001 / 27 FEB 15
Applicable to: ALL

ON GROUND
Inform the cabin crew that if the cabin altitude exceeds 12 500 ft, the oxygen masks may drop
down.

LAN COLOMBIA FLEET MO-35-01-01 P 1/2

MEL A to B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
35 - OXYGEN
35-01 - Overhead Panels
COLOMBIA
LAN COLOMBIA AIRLINES 35-01-01 - OXYGEN Overhead Panel
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-35-01-01 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
35 - OXYGEN
35-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

35-07-01A Crew OXY High Pressure Indication on the DOOR/OXY SD page

Ident.: MO-35-07-00008921.0001001 / 12 SEP 11
Applicable to: ALL

DURING COCKPIT PREPARATION

After application of the maintenance procedure:
Check that the oxygen pressure is sufficient for the intended flight. Refer to FCOM/ Cockpit
Fixed Oxygen System.

35-07-02A Crew Oxygen REGUL LO PR Indication on the DOOR/OXY SD page

Ident.: MO-35-07-00008924.0001001 / 11 MAR 10
Applicable to: ALL

GENERAL INFORMATION
On the DOOR/OXY SD page, disregard the REGUL LO PR indication and the associated OXY
indication.

LAN COLOMBIA FLEET MO-35-07 P 1/2

MEL A to B 05 NOV 13
 MEL OPERATIONAL PROCEDURES
35 - OXYGEN
35-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-35-07 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
35 - OXYGEN
35-10 - Crew Oxygen
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

35-10-03A Exterior Crew Oxygen Overpressure Indicator Disc (Green Disc)

Ident.: MO-35-10-00008910.0001001 / 11 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Before the first flight of each day, check that the oxygen pressure does not decrease:
On the DOOR/OXY SD page, check the OXY pressure indication twice.
A 15 min interval must be applied between both checks.

LAN COLOMBIA FLEET MO-35-10 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
35 - OXYGEN
35-10 - Crew Oxygen
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-35-10 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
35 - OXYGEN
35-20 - Passenger Oxygen
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

35-20-01B Passenger Oxygen Unit

Ident.: MO-35-20-00008911.0001001 / 27 FEB 15
Applicable to: ALL
1
FLIGHT PREPARATION/LIMITATIONS
The flight crew shall brief the cabin crew on the alternate emergency procedures that will be
used.
The affected occupants are briefed appropriately.
The quantity of oxygen needed for the intended flight is in accordance with PART
CAT.IDE.A.235.

35-20-02B Cabin Attendant Oxygen Unit

Ident.: MO-35-20-00008912.0001001 / 27 FEB 15
Applicable to: ALL
2
FLIGHT PREPARATION/LIMITATIONS
The flight crew shall brief the cabin crew on the alternate emergency procedures that will be
used.
The quantity of oxygen needed for the intended flight is in accordance with PART
CAT.IDE.A.235.

Galley Oxygen Unit (cabin attendant

35-20-04A
oxygen unit available near the galley)
Ident.: MO-35-20-00008914.0001001 / 11 MAR 10
Applicable to: ALL

IN FLIGHT
The number of galley area occupants must be in accordance with the available adjacent cabin
attendant oxygen units.

LAN COLOMBIA FLEET MO-35-20 P 1/2

MEL A to C 27 FEB 15
 MEL OPERATIONAL PROCEDURES
35 - OXYGEN
35-20 - Passenger Oxygen
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Galley Oxygen Unit (cabin attendant portable

35-20-04B
oxygen device available near the galley)
Ident.: MO-35-20-00008915.0001001 / 18 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
Before the flight, the flight crew shall brief the cabin crew that the galley oxygen unit is inoperative
and that the cabin attendant portable oxygen device should be used instead.

LAN COLOMBIA FLEET MO-35-20 P 2/2

MEL D 27 FEB 15
 MEL OPERATIONAL PROCEDURES
36 - PNEUMATIC
36-11 - Engine Bleed Air Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

36-11-01A
Engine Bleed Air Supply System (non-ETOPS flights)
36-11-01E
Ident.: MO-36-11-00008868.0001001 / 27 FEB 15
1 Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453

2
FLIGHT PREPARATION/LIMITATIONS
The flight crew should take into account the severity of forecast icing conditions. The wing anti-ice
will be lost if the remaining engine bleed air supply system becomes inoperative.
If the cargo heating is switched off:
For live animal transportation, use the Live Animal Transportation Calculation Tool.
AFTER ENGINE START
ENG BLEED (AFFECTED) pb-sw ......................................................................................... OFF
X BLEED rotary selector .................................................................................................... OPEN
If both PACKs are operative:
If Wing Anti-Ice is not required:
PACK FLOW selector ......................................................................................................LO
The PACK FLOW selector must be set to LO due to precooler performance.
AFT CARGO HOT AIR pb-sw ...............................................................................OFF
If Wing Anti-Ice is required:
PACK (AFFECTED) pb-sw ............................................................................................OFF
If one PACK is inoperative:
PACK FLOW selector ..............................................................................................................HI
FOR TAKEOFF
Set at least one air conditioning pack to off, or use the APU bleed air supply system.
AFTER TAKEOFF
If the APU has been used to supply the air conditioning during the takeoff:
APU BLEED pb-sw ................................................................................................................ Off
IN FLIGHT
If Wing Anti-Ice is required:
PACK (affected side) pb-sw ................................................................................................ OFF
Continued on the following page

LAN COLOMBIA FLEET MO-36-11 P 1/8

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
36 - PNEUMATIC
36-11 - Engine Bleed Air Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

In the case of failure of the remaining engine bleed air supply system, or in the case of
failure of the associated engine:
Apply the associated ECAM procedure, then
Refer to QRH/ AIR ENG 1+2 BLEED FAULT.

36-11-01A
Engine Bleed Air Supply System (non-ETOPS flights)
36-11-01E
Ident.: MO-36-11-00008868.0002001 / 27 FEB 15
3 Applicable to: MSN 4892-4943, 5229, 5263-5364

4
FLIGHT PREPARATION/LIMITATIONS
The flight crew should take into account the severity of forecast icing conditions. The wing anti-ice
will be lost if the remaining engine bleed air supply system becomes inoperative.
If the cargo heating is switched off:
For live animal transportation, use the Live Animal Transportation Calculation Tool.
AFTER ENGINE START
ENG BLEED (AFFECTED) pb-sw ......................................................................................... OFF
X BLEED rotary selector .................................................................................................... OPEN
If both PACKs are operative:
If Wing Anti-Ice is not required:
PACK FLOW selector ......................................................................................................LO
The PACK FLOW selector must be set to LO due to precooler performance.
AFT CARGO HOT AIR pb-sw ...............................................................................OFF
If Wing Anti-Ice is required:
PACK (AFFECTED) pb-sw ............................................................................................OFF
If one PACK is inoperative:
PACK FLOW selector ..............................................................................................................HI
FOR TAKEOFF
Set at least one air conditioning pack to off, or use the APU bleed air supply system.
AFTER TAKEOFF
If the APU has been used to supply the air conditioning during the takeoff:
APU BLEED pb-sw ................................................................................................................ Off
BLEED SD page ..................................................................................SELECT and MONITOR
Continued on the following page

LAN COLOMBIA FLEET MO-36-11 P 2/8

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
36 - PNEUMATIC
36-11 - Engine Bleed Air Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

If the precooler outlet temperature of the remaining bleed exceeds 240 C within 2 min
after the selection of both PACKs or the APU BLEED OFF:
PACK (affected side) pb-sw ................................................................................................ OFF
IN FLIGHT
If Wing Anti-Ice is required and both PACKs are operative::
PACK (affected side) pb-sw ................................................................................................ OFF
BLEED SD page ..................................................................................SELECT and MONITOR
If the precooler outlet temperature of the remaining bleed exceeds 240 C within
2 min after the selection of the Wing Anti-Ice ON:
BLEED AIR DEMAND............................................................................................ REDUCE
Consider reducing the bleed air demand by, depending on the flight conditions:
Switching OFF the remaining PACK (if aircraft's altitude permits), or
Switching OFF the Wing Anti-Ice (if no longer icing conditions).
In the case of failure of the remaining engine bleed air supply system, or in the case of
failure of the associated engine:
Apply the associated ECAM procedure, then
Refer to QRH/ AIR ENG 1+2 BLEED FAULT

Engine Bleed Air Supply System (ETOPS flights)

Ident.: MO-36-11-00008869.0002001 / 27 FEB 15
5 Applicable to: MSN 4892-4943, 5229, 5263-5364

6
FLIGHT PREPARATION/LIMITATIONS
APU fuel consumption with the APU ON (APU GEN OFF and APU BLEED OFF):
APU ON (IDLE)
FL GND 100 200 315 354 370 390
KG/H 80 60 42 28 24 22 20
LB/H 176 132 93 62 53 49 44

The flight crew should take into account the severity of forecast icing conditions. The wing anti-ice
will be lost if the remaining engine bleed air supply system becomes inoperative.
If the cargo heating is switched off:
For live animal transportation, use the Live Animal Transportation Calculation Tool.
Continued on the following page

LAN COLOMBIA FLEET MO-36-11 P 3/8

MEL A to B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
36 - PNEUMATIC
36-11 - Engine Bleed Air Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

AFTER ENGINE START
ENG BLEED (AFFECTED) pb-sw ......................................................................................... OFF
X BLEED rotary selector .................................................................................................... OPEN
If both PACKs are operative:
If Wing Anti-Ice is not required:
PACK FLOW selector ......................................................................................................LO
The PACK FLOW selector must be set to LO due to precooler performance.
AFT CARGO HOT AIR pb-sw ...............................................................................OFF
If Wing Anti-Ice is required:
PACK (AFFECTED) pb-sw ............................................................................................OFF
If one PACK is inoperative:
PACK FLOW selector ..............................................................................................................HI
BEFORE TAKEOFF
APU MASTER SW pb-sw ............................................................................................................ ON
FOR TAKEOFF
Set at least one air conditioning pack to off, or use the APU bleed air supply system.
AFTER TAKEOFF
If the APU has been used to supply the air conditioning during the takeoff:
APU BLEED pb-sw ................................................................................................................ Off
BLEED SD page ..................................................................................SELECT and MONITOR
If the precooler outlet temperature of the remaining bleed exceeds 240 C within 2 min
after the selection of both PACKs or the APU BLEED OFF:
PACK (affected side) pb-sw ................................................................................................ OFF
IN FLIGHT
If Wing Anti-Ice is required and both PACKs are operative::
PACK (affected side) pb-sw ................................................................................................ OFF
BLEED SD page ..................................................................................SELECT and MONITOR
Continued on the following page

LAN COLOMBIA FLEET MO-36-11 P 4/8

MEL B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
36 - PNEUMATIC
36-11 - Engine Bleed Air Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

If the precooler outlet temperature of the remaining bleed exceeds 240 C within
2 min after the selection of the Wing Anti-Ice ON:
BLEED AIR DEMAND............................................................................................ REDUCE
Consider reducing the bleed air demand by, depending on the flight conditions:
Switching OFF the remaining PACK (if aircraft's altitude permits), or
Switching OFF the Wing Anti-Ice (if no longer icing conditions).
In the case of failure of the remaining engine bleed air supply system, or in the case of
failure of the associated engine:
Apply the associated ECAM procedure, then
Refer to QRH/ AIR ENG 1+2 BLEED FAULT.

Engine Bleed Air Supply System (ETOPS flights)

Ident.: MO-36-11-00008869.0003001 / 27 FEB 15
7 Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453

8
FLIGHT PREPARATION/LIMITATIONS
APU fuel consumption with the APU ON (APU GEN OFF and APU BLEED OFF):
APU ON (IDLE)
FL GND 100 200 315 354 370 390
KG/H 80 60 42 28 24 22 20
LB/H 176 132 93 62 53 49 44

The flight crew should take into account the severity of forecast icing conditions. The wing anti-ice
will be lost if the remaining engine bleed air supply system becomes inoperative.
If the cargo heating is switched off:
For live animal transportation, use the Live Animal Transportation Calculation Tool.
AFTER ENGINE START
ENG BLEED (AFFECTED) pb-sw ......................................................................................... OFF
X BLEED rotary selector .................................................................................................... OPEN
If both PACKs are operative:
If Wing Anti-Ice is not required:
PACK FLOW selector ......................................................................................................LO
The PACK FLOW selector must be set to LO due to precooler performance.
AFT CARGO HOT AIR pb-sw ...............................................................................OFF
Continued on the following page

LAN COLOMBIA FLEET MO-36-11 P 5/8

MEL B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
36 - PNEUMATIC
36-11 - Engine Bleed Air Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

If Wing Anti-Ice is required:
PACK (AFFECTED) pb-sw ............................................................................................OFF
If one PACK is inoperative:
PACK FLOW selector ..............................................................................................................HI
BEFORE TAKEOFF
APU MASTER SW pb-sw ............................................................................................................ ON
FOR TAKEOFF
Set at least one air conditioning pack to off, or use the APU bleed air supply system.
AFTER TAKEOFF
If the APU has been used to supply the air conditioning during the takeoff:
APU BLEED pb-sw ................................................................................................................ Off
IN FLIGHT
If Wing Anti-Ice is required:
PACK (affected side) pb-sw ................................................................................................ OFF
In the case of failure of the remaining engine bleed air supply system, or in the case of
failure of the associated engine:
Apply the associated ECAM procedure, then
Refer to QRH/ AIR ENG 1+2 BLEED FAULT.

36-11-06B Engine Bleed IP Check Valve

Ident.: MO-36-11-00008870.0001001 / 27 FEB 15
Applicable to: ALL

DURING TAXI
When the engines operate in idle thrust:
ENG (affected side) BLEED pb-sw ....................................................................................... OFF
X BLEED selector ...............................................................................................................OPEN
If wing anti-ice is required:
One PACK pb-sw ................................................................................................................ OFF
Continued on the following page

LAN COLOMBIA FLEET MO-36-11 P 6/8

MEL B to C 27 FEB 15
 MEL OPERATIONAL PROCEDURES
36 - PNEUMATIC
36-11 - Engine Bleed Air Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

9
BEFORE TAKEOFF AND UNTIL DESCENT
Just before applying takeoff thrust
ENG (affected side) BLEED pb-sw ..........................................................................................On
X BLEED selector ............................................................................................................... AUTO
DURING DESCENT
When the engines operate in idle thrust:
ENG (affected side) BLEED pb-sw ....................................................................................... OFF
X BLEED selector ...............................................................................................................OPEN
If wing anti-ice is required:
One PACK pb-sw ................................................................................................................ OFF

36-11-07B Engine Bleed HP Valve

Ident.: MO-36-11-00008872.0001001 / 11 MAR 10
Applicable to: ALL

Refer to OpsProc 36-11-06B Engine Bleed IP Check Valve

LAN COLOMBIA FLEET MO-36-11 P 7/8

MEL C to D 27 FEB 15
 MEL OPERATIONAL PROCEDURES
36 - PNEUMATIC
36-11 - Engine Bleed Air Supply System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-36-11 P 8/8

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
36 - PNEUMATIC
36-12 - APU Bleed Air Supply and Crossbleed Systems
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

36-12-02B APU Bleed Valve

Ident.: MO-36-12-00008878.0001001 / 11 MAR 10
Applicable to: ALL

ON GROUND OR IN FLIGHT
When the APU runs:
APU BLEED pb-sw ................................................................................................................ON
After APU shutdown:
APU BLEED pb-sw ................................................................................................................ Off

36-12-04A Automatic control of the X Bleed Valve

Ident.: MO-36-12-00008879.0001001 / 12 MAR 10
Applicable to: ALL

DURING COCKPIT PREPARATION

Check of the manual control of the X BLEED valve:
X BLEED selector ...............................................................................................................OPEN
On the BLEED, check that the cross bleed valve is indicated open.
X BLEED selector ............................................................................................................... SHUT
On the BLEED, check that the cross bleed valve is indicated closed.
X BLEED selector ............................................................................................................... AUTO

36-12-05A Manual Control of the X Bleed Valve

Ident.: MO-36-12-00015757.0001001 / 27 FEB 15
Applicable to: ALL

DURING COCKPIT PREPARATION

X BLEED selector ....................................................................................................................AUTO
Check of the Manual Control of the X BLEED valve:
Check that the APU is started.
APU BLEED pb-sw .................................................................................................................. Off
On the BLEED SD page, check that the cross bleed valve is indicated closed.
APU BLEED pb-sw ..................................................................................................................ON
On the BLEED SD page, check that the cross bleed valve is indicated open.

LAN COLOMBIA FLEET MO-36-12 P 1/2

MEL A to C 27 FEB 15
 MEL OPERATIONAL PROCEDURES
36 - PNEUMATIC
36-12 - APU Bleed Air Supply and Crossbleed Systems
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-36-12 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
36 - PNEUMATIC
36-22 - Leak Detection Loop
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

36-22-03B
APU Leak Detection Loop
36-22-03C
Ident.: MO-36-22-00016005.0001001 / 27 FEB 15
Applicable to: ALL

DURING COCKPIT PREPARATION

ENG 1 BLEED pb-sw .................................................................................................................OFF
PACK 1 pb-sw ............................................................................................................................OFF
X BLEED selector ....................................................................................................................SHUT
APU BLEED pb-sw .................................................................................................................... OFF
Note: The use of the APU bleed air supply system for Main Engine Start is permitted.

IN FLIGHT
In the case of failure of the remaining engine bleed air supply system, or in the case of
failure of the associated engine:
Apply the associated ECAM procedure, then
Refer to QRH/ABN-36 AIR ENG 1+2 BLEED FAULT.

LAN COLOMBIA FLEET MO-36-22 P 1/2

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
36 - PNEUMATIC
36-22 - Leak Detection Loop
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-36-22 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
49 - AIRBORNE POWER UNIT
49-10 - Power Plant
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

49-10-01A
49-10-01B Power Plant (APU)
49-10-01C
Ident.: MO-49-10-00008864.0001001 / 27 FEB 15
Applicable to: ALL

GENERAL INFORMATION
No APU bleed air will be available for Main Engine Start (MES) or air conditioning.
No electrical power will be available from the APU generator.
In the case of both APU unserviceable and absence of suitable ground support equipment at
destination, an engine opposite to the refueling point will need to be operated during refueling to
ensure the continued availability of bleed air and electrical power for engine starting.
Refer to FCOM/PER-LOD-FUL REFUELING WITH ONE ENGINE RUNNING.
DURING COCKPIT PREPARATION
APU MASTER SW pb-sw .............................................................................................................Off

LAN COLOMBIA FLEET MO-49-10 P 1/2

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
49 - AIRBORNE POWER UNIT
49-10 - Power Plant
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-49-10 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
52 - DOORS
52-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Passenger Door Permanently Indicated Open on the

52-07-01A
DOOR/OXY SD page (SLIDE ARMED light operative)
Ident.: MO-52-07-00008846.0001001 / 10 OCT 14
Applicable to: ALL

GENERAL INFORMATION
If passenger doors are affected, indications on the PTP or the FAP may be affected.
If passenger doors are affected, the time recorded in the ACARS movement report may be wrong.
AFTER ENGINE START
In the case of false door alert:
EMER CANC pb ................................................................................................................ Press
Note: the limitation MAX FL : 100/MEA-MORA remains displayed on the STATUS SD
page.
BEFORE TAKEOFF
CAUTION The T.O CONFIG pb must be maintained pressed to check that there is no alert.
T.O CONFIG pb ...................................................................................................................Press
In the T.O MEMO, the "T.O CONFIG NORMAL" line will not replace the "T.O CONFIG . . TEST"
line.
Consider normal configuration for takeoff provided that no alert was displayed during the T.O
CONFIG TEST.

52-07-01B
Passenger Door Permanently Indicated Open on the DOOR/OXY
52-07-01C
SD page (SLIDE ARMED light may be permanently illuminated)
52-07-01D
Ident.: MO-52-07-00008847.0001001 / 10 OCT 14
Applicable to: ALL

GENERAL INFORMATION
If passenger doors are affected, indications on the PTP or the FAP may be affected.
If passenger doors are affected, the time recorded in the ACARS movement report may be wrong.
The SLIDE ARMED light on passenger doors may be permanently illuminated.
Continued on the following page

LAN COLOMBIA FLEET MO-52-07 P 1/4

MEL A to B 10 OCT 14
 MEL OPERATIONAL PROCEDURES
52 - DOORS
52-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

AFTER ENGINE START
In the case of false door alert:
EMER CANC pb ................................................................................................................ Press
Note: the limitation MAX FL : 100/MEA-MORA remains displayed on the STATUS SD
page.
BEFORE TAKEOFF
CAUTION The T.O CONFIG pb must be maintained pressed to check that there is no alert.
T.O CONFIG pb ...................................................................................................................Press
In the T.O MEMO, the "T.O CONFIG NORMAL" line will not replace the "T.O CONFIG . . TEST"
line.
Consider normal configuration for takeoff provided that no alert was displayed during the T.O
CONFIG TEST.

52-07-02A Passenger Door Permanently Indicated

52-07-02B Closed on the DOOR/OXY SD page
Ident.: MO-52-07-00008848.0001001 / 10 OCT 14
Applicable to: ALL

GENERAL INFORMATION
If passenger doors are affected, indications on the PTP or the FAP may be affected.
If passenger doors are affected, the time recorded in the ACARS movement report may be wrong.

52-07-03A
52-07-03B Overwing Emergency Exit Permanently
52-07-03C Indicated Open on the DOOR/OXY SD page
52-07-03D
Ident.: MO-52-07-00008849.0001001 / 10 OCT 14
Applicable to: ALL

GENERAL INFORMATION
Indications on the PTP or the FAP may be affected.
Continued on the following page

LAN COLOMBIA FLEET MO-52-07 P 2/4

MEL B to D 10 OCT 14
 MEL OPERATIONAL PROCEDURES
52 - DOORS
52-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

AFTER ENGINE START
In the case of false door alert:
EMER CANC pb ................................................................................................................ Press
Note: the limitation MAX FL : 100/MEA-MORA remains displayed on the STATUS SD
page.
BEFORE TAKEOFF
CAUTION The T.O CONFIG pb must be maintained pressed to check that there is no alert.
T.O CONFIG pb ...................................................................................................................Press
In the T.O MEMO, the "T.O CONFIG NORMAL" line will not replace the "T.O CONFIG . . TEST"
line.
Consider normal configuration for takeoff provided that no alert was displayed during the T.O
CONFIG TEST.

52-07-04A Overwing Emergency Exit Permanently

52-07-04B Indicated Closed on the DOOR/OXY SD page
Ident.: MO-52-07-00008850.0001001 / 10 OCT 14
Applicable to: ALL

GENERAL INFORMATION
Indications on the PTP or the FAP may be affected.

52-07-05A Cargo Door Indication on the DOOR/OXY SD page

Ident.: MO-52-07-00008851.0001001 / 10 OCT 14
Applicable to: ALL

GENERAL INFORMATION
If the cargo doors are affected, the time recorded in the ACARS movement report may be wrong.
If cargo indication is inoperative due to a proximity switch failure:
The relevant cargo heating is inhibited. For live animal transportation, use the Live Animal
Transportation Calculation Tool.
Continued on the following page

LAN COLOMBIA FLEET MO-52-07 P 3/4

MEL D to F 10 OCT 14
 MEL OPERATIONAL PROCEDURES
52 - DOORS
52-07 - Indications on the DOOR/OXY SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

AFTER ENGINE START
In the case of false door alert:
EMER CANC pb ................................................................................................................ Press
Note: the limitation MAX FL : 100/MEA-MORA remains displayed on the STATUS SD
page.
BEFORE TAKEOFF
CAUTION The T.O CONFIG pb must be maintained pressed to check that there is no alert.
T.O CONFIG pb ...................................................................................................................Press
In the T.O MEMO, the "T.O CONFIG NORMAL" line will not replace the "T.O CONFIG . . TEST"
line.
Consider normal configuration for takeoff provided that no alert was displayed during the T.O
CONFIG TEST.

Avionics Compartment Access Door

52-07-06A
Indication on the DOOR/OXY SD page
Ident.: MO-52-07-00008852.0001001 / 10 OCT 14
Applicable to: ALL

AFTER ENGINE START

In the case of false door alert:
EMER CANC pb ................................................................................................................ Press
Note: the limitation MAX FL : 100/MEA-MORA remains displayed on the STATUS SD
page.
BEFORE TAKEOFF
CAUTION The T.O CONFIG pb must be maintained pressed to check that there is no alert.
T.O CONFIG pb ...................................................................................................................Press
In the T.O MEMO, the "T.O CONFIG NORMAL" line will not replace the "T.O CONFIG . . TEST"
line.
Consider normal configuration for takeoff provided that no alert was displayed during the T.O
CONFIG TEST.

LAN COLOMBIA FLEET MO-52-07 P 4/4

MEL F to G 10 OCT 14
 MEL OPERATIONAL PROCEDURES
52 - DOORS
52-30 - Cargo Door
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-30-07A Cargo Door Open/Locked Indicator light

Ident.: MO-52-30-00009614.0001001 / 11 MAR 10
Applicable to: ALL

ON GROUND
When the Cargo Door Open/Locked Indicator light is inoperative, it is necessary to
inform the ground personnel:
To visually check that the affected cargo door is in the fully open position, with no
downward movement after releasing the lever of the manual selector valve.
To visually check that the lever of the manual selector valve stays in the neutral position.

LAN COLOMBIA FLEET MO-52-30 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
52 - DOORS
52-30 - Cargo Door
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-52-30 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
52 - DOORS
52-51 - Reinforced Cockpit Door (CDLS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-51-01B Normal System.

Ident.: MO-52-51-20800308.9001001 / 10 OCT 14
Applicable to: ALL

NORMAL CONTROL UNIT, TOGGLE SWITCH AND LIGHTS ON COCKPIT DOOR PANEL,
BUZZER, KEYPAD, DOOR STRIKE RELEASE.
Only the Aircraft equipped with DeadBolt, the CDLS may be deactivated in unlocked position. The
DeadBolt is used to lock the Cockpit Door.
In case of Normal System is completed deactivated:
Ensure communication between cockpit crew and cabin crew via cockpit/cabin interphone
system. Before the flight captain in command should establish a protocol of routine and
emergency to access to cockpit via inerphone system. In addition, two persons must be
permanently present in the cockpit throughout the flight.

52-51-04A CDLSKeypad
Ident.: MO-52-51-20800641.9001001 / 18 MAY 11
Applicable to: ALL

KEYPAD
Alternate normal procedures must be established before departure in order to remind the cabin
crew to use the cabin interphone to communicate with cockpit crew to request access to the
cockpit.
The cockpit crew must brief the cabin crew that the CDLS keypad is inoperative. Ensure
communication between cockpit crew and cabin crew via cockpit/cabin interphone system. Before
the flight captain in command should establish a protocol of routine and emergency to access to
cockpit via inerphone system.
IN FLIGHT
At least two people must always be present in the cockpit throughout the entire flight.

LAN COLOMBIA FLEET MO-52-51 P 1/2

MEL A to B 10 OCT 14
 MEL OPERATIONAL PROCEDURES
52 - DOORS
52-51 - Reinforced Cockpit Door (CDLS)
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-51-05A LEDS
Ident.: MO-52-51-20800314.9001001 / 18 MAY 11
Applicable to: ALL

ON NORMAL CKPT DOOR CONT PANEL

Check that the FAULT light comes on when lamp test is performed by setting the ANN LT switch
to TEST position.
Push the door manually to confirm that the door is locked or unlocked since the green and/or red
LEDs on the keypad are inoperative.

LAN COLOMBIA FLEET MO-52-51 P 2/2

MEL C 10 OCT 14
 MEL OPERATIONAL PROCEDURES
52 - DOORS
52-53 - Cockpit Door Panel on the Center Pedestal
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-53-01A Fault light

Ident.: MO-52-53-20800312.9001001 / 18 MAY 11
Applicable to: ALL

ON THE COCKPIT DOOR PANEL

Before the first flight under this item, check that with Cockpit Door toggle switch in the NORM
position the three latches of the door are maintained in the lock position. This can be performed
by a manual inspection: pushing the latches and visually confirming they remain in their position.
Perform a regular check of correct strickes operation. This can be performed by a visual check of
the Strike LEDs on the Cockpit Door Control Panel.

52-53-02A Open Light

Ident.: MO-52-53-20800311.9001001 / 18 MAY 11
Applicable to: ALL

ON THE COCKPIT DOOR PANEL

Check that the three STRIKE LEDs are not illuminated on the CKPT DOOR CONT panel to
ensure the door is closed and locked.

52-53-03A Toggle Switch on Cockpit Door Panel.

Ident.: MO-52-53-20800310.9001001 / 25 MAY 11
Applicable to: ALL

LOCK FUNCTION
Ensure communication between cockpit crew and cabin crew via cockpit/cabin interphone system.
Before the flight captain in command should establish a protocol of routine and emergency to
access to cockpit via inerphone system. In addition, two persons must be permanently present in
the cockpit throughout the flight.

LAN COLOMBIA FLEET MO-52-53 P 1/2

MEL A to C 05 NOV 13
 MEL OPERATIONAL PROCEDURES
52 - DOORS
52-53 - Cockpit Door Panel on the Center Pedestal
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

52-53-04A Toggle Switch on Cockpit Door Panel.

Ident.: MO-52-53-20800309.9001001 / 09 AUG 11
Applicable to: ALL

UNLOCK FUNCTION
In case of inoperative toggle switch electrical command ( Impossibility to unlock the
door ), the door can be opened from the cockpit by using the D - shaped hanle fitted on
the center catch of the door.
Ensure communication between cockpit crew and cabin crew via cockpit/cabin interphone
system. Before the flight captain in command should establish a protocol of routine and
emergency to access to cockpit via inerphone system. In addition, two persons must be
permanently present in the cockpit throughout the flight.

LAN COLOMBIA FLEET MO-52-53 P 2/2

MEL D 05 NOV 13
 MEL OPERATIONAL PROCEDURES
56 - WINDOWS
56-10 - Cockpit
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

56-10-01A
56-10-01B
Front Windshield
56-10-01C
56-10-01D
Ident.: MO-56-10-00008835.0001001 / 18 MAR 10
Applicable to: ALL

FLIGHT PREPARATION/LIMITATIONS
When PF side is affected:
Maximum landing capability is CAT 1
When PNF side is affected:
Maximum landing capability is not affected and is still CAT 3 DUAL.

LAN COLOMBIA FLEET MO-56-10 P 1/2

MEL A 05 NOV 13
 MEL OPERATIONAL PROCEDURES
56 - WINDOWS
56-10 - Cockpit
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Intentionally left blank

LAN COLOMBIA FLEET MO-56-10 P 2/2

MEL 05 NOV 13
 MEL OPERATIONAL PROCEDURES
73 - ENGINE FUEL AND CONTROL
73-20 - Controlling
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

73-20-04A EPR Control Mode

Ident.: MO-73-20-00008833.0009001 / 10 OCT 14
Applicable to: MSN 4516-4546

GENERAL INFORMATION
The autothrust function is inoperative.
floor is not available.
target is not available.
Bump is inoperative.
Maximum landing capability is CAT 1.
FLIGHT PREPARATION/LIMITATIONS
Takeoff performance:
The following method may be used for takeoff performance determination if no takeoff data
(Predetermined by using OCTOPUS program or other equivalent program with present failure
case taken into account) is available.
Method:
Determine the MTOW and the associated speeds in normal conditions.
Apply the following decrements function of the MTOW in normal conditions:
Normal TOW 40 000 45 000 50 000 55 000 60 000
kg (lb) (90 000) (100 000) (110 000) (120 000) (130 000)
5 900
Weight decrement 5 200 6 500 7 200 7 800
(
kg (lb) (11 700)
13 000)
(14 300) (15 600) (16 900)

V1, VR and V2 decrement

7 8 9 9 10
(kt)
Normal TOW 65 000 70 000 75 000 80 000 85 000
kg (lb) (140 000) (160 000) (170 000) (180 000) (190 000)
Weight decrement 8 500 9 100 9 800 10 400 11 000
kg (lb) (18 200) (20 800) (22 100) (23 400) (24 700)
V1, VR and V2 decrement
11 12 13 14 15
(kt)
Continued on the following page

LAN COLOMBIA FLEET MO-73-20 P 1/6

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
73 - ENGINE FUEL AND CONTROL
73-20 - Controlling
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Check that the takeoff speeds are equal to or above the minimum control speeds.
If no minimum speed value is available on the RTOW charts, use the conservative values
provided in Refer to FCOM/ MINIMUM V2 LIMITED BY VMU/VMCA (KT IAS).
Check that the corrected V1 is equal to or above the minimum V1 value shown on the RTOW
chart (due to VMCG limitation).
If the corrected V1 is lower than the minimum V1:
Take this last value as V1.
Further decrease the weight by 1 000 kg (2 200 lb) per kt difference between both values.
Decrease VR and V2 by 1.3 kt per kt increase in V1
Check that the corrected VR is equal to or above the minimum VR value shown on the RTOW
chart (due to VMCA limitation).
If the corrected VR is lower than the minimum VR:
Takeoff cannot be performed using this method.
Check that the corrected V2 is equal to or above the minimum V2 value shown on the RTOW
chart (due to VMU/VMCA limitation).
If the corrected V2 is lower than the minimum V2:
Takeoff cannot be performed using this method.
If the actual TOW is lower than the MTOW calculated using above method:
Determine V1, VR and V2 for the MTOW
Decrease V1, VR and V2 by 1.3 kt per 1 000 kg (0.6 kt per 1 000 lb) difference between
the MTOW and the actual TOW
V1, VR, and V2 must not decrease below the minimum speeds defined above.
Single engine cruise:
See "N1 MODE THRUST CONTROL" in Refer to FCOM/PER-THR-N1 MODE THRUST
CONTROL.
Go-Around performance:
See "N1 MODE THRUST CONTROL" in Refer to FCOM/PER-THR-N1 MODE THRUST
CONTROL.
BEFORE ENGINE START
ENG 1 N1 MODE pb-sw ......................................................................................................... ON
ENG 2 N1 MODE pb-sw ......................................................................................................... ON
Continued on the following page

LAN COLOMBIA FLEET MO-73-20 P 2/6

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
73 - ENGINE FUEL AND CONTROL
73-20 - Controlling
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

FOR TAKEOFF
Flexible takeoff is not permitted.
The takeoff must be performed without FDs as follows:
Set both FDs to OFF
Select V2 on the FCU
Acquire pitch attitude about 15 to maintain the speed target with two engines operative, about
12.5 in the case of an engine failure.
Above 100 ft AGL, when appropriate:
Set both FDs to ON (basic guidance modes engage)
Engage OP CLB and select appropriate speed and lateral mode
AP use as required.
When reaching the thrust reduction altitude :
Set both thrust levers to CL detent.
When reaching the acceleration altitude :
Resume normal acceleration and climb procedures.
Note: CLB or LVR CLB will not flash on the FMA as the A/THR is not available.
GO-AROUND
Note: To perform a manual Go-Around with no FD, the PF simultaneously announces his/her
intention, disengages the AP, applies TOGA and initiates the rotation.
The Go-Around must be performed without FDs as follows:
Set AP (if engaged) to OFF
Set both FDs (ifengaged) to OFF
Acquire pitch attitude about 15 to maintain the speed target with two engines operative, about
12.5 in the case of an engine failure.
Adjust pitch to maintain VAPP.
When appropriate:
Set both FDs to ON (basic guidance modes engage)
Engage OP CLB and select appropriate speed and lateral mode
AP use as required.
When reaching the thrust reduction altitude :
Set both thrust levers to CL detent.
Continued on the following page

LAN COLOMBIA FLEET MO-73-20 P 3/6

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
73 - ENGINE FUEL AND CONTROL
73-20 - Controlling
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

When reaching the acceleration altitude :
Resume normal acceleration and climb procedures.
Note: CLB or LVR CLB will not flash on the FMA as the A/THR is not available. FMS does not
engage the GO AROUND phase.

73-20-05A Minimum Idle on Ground

Ident.: MO-73-20-00008834.0018001 / 18 JUL 14
Applicable to: MSN 4758-5364

FLIGHT PREPARATION/LIMITATIONS
Takeoff performance:
Use the following penalties for takeoff performance determination if no takeoff data
(predetermined by using OCTOPUS program or other equivalent program with present failure
case taken into account) is available. Takeoff must be performed with full thrust.
VMCG/VMCA limitation No VMCG/VMCA limitation
Weight decrement (kg/lb) 1 500/3 400 200/500
V1, VR, V2 decrement (kt IAS) 0 1

Landing performance:
No penalty.

73-20-05A Minimum Idle on Ground

Ident.: MO-73-20-00008834.0024001 / 27 FEB 15
Applicable to: MSN 5443-5453

FLIGHT PREPARATION/LIMITATIONS
Takeoff performance:
The takeoff performance must be determined by using OCTOPUS program or other equivalent
program with present failure case.

Launch PEP.
Landing performance:
No penalty.

LAN COLOMBIA FLEET MO-73-20 P 4/6

MEL A to B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
73 - ENGINE FUEL AND CONTROL
73-20 - Controlling
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

73-20-05A Minimum Idle on Ground

Ident.: MO-73-20-00008834.0008001 / 10 OCT 14
Applicable to: MSN 4516-4546

GENERAL INFORMATION
Continuous ignition is permanently on.
FLIGHT PREPARATION/LIMITATIONS
Takeoff performance:
Use the following penalties for takeoff performance determination if no takeoff data
(predetermined by using OCTOPUS program or other equivalent program with present failure
case taken into account) is available. Takeoff must be performed with full thrust.
VMCG/VMCA limitation No VMCG/VMCA limitation
Weight decrement (kg/lb) 2 900/6 400 400/900
V1, VR, V2 decrement (kt IAS) 0 1

Landing performance:
No penalty.

LAN COLOMBIA FLEET MO-73-20 P 5/6

MEL B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
73 - ENGINE FUEL AND CONTROL
73-20 - Controlling
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-73-20 P 6/6

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
74 - IGNITION
74-07 - Indications on the ENGINE SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

74-07-01A Selected Igniter Indication on the ENGINE SD page

Ident.: MO-74-07-00008832.0001001 / 27 FEB 15
Applicable to: ALL

AFTER ENGINE START

If engine 1 is affected:
ENGINE/1 AND 2/IGN/SYS A (49VU A03) C/B ............................................................PULL
ENGINE/IGN/ENG 1/ SYS A BAT (121VU P39) C/B ....................................................PULL
ENGINE/IGN/ENG 1/ SYS B (121VU P41) C/B ............................................................PULL
If engine 2 is affected:
ENGINE/1 AND 2/IGN/SYS A (49VU A03) C/B ............................................................PULL
ENGINE/IGN/ENG 2/ SYS A BAT (121VU P40) C/B ....................................................PULL
ENGINE/IGN/ENG 2/ SYS B (121VU P42) C/B ............................................................PULL
On the EWD, check that the ENG 1(2) A+B IGN FAULT alert is displayed.
If engine 1 is affected:
ENGINE/1 AND 2/IGN/SYS A (49VU A03) C/B ...........................................................PUSH
ENGINE/IGN/ENG 1/ SYS A BAT (121VU P39) C/B ...................................................PUSH
ENGINE/IGN/ENG 1/ SYS B (121VU P41) C/B ...........................................................PUSH
If engine 2 is affected:
ENGINE/1 AND 2/IGN/SYS A (49VU A03) C/B ...........................................................PUSH
ENGINE/IGN/ENG 2/ SYS A BAT (121VU P40) C/B ...................................................PUSH
ENGINE/IGN/ENG 2/ SYS B (121VU P42) C/B ...........................................................PUSH

LAN COLOMBIA FLEET MO-74-07 P 1/2

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
74 - IGNITION
74-07 - Indications on the ENGINE SD page
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-74-07 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
74 - IGNITION
74-31 - Ignition Starting and Continuous Relight
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

74-31-01A Ignition System A

Ident.: MO-74-31-00008828.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

BEFORE ENGINE START

ENGINE/1 AND 2/IGN/SYS A (49 VU A03) C/B ......................................................................PULL
AFTER ENGINE START
ENGINE/1 AND 2/IGN/SYS A (49 VU A03) C/B .....................................................................PUSH

74-31-01A Ignition System A

Ident.: MO-74-31-00008828.0002001 / 10 OCT 14
Applicable to: MSN 4516-4546

BEFORE ENGINE START

For the affected engine, prefer a manual engine start.

74-31-02A Ignition System B

Ident.: MO-74-31-00008829.0001001 / 27 FEB 15
Applicable to: MSN 4758-5453

BEFORE ENGINE START

ENGINE/IGN/ENG (1 and/or 2)/SYS B (121 VU P41/P42) C/B ...............................................PULL

74-31-02A Ignition System B

Ident.: MO-74-31-00008829.0004001 / 10 OCT 14
Applicable to: MSN 4516-4546

BEFORE ENGINE START

For the affected engine, prefer a manual engine start.

LAN COLOMBIA FLEET MO-74-31 P 1/2

MEL A to B 27 FEB 15
 MEL OPERATIONAL PROCEDURES
74 - IGNITION
74-31 - Ignition Starting and Continuous Relight
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-74-31 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
78 - EXHAUST
78-30 - Thrust Reversers
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

78-30-01A Thrust Reverser

Ident.: MO-78-30-00008825.0002001 / 27 FEB 15
1 Applicable to: MSN 4516-4972, 5229, 5263-5364

FLIGHT PREPARATION/LIMITATIONS
Performance Adjustments:
Runway State Performance Adjustments
Takeoff Dry, or
No performance adjustments necessary (basic
Landing Dry, or
performance data is computed without thrust reversers).
Landing Wet
One Thrust Reverser
Inoperative Takeoff Wet, or Use performance data computed with either:
Takeoff Contaminated, or All thrust reversers inoperative, or
Landing Contaminated One thrust reverser inoperative.

Runway State Performance Adjustments

Takeoff Dry, or
No performance adjustments necessary (basic
Landing Dry, or
performance data is computed without thrust reversers).
Both Thrust Landing Wet
Reversers Inoperative Takeoff Wet, or
Use performance data computed with all thrust
Takeoff Contaminated, or
reversers inoperative.
Landing Contaminated

FOR TAKEOFF
During the takeoff briefing, the flight crew must review:
The status of the thrust reversers, and
The use of the thrust reversers
REJECTED TAKEOFF
Ensure that both engine thrust levers are set to IDLE detent, then:
If one thrust reverser is inoperative:
Use both thrust levers when applying reverse thrust.
Note: ENG (AFFECTED SIDE) REVERSER FAULT alert is displayed on the EWD after
selection of the reverse thrust.
If both thrust reversers are inoperative:
Do not move the thrust levers to reverse.
Continued on the following page

LAN COLOMBIA FLEET MO-78-30 P 1/6

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
78 - EXHAUST
78-30 - Thrust Reversers
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

IN FLIGHT
Should a failure occur with "LDG DIST PROC.......APPLY" message displayed on the
STATUS SD page,
and
Whatever the actual thrust reversers selection at landing:
To calculate the LDG DIST with the in-flight failure, do not take credit of the inoperative thrust
reversers (Refer to QRH PER-C).
DURING APPROACH
During the approach briefing, the flight crew must review:
The status of the thrust reversers, and
The use of the thrust reversers
FOR LANDING
Before the touchdown, ensure that both engine thrust levers are set to IDLE detent for the flare.
After touchdown, if one thrust reverser is inoperative:
Use both thrust levers when applying reverse thrust.
Note: ENG (AFFECTED SIDE) REVERSER FAULT alert is displayed on the EWD after
selection of the reverse thrust.
After touchdown, if both thrust reversers are inoperative:
Do not move the thrust levers to reverse.

78-30-01A Thrust Reverser

Ident.: MO-78-30-00008825.0015001 / 27 FEB 15
Applicable to: MSN 5443-5453

FLIGHT PREPARATION/LIMITATIONS
Performance Adjustments:
Runway State Performance Adjustments
Takeoff Dry, or
No performance adjustments necessary (basic
Landing Dry, or
performance data is computed without thrust reversers).
Landing Wet
One Thrust Reverser
Inoperative Takeoff Wet, or Use performance data computed with either:
Takeoff Contaminated, or All thrust reversers inoperative, or
Landing Contaminated One thrust reverser inoperative.
Continued on the following page

LAN COLOMBIA FLEET MO-78-30 P 2/6

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
78 - EXHAUST
78-30 - Thrust Reversers
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

Runway State Performance Adjustments
Takeoff Dry, or
No performance adjustments necessary (basic
Landing Dry, or
performance data is computed without thrust reversers).
Both Thrust Landing Wet
Reversers Inoperative Takeoff Wet, or
Use performance data computed with all thrust
Takeoff Contaminated, or
reversers inoperative.
Landing Contaminated

DURING COCKPIT PREPARATION

After application of the maintenance procedure
and
When the FADEC have power:
Check that the ENG (AFFECTED SIDE) REV INHIBITED alert is displayed on the EWD.
FOR TAKEOFF
During the takeoff briefing, the flight crew must review:
The status of the thrust reversers, and
The use of the thrust reversers
REJECTED TAKEOFF
Ensure that both engine thrust levers are set to IDLE detent, then:
If one thrust reverser is inoperative:
Use both thrust levers when applying reverse thrust.
If both thrust reversers are inoperative:
Do not move the thrust levers to reverse.
IN FLIGHT
Should a failure occur with "LDG DIST PROC.......APPLY" message displayed on the
STATUS SD page,
and
Whatever the actual thrust reversers selection at landing:
To calculate the LDG DIST with the in-flight failure, do not take credit of the inoperative thrust
reversers (Refer to QRH PER-C).
Continued on the following page

LAN COLOMBIA FLEET MO-78-30 P 3/6

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
78 - EXHAUST
78-30 - Thrust Reversers
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

DURING APPROACH
During the approach briefing, the flight crew must review:
The status of the thrust reversers, and
The use of the thrust reversers
FOR LANDING
Before the touchdown, ensure that both engine thrust levers are set to IDLE detent for the flare.
After touchdown, if one thrust reverser is inoperative:
Use both thrust levers when applying reverse thrust.
For automatic roll-out with one thrust reverser inoperative, Refer to AFM/LIM-22-FGS CAT II /
CAT III Operations.
After touchdown, if both thrust reversers are inoperative:
Do not move the thrust levers to reverse.

78-30-01A Thrust Reverser

2 Ident.: MO-78-30-00008825.0014001 / 27 FEB 15

Applicable to: MSN 5178, 5234

FLIGHT PREPARATION/LIMITATIONS
Performance Adjustments:
Runway State Performance Adjustments
Takeoff Dry, or
No performance adjustments necessary (basic
Landing Dry, or
performance data is computed without thrust reversers).
Landing Wet
One Thrust Reverser
Inoperative Takeoff Wet, or Use performance data computed with either:
Takeoff Contaminated, or All thrust reversers inoperative, or
Landing Contaminated One thrust reverser inoperative.

Runway State Performance Adjustments

Takeoff Dry, or
No performance adjustments necessary (basic
Landing Dry, or
performance data is computed without thrust reversers).
Both Thrust Landing Wet
Reversers Inoperative Takeoff Wet, or
Use performance data computed with all thrust
Takeoff Contaminated, or
reversers inoperative.

Landing Contaminated
Continued on the following page

LAN COLOMBIA FLEET MO-78-30 P 4/6

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
78 - EXHAUST
78-30 - Thrust Reversers
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

DURING COCKPIT PREPARATION
After application of the maintenance procedure
and
When the FADEC have power:
Check that the ENG (AFFECTED SIDE) REV INHIBITED alert is displayed on the EWD.
FOR TAKEOFF
During the takeoff briefing, the flight crew must review:
The status of the thrust reversers, and
The use of the thrust reversers
REJECTED TAKEOFF
Ensure that both engine thrust levers are set to IDLE detent, then:
If one thrust reverser is inoperative:
Use both thrust levers when applying reverse thrust.
If both thrust reversers are inoperative:
Do not move the thrust levers to reverse.
IN FLIGHT
Should a failure occur with "LDG DIST PROC.......APPLY" message displayed on the
STATUS SD page,
and
Whatever the actual thrust reversers selection at landing:
To calculate the LDG DIST with the in-flight failure, do not take credit of the inoperative thrust
reversers (Refer to QRH PER-C).
DURING APPROACH
During the approach briefing, the flight crew must review:
The status of the thrust reversers, and
The use of the thrust reversers
FOR LANDING
Before the touchdown, ensure that both engine thrust levers are set to IDLE detent for the flare.
After touchdown, if one thrust reverser is inoperative:
Use both thrust levers when applying reverse thrust.
Continued on the following page

LAN COLOMBIA FLEET MO-78-30 P 5/6

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
78 - EXHAUST
78-30 - Thrust Reversers
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

Continued from the previous page

After touchdown, if both thrust reversers are inoperative:

Do not move the thrust levers to reverse.

LAN COLOMBIA FLEET MO-78-30 P 6/6

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
79 - OIL
79-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

79-09-01A ENG 1(2) OIL LO PR Alert

Ident.: MO-79-09-00008824.0001001 / 27 FEB 15
Applicable to: ALL

AFTER ENGINE START

If both engines are affected:
RCDR GND CTL pb-sw ...........................................................................................CHECK ON

LAN COLOMBIA FLEET MO-79-09 P 1/2

MEL A 27 FEB 15
 MEL OPERATIONAL PROCEDURES
79 - OIL
79-09 - ECAM Alerts
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-79-09 P 2/2

MEL 27 FEB 15
 MEL OPERATIONAL PROCEDURES
79 - OIL
79-20 - Distribution
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

79-20-01A Air Cooled Oil Cooler (ACOC) Modulating Valve

Ident.: MO-79-20-00008822.0001001 / 10 OCT 14
Applicable to: MSN 4516-4546

BEFORE TAKEOFF
On the FUEL SD page, check that the fuel temperature in the inner tank is above -20 C.

LAN COLOMBIA FLEET MO-79-20 P 1/2

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
79 - OIL
79-20 - Distribution
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-79-20 P 2/2

MEL 10 OCT 14
 MEL OPERATIONAL PROCEDURES
80 - STARTING
80-11 - Pneumatic Starter and Valve System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

80-11-01A Start Valve

Ident.: MO-80-11-00008815.0001001 / 10 OCT 14
Applicable to: ALL

BEFORE ENGINE START

Refer to FCOM/ Start Valve Manual Operation
IN FLIGHT
If the affected engine shuts down, attempt to restart it only using windmilling relight.

LAN COLOMBIA FLEET MO-80-11 P 1/2

MEL A 10 OCT 14
 MEL OPERATIONAL PROCEDURES
80 - STARTING
80-11 - Pneumatic Starter and Valve System
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET MO-80-11 P 2/2

MEL 10 OCT 14


NEF NON-ESSENTIAL
EQUIPMENT & FURNISHINGS
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 NEF NON-ESSENTIAL EQUIPMENT & FURNISHINGS
PRELIMINARY PAGES - TABLE OF CONTENTS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

INTRODUCTION TO THE NEF.............................................................................................................................. A

LAN COLOMBIA FLEET NEF -PLP-TOC P 1/2

MEL 10 OCT 14
 NEF NON-ESSENTIAL EQUIPMENT & FURNISHINGS
PRELIMINARY PAGES - TABLE OF CONTENTS
COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET NEF -PLP-TOC P 2/2

MEL 10 OCT 14
 NEF NON-ESSENTIAL EQUIPMENT & FURNISHINGS

COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

INTRODUCTION TO THE NEF

Ident.: NEF -20801644.9001001 / 10 OCT 14
Applicable to: ALL

Non-Essential Equipment and Furnishings (NEF) are those items installed on the aircraft as part of
the original type certification, supplemental type certificate, or other form of alteration that have no
effect on the safe operation of flight and would not be required by the applicable certification rules
or operational rules. They are those items that, if damaged, inoperative, or missing, have no effect
on the aircrafts ability be operated safely under all operational conditions. These nonessential items
may be installed in areas including, but not limited to:
Cargo Areas
Crew Rest Areas
Flight Deck Area
Galley Area
Lavatories
Passenger Compartment
Service Areas

LAN COLOMBIA FLEET NEF P 1/2

MEL A 10 OCT 14
 NEF NON-ESSENTIAL EQUIPMENT & FURNISHINGS

COLOMBIA
LAN COLOMBIA AIRLINES
MINIMUM EQUIPMENT LIST

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LAN COLOMBIA FLEET NEF P 2/2

MEL 10 OCT 14