U.S.

Department of Transportation
Federal Aviation Administration
Washington, D.C.

Master Minimum Equipment List

Revision: 9
Date: 01/24/2014

BOEING 787

James M. Eitel
Flight Operations Evaluation Board (FOEB)

Federal Aviation Administration

Seattle Aircraft Evaluation Group
1601 Lind Ave SW
Renton, WA 98057

Telephone: (425) 917-6600

FAX: (425) 917-6638
 FEDERAL AVIATION ADMINISTRATION Page: II
Revision: 9
MASTER MINIMUM EQUIPMENT LIST Date: 01/24/2014

(BOEING B-787)

No Contents

SYSTEM PAGES REVISION DATE

Title Page 9 01/24/2014

Contents II 9 01/24/2014
Highlights of Change III thru VI 9 01/24/2014
Definitions VII 9 01/24/2014
Preamble VII 9 01/24/2014
21 Air Conditioning 21-1 thru 21-43 9 01/24/2014
22 Autoflight 22-1 thru 22-8 9 01/24/2014
23 Communications 23-1 thru 23-9 9 01/24/2014
24 Electrical Power 24-1 thru 24-10 9 01/24/2014
25 Equipment/Furnishings 25-1 thru 25-17 9 01/24/2014
26 Fire Protection 26-1 thru 26-9 9 01/24/2014
27 Flight Controls 27-1 thru 27-9 9 01/24/2014
28 Fuel 28-1 thru 28-10 9 01/24/2014
29 Hydraulic Power 29-1 thru 29-6 9 01/24/2014
30 Ice and Rain Protection 30-1 thru 30-9 6 11/21/2012
31 Indicating/Recording Systems 31-1 thru 31-10 2 01/25/2012
32 Landing Gear 32-1 thru 32-11 9 01/24/2014
33 Lights 33-1 thru 33-6 9 01/24/2014
34 Navigation 34-1 thru 34-11 9 01/24/2014
35 Oxygen 35-1 thru 35-3 9 01/24/2014
38 Water/Waste 38-1 thru 38-2 7 03/22/2013
42 Integrated Modular Avionics 42-1 thru 42-2 6 11/21/2012
44 Cabin Systems 44-1 thru 44-6 9 01/24/2014
45 Central Maintenance System 45-1 Original 09/01/2011
46 Information Systems 46-1 Original 09/01/2011
47 Inert Gas System 47-1 Original 09/01/2011
49 Airborne Auxiliary Power 49-1 thru 49-2 9 01/24/2014
50 Cargo & Accessory Compartments 50-1 Original 09/01/2011
52 Doors 52-1 thru 52-11 9 01/24/2014
73 Engine Fuel and Control 73-1 thru 73-2 9 01/24/2014
74 Ignition 74-1 Original 09/01/2011
75 Bleed Air 75-1 thru 75-2 1 10/24/2011
77 Engine Indicating 77-1 Original 09/01/2011
78 Engine Exhaust 78-1 thru 78-2 6 11/21/2012
79 Engine Oil 79-1 2 01/25/2012
80 Starting 80-1 Original 09/01/2011

.
 FEDERAL AVIATION ADMINISTRATION Page: III
Revision: 9
MASTER MINIMUM EQUIPMENT LIST Date: 01/24/2014

(BOEING B-787)

Highlights of Change

EFFECTIVE ABOVE DATE, the Boeing 787 Master Minimum Equipment List has been revised.
The changes in this revision were made to align with FAA policy letters and to increase dispatch
flexibility. All changes are reflected in the highlights of change listed below and are indicated by
revision bars in the associated ATA section. For any change affecting an ATA section, all pages
in that associated ATA section are re-dated accordingly, with the exception of nomenclature
changes for ATA chapter headings.

ATA 21 AIR CONDITIONING

Item –27-24: Added requirements for forward and aft outflow valves.

Item –31-01: Revised requirement for lavatory smoke detectors.

Item –31-02: Revised position for locking, added requirements for forward and aft outflow
valves and revised lavatory smoke detection requirement.

Item –31-03: Revised position for locking, added requirements for forward and aft outflow
valves and revised lavatory smoke detection requirement.

Item –31-05: Revised lavatory smoke detection requirement.

Item –31-06: Revised lavatory smoke detection requirement.

Item –31-07: Revised lavatory smoke detection requirement.

Item –32-01: Revised lavatory smoke detection requirement.

Item –32-02: Revised lavatory smoke detection requirement.

Item –44-03: Reformatted to sub items for various configurations.

Item –51-01: Previous sub items options B relief deleted and replaced with previous sub
items options C relief.

Item –51-03: Revised to require both CAC inlet pressure sensors operate normally.

Item –52-09: Revised to associated pack is considered inoperative.

Item –52-12: Added requirements for VFSGs to operate normally.

ATA 22 AUTOFLIGHT

Item –11-07: Revised to reflect CN incorporated for all airplanes.

Item –31-01: Revised relief for RR to be the same as GE.

 FEDERAL AVIATION ADMINISTRATION Page: IV
Revision: 9
MASTER MINIMUM EQUIPMENT LIST Date: 01/24/2014

(BOEING B-787)

ATA 23 COMMUNICATIONS

Item –11-01: Revised per PL-106.

Item –21-01-01: Revised number installed.

Item –51-03-01: Revised per PL-58.

ATA 24 ELECTRICAL POWER

Item –15-01-01: Revised proviso requirement.

Item –15-01-02: Deleted (O).

Item –21-01: Revised to include fault relief previously in 24-22-01.

Item –22-01-01: Fault relief now provided by 24-21-01. Revised for RR FRTT system no
longer installed. Relief added for RR modification 72-H666. Renumbered
sub items.

Item –22-02: Revised and reformatted relief.

Item –22-03: Revised proviso system to generator.

Item –31-02: Revised proviso system to generator.

Item –31-03: Revised proviso system to generator.

Item –38-01: Revised repair interval and deleted remarks.

ATA 25 EQUIPMENT/FURNISHINGS

Item –41-01: Revised per FAA Policy Letter 85.

ATA 26 FIRE PROTECTION

Item –17-01-01: Revised item nomenclature.

 FEDERAL AVIATION ADMINISTRATION Page: V
Revision: 9
MASTER MINIMUM EQUIPMENT LIST Date: 01/24/2014

(BOEING B-787)

ATA 27 FLIGHT CONTROLS

Item –02-02: Revised to reflect CN incorporated for all airplanes.

Item –41-03: Deleted (O).

Item –48-01: Revised to sub items for clarification.

Item –51-02: Added requirement for spoiler actuator system.

Item –61-02: Revised to reflect CN incorporated for all airplanes.

Item –61-03: Revised to reflect CN incorporated for all airplanes.

ATA 28 FUEL

Item –22-07: RR item no longer installed.

Item –22-08: RR item no longer installed.

Item –22-09: RR item no longer installed.

Item –25-02: Added requirement for left AGCU to operate normally.

ATA 29 HYDRAULIC POWER

Item –11-02: Deleted redundant proviso.

Item –21-02: Added new relief.

Item –31-03: Added new relief to previous item.

ATA 32 LANDING GEAR

Item –49-01: Revised to sub items for nose wheel and main wheels.

ATA 33 LIGHTS

Item –43-01: Clarified provisos.

 FEDERAL AVIATION ADMINISTRATION Page: VI
Revision: 9
MASTER MINIMUM EQUIPMENT LIST Date: 01/24/2014

(BOEING B-787)

ATA 34 NAVIGATION

Item –33-01: Revised to include modified airplanes.

Item –42-03: Revised per PL-76.

ATA 35 OXYGEN

Item –21-01: Reformatted relief.

ATA 44 CABIN SYSTEMS

Item –12-01: Revised requirements.

Item –14-02: Revised requirements.

ATA 49 AIRBORNE AUXILIARY POWER

Item –15-01: Added requirement for left AGCU to operate normally.

Item –41-01: Added requirement for left AGCU to operate normally.

Item –94-01: Added requirement for left AGCU to operate normally.

ATA 52 DOORS

Item –11-02: Revised lavatory smoke detection requirement.

Item –11-07-01: Title revised for clarification.

Item –11-08: Title revised for clarification.

ATA 73 ENGINE FUEL AND CONTROL

Item –21-01: Added autothrottle requirement for RR.

 FEDERAL AVIATION ADMINISTRATION Page: VII
Revision: 9
MASTER MINIMUM EQUIPMENT LIST Date: 01/24/2014

(BOEING B-787)

Definitions

The Definitions are as published in FAA Policy Letter 25.

Preamble

The Preamble is as published in FAA Policy Letter 34.

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-00-01 Air Synoptic Display C 1 0

-21-01 Alternate Ventilation C 1 0 (M) May be inoperative provided:

System a) Alternate ventilation inlet valve is
deactivated closed, and
b) Air conditioning packs operate normally.

-22-01 Flight Deck Boost C 1 0 (M) May be inoperative provided:

Fan a) Fan is deactivated, and
b) Air conditioning packs operate normally.

-22-02 Flight Deck Boost C 1 0 (M) May be inoperative provided:

Isolation Valve a) Flight deck boost isolation valve is
deactivated closed, and
b) Air conditioning packs operate normally.

-25-01 Recirculation Fans

-25-01-01
Upper Recirculation C 1 0 (M) May be inoperative deactivated.
Fan

-25-01-02
Lower Recirculation C 2 1 (M) One may be inoperative provided:
Fans a) Fan is deactivated,
b) Air conditioning packs operate normally,
and
c) At least three cabin air compressors
operate normally.

-25-02 Lavatory/Galley C 1 0
Crown Temperature
Sensor System
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-26-01 Lavatory/Galley C 2 1 (M) One may be inoperative deactivated.

Ventilation Fans

-26-02 Lavatory/Galley C 1 0
Flow and
Temperature
Sensor

-26-03 Lavatory/Galley C 1 0 (M) May be inoperative provided filter is

Ventilation PECS removed.
Liquid Heat
Exchanger Barrier
Filter

-27-01 Forward EE Cooling C 1 0 (M) May be inoperative provided filter is

Supply Barrier Filter removed.

-27-02 Forward EE Cooling

Exhaust Fan
-27-02-01
Airplanes Without C 1 0 (M)(O) May be inoperative provided:
FCAC Installed a) Fan is deactivated,
b) Flight is conducted pressurized,
c) Forward equipment cooling supply fan
smoke detector operates normally,
d) For ground operations at OAT 30
degrees C or higher, both packs are
selected on or conditioned air is
supplied to the airplane, and
e) Forward cargo heat remains OFF.

-27-02-02
Airplanes With C 1 0 (M)(O) May be inoperative provided:
FCAC Installed a) Fan is deactivated,
b) Flight is conducted pressurized,
c) Forward equipment cooling supply fan
smoke detector operates normally, and
d) For ground operations at OAT 30
degrees C or higher, both packs are
selected on or conditioned air is
supplied to the airplane.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-3
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-27-03 Forward EE Cooling C 2 1

Supply Flow/
Temperature
Sensors 

-27-04 Forward EE Cooling C 1 0 (M) May be inoperative deactivated open.

Exhaust Overboard
Vent Valve

-27-05 Forward EE Cooling C 2 1 (M) One may be inoperative deactivated.

Override/Smoke
Clearance Valve
Motors 

-27-06 Forward EE Cooling C 2 1 (M) One may be inoperative provided:

Supply Fans a) Forward equipment cooling supply fan
is deactivated, and
b) Flight is conducted pressurized.

-27-07 Forward EE Cooling

Smoke Detectors

-27-07-01
Supply Fan Smoke C 1 0 May be inoperative provided:
Detector a) Forward equipment cooling exhaust fan
operates normally, and
b) Forward equipment cooling exhaust fan
smoke detector operates normally.

-27-07-02
Exhaust Fan Smoke C 1 0 May be inoperative provided forward equipment
Detector cooling supply fan smoke detector operates
normally.

-27-21 Aft EE Cooling C 1 0 (M) May be inoperative provided filter is

Supply Barrier Filter removed.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-4
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-27-22 Aft EE Cooling C 1 0 (M) May be inoperative provided:

Exhaust Fan a) Fan is deactivated,
b) Aft equipment cooling supply fan smoke
detector operates normally,
c) For ground operations at OAT 30
degrees C or higher, both packs are
selected on or conditioned air is
supplied to the airplane, and
d) Flight is conducted pressurized.

-27-23 Aft EE Cooling C 2 1

Flow/Temperature
Sensors

-27-24 Aft EE Cooling C 1 0 (M) May be inoperative provided:

Overboard Exhaust a) Valve is deactivated closed,
(Skin Flush) Valve b) Aft equipment cooling supply fan smoke
detector operates normally,
c) For ground operations at pressure |
altitudes 8,000 feet or higher, forward |
and aft outflow valves operate normally, |
d) For ground operations at OAT 24 |
degrees C or higher, aft outflow valve |
operates normally, and |
e) For ground operations at OAT 30
degrees C or higher, both packs are
selected on or conditioned air is
supplied to the airplane.

-27-25 Aft EE Cooling C 2 1 (M) One may be inoperative deactivated.

Supply
Override/Smoke
Clearance
Valve Motors 

-27-26 Aft EE Cooling C 2 1 (M) One may be inoperative provided:

Supply Fan a) Inoperative aft equipment cooling
supply fan is deactivated, and
b) Flight is conducted pressurized.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-5
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-27-27 Aft EE Cooling

Smoke Detectors

-27-27-01
Supply Fan Smoke C 1 0 May be inoperative provided:
Detector a) Aft equipment cooling exhaust fan
operates normally,
b) Aft equipment cooling exhaust fan
smoke detector operates normally,
c) Aft equipment cooling overboard
exhaust valve operates normally, and
d) Aft cargo heat supply valve operates
normally.

-27-27-02
Exhaust Fan Smoke C 1 0 May be inoperative provided aft equipment
Detector cooling supply fan smoke detector operates
normally.

-27-28 Aft Cargo Heat C 1 0 (M) May be inoperative provided:

Valve a) Valve is deactivated closed,
b) Aft equipment cooling supply fan smoke
detector operates normally, and
c) For ground operations at OAT 30
degrees C or higher, both packs are
selected on or conditioned air is
supplied to the airplane.

-27-31 Miscellaneous EE C 1 0 (M)(O) May be inoperative provided:

Cooling Exhaust a) Fan is deactivated,
Fan b) Cabin equipment center is deactivated,
and
c) Alternate procedures are established
and used.

-27-32 Miscellaneous EE C 1 0 May be inoperative provided miscellaneous

Cooling Exhaust equipment cooling exhaust fan is considered
Fan Smoke inoperative.
Detector
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-6
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-29-01 Overhead Flight

*** Crew Rest (OFCR)
Supply Shutoff and
Smoke
Clearance/Exhaust
Valves

-29-01A C 2 0 (M)(O) May be inoperative provided:

a) Supply shutoff valve is deactivated
closed,
b) Exhaust valve is deactivated closed,
c) OFCR is deactivated closed, and
d) Alternate procedures are established
and used.

NOTE: These provisions are not intended to

prohibit OFCR inspections by crew
members.

-29-01B D 2 0 (M)(O) May be inoperative provided:

a) Supply shutoff valve is deactivated
closed,
b) Exhaust valve is deactivated closed,
c) OFCR is deactivated closed, and
d) Procedures do not require its use.

NOTE: These provisions are not intended to

prohibit OFCR inspections by crew
members.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-7
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-29-02 Overhead Flight

*** Attendant Rest
(OFAR) Supply
Shutoff and
Smoke
Clearance/Exhaust
Valves 

-29-02A  C 2 0 (M)(O) May be inoperative provided:

a) Supply shutoff valve is deactivated
closed,
b) Exhaust valve is deactivated closed,
c) OFAR is deactivated closed, and
d) Alternate procedures are established
and used.

NOTE: These provisions are not intended to

prohibit OFAR inspections by crew
members.

-29-02B D 2 0 (M)(O) May be inoperative provided:

a) Supply shutoff valve is deactivated
closed,
b) Exhaust valve is deactivated closed,
c) OFAR is deactivated closed, and
d) Procedures do not require its use.

NOTE: These provisions are not intended to

prohibit OFAR inspections by crew
members.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-8
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-31-01 Automatic Cabin

Pressure Control
Channels

-31-01A C 4 2 (M) One control channel in each valve control

unit may be inoperative provided manual cabin
pressure control is verified to operate normally
on both outflow valves before each departure.

-31-01B C 4 0 (M)(O) May be inoperative provided:

a) For extended overwater flight, manual
cabin pressure control is verified to
operate normally on both outflow
valves,
b) Procedures are established and used to
verify cargo compartments remain
empty or contain only ballast, empty
cargo handling equipment (ballast may
be loaded in ULDs), or fly away kits,
c) Flight is conducted unpressurized, and
d) Smoke detection systems in all |
centerline lavatories and lavatories aft |
of door 4 are considered inoperative. |

NOTE: Operator MELs must define which items

are approved for inclusion in the fly
away kits and which materials can be
used as ballast.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-9
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-31-02 Manual Cabin

Pressure Outflow
Valve Controls
(FWD and AFT)

-31-02-01 
Airplanes Without
OFCR and OFAR
Installed

-31-02-01A  C 2 1 One may be inoperative provided:

a) Automatic cabin pressure control
channels on associated valve control
unit operate normally, and
b) Extended overwater flight is prohibited.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-10
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-31-02 Manual Cabin

Pressure Outflow
Valve Controls
(FWD and AFT)
(Cont’d)

-31-02-01 
Airplanes Without
OFCR and OFAR
Installed
(Cont’d)

-31-02-01B  C 2 1 (M) One may be inoperative provided:

a) Inoperative outflow valve is locked four |
square inches open, |
b) Manual mode is verified to operate
normally on remaining outflow valve,
c) Automatic cabin pressure control
channels operate normally on remaining
outflow valve,
d) Air conditioning packs operate normally,
e) At least three cabin air compressors
operate normally,
f) For ground operations at pressure |
altitudes 8,000 feet or higher, aft EE |
cooling overboard exhaust (skin flush) |
valve operates normally, |
g) For ground operations with aft outflow |
valve inoperative and OAT 24 degrees |
C or higher, aft EE cooling overboard |
exhaust (skin flush) valve operates |
normally, and |
h) For ground operations with forward
outflow valve inoperative and OAT 24
degrees C or higher, both packs are
selected on or conditioned air is
supplied to the airplane.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-11
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-31-02 Manual Cabin

Pressure Outflow
Valve Controls
(FWD and AFT)
(Cont’d) 

-31-02-01 
Airplanes Without
OFCR and OFAR
Installed
(Cont’d)

-31-02-01C C 2 0 (M) May be inoperative provided:

a) Procedures are established and used to
verify cargo compartments remain
empty or contain only ballast, empty
cargo handling equipment (ballast may
be loaded in ULDs), or fly away kits,
b) Flight is conducted unpressurized,
c) Extended overwater flight is prohibited,
and
d) Smoke detection systems in all |
centerline lavatories and in lavatories |
aft of door 4 are considered inoperative. |

NOTE: Operator MELs must define which items

are approved for inclusion in the fly
away kits and which materials can be
used as ballast.

-31-02-02 
Airplanes With
OFCR or OFAR
Installed

-31-02-02A  C 2 1 One may be inoperative provided:

a) Automatic cabin pressure control
channels on associated valve control
unit operate normally, and
b) Extended overwater flight is prohibited.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-12
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-31-02 Manual Cabin

Pressure Outflow
Valve Controls
(FWD and AFT)
(Cont’d) 

-31-02-02 
Airplanes With
OFCR or OFAR
Installed
(Cont’d)

-31-02-02B  C 2 1 (M)(O) One may be inoperative provided:

a) Inoperative outflow valve is locked four |
square inches open, |
b) Manual mode is verified to operate
normally on remaining outflow valve,
c) Automatic cabin pressure control
channels operate normally on remaining
outflow valve,
d) Air conditioning packs operate normally,
e) At least three cabin air compressors
operate normally,
f) For ground operations at pressure |
altitudes 8,000 feet or higher, aft EE |
cooling overboard exhaust (skin flush) |
valve operates normally, |
g) For ground operations with aft outflow |
valve inoperative and OAT 24 degrees |
C or higher, aft EE cooling overboard |
exhaust (skin flush) valve operates |
normally, |
h) For ground operations with forward
outflow valve inoperative and OAT 24
degrees C or higher, both packs are
selected on or conditioned air is
supplied to the airplane, and
i) For aft outflow valve inoperative, the
OFCR or OFAR is deactivated closed.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-13
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-31-02 Manual Cabin

Pressure Outflow
Valve Controls
(FWD and AFT)
(Cont’d) 

-31-02-02
Airplanes With
OFCR or OFAR
Installed
(Cont’d)

-31-02-02C C 2 0 (M)(O) May be inoperative provided:

a) Procedures are established and used to
verify cargo compartments remain
empty or contain only ballast, empty
cargo handling equipment (ballast may
be loaded in ULDs), or fly away kits,
b) Flight is conducted unpressurized,
c) Extended overwater flight is prohibited,
and
d) Smoke detection systems in all |
centerline lavatories and in lavatories |
aft of door 4 are considered inoperative. |

NOTE: Operator MELs must define which items

are approved for inclusion in the fly
away kits and which materials can be
used as ballast.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-14
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-31-03 Forward and Aft

Outflow Valves

-31-03-01
Airplanes Without
OFCR and OFAR
Installed

-31-03-01A C 2 1 (M)(O) One may be inoperative provided:

a) Inoperative outflow valve is locked four |
square inches open, |
b) Manual cabin pressure control is
verified to operate normally on
remaining outflow valve,
c) Air conditioning packs operate normally,
d) At least three cabin air compressors
operate normally,
e) For ground operations at pressure |
altitudes 8,000 feet or higher, aft EE |
cooling overboard exhaust (skin flush) |
valve operates normally, |
f) For ground operations with aft outflow |
valve inoperative and OAT 24 degrees |
C or higher, aft EE cooling overboard |
exhaust (skin flush) valve operates |
normally, and |
g) For ground operations with forward
outflow valve inoperative and OAT 24
degrees C or higher, both packs are
selected on or conditioned air is
supplied to the airplane.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-15
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-31-03 Forward and Aft

Outflow Valves
(Cont’d)

-31-03-01
Airplanes Without
OFCR and OFAR
Installed
(Cont’d)

-31-03-01B C 2 0 (M)(O) May be inoperative provided:

a) Procedures are established and used to
verify cargo compartments remain
empty or contain only ballast, empty
cargo handling equipment (ballast may
be loaded in ULDs), or fly away kits,
b) Flight is conducted unpressurized,
c) Extended overwater flight is prohibited,
and
d) Smoke detection systems in all |
centerline lavatories and in lavatories |
aft of door 4 are considered inoperative. |

NOTE: Operator MELs must define which items

are approved for inclusion in the fly
away kits and which materials can be
used as ballast.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-16
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-31-03 Forward and Aft

Outflow Valves
(Cont’d)

-31-03-02
Airplanes With
OFCR or OFAR
Installed

-31-03-02A C 2 1 (M)(O) One may be inoperative provided:

a) Inoperative outflow valve is locked four |
square inches open, |
b) Manual cabin pressure control is
verified to operate normally on
remaining outflow valve,
c) Air conditioning packs operate normally,
d) At least three cabin air compressors
operate normally,
e) For ground operations at pressure |
altitudes 8,000 feet or higher, aft EE |
cooling overboard exhaust (skin flush) |
valve operates normally, |
f) For ground operations with aft outflow |
valve inoperative and OAT 24 degrees |
C or higher, aft EE cooling overboard |
exhaust (skin flush) valve operates |
normally, |
g) For ground operations with forward
outflow valve inoperative and OAT 24
degrees C or higher, both packs are
selected on or conditioned air is
supplied to the airplane, and
h) For aft outflow valve inoperative, the
OFCR or OFAR is deactivated closed.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-17
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-31-03 Forward and Aft

Outflow Valves
(Cont’d)

-31-03-02
Airplanes With
OFCR or OFAR
Installed
(Cont’d)

-31-03-02B C 2 0 (M)(O) May be inoperative provided:

a) Procedures are established and used to
verify cargo compartments remain
empty or contain only ballast, empty
cargo handling equipment (ballast may
be loaded in ULDs), or fly away kits,
b) Flight is conducted unpressurized,
c) Extended overwater flight is prohibited,
and
d) Smoke detection systems in all |
centerline lavatories and in lavatories |
aft of door 4 are considered inoperative. |

NOTE: Operator MELs must define which items

are approved for inclusion in the fly
away kits and which materials can be
used as ballast.

-31-04 Remote Sensor C 2 1 (M) One may be inoperative deactivated.

Units
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-18
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-31-05 Cabin Rate Of

Climb Indication

-31-05A C 1 0 May be inoperative provided automatic cabin

pressure control channels operate normally.

-31-05B C 1 0 (M)(O) May be inoperative provided:

a) Flight is conducted unpressurized,
b) Procedures are established and used to
verify cargo compartments remain
empty or contain only ballast, empty
cargo handling equipment (ballast may
be loaded in ULDs), or fly away kits,
and
c) Smoke detection systems in all |
centerline lavatories and in lavatories |
aft of door 4 are considered inoperative. |

NOTE: Operator MELs must define which items

are approved for inclusion in the fly
away kits and which materials can be
used as ballast.

-31-06 Cabin Differential

Pressure Indication

-31-06A C 1 0 (O) May be inoperative provided:

a) Cabin altitude indication operates
normally, and
b) A chart is provided to convert cabin
altitude to cabin differential pressure.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-19
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-31-06 Cabin Differential

Pressure Indication
(Cont’d)

-31-06B C 1 0 (M)(O) May be inoperative provided:

a) Flight is conducted unpressurized,
b) Procedures are established and used to
verify cargo compartments remain
empty or contain only ballast, empty
cargo handling equipment (ballast may
be loaded in ULDs), or fly away kits,
and
c) Smoke detection systems in all |
centerline lavatories and in lavatories |
aft of door 4 are considered inoperative. |

NOTE: Operator MELs must define which items

are approved for inclusion in the fly
away kits and which materials can be
used as ballast.

-31-07 Cabin Altitude

Indication

-31-07A C 1 0 (O) May be inoperative provided:

a) Cabin differential pressure indication
operates normally, and
b) A chart is provided to convert cabin
differential pressure to cabin altitude.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-20
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-31-07 Cabin Altitude

Indication (Cont’d)

-31-07B C 1 0 (M)(O) May be inoperative provided:

a) Flight is conducted unpressurized,
b) Procedures are established and used to
verify cargo compartments remain
empty or contain only ballast, empty
cargo handling equipment (ballast may
be loaded in ULDs), or fly away kits,
and
c) Smoke detection systems in all |
centerline lavatories and in lavatories |
aft of door 4 are considered inoperative. |

NOTE: Operator MELs must define which items

are approved for inclusion in the fly
away kits and which materials can be
used as ballast.

-31-08 Outflow Valve C 2 0

Position Indications

-31-09 Auto Cabin C 1 0

Pressure Control
Communication
System

-32-01 Positive Pressure

Relief Valves

-32-01A C 2 1 (M) One may be inoperative deactivated closed.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-21
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-32-01 Positive Pressure

Relief Valves
(Cont’d)

-32-01B C 2 0 (M)(O) May be inoperative provided:

a) Flight is conducted unpressurized,
b) Procedures are established and used to
verify cargo compartments remain
empty or contain only ballast, empty
cargo handling equipment (ballast may
be loaded in ULDs), or fly away kits,
and
c) Smoke detection systems in all |
centerline lavatories and in lavatories |
aft of door 4 are considered inoperative. |

NOTE: Operator MELs must define which items

are approved for inclusion in the fly
away kits and which materials can be
used as ballast.

-32-02 Negative Pressure C 4 0 (M)(O) May be inoperative provided:

Relief Valve a) Flight is conducted unpressurized,
b) Procedures are established and used to
verify cargo compartments remain
empty or contain only ballast, empty
cargo handling equipment (ballast may
be loaded in ULDs), or fly away kits,
and
c) Smoke detection systems in all |
centerline lavatories and in lavatories |
aft of door 4 are considered inoperative. |

NOTE: Operator MELs must define which items

are approved for inclusion in the fly
away kits and which materials can be
used as ballast.

-41-01 Overhead Flight C 1 0 (M) May be inoperative deactivated.

*** Crew Rest (OFCR)
Duct Heater System
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-22
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-41-02 Overhead Flight C 1 0 (M) May be inoperative deactivated.

*** Attendant Rest
(OFAR) Duct
Heater System

-43-01 Forward Cargo C 1 0 (M)(O) May be inoperative provided:

Heat Supply Shutoff a) Valve is deactivated closed, and
Valve b) Forward EE cooling exhaust overboard
vent valve is deactivated open.

-43-02 Forward Cargo C 1 0 (M) May be inoperative provided:

Heat Exhaust a) Exhaust shutoff valve is deactivated
System closed, and
b) Exhaust fan is deactivated.

-43-03 Forward Cargo C 1 0 (M) May be inoperative deactivated.

Heat Electric Heater

-43-04 Forward Cargo C 1 0

Heat OFF Light

-44-01 Bulk Cargo Heat C 1 0 (M)(O) May be inoperative provided:

Supply Fan a) Bulk cargo heat supply fan is
deactivated, and
b) Bulk cargo electric heater is
deactivated.

-44-02 Bulk Cargo Heat C 1 0 (M)(O) May be inoperative provided:

Supply Shutoff a) Bulk cargo heat supply valve is
Valve deactivated closed,
b) Bulk cargo heat supply fan is
deactivated, and
c) Bulk cargo heat electric heater is
deactivated.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-23
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-44-03 Bulk Cargo Heat |

Electric Heater |

-44-03-01 |
CN-AA29229 (Part C 1 0 (M)(O) May be inoperative deactivated. |
C or D) Not |
Incorporated |

-44-03-02 |
CN-AA29229 (Part C 2 0 (M)(O) May be inoperative deactivated. |
C or D) |
Incorporated |

-44-04 Bulk Cargo Heat C 1 0

OFF Light

-45-01 Flight Deck Foot C 4 0 (M) May be inoperative deactivated.

Rest Surface
Heaters

-45-02 Flight Deck C 2 0 (M) May be inoperative deactivated.

Shoulder Duct
Heaters

-45-03 Galley Area Duct C - 0 (M) May be inoperative deactivated.

Heaters

-45-04 Passenger Entry C 8 0 (M) May be inoperative deactivated.

Door Area Floor
Panel Surface
Heater

-45-05 Zonal Duct Heaters C 2 0 (M) May be inoperative deactivated.

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-24
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-51-01 Cabin Air

Compressor (CAC)
Systems

-51-01-01
Airplanes Without
OFCR and OFAR
Installed

-51-01-01-01
Left CACs

-51-01-01-01A C 2 1 (M) One may be inoperative provided:

a) Inoperative CAC is deactivated,
b) Left air conditioning pack operates
normally,
c) VFSGs associated with operating CACs
operate normally,
d) Integrated cooling recirculation air
system operates normally,
e) Center hydraulic system electric motor-
driven pumps operate normally, and
f) Trim air systems operate normally.

-51-01-01-01B C 2 0 (M) May be inoperative provided: |

a) Left CACs are deactivated,
b) Left air conditioning pack is considered
inoperative, and
c) Right trim air system operates normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-25
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-51-01 Cabin Air

Compressor (CAC)
Systems
(Cont’d)

-51-01-01
Airplanes Without
OFCR and OFAR
Installed
(Cont’d)

-51-01-01-02
Right CACs

-51-01-01-02A C 2 1 (M) One may be inoperative provided:

a) Inoperative CAC is deactivated,
b) Right air conditioning pack operates
normally,
c) VFSGs associated with operating CACs
operate normally,
d) Integrated cooling recirculation air
system operates normally,
e) Center hydraulic system electric motor-
driven pumps operate normally, and
f) Trim air systems operate normally.

-51-01-01-02B C 2 0 (M) May be inoperative provided: |

a) Right CACs are deactivated,
b) Right air conditioning pack is
considered inoperative, and
c) Left trim air system operates normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-26
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-51-01 Cabin Air

Compressor (CAC)
Systems
(Cont’d)

-51-01-02
Airplanes With
OFCR or OFAR
Installed

-51-01-02-01
Left CACs

-51-01-02-01A C 2 1 (M) One may be inoperative provided:

a) Inoperative CAC is deactivated,
b) Left air conditioning pack operates
normally,
c) VFSGs associated with operating CACs
operate normally,
d) Integrated cooling recirculation air
system operates normally,
e) Center hydraulic system electric motor-
driven pumps operate normally,
f) Trim air systems operate normally, and
g) For OFCR or OFAR occupied, airplane
remains at or below FL 350.

-51-01-02-01B C 2 0 (M) May be inoperative provided: |

a) Left CACs are deactivated,
b) Left air conditioning pack is considered
inoperative,
c) Right trim air system operates normally,
and
d) For OFCR or OFAR occupied, airplane
remains at or below FL 350.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-27
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-51-01 Cabin Air

Compressor (CAC)
Systems
(Cont’d)

-51-01-02
Airplanes With
OFCR or OFAR
Installed (Cont’d)

-51-01-02-02
Right CACs

-51-01-02-02A C 2 1 (M) One may be inoperative provided:

a) Inoperative CAC is deactivated,
b) Right air conditioning pack operates
normally,
c) VFSGs associated with operating CACs
operate normally,
d) Integrated cooling recirculation air
system operates normally,
e) Center hydraulic system electric motor-
driven pumps operate normally,
f) Trim air systems operate normally, and
g) For OFCR or OFAR occupied, airplane
remains at or below FL350.

-51-01-02-02B C 2 0 (M) May be inoperative provided: |

a) Right CACs are deactivated,
b) Right air conditioning pack is
considered inoperative,
c) Left trim air system operates normally,
and
d) For OFCR or OFAR occupied, airplane
remains at or below FL 350.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-28
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-51-02 Cabin Air C 2 0 (M) May be inoperative provided:

Compressor (CAC) a) Door is deactivated in retracted
Deflector Doors position, and
b) Associated air conditioning pack
operates normally.

-51-03 Cabin Air .

Compressor (CAC)
Inlet Pressure
Sensors

-51-03-01
Left Inlet Pressure
Sensors

-51-03-01A C 2 1

-51-03-01B C 2 0 May be inoperative provided:

a) Right CAC inlet pressure sensors |
operate normally, and |
b) Left air conditioning pack is considered
inoperative.

-51-03-02
Right Inlet Pressure
Sensors

-51-03-02A C 2 1

-51-03-02B C 2 0 May be inoperative provided:

a) Left CAC inlet pressure sensors operate |
normally, and |
b) Right air conditioning pack is
considered inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-29
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-51-04 Cabin Air C 4 2 May be inoperative provided associated CAC is

Compressor (CAC) considered inoperative.
Variable Diffusers

-51-05 Cabin Air C 4 2 May be inoperative provided associated CAC is

Compressor (CAC) considered inoperative.
Add Heat Valves

-51-06 Cabin Air C 4 2 May be inoperative provided associated CAC is

Compressor (CAC) considered inoperative.
Outlet Pressure
Sensors

-51-07 Cabin Air C 4 2 May be inoperative provided associated cabin

Compressor (CAC) air compressor is considered inoperative.
Outlet Temperature
Sensor Systems 

-51-08 Cabin Air C 2 1 (M) One may be inoperative provided one of the
Compressor (CAC) associated CACs is deactivated.
Flow Sensors

-51-09 Pack Control Unit .

(PCU) Channels

-51-09-01
Left PCU Channels

-51-09-01A C 2 1

-51-09-01B C 2 0 May be inoperative provided:

a) At least one right PCU channel
operates normally, and
b) Left air conditioning pack is considered
inoperative.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-30
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-51-09 Pack Control Unit .

(PCU) Channels
(Cont’d)

-51-09-02
Right PCU
Channels

-51-09-02A C 2 1

-51-09-02B C 2 0 May be inoperative provided:

a) At least one left PCU channel operates
normally, and
b) Right air conditioning pack is
considered inoperative.

-52-01 Air Conditioning

Packs

-52-01-01
Airplanes Without C 2 1 (M)(O) One may be inoperative provided:
OFCR and OFAR a) Cabin air compressors associated with
Installed operating pack operate normally,
b) VFSGs associated with operating CACs
operate normally,
c) Integrated cooling recirculation air
system operates normally,
d) Center hydraulic electric motor-driven
pumps operate normally,
e) Alternate ventilation system operates
normally,
f) Opposite trim air system operates
normally,
g) Flight remains within 60 minutes of
landing at a suitable airport, and
h) Appropriate performance adjustments
are applied.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-31
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-52-01 Air Conditioning

Packs
(Cont’d)

-52-01-02
Airplanes With C 2 1 (M)(O) One may be inoperative provided:
OFCR or OFAR a) Cabin air compressors associated with
Installed operating pack operate normally,
b) VFSGs associated with operating CACs
operate normally,
c) Integrated cooling recirculation air
system operates normally,
d) Center hydraulic electric motor-driven
pumps operate normally,
e) Alternate ventilation system operates
normally,
f) Opposite trim air system operates
normally,
g) For OFCR or OFAR occupied, airplane
remains at or below FL 350,
h) Flight remains within 60 minutes of
landing at a suitable airport, and
i) Appropriate performance adjustments
are applied.

-52-02 Pack OFF Lights C 2 0

-52-03 Air Cycle Machines C 2 1 One may be inoperative provided associated air
(ACM) conditioning pack is considered inoperative.

-52-04 Air Cycle Machine C 2 1 One may be inoperative provided:

(ACM) Compressor a) Associated ram air inlet and exit doors
Outlet Temperature operate normally,
Sensor Systems b) Opposite air conditioning pack operates
normally,
c) Opposite cabin air compressors operate
normally, and
d) Opposite trim air system operates
normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-32
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-52-05 Condenser Inlet

Temperature
Control Systems

-52-05-01
Low Limit Valve C 2 1 (M) One may be inoperative provided:
a) Associated low limit valve is deactivated
open,
b) Opposite condenser inlet temperature
sensor system operates normally,
c) Opposite air conditioning pack operates
normally,
d) Opposite cabin air compressors operate
normally, and
e) Opposite trim air system operates
normally.

-52-05-02
Condenser Inlet C 2 1 (M) One may be inoperative provided:
Temperature a) Associated low limit valve is deactivated
Sensor Systems open,
b) Opposite low limit valve operates
normally,
c) Opposite air conditioning pack operates
normally,
d) Opposite cabin air compressors operate
normally, and
e) Opposite trim air system operates
normally.

-52-06 Secondary Heat C 2 0 May be inoperative provided associated

Exchanger Outlet condenser inlet temperature sensor system
Temperature operates normally.
Sensor Systems
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-33
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-52-07 Pack Outlet C 2 1 One may be inoperative provided:

Temperature a) Associated flight deck duct temperature
Sensor Systems sensor operates normally,
b) Opposite air conditioning pack operates
normally,
c) Opposite flight deck zone trim valve
operates normally,
d) Opposite trim air pressure regulator
valve operates normally, and
e) Flight remains within 60 minutes of
landing at a suitable airport.

-52-08 Economy Cooling C 2 1 (M) One may be inoperative provided:

Valves (ECV) a) Valve is deactivated open,
b) Opposite air conditioning pack operates
normally,
c) Opposite cabin air compressors operate
normally, and
d) Opposite trim air system operates
normally.

-52-09 Air Cycle Machine C 2 1 One may be inoperative provided the |

Bypass Valves associated air conditioning pack is considered |
inoperative. |

-52-10 Ram Air Inlet Door C 2 1 (M)(O) One may be inoperative provided:
Systems a) Door is deactivated in open position,
b) Associated ram air exit door operates
normally,
c) Trim air systems operate normally,
d) Associated air conditioning pack is
considered inoperative, and
e) Appropriate performance adjustments
are applied.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-34
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-52-11 Ram Air Outlet Door C 2 1 (M)(O) One may be inoperative provided:
Systems a) Associated outlet door is deactivated
17.5 degrees open,
b) Associated ram air inlet door operates
normally,
c) Trim air systems operate normally,
d) Airplane remains at or below FL 350,
e) Appropriate performance adjustments
are applied, and
f) Flight remains within 60 minutes of
landing at a suitable airport.

-52-12 Ram Air Fan

-52-12-01
Left Ram Air Fan C 1 0 (M)(O) May be inoperative provided:
a) Left ram air fan is deactivated,
b) Right ram air fan operates normally,
c) Right air conditioning pack operates
normally,
d) Right cabin air compressors operate
normally,
e) L2 VFSG operates normally, |
f) R2 VFSG operates normally, |
g) Center hydraulic pump C2 operates
normally,
h) Left PECS aft section operates
normally,
i) Left PECS temperature sensor operates
normally,
j) APU operates normally, and
k) OAT at departure and destination
airport is less than 43 degrees C.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-35
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-52-12 Ram Air Fan

(Cont’d)

-52-12-02
Right Ram Air Fan C 1 0 (M)(O) May be inoperative provided:
a) Right ram air fan is deactivated,
b) Left ram air fan operates normally,
c) Left air conditioning pack operates
normally,
d) Left cabin air compressors operate
normally,
e) L1 VFSG operates normally, |
f) R1 VFSG operates normally, |
g) Center hydraulic pump C1 operates
normally,
h) Right PECS aft section operates
normally,
i) Right PECS temperature sensor
operates normally,
j) APU operates normally, and
k) OAT at departure and destination
airport is less than 43 degrees C.

-52-12-03
Left Ram Air Fan C 1 0 One may be inoperative provided:
Motor Controller a) Right ram air fan motor controller
operates normally,
b) L2 cabin air compressor CMSC
operates normally,
c) L2 VFSG operates normally, |
d) R2 VFSG operates normally, and |
e) Left ram inlet door or ram air exit door
operates normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-36
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-52-12 Ram Air Fan

(Cont’d)

-52-12-04
Right Ram Air Fan C 1 0 One may be inoperative provided:
Motor Controller a) Left ram air fan motor controller
operates normally,
b) R2 cabin air compressor CMSC
operates normally,
c) L1 VFSG operates normally, |
d) R1 VFSG operates normally, and |
e) Right ram inlet door or ram air exit door
operates normally.

-52-12-05
Ram Air Fan C 2 1
Primary Control

-52-12-06
Ram Air Fan C 2 0 May be inoperative provided air conditioning
Backup Control packs operate normally.

-52-13 Pack Bay Overheat

Detection System
(ODS)

-52-13-01
Pack Bay Overheat C 2 1
Detection Channels

-52-13-02
Loops C 4 2 ODS loops associated with one air conditioning
pack may be inoperative provided pack is
considered inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-37
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-53-01 Integrated Cooling

System (ICS)

-53-01-01
Recirculation C 1 0
Cooling Air System

-53-01-02
Individual
Components

-53-01-02A C - 0 (M) Integrated cooling system may be

inoperative deactivated.

-53-01-02B C - 0 (M) Individual components may be inoperative

provided components are deactivated or
isolated.

-54-01 Forward Cargo Air D 1 0 May be inoperative provided FCAC remains

*** Conditioning OFF.
(FCAC) System

-54-01-01
Liquid Cooling D 1 0 (M) May be dispatched with CARGO A/C FWD
System LEAK fault provided FCAC remains OFF.

-54-02 Forward Cargo Air D 1 0 (M) May be inoperative provided:

*** Conditioning a) FCAC boost fan is deactivated,
(FCAC) Boost Fan b) Forward cargo electric heater is
deactivated, and
c) FCAC remains OFF.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-38
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-54-03 Forward Cargo Air

*** Conditioning
(FCAC) Bypass
Valve

-54-03A D 1 0 (M) May be inoperative provided bypass valve is

deactivated open.

-54-03B D 1 0 May be inoperative provided FCAC remains

OFF.

-54-04 Forward Cargo Air D 2 1

*** Conditioning
(FCAC)
Compressor
Systems

-54-05 Forward Cargo Air D 1 0

*** Conditioning
(FCAC) Switch OFF
Light

-61-01 Flight Deck Zone C 2 1 (M) One may be inoperative provided:

Trim Valves a) Valve is deactivated closed, and
b) Opposite trim air pressure regulator
valve operates normally, and
c) Flight remains within 60 minutes of
landing at a suitable airport.

-61-02 Flight Deck Zone C 2 1 (M) One may be inoperative provided:

Duct Temperature a) Associated flight deck trim zone valve
Sensor Systems is deactivated closed,
b) Opposite trim air pressure regulator
valve operates normally,
c) Opposite flight deck zone trim valve
operates normally, and
d) Flight remains within 60 minutes of
landing at a suitable airport.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-39
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-61-03 Flight Deck Zone C 1 0 May be inoperative provided:

Air Temperature a) At least one air conditioning pack
Sensor System operates normally,
b) Trim air pressure regulator valve
associated with operating pack
operates normally,
c) Flight deck zone duct temperature
sensor system associated with
operating pack operates normally, and
d) Flight deck zone trim valve associated
with operating pack operates normally.

-61-04 Cabin Zone Trim C 4 2 (M) May be inoperative provided:

Valves a) Valve is deactivated closed, and
b) Opposite trim air pressure regulator
valve operates normally, and
c) Flight remains within 60 minutes of
landing at a suitable airport..

-61-05 Cabin Zone Duct

Temperature
Sensor Systems

-61-05-01
Zones A1 and B1 C 2 0 (M) May be inoperative provided associated
cabin zone heater is deactivated.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-40
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-61-05 Cabin Zone Duct

Temperature
Sensor Systems
(Cont’d)

-61-05-02
Zones A2, B2, C,
and D

-61-05-02A C 4 2 (M) May be inoperative provided:

a) Associated zone trim valve is
deactivated closed,
b) Opposite trim air pressure regulator
valve operates normally, and
c) Flight remains within 60 minutes of
landing at a suitable airport.

-61-05-02B C 4 2 May be inoperative provided:

a) Opposite trim air pressure regulator
valve operates normally,
b) For sensor A2 or C inoperative, right
trim air switch remains off,
c) For sensor B2 or D inoperative, left trim
air switch remains off, and
d) Flight remains within 60 minutes of
landing at a suitable airport.

-62-01 Trim Air Pressure C 2 1 (M)(O) One may be inoperative provided:

Regulator Valves a) Valve is deactivated closed,
b) Opposite flight deck zone trim valve
operates normally, and
c) Flight remains within 60 minutes of
landing at a suitable airport.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-41
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-62-02 Trim Air Pressure C 2 0

Sensor Systems

-62-03 Trim Air FAULT C 2 0

Lights

-71-01 Flight Deck D 1 0 (M) May be inoperative provided water supply

*** Humidification valve is deactivated closed.
System

-71-02 Overhead Flight D 1 0 (M) May be inoperative provided water supply

*** Crew Rest (OFCR) valve is deactivated closed.
Humidification
System

-71-03 Overhead Flight D 1 0 (M) May be inoperative provided water supply

*** Attendant Rest valve is deactivated closed.
(OFAR)
Humidification
System

-72-01 Zonal Dryer C 2 0 (M) May be inoperative deactivated.

Systems

-73-01 Ozone Converters C 2 - As required by FAR.

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-42
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-81-01 Power Electronics C 2 1 (M) One may be inoperative provided:

Cooling System a) Leak is verified to be in aft section of
(PECS) Aft the loop,
Section b) Associated isolation valve is
deactivated closed,
c) Associated fluid level is verified to be
adequate, and
d) Associated ram air fan operates
normally.

-81-02 Power Electronics C 2 1 (M) One may be inoperative provided:

Cooling System a) Associated PECS loop fluid level is
(PECS) Fluid verified to be within limits every five
Level Sensor flight days,
Systems b) Associated PECS liquid ICS/SCU
supply pressure sensor operates
normally, and
c) Associated PECS liquid cooling
temperature sensor operates normally.

-81-03 Power Electronics C 2 1 (M) One may be inoperative deactivated open.

Cooling System
(PECS) Liquid
ICS/SCU Supply
Shutoff Valve

-81-04 Power Electronics C 2 1 One may be inoperative provided associated

Cooling System PECS fluid level sensor system operates
(PECS) Liquid normally.
ICS/SCU Supply
Pressure Sensor
Systems

-81-05 Power Electronics C 4 3 (M) One may be inoperative deactivated.

Cooling System
(PECS) Pumps
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 21-43
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
21 AIR CONDITIONING

-81-06 Power Electronics

Cooling System
(PECS)
Temperature
Control Systems

-81-06-01
Liquid Cooling C 2 1 (M) One may be inoperative provided
Temperature associated temperature control valve is
Control Valves deactivated open.

-81-06-02
Liquid Cooling C 2 1 (M) One may be inoperative provided
Temperature associated temperature control valve is
Sensors deactivated open.

-81-07 Power Electronics C 2 0

Cooling System
(PECS) Liquid
Pump Filter
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 22-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
22 AUTOFLIGHT

-11-01 Autoflight Function C 1 0 (M) May be dispatched with AUTOFLIGHT

FUNCTION faults provided A/P DISENGAGE bar
is verified to operate normally.

-11-02 Autopilot Backdrive

Actuator Systems

-11-02A C 3 2 (M)(O) One may be inoperative provided:

a) Associated backdrive actuator is
deactivated, and
b) Autopilot disconnect warning indications
are verified to operate normally before
each departure.

-11-02B B 3 0 (M)(O) May be inoperative provided:

a) Associated backdrive actuator is
deactivated, and
b) Autopilot disconnect warning indications
are verified to operate normally before
each departure.

-11-03 Flight Director C 2 0 May be inoperative provided procedures do not

Systems require their use.

-11-04 Mode Control Panel

Windows

-11-04-01
Airspeed C 1 0
(IAS - MACH)

-11-04-02
Heading C 1 0
(HDG - TRK)

-11-04-03
Vertical Speed C 1 0
(V/S - FPA)

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 22-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
22 AUTOFLIGHT

-11-04 Mode Control Panel

Windows
(Cont’d)

-11-04-04
Altitude (ALTITUDE) C 1 0

-11-04-05
Uplink (UL) Windows

-11-04-05A C 3 0 (O) May be inoperative provided alternate

procedures are established and used.

-11-04-05B D 3 0 May be inoperative provided procedures do not

require their use.

-11-04-06
Window Lighting B 1 0 May be inoperative provided MCP uplink (UL)
windows are considered inoperative.

-11-05 Mode Control Panel

Selectors

-11-05-01
V/S - FPA Selector C 1 0
(DOWN, UP)

-11-05-02
BANK LIMIT Selector C 1 0
(AUTO, 5, 10, 15, 20,
25, 30)
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 22-3
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
22 AUTOFLIGHT

-11-05 Mode Control Panel

Selectors
(Cont’d)

-11-05-03
Altitude Increment C 1 0 May be inoperative provided AUTO position
Selector operates normally.
(AUTO, 1000)

-11-05-04
Selector Push
Functions

-11-05-04-01
IAS - MACH C 1 0

-11-05-04-02
HDG - TRK SEL C 1 0

-11-05-04-03
ALTITUDE C 1 0

-11-06 Mode Control Panel

Switches

-11-06-01
A/P Engage Switches

-11-06-01A C 2 1

-11-06-01B B 2 0 May be inoperative provided:

a) Approach minimums do not require use
of the autopilots,
b) Number of flight segments and segment
duration is acceptable to flight crew, and
c) Enroute operations do not require use of
the autopilots.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 22-4
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
22 AUTOFLIGHT

-11-06 Mode Control Panel

Switches
(Cont’d)

-11-06-02
Autothrottle Arm
Switches
(A/T ARM L, R)

-11-06-02A C 2 1 (M)(O) One may be inoperative provided:

a) Associated servo motor is deactivated,
b) EEC normal mode operates normally,
and
c) Both thrust levers are manually set for
takeoff and go-around thrust.

-11-06-02B C 2 0 May be inoperative provided:

a) EEC normal mode operates normally,
b) Approach minimums do not require
autothrottle use, and
c) Flight remains within 180 minutes of
landing at a suitable airport.

-11-06-03
A/T Engage Switch C 1 0 May be inoperative provided:
a) Approach minimums do not require
autothrottle use,
b) EEC normal mode operates normally,
and
c) Flight remains within 180 minutes of
landing at a suitable airport.

-11-06-04
F/D Switches C 2 0 May be inoperative provided procedures do not
require flight director use.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 22-5
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
22 AUTOFLIGHT

-11-06 Mode Control Panel

Switches
(Cont’d)

-11-06-05
IAS - MACH C 1 0 May be inoperative provided IAS is displayed in
Reference Switch associated window.

-11-06-06
HDG - TRK C 1 0 May be inoperative provided HDG is displayed in
Reference Switch associated window.

-11-06-07
V/S - FPA Reference C 1 0
Switch

-11-06-08
APP Switch C 1 0 May be inoperative provided approach minimums
do not require use of autopilot or flight director.

-11-06-09
CLB CON, LNAV, C 8 0 May be inoperative provided enroute operations
VNAV, FLCH, do not require their use.
VS/FPA,
Heading/Track HOLD,
Altitude HOLD, and
LOC/FAC Switches

-11-06-10
Arm/Engage Lights C 11 0 May be inoperative provided the associated
mode indications on both PFDs operate normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 22-6
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
22 AUTOFLIGHT

-11-06 Mode Control Panel

Switches
(Cont’d)

-11-06-11
Uplink (UL) XFR
Switches

-11-06-11A C 3 0 (O) May be inoperative provided alternate

procedures are established and used.

-11-06-11B D 3 0 May be inoperative provided procedures do not

require their use.

-11-07 Automatic Landing C 1 0 May be inoperative provided approach minimums |

System (Autoland) do not require its use. |

-11-07-01 |
Triple Channel C 1 0 May be inoperative provided approach minimums |
Autoland (LAND 3) do not require its use. |

-11-08 Control Wheel

Autopilot Disconnect
Switches

-11-08A C 2 1 One may be inoperative provided:

a) Autopilot is not used below 1,500 feet
AGL, and
b) Approach minimums do not require the
use of the autopilot.

-11-08B B 2 0 May be inoperative provided:

a) Autopilot is not used,
b) Approach minimums do not require use
of the autopilot,
c) Number of flight segments and segment
duration is acceptable to flight crew, and
d) Enroute operations do not require use of
the autopilot.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 22-7
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
22 AUTOFLIGHT

-11-09 Takeoff/Go-Around
(TO/GA) Switches

-11-09A C 2 1 One may be inoperative provided approach

minimums do not require its use.

-11-09B C 2 0 May be inoperative provided:

a) EEC normal mode operates normally,
b) Both thrust levers are operated manually
for takeoff and go-around, and
c) Autopilot and flight director are not used
below 500 feet AGL or MDA, whichever
is higher.

-31-01 Autothrottle System C 1 0 May be inoperative provided: |

a) EEC normal mode operates normally, |
b) Approach minimums do not require its |
use, and |
c) Flight remains within 180 minutes of |
landing at a suitable airport. |
|
NOTE: Any mode which operates normally may |
be used. |

-31-02 Autothrottle Servo

Motors

-31-02A C 2 1 (M)(O) One may be inoperative provided:

a) Associated servo motor is deactivated,
b) EEC normal mode operates normally,
and
c) Both thrust levers are manually set for
takeoff and go-around thrust.

-31-02B C 2 0 (M)(O) May be inoperative provided:

a) Both servo motors are deactivated,
b) EEC normal mode operates normally,
c) Approach minimums do not require use
of the autothrottles, and
d) Flight remains within 180 minutes of
landing at a suitable airport.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 22-8
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
22 AUTOFLIGHT

-31-03 Autothrottle
Disconnect Switches

-31-03A C 2 1 One may be inoperative provided both A/T ARM

switches operate normally.

-31-03B C 2 0 May be inoperative provided:

a) EEC normal mode operates normally,
b) Autothrottles are not armed,
c) Approach minimums do not require use
of autothrottles, and
d) Flight remains within 180 minutes of
landing at a suitable airport.

-31-04 Takeoff Thrust C 1 0 (O) May be dispatched with T/O THRUST

Disagree Monitor DISAGREE fault.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 23-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
23 COMMUNICATIONS

-11-01 High Frequency (HF)

Communication
Systems

-11-01A C 2 1 (O) One may be inoperative while conducting

operations that require two LRCS provided:
a) SATCOM voice or datalink operates
normally,
b) Alternate procedures are established and
used,
c) SATCOM voice coverage is available |
over the intended route of flight, and |
d) If SATCOM voice is to be used over the |
intended route of flight, SATCOM voice |
short codes (INMARSAT) or direct dial |
commercial numbers (IRIDIUM) must be |
available. If not available, prior |
coordination with the appropriate ATS |
(FIR) facility is required. |

NOTE: SATCOM is to be used only as a backup |

to normal HF communications. |

-11-01B D 2 - Any in excess of those required by FAR may be

inoperative.

-11-01-01
HF Datalink

-11-01-01A C 1 0 (O) May be inoperative provided alternate

procedures are established and used.

-11-01-01B D 1 0 May be inoperative provided procedures do not

require its use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 23-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
23 COMMUNICATIONS

-12-01 VHF Communications D 3 - Any in excess of those required by FAR may be

Systems inoperative provided left VHF radio operates
normally.

-12-01-01
VHF Datalink

-12-01-01A C 1 0 (O) May be inoperative provided alternate

procedures are established and used.

-12-01-01B D 1 0 May be inoperative provided procedures do not

require its use.

-15-01 Satellite
*** Communication
(SATCOM) Systems

-15-01A C 1 0 (O) May be inoperative provided:

a) Alternate procedures are established and
used, and
b) Flight remains within 180 minutes of
landing at a suitable airport.

-15-01B D 1 0 May be inoperative provided procedures do not

require its use.

-15-01-01
SATCOM Datalink

-15-01-01A C 1 0 (O) May be inoperative provided alternate

procedures are established and used.

-15-01-01B D 1 0 May be inoperative provided procedures do not

require its use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 23-3
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
23 COMMUNICATIONS

-21-01 Selective Call

Function (SELCAL)

-21-01A C 1 0 (O) May be inoperative provided alternate

procedures are established and used.

-21-01B D 1 0 May be inoperative provided procedures do not

require its use.

-21-01-01
Channels

-21-01-01A C 5 0 (O) May be inoperative provided alternate |

procedures are established and used.

-21-01-01B D 5 0 May be inoperative provided procedures do not |

require its use.

-24-01 Tuning and Control C 3 2 One may be inoperative provided:

Panels (TCP) a) Left tuning and control panel operates
normally, and
b) Inoperative tuning and control panel
remains OFF.

-24-01-01
Left TCP Backup C 1 0
Navigation Function
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 23-4
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
23 COMMUNICATIONS

24-02 Emergency Locator

Transmitter (ELT)
(Fixed)

24-02A A 1 0 (M) May be inoperative provided:

a) System is deactivated, and
b) Repairs are made within 90 days.

24-02B A 1 0 May be missing provided repairs are made within

90 days.

24-02C D 1 0 (M) Any in excess of those required by FAR may

be inoperative provided system is deactivated.

24-02D D 1 0 Any in excess of those required by FAR may be

missing.

-27-01 Communication
Management System
(Datalink)

-27-01A C 2 1

-27-01B C 2 0 (O) May be inoperative provided:

a) Alternate procedures are established and
used, and
b) Flight remains within 180 minutes of
landing at a suitable airport.

-27-01C D 2 0 May be inoperative provided procedures do not

require its use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 23-5
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
23 COMMUNICATIONS

-41-01 Service Interphone

System

-41-01-01
Nose Gear Jack

-41-01-01A C 1 0 (O) Service interphone flight deck to

ground/ground to flight deck function may be
inoperative provided:
a) Nose gear flight interphone jack operates
normally, and
b) Alternate procedures are established and
used.

-41-01-01B B 1 0 (O) May be inoperative provided alternate

procedures are established and used.

-41-01-02
Left Main Gear Jack D 1 0 May be inoperative provided procedures do not
require its use.

-51-01 Flight Crew Audio C 2 1 (O) First officer’s audio control panel may be
Control Panels (ACP) inoperative provided first observer’s audio control
panel operates normally.

-51-01-01
Network Channels C 4 2 One may be inoperative for each audio control
panel.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 23-6
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
23 COMMUNICATIONS

-51-02 Flight Deck Hand

*** Microphones

-51-02A C - 0 May be inoperative or missing provided

associated boom microphone operates normally.

-51-02B D - 0 May be inoperative or missing provided

procedures do not require their use.

-51-03 Flight Deck Headsets/ D - - Any in excess of those required by 14 CFR may |
Headphones be inoperative.

-51-03-01
Headset Boom A - 0 May be inoperative provided:
Microphones a) Associated hand microphone is installed
and operates normally, and |
b) Repairs are made within three flight |
days.

-51-03-02
Headset Earphones/ C - 1 Either captain’s or first officer’s
Headphones earphones/headphones may be inoperative
provided associated flight deck speaker system
operates normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 23-7
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
23 COMMUNICATIONS

-51-04 Microphone
(MIC)/Interphone
Switches

-51-04-01
Control Wheel C 2 1 (M) One may be inoperative provided:
MIC/Interphone a) Affected switch is deactivated open, and
Switches b) Associated audio control panel
MIC/interphone switch operates
normally.

-51-04-02
Flight Crew Audio C 2 1 (M) One may be inoperative provided:
Control Panel a) Affected switch is verified inoperative
MIC/Interphone open, and
Switches b) Associated control wheel MIC/interphone
switch operates normally.

-51-04-03
Glareshield MIC C 2 0 (M) May be inoperative provided the affected
Switches switch is deactivated open.

-51-05 Flight Deck Speaker C 2 1 One may be inoperative provided:

Systems a) Associated headset earphones or
headphones are installed and operate
normally,
b) Master warning lights operate normally,
and
c) Master caution lights operate normally.

-51-06 Audio Gateway Units C 4 3 (O) Forward right audio gateway unit may be
inoperative provided:
a) Service interphone nose gear jack is
considered inoperative, and
b) Alternate procedures are established and
used.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 23-8
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
23 COMMUNICATIONS

-51-07 Flight Deck Analog C 1 0

Audio Communication

-75-01 Flight Deck Door

Visual Surveillance
Systems

-75-01-01
***
Video Surveillance
System

-75-01-01A A 1 0 (O) May be inoperative and components may be

missing provided:
a) Alternate procedures are established and
used, and
b) Repairs are made within three flight
days.

NOTE: Any portion of the system which operates

normally may be used.

-75-01-01B C 1 0 (O) May be inoperative and components may be

missing provided:
a) Flight deck door viewing port operates
normally, and
b) Alternate procedures are established and
used.

NOTE: Any portion of the system which operates

normally may be used.

-75-01-01C D 1 0 May be inoperative and components may be

missing provided procedures do not require its
use.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 23-9
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
23 COMMUNICATIONS

-75-01 Flight Deck Door

Visual Surveillance
Systems
(Cont’d)

-75-01-02
Flight Deck Door
Viewing Port

-75-01-02A A 1 0 (O) May be inoperative provided:

a) Alternate procedures are established and
used, and
b) Repairs are made within three flight
days.

-75-01-02B C 1 0 (O) May be inoperative provided:

a) Video surveillance system is installed
and operates normally, and
b) Alternate procedures are established and
used.

-93-01 Pilots’ Overhead C 22 11 One control/communication channel (A or B) for

Panel Control/ each overhead control panel may be inoperative.
Communication
Channels
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 24-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER

-00-01 Electrical Synoptic C 1 0

Display

-11-01 Variable Frequency C 4 0

Starter Generator
(VFSG) DRIVE
Lights

-11-02 Variable Frequency C 4 0 (M)(O) May be inoperative locked open.

Starter Generator
(VFSG)
Air/Oil Heat
Exchanger Air
Control Valves (RR)

-15-01 Common Motor Start

Controller (CMSC)

-15-01-01
Main Engine C 4 3 (M)(O) One may be inoperative provided:
Start/Cabin Air a) Inoperative CMSC is deactivated,
Compressor b) Associated VFSG starter system is
considered inoperative,
c) Associated cabin air compressor is
considered inoperative, and
d) For CMSC L1 inoperative, left ASG |
starter is considered inoperative

-15-01-02
Center Hydraulic C 2 1 One may be inoperative provided associated |
System center hydraulic system electric motor-driven
pump is considered inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 24-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER

-21-01 Variable Frequency C 4 0 |

Starter Generator |
(VFSG) Electronic |
Chip Detector |
Systems |

-22-01 Variable Frequency

Starter Generator
(VFSG) Systems

-22-01-01 |
RR Without RR A 4 3 (M)(O) One may be inoperative provided: |
Modification 72-H666 a) Inoperative VFSG is disconnected, |
Installed b) Both APU starter generator (ASG) |
systems operate normally,
c) Left APU generator control unit operates
normally,
d) APU battery operates normally,
e) APU battery charger operates normally,
f) Integrated cooling recirculation air
system operates normally,
g) Associated engine fuel return-to-tank
system operates normally,
h) APU is started before departure and
operated continuously throughout the
flight,
i) For L2 or R2 VFSG inoperative,
scheduled flight time does not exceed 6
hours,
j) For L2 or R2 VFSG inoperative,
associated engine oil quantity is verified
to be 18 quarts or greater before each
departure,
k) Flight remains within 180 minutes of
landing at a suitable airport, and
l) Repairs are made within three flight
days.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 24-3
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER

-22-01 Variable Frequency

Starter Generator
(VFSG) Systems
(Cont’d)

-22-01-02 |
RR With RR A 4 3 (M)(O) One may be inoperative provided: |
Modification 72-H666 a) Inoperative VFSG is disconnected, |
Installed b) Both APU starter generator (ASG) |
systems operate normally,
c) Left APU generator control unit operates
normally,
d) APU battery operates normally,
e) APU battery charger operates normally,
f) Integrated cooling recirculation air
system operates normally,
g) Associated engine is not started on the
ground at OAT above 45 degrees C
unless remaining VFSG oil temperature
is at or below 80 degrees C,
h) APU is started before departure and
operated continuously throughout the
flight,
i) Flight remains within 180 minutes of
landing at a suitable airport, and
j) Repairs are made within three flight
days.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 24-4
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER

-22-01 Variable Frequency

Starter Generator
(VFSG) Systems
(Cont’d)

-22-01-03 |
GE A 4 3 (M)(O) One may be inoperative provided:
a) Inoperative VFSG is disconnected,
b) Both APU starter generator (ASG)
systems operate normally,
c) Left APU generator control unit operates
normally,
d) APU battery operates normally,
e) APU battery charger operates normally,
f) Integrated cooling recirculation air
system operates normally,
g) APU is started before departure and
operated continuously throughout the
flight,
h) Flight remains within 180 minutes of
landing at a suitable airport, and
i) Repairs are made within three flight
days.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 24-5
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER

-22-01 Variable Frequency

Starter Generator
(VFSG) Systems
(Cont’d)

-22-01-04 |
Starter Systems

-22-01-04-01 |
RR |

-22-01-04-01A C 4 2 One starter system on each engine may be |

inoperative provided associated engine is not
started on the ground at OAT above 45 degrees
C.

-22-01-04-01B C 4 2 (M) One starter system on each engine may be |

inoperative provided associated engine is not
started on the ground at OAT above 45 degrees
C unless remaining starter VFSG oil temperature
is at or below 80 degrees C.

-22-01-04-02 |
GE C 4 2 One starter system on each engine may be
inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 24-6
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER

-22-02 APU Starter C 2 0 (O) May be inoperative provided:

Generator (ASG) a) APU is not used,
Systems b) Left AGCU operates normally,
c) VFSG systems operate normally, and
d) Flight remains within 180 minutes of
landing at a suitable airport.

-22-02-01 |
Left ASG Generator C 1 0 (M)(O) May be inoperative provided: |
a) Left ASG starter is deactivated, |
b) APU battery operates normally, |
c) APU SPU operates normally, |
d) Right ASG generator operates normally, |
e) Right ASG starter operates normally, |
f) VFSG systems operate normally, and |
g) Flight remains within 180 minutes of |
landing at a suitable airport. |

-22-02-02 |
Left ASG Starter C 1 0 May be inoperative provided: |
a) APU battery operates normally,
b) APU SPU operates normally,
c) Right ASG generator operates normally,
and
d) Right ASG starter operates normally.

-22-02-03 |
Right ASG C 1 0 (M)(O) May be inoperative provided: |
Generator a) Right ASG starter is deactivated, |
b) Left AGCU operates normally,
c) Left ASG generator operates normally,
d) Left ASG starter operates normally,
e) VFSG systems operate normally, and
f) Flight remains within 180 minutes of
landing at a suitable airport.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 24-7
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER

-22-02 APU Starter

Generator (ASG)
Systems
(Cont’d)

-22-02-04 |
Right ASG Starter C 1 0 May be inoperative provided: |
a) Left AGCU operates normally, |
b) Left ASG generator operates normally, |
and |
c) Left ASG starter operates normally, |

-22-03 APU Generator

Control Units
(AGCU)

-22-03-01
Left AGCU C 1 0 (O) May be inoperative provided:
a) APU operates normally,
b) APU battery operates normally,
c) APU SPU operates normally,
d) Right ASG generator operates normally, |
e) Right ASG starter operates normally,
f) VFSG systems operate normally, and
g) Flight remains within 180 minutes of
landing at a suitable airport.

-25-01 Galley C 1 0 (M) May be inoperative deactivated.

Autotransformer Unit
(GATU)

-28-01 GEN CTRL OFF C 4 0

Lights

-28-02 APU GEN OFF C 2 0

Lights
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 24-8
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER

-28-03 IFE/PASS SEATS C 1 0

OFF Light

-28-04 CABIN/UTILITY OFF C 1 0

Light

-31-01 APU Battery C 1 0 (M)(O) May be inoperative provided:

a) APU is not used,
b) Left AGCU operates normally,
c) VFSG systems operate normally, and
d) Flight remains within 180 minutes of
landing at a suitable airport.

-31-02 APU Start Power

Unit (SPU)

-31-02A C 1 0 May be inoperative provided:

a) APU operates normally,
b) APU battery operates normally,
c) Left AGCU operates normally,
d) Left ASG generator operates normally, |
e) Left ASG starter operates normally, and
f) Right ASG system operates normally.

-31-02B C 1 0 (O) May be inoperative provided:

a) APU is not used,
b) Left AGCU operates normally,
c) VFSG systems operate normally, and
d) Flight remains within 180 minutes of
landing at a suitable airport.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 24-9
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER

-31-03 APU Battery Charger

-31-03A C 1 0 (M) May be inoperative provided:

a) APU battery charger is deactivated,
b) APU battery voltage is verified to be
sufficient for APU start before each
departure,
c) APU operates normally,
d) One ASG starter operates normally,
e) Left ASG generator operates normally, |
and |
f) Right ASG generator operates normally. |

-31-03B C 1 0 (M)(O) May be inoperative provided:

a) APU battery charger is deactivated,
b) APU is not used,
c) Left AGCU operates normally,
d) VFSG systems operate normally, and
e) Flight remains within 180 minutes of
landing at a suitable airport.

-38-01 Main and APU

Battery Enclosure
Systems

-38-01-01
Pressure Burst Discs C 2 0 |

-38-01-02
Burst Disc Indicators C 2 0 |

-41-01 External Power C 3 0

Systems

-41-01-01
AVAIL Lights C 3 0 (O) May be inoperative provided alternate
(Flight Deck) procedures are established and used.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 24-10
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER

-41-01-02
ON Lights C 3 0 (O) May be inoperative provided alternate
(Flight Deck) procedures are established and used.

-41-01-03
CONNECTED Lights C 3 0 (O) May be inoperative provided alternate
(External Power procedures are established and used.
Panels)

-41-01-04
NOT IN USE Lights C 3 0 (O) May be inoperative provided alternate
(External Power procedures are established and used.
Panels)

-71-01 Remote Power

Distribution Unit
(RPDU) Channels

-71-01-01
Standard RPDU
Channels

-71-01-01A C 26 13 One channel in each standard RPDU may be

inoperative provided gateway RPDU channels
operate normally.

-71-01-01B B 26 22 One channel in each standard RPDU associated

with an inoperative gateway RPDU channel may
be inoperative.

-71-01-02
Gateway RPDU B 8 7 One may be inoperative provided any inoperative
Channels standard RPDU channels are associated with the
inoperative gateway RPDU channel.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-00-01 Non-Essential - 0 May be inoperative, damaged or missing

*** Equipment and provided that the item(s) is deferred in
Furnishings (NEF) accordance with the operator’s NEF deferral
program. The NEF program, procedures and
processes must be outlined in the operator’s
appropriate document. (M) and (O) procedures,
if required, must be available to the flight crew
and included in the operator’s appropriate
document.

NOTE: Exterior lavatory door ash trays are not

considered NEF items.

-10-01 Secondary Flight

*** Deck Door (Privacy
Barrier)

-10-01A C 1 0 (O) May be inoperative in retracted position or

missing provided alternate procedures are
established and used.

-10-01B D 1 0 May be inoperative in retracted position or

missing provided procedures do not require its
use.

-11-01 Flight Crew Seats

-11-01-01
Power Adjustment D 2 0 (M) May be inoperative deactivated.
Systems

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-11-01 Flight Crew Seats

(Cont’d)

-11-01-02
Manual Adjustment
System

-11-01-02-01
Recline Systems A 2 0 (M) May be inoperative provided:
a) Seat is secured in an upright position
acceptable to the affected crew member,
and
b) Repairs are made within two flight days.

-11-01-02-02
Vertical Adjustments C 2 0 May be inoperative provided associated vertical power
adjustment system operates normally.

-11-01-02-03
Armrests B 4 0 (M) May be inoperative provided:
a) Affected armrest is stowed in the
retracted position or removed, and
b) Seat is acceptable to affected crew
member.

-11-01-02-04
Lumbar/Thigh C 4 0 May be inoperative provided seat is acceptable
Supports to the affected crew member.

-11-01-02-05
Headrests C 2 0 May be inoperative provided seat is acceptable
to the affected crew member.

-11-01-02-06
Seat Pan Tilt C 2 0 (M) May be inoperative provided:
a) Associated seat pan is secured in the
horizontal (untilted) position, and
b) Seat is acceptable to affected crew
member.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-3
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-11-02 Observer Seats

-11-02-01
First Observer Seat
(Including Associated
Equipment)

-11-02-01A A 1 0 May be inoperative provided:

a) A passenger seat in the passenger cabin
is made available to an FAA inspector for
the performance of official duties, and
b) Repairs are made within two flight days.

-11-02-01B A 1 0 May be inoperative provided:

a) Second observer seat is available, and
acceptable to an FAA inspector for the
performance of official duties, and
b) Repairs are made within two flight days.

-11-02-01C A 1 0 May be inoperative provided:

a) First observer seat is acceptable to the
FAA inspector for the performance of
official duties,
b) Required minimum safety equipment
(safety belt, oxygen and life vest) is
available, and
c) Repairs are made within two flight days.

NOTE 1: These provisos are intended to provide

for occupancy of the above seat by an
FAA inspector when the minimum
safety equipment (safety belt, oxygen
and life vest) is functional and the
inspector determines the conditions to
be acceptable.

NOTE 2: The Pilot-in-Command will determine if

the minimum safety equipment is
functional for the other persons
authorized to occupy an observer seat.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-4
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-11-02 Observer Seats

(Cont’d)

-11-02-02
Second Observer D 1 0 NOTE: The Pilot-in-Command will determine if
Seat (Including the minimum safety equipment is
Associated functional for the other persons
Equipment) authorized to occupy an observer seat.

-18-01 Flotation Equipment D - - Any in excess of those required by FAR may be

inoperative or missing provided required
distribution is maintained.

-25-01 Flight Attendant Seat

Assembly (Single or
Dual Position)

-25-01-01
Required Flight
Attendant Seats

-25-01-01A B - - (M)(O) One seat position or assembly (dual

position) may be inoperative provided:
a) Folding type seat stows automatically or
is secured in the retracted position,
b) Passenger seat assigned to flight
attendant is placarded FOR FLIGHT
ATTENDANT USE ONLY,
c) Affected seat position or seat assembly
is not occupied,
d) Flight attendant(s) displaced by
inoperative seat(s) occupies either an
adjacent flight attendant seat or the
passenger seat which is most accessible
to the inoperative seat(s), so as to most
effectively perform assigned duties, and
e) Alternate procedures are established and
used as published in crew member
manuals.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-5
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-25-01 Flight Attendant Seat

Assembly (Single or
Dual Position)
(Cont’d)

-25-01-01
Required Flight
Attendant Seats
(Cont’d)

-25-01-01A (Cont’d) NOTE 1: An automatic folding seat that will not

stow automatically is considered
inoperative.

NOTE 2: A seat position with an inoperative or

missing restraint system is considered
inoperative.

NOTE 3: Individual operators, when operating

with inoperative seats, will consider the
locations and combinations of seats to
ensure that proximity to exits and
distribution requirements of the
applicable FARs are met.

NOTE 4: If one side of a dual seat assembly is

inoperative and a flight attendant is
displaced to the adjacent seat, the
adjacent seat must operate normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-6
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-25-01 Flight Attendant Seat

Assembly (Single or
Dual Position)
(Cont’d)

-25-01-01
Required Flight
Attendant Seats
(Cont’d)

-25-01-01B C - 0 (M)(O) May be inoperative provided:

a) No passengers are carried,
b) A maximum of 19 persons authorized by
14 CFR for non-passenger carrying
operations are carried,
c) Folding type seat stows automatically or
is secured in the retracted position,
d) Affected seat position or seat assembly
is not occupied, and
e) Alternate procedures are established and
used.

NOTE 1: An automatic folding seat that will not

stow automatically is considered
inoperative.

NOTE 2: A seat position with an inoperative or

missing restraint system is considered
inoperative.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-7
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-25-01 Flight Attendant Seat

Assembly (Single or
Dual Position)
(Cont’d)

-25-01-02
Excess Flight C - - (M) May be inoperative provided:
Attendant Seats a) Folding type seat stows automatically or
is secured in the retracted position, and
b) Affected seat position or seat assembly
is not occupied.

NOTE 1: An automatic folding seat that will not

stow automatically is considered
inoperative.

NOTE 2: A seat position with an inoperative or

missing restraint system is considered
inoperative.

-25-02 Passenger Seats D - - May be inoperative provided:

a) Seat does not block an emergency exit,
b) Seat does not restrict any passenger
from access to the main airplane aisle,
and
c) Affected seat(s) is blocked and
placarded DO NOT OCCUPY.

NOTE 1: A seat with an inoperative seat belt is

considered inoperative.

NOTE 2: Inoperative seats do not affect the

required number of flight attendants.

NOTE 3: Affected seats may include the seats

behind and/or adjacent outboard seats.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-8
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-25-02 Passenger Seats

(Cont’d)

-25-02-01
Recline Mechanism

-25-02-01A D - - (M) May be inoperative and seat occupied

provided seat is secured in the full upright
position.

-25-02-01B D - - May be inoperative and seat occupied provided

seat back is immovable in the full upright
position.

-25-02-02
Underseat Baggage C - - (O) May be inoperative provided:
Restraining Bars a) Baggage is not stowed under seat with
inoperative restraining bar,
b) Associated seat is placarded DO NOT
STOW BAGGAGE UNDER THIS SEAT,
and
c) Procedures are established to alert cabin
crew of inoperative restraining bar.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-9
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-25-02 Passenger Seats

(Cont’d)

-25-02-03
Armrests with Recline D - - (M) May be inoperative or missing and seat
Mechanism occupied provided:
a) Armrest does not block an emergency
exit,
b) Armrest does not restrict any passenger
from access to the main airplane aisle,
and
c) If armrest is missing, associated seat is
secured in the full upright position.

-25-02-04
Armrests without D - - May be inoperative or missing and seat occupied
Recline Mechanism provided:
a) Armrest does not block an emergency
exit, and
b) Armrest does not restrict any passenger
from access to the main airplane aisle.

-25-02-05
***
Delethalization Pads D - - May be inoperative or missing provided affected
seat is blocked and placarded DO NOT
OCCUPY.

-25-02-06
***
Seat Belt Air Bag
Restraint Systems

-25-02-06A D - - May be inoperative provided affected seat is

blocked and placarded DO NOT OCCUPY.

-25-02-06B D - - May be inoperative provided affected seat is

blocked and placarded DO NOT OCCUPY.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-10
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-28-01 Storage Bins/Cabin,

Galley and Lavatory
Storage
Compartments/
Closets

-28-01A C - - (M) May be inoperative provided:

a) Procedures are established to secure the
affected bin, compartment or closet in
the closed position,
b) Affected bin, compartment or closet is
prominently placarded DO NOT USE,
c) Any emergency equipment located in
affected bin, compartment or closet is
considered inoperative, and
d) Affected bin, compartment or closet is
not used for storage of any items except
for those permanently affixed.

NOTE: For overhead bins, if no partitions are

installed, the entire overhead bin is
considered inoperative.

-28-01B C - - (M)(O) May be inoperative provided:

a) For non-retractable doors, affected door
is removed,
b) For retractable doors, affected door is
removed or secured in the retracted (fully
open) position,
c) Affected bin, compartment or closet is
not used for storage of any items, except
those permanently affixed,
d) Affected bin, compartment or closet is
prominently placarded DO NOT USE,
e) Procedures are established and used to
alert crew members and passengers of
inoperative bins, compartments or
closets and
f) Passengers are briefed that affected bin,
compartment or closet is not to be used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-11
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-28-01 Storage Bins/Cabin,

Galley and Lavatory
Storage
Compartments/
Closets
(Cont’d)

-28-01B NOTE 1: For overhead bins, if no partitions are

installed, the entire overhead bin is
considered inoperative.

NOTE 2: Any emergency equipment located in

the associated compartment
(permanently affixed) is available for
use.

-28-01-01
Multi Latch/Quarter C - - One latch/lug per compartment may be
Turn Lug Installations inoperative provided:
a) Remaining latch(es)/lug(s) on affected
compartments operate normally, and
b) If affected compartment is used for a
galley cart, the cart remains empty.

-28-01-02
***
Storage Compartment D - 0 (M) May be inoperative in the unlocked position
Key Locks provided doors can be secured by other means.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-12
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-29-01 Overhead Flight Crew

*** Rest (OFCR)

-29-01A C 1 0 (M) May be inoperative provided OFCR is

deactivated closed.

NOTE: This provision is not intended to prohibit

OFCR inspections by crew members.

-29-01B D 1 0 May be inoperative provided procedures do not

require its use.

-29-01-01
Door C 1 0 (M) May be inoperative provided associated
OFCR door is removed.

-29-01-02
Door Lock C 1 0 (M) May be inoperative provided:
a) OFCR door is verified to open from the
outside using the override feature, and
b) OFCR door is verified to open and close
normally from the inside.

-29-01-03
Seat C 1 0 (M) May be inoperative provided:
a) Seat position or seat assembly is not
occupied, and
b) Folding type seat stows automatically or
is secured in the retracted position.

NOTE 1: An automatic folding seat that will not

stow automatically is considered
inoperative.

NOTE 2: A seat position with an inoperative or

missing restraint system is considered
inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-13
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-29-02 Overhead Flight

*** Attendant Rest
(OFAR)

-29-02A C 1 0 (M) May be inoperative provided OFAR is

deactivated closed.

NOTE: This provision is not intended to prohibit

OFAR inspections by crew members.

-29-02B D 1 0 May be inoperative provided procedures do not

require its use.

-29-02-01
Door C 1 0 (M) May be inoperative provided associated
OFAR door is removed.

-29-02-02
Door Lock C 1 0 (M) May be inoperative provided:
a) OFAR door is verified to open from the
outside using the override feature, and
b) OFAR door is verified to open and close
normally from the inside.

-30-01 Galley/Cabin Waste C - - (M)(O) May be inoperative provided:

Receptacles Access a) Container is empty and access is
Door/Covers secured to prevent waste introduction
into the compartment, and
b) Procedures are established to ensure
that sufficient galley/cabin waste
receptacles are available to
accommodate all waste that may be
generated on a flight.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-14
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-41-01 Exterior Lavatory A - - Fifty percent may be inoperative or missing |

Ashtrays provided repairs are made within 10 calendar |
days. |
|
-41-02 Lavatory Waste C - - (M) May be inoperative provided:
Container a) Associated waste container is empty and
Flapper/Access Doors access is secured to prevent waste
introduction into the waste container,
b) Associated lavatory is used only by crew
members, and
c) Associated lavatory entrance door is
locked closed and placarded,
INOPERATIVE – DO NOT ENTER.

NOTE: These provisions are not intended to

prohibit lavatory use or inspections by
crew members.

-41-03 Deleted ATA number reserved for future use.

-61-01 Emergency Descent C 4 2 (M) May be inoperative or missing provided:

Devices (Escape a) The number of flight crew members plus
Reels) observer seat occupants is limited to the
number of operative escape reels
installed, and
b) Inoperative escape reels are removed.

-63-01 Emergency C 1 0 (O) May be inoperative provided alternate

Evacuation Signal procedures are used.
System
NOTE: Any portion of the system which operates
normally may be used.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-15
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-63-02 FASTEN SEAT BELT C - - One or more signs or placards may be illegible or
WHILE SEATED missing provided a legible sign or placard is
Signs or Placards visible from each occupied passenger seat.

-63-03 Emergency Locator D - - Any in excess of those required by FAR may be

*** Transmitter (ELT) inoperative or missing.
(Survival)

-64-01 Megaphones

-64-01A D - 2 Any in excess of those required by FAR may be

inoperative or missing provided:
a) Inoperative megaphone is removed from
passenger cabin,
b) Associated placard is removed or
obscured, and
c) Required distribution is maintained.

-64-01B C - 0 (O) May be inoperative or missing provided:

a) No passengers are carried,
b) A maximum of 19 persons authorized by
14 CFR for non-passenger carrying
operations are carried, and
c) Alternate procedures are established and
used.

-64-02 Flashlight Holder

Assemblies (Including
Flashlight)

-64-02A C - - May be inoperative or missing provided crew

member has a flashlight of equivalent
characteristics readily available.

-64-02B C - 0 (O) May be inoperative or missing provided:

a) No passengers are carried,
b) A maximum of 19 persons authorized by
14 CFR for non-passenger carrying
operations are carried, and
c) Alternate procedures are established and
used.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-16
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-64-03 Emergency Medical

Equipment

-64-03-01
Automatic External
Defibrillator (AED)
and/or Associated
Equipment

-64-03-01A A - 0 (O) May be incomplete, missing or inoperative

provided:
a) AED is resealed in a manner that will
identify it as a unit that cannot be
mistaken for a fully serviceable unit, and
b) Repairs or replacements are made within
one flight.

-64-03-01B D - - Any in excess of those required by FAR may be

incomplete, missing or inoperative.

-64-03-02
Emergency Medical
Kit (EMK) and/or
Associated
Equipment

-64-03-02A A - 0 (O) May be incomplete, missing or inoperative

provided:
a) EMK is resealed in a manner that will
identify it as a unit that cannot be
mistaken for a fully serviceable unit, and
b) Repairs or replacements are made within
one flight.

-64-03-02B D - - Any in excess of those required by FAR may be

incomplete, missing or inoperative.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 25-17
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS

-64-03 Emergency Medical

Equipment
(Cont’d)

-64-03-03
First Aid Kit (FAK)
and/or Associated
Equipment

-64-03-03A A - - (O) If more than one is required by FAR, only one

of the required first aid kits may be incomplete,
missing or inoperative provided:
a) FAK is resealed in a manner that will
identify it as a unit that cannot be
mistaken for a fully serviceable unit, and
b) Repairs or replacements are made within
one flight.

-64-03-03B D - - Any in excess of those required by FAR may be

incomplete, missing or inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 26-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
26 FIRE PROTECTION

-11-01 Engine Fire Detector

Elements

-11-01-01
RR C 24 12 One element in each detector assembly may be
inoperative.

-11-01-02
GE C 20 10 One element in each detector assembly may be
inoperative.

-11-02 Main Engine Data

Concentrator (MEDC)
Channels

-11-02-01
MEDC Channel A A 2 1 (M) One may be inoperative provided:
a) MEDC Channel A is deactivated,
b) MEDC Channel B operates normally on
both engines,
c) Associated engine oil quantity indicating
system is considered inoperative, and
d) Repairs are made within three flight
days.

-11-02-02
MEDC Channel B C 2 1 (M) One may be inoperative provided:
a) MEDC Channel B is deactivated, and
b) MEDC Channel A operates normally on
both engines.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 26-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
26 FIRE PROTECTION

-13-01 Lavatory Smoke C - - (M)(O) For each lavatory, may be inoperative

Detection Systems provided associated:
a) Lavatory waste receptacle is empty,
b) Lavatory door is locked closed and
placarded, INOPERATIVE - DO NOT
ENTER, and
c) Lavatory is used only by crew members.

NOTE: These provisions are not intended to

prohibit lavatory use or inspections by
crew members.

-13-01-01
Lavatory Call Light C - 0 NOTE: Attendant call and occupancy indications
Smoke Detected are considered NEF.
Function

-14-01 Overhead Flight C 8 0 (M)(O) May be inoperative provided:

*** Attendant Rest a) Inoperative smoke detection system is
(OFAR) Smoke deactivated, and
Detection Systems b) OFAR is deactivated closed.

NOTE: These provisions are not intended to

prohibit OFAR inspections by crew
members.

-14-01-01
Individual Bunk C 6 0 (M)(O) May be inoperative provided:
Smoke Detectors a) Associated bunk is not used and
personal items are removed, and
b) A conspicuous barrier strap or rope is
placed across the associated bunk with a
placard attached stating that the bunk is
not to be used.

-14-01-02
Entrance Area Smoke C 2 1 One may be inoperative provided:
Detectors a) Bunk smoke detectors operate normally,
and
b) For entrance area curtain installed,
entrance area curtain is secured open or
removed.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 26-3
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
26 FIRE PROTECTION

-14-02 Overhead Flight Crew C 4 0 (M)(O) May be inoperative provided:

*** Rest (OFCR) Smoke a) Inoperative smoke detection system is
Detection Systems deactivated, and
b) OFCR is deactivated closed.

NOTE: These provisions are not intended to

prohibit OFCR inspections by crew
members.

-14-02-01
Individual Bunk C 2 0 (M)(O) May be inoperative provided:
Smoke Detectors a) Associated bunk is not used and
personal items are removed, and
b) A conspicuous barrier strap or rope is
placed across the associated bunk with a
placard attached stating that the bunk is
not to be used.

-14-02-02
Entrance Area Smoke C 2 1 One may be inoperative provided:
Detectors c) Bunk smoke detectors operate normally,
and
d) For entrance area curtain installed,
entrance area curtain is secured open or
removed.

-15-01 APU Fire Detection

System

-15-01A C 1 0 May be inoperative provided:

a) APU selector switch remains in OFF
position,
b) VFSG systems operate normally, and
c) Flight remains within 180 minutes of
landing at a suitable airport.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 26-4
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
26 FIRE PROTECTION

-15-01 APU Fire Detection

System (Cont’d)

-15-01B C 1 0 (M) May be inoperative provided:

a) APU is used for ground operations only,
b) APU is continuously monitored by
ground personnel when operating,
c) APU external control system operates
normally,
d) APU is not used during taxi,
e) VFSG systems operate normally, and
f) Flight remains within 180 minutes of
landing at a suitable airport.

-15-01-01
APU Fire Detection C 2 1
Loops

-16-01 Lower Cargo

Compartment Smoke
Detectors

-16-01A C 22 16 May be inoperative provided adjacent cargo

compartment smoke detectors operate normally.

-16-01B C 22 0 (O) May be inoperative provided procedures are

established and used to verify the associated
compartment or area remains empty or contains
only ballast, empty cargo handling equipment
(ballast may be loaded in ULDs), or fly away kits.

NOTE: Operator MELs must define which items

are approved for inclusion in the fly away
kits and which materials can be used as
ballast.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 26-5
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
26 FIRE PROTECTION

-17-01 Wheel Well Fire C 1 0 (O) May be inoperative provided landing gear
Detection System remain extended for ten minutes after takeoff.

NOTE: In case of engine failure after V1, landing

gear should be retracted until takeoff
obstacles are cleared.

-17-01-01
Wheel Well Fire C 12 8 One detector per wheel axle may be inoperative |
Temperature provided outboard detectors operate normally. |
Detectors |

-18-01 Duct Leak Overheat C 2 1 May be inoperative provided:

Detection Systems a) Associated engine anti-ice control switch
remains OFF,
b) Airplane is not operated in known or
forecast icing conditions, and
c) Flight remains within 120 minutes of
landing at a suitable airport.

-18-01-01
Duct Leak Overheat C 4 2 One channel per engine may be inoperative.
Detection Channels

-21-01 Fire BTL DISCH C 4 0

Lights (Engine, APU,
Cargo)

-22-01 APU Fire C 1 0 May be inoperative provided:

Extinguishing a) APU is not used,
System b) VFSG systems operate normally, and
c) Flight remains within 180 minutes of
landing at a suitable airport.

-22-02 APU Auto Discharge C 1 0 (M) May be inoperative provided APU fire
warning indicator is monitored during APU
ground operations.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 26-6
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
26 FIRE PROTECTION

-23-01 Lower Cargo C - 0 (O) May be inoperative provided procedures are

Compartment Fire established and used to verify cargo
Extinguishing Bottles compartments remain empty or contain only
ballast, empty cargo handling equipment (ballast
may be loaded in ULDs), or fly away kits.

NOTE: Operator MELs must define which items

are approved for inclusion in the fly away
kits and which materials can be used as
ballast.
(Continued)
-23-01-01
Bottles 2A, 2B and 2C C 3 1 (M)(O) May be inoperative provided:
a) Bottle is deactivated,
b) Airplane is operated pressurized, and
c) Total fire extinguisher bottle capability is
greater than or equal to maximum time to
land at a suitable airport.

-23-01-02
***
Bottles 2D and 2E C - 0 (M)(O) May be inoperative provided:
a) Bottle is deactivated,
b) Airplane is operated pressurized, and
c) Total fire extinguisher bottle capability is
greater than or equal to maximum time to
land at a suitable airport.

-23-01-03
Bottle Pressure C - 0 (M) May be inoperative provided associated
Monitors bottle is verified to be fully charged.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 26-7
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
26 FIRE PROTECTION

-23-02 Lower Cargo

Compartment Fire
Extinguishing Flow
Valves (Forward and
Aft)

-23-02A C 2 1 (M)(O) One may be inoperative provided:

a) Flow valve is deactivated, and
b) Procedures are established and used to
verify the associated cargo compartment
remains empty or contains only ballast,
empty cargo handling equipment (ballast
may be loaded in ULDs), or fly away kits.

NOTE: Operator MELs must define which items

are approved for inclusion in the fly away
kits and which materials can be used as
ballast.

-23-02B C 2 0 (O) May be inoperative provided procedures are

established and used to verify cargo
compartments remain empty or contain only
ballast, empty cargo handling equipment (ballast
may be loaded in ULDs), or fly away kits.

NOTE: Operator MELs must define which items

are approved for inclusion in the fly away
kits and which materials can be used as
ballast.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 26-8
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
26 FIRE PROTECTION

-23-03 Lower Cargo

Compartment Fire
Extinguishing Squib
Control Channels

-23-03A C 2 1

-23-03B C 2 0 (O) May be inoperative provided procedures are

established and used to verify cargo
compartments remain empty or contain only
ballast, empty cargo handling equipment (ballast
may be loaded in ULDs), or fly away kits.

NOTE: Operator MELs must define which items

are approved for inclusion in the fly away
kits and which materials can be used as
ballast.

-23-04 Lower Cargo C 1 0 (O) May be inoperative provided procedures are

Compartment Fire established and used to verify cargo
Extinguishing compartments remain empty or contain only
Filter/Regulator ballast, empty cargo handling equipment (ballast
may be loaded in ULDs), or fly away kits.

NOTE: Operator MELs must define which items

are approved for inclusion in the fly away kits and
which materials can be used as ballast.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 26-9
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
26 FIRE PROTECTION

-24-01 Lavatory Waste

Compartment Fire
Extinguishing
Systems

-24-01A C - - (O) May be inoperative for each lavatory

provided associated lavatory smoke detection
system operates normally.

-24-01B C - - (M)(O) May be inoperative for each lavatory

provided associated:
a) Lavatory waste receptacle is empty,
b) Lavatory door is locked closed and
placarded, INOPERATIVE - DO NOT
ENTER, and
c) Lavatory is used only by crew members.

NOTE: These provisions are not intended to

prohibit lavatory use or inspections by
crew members.

-26-01 Portable Fire D - - (M) Any in excess of those required by FAR may
Extinguishers be inoperative or missing provided:
a) The inoperative fire extinguisher is
tagged inoperative, removed from the
installation location, and placed out of
sight so it cannot be mistaken for a
functional unit, and
b) Required distribution is maintained.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 27-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS

-00-01 Flight Controls C 1 0

Synoptic Display

-02-01 Bank Angle C 1 0

Protection

-02-02 Flight Control

Modules (FCM)

-02-02-01
Center FCM B 1 0 (M) May be inoperative provided: |
a) Center FCM is deactivated, |
b) Left and right FCMs operate normally, |
and
c) Flap/slat hydraulic control module (HCM)
solenoid coils are considered
inoperative.

-02-02-02
Left FCM B 1 0 (M) May be inoperative provided: |
a) Left FCM is deactivated, and |
b) Center and right FCMs operate normally. |

-02-02-03
Right FCM B 1 0 (M) May be inoperative provided: |
a) Right FCM is deactivated, |
b) Center and left FCMs operate normally, |
and
c) Flap/slat hydraulic control module (HCM)
solenoid coils are considered
inoperative, and
d) Trailing edge variable camber (cruise
flaps) function is considered inoperative.

-02-03 PFCS Interface C 1 0 May be dispatched with PFCS INTERFACE

faults.

-02-04 Actuator Delta A 1 0 May be dispatched with ACTUATOR DELTA

Pressure PRESS faults provided repairs are made within 3
flight days.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 27-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS

-02-05 Flight Control C 2 0 May be inoperative provided FLT CONTROLS

Surfaces Lockout LOCKED advisory message is not displayed.
Function

-02-06 Direct Mode Rate C 4 3 One may be inoperative provided:

Sensors a) Control wheel position transducers
operate normally,
b) Rudder pedal position transducers
operate normally, and
c) Control column position transducers
operate normally.

-11-01 Control Wheel C 6 5 One may be inoperative provided direct mode

Position Transducers rate sensors operate normally.

-11-02 Alternate Control C 2 0

Wheel Position
Transducers

-21-01 Rudder Trim Switch C 1 0

High Rate Function

-21-02 Rudder Pedal C 6 5 One may be inoperative provided direct mode

Position Transducers rate sensors operate normally.

-31-01 Control Column C 6 5 One may be inoperative provided direct mode

Position Transducers rate sensors operate normally.

-32-01 Stick Shaker Systems C 2 1

-41-01 Control Wheel Pitch C 2 1 One may be inoperative provided alternate pitch
Trim Switches trim switch operates normally.

-41-02 Alternate Pitch Trim C 1 0 May be inoperative provided control wheel pitch
Switch trim switches operate normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 27-3
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS

-41-03 Stabilizer Control A 2 1 (M) One may be inoperative provided: |

Channels a) Inoperative channel is deactivated, and
b) Repairs are made within 10 flights.

-48-01 Stabilizer Position |

Transducers |

-48-01-01 |
Transducer 1 A 1 0 (M) May be inoperative provided: |
a) Transducer 1 is deactivated, |
b) Transducers 2 and 3 operate |
normally, and |
c) Repairs are made within 10 flights. |

-48-01-02 |
Transducers 2 and 3 A 2 1 (M) One may be inoperative provided: |
a) Associated stabilizer control channel |
is deactivated, |
b) Transducer 1 operates normally, and |
c) Repairs are made within 10 flights. |

-48-02 Stabilizer Load A 3 2 One may be inoperative provided repairs are

Transducers made within 10 flights.

-51-01 Flap Lever Position C 4 3 (M) One may be inoperative provided:

Transducers a) Remaining transducers are verified to
operate normally before each departure,
and
b) Slats and flaps alternate mode is verified
to operate normally before each
departure.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 27-4
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS

-51-02 Trailing Edge Variable

Camber (Cruise
Flaps) Function

-51-02-01
Faired Position

-51-02-01A C 1 0 (M)(O) May be inoperative provided:

a) Flap secondary mode is verified to
operate normally,
b) Spoiler actuator system operates |
normally, |
c) Appropriate weight and center-of-gravity
limits are observed, and
d) Appropriate performance adjustments
are applied.

-51-02-01B C 1 0 (O) May be inoperative provided:

a) Flap secondary mode is inoperative,
b) Spoiler actuator system operates |
normally, |
c) Appropriate weight and center-of-gravity
limits are observed, and
d) Appropriate performance adjustments
are applied.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 27-5
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS

-51-02 Trailing Edge Variable

Camber (Cruise
Flaps) Function
(Cont’d)

-51-02-02
Extended or Split
Position

-51-02-02A C 1 0 (M)(O) May be inoperative provided:

a) Flap secondary mode is verified to
operate normally,
b) Spoiler actuator system operates |
normally, |
c) Appropriate weight and center-of-gravity
limits are observed, and
d) Appropriate performance adjustments
are applied.

-51-02-02B C 1 0 (O) May be inoperative provided:

a) Flap secondary mode is inoperative,
b) Spoiler actuator system operates |
normally, |
c) Appropriate weight and center-of-gravity
limits are observed, and
d) Appropriate performance adjustments
are applied.

-51-03 Flap Secondary Mode C 1 0 (M) May be inoperative provided:

a) Center hydraulic system electric motor-
driven pumps operate normally,
b) Slat secondary mode is verified to
operate normally once each flight day,
c) Trailing edge variable camber (cruise
flaps) function is considered inoperative,
and
d) Main landing gear priority valve is
verified to operate normally once each
flight day.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 27-6
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS

-51-04 Flap/Slat Shutoff Deleted, Revision 7.

Valves

-51-05 Flap/Slat Hydraulic C 14 7 (M) One coil per solenoid coil pair may be
Control Module inoperative provided:
(HCM) Solenoid Coils a) Slat secondary mode is verified to
operate normally once each flight day,
and
b) Flap secondary mode is verified to
operate normally once each flight day.

-51-06 Flap/Slat Hydraulic C 2 1 (M) One may be inoperative provided:

Control Module a) The associated hydraulic control module
(HCM) Power Control channel is deactivated,
b) Slat secondary mode is verified to
operate normally once each flight day,
and
c) Flap secondary mode is verified to
operate normally once each flight day.

-51-07 Flap Variable Camber C 1 0

Trim Unit (VCTU)
Power Control

-51-08 Alternate Flap/Slat C 2 1 (M)(O) Slat or flap alternate mode may be

Control Modes inoperative provided:
a) Flap lever position transducers operate
normally, and
b) Remaining alternate mode is verified to
operate normally once each flight day.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 27-7
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS

-58-01 Flap Position/Skew C 24 10 One sensor per sensor pair and all inboard flap
Sensors position sensors may be inoperative provided:
a) Slat position sensors operate normally,
and
b) Spoiler actuator systems operate
normally.

-61-01 Speedbrake Lever B 4 3 (O) One may be inoperative provided:

Position Transducers a) Automatic speedbrake function operates
normally, and
b) Speedbrakes are verified to operate
normally prior to each landing.

-61-02 Spoiler Actuator

Systems

-61-02-01
Electro-Mechanical C 4 3 (M)(O) One may be inoperative provided:
(EMA) Spoilers (4, 5, a) Spoiler actuator is deactivated,
10, 11) b) Position of deactivated spoiler is verified
before each departure,
c) Trailing edge variable camber (cruise |
flaps) function operates normally, |
d) Hydraulic spoilers operate normally,
e) Flap position/skew sensors operate
normally,
f) Slat position sensors operate normally,
g) Appropriate weight and center-of-gravity
limits are observed, and
h) Appropriate performance adjustments
are applied.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 27-8
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS

-61-02 Spoiler Actuator

Systems
(Cont’d)

-61-02-02
Hydraulic-Spoilers (1, C 10 9 (M)(O) One may be inoperative provided:
2, 3, 6, 7, 8, 9, 12, 13, a) Spoiler actuator is deactivated,
14) b) Position of deactivated spoiler is verified |
before each departure, |
c) Trailing edge variable camber (cruise |
flaps) function operates normally, |
d) Electro-mechanical (EMA) spoilers
operate normally,
e) Flap position/skew sensors operate
normally,
f) Slat position sensors operate normally,
g) Appropriate weight and center-of-gravity
limits are observed, and
h) Appropriate performance adjustments
are applied.

-61-03 Automatic C 1 0 (O) May be inoperative provided: |

Speedbrake Function a) Speedbrake lever position transducers |
operate normally, |
b) ARMED detent is not used, and |
c) Appropriate performance adjustments |
are applied. |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 27-9
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS

-81-01 Slat Secondary Mode

-81-01A C 1 0 (M) May be inoperative provided:

a) Trailing edge variable camber (cruise
flaps) function operates normally, and
b) Main landing gear priority valve is
verified to operate normally once each
flight day.

-81-01B C 1 0 (M) May be inoperative provided:

a) Center hydraulic system electric motor-
driven pumps operate normally,
b) Flap secondary mode is verified to
operate normally once each flight day,
and
c) Main landing gear priority valve is
verified to operate normally once each
flight day.

-88-01 Slat Position Sensors

-88-01A C 4 2 One sensor per sensor pair may be inoperative

provided:
a) Flap position/skew sensors operate
normally,
b) Spoiler actuator systems operate
normally, and
c) Trailing edge variable camber (cruise
flaps) function operates normally.

-88-01B C 4 2 (M) One sensor per sensor pair may be

inoperative provided:
a) Flap position/skew sensors operate
normally,
b) Spoiler actuator systems operate
normally, and
c) Flap secondary mode is verified to
operate normally once each flight day.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 28-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
28 FUEL

-11-01 Sump Drain Valves

-11-01-01
Surge Tanks C 2 0 (M) May be inoperative provided there is no
evidence of leakage.

-11-01-02
Main and Center C 4 3 (M) One may be inoperative provided:
Tanks a) There is no evidence of leakage, and
b) Alternate procedures are used to prevent
water accumulation in associated tank.

-21-01 Pressure Refueling

System

-21-01-01
Main Tank Refuel C 4 2 (M)(O) One valve in each main tank may be
Valves inoperative provided:
a) Inoperative valve is locked closed,
b) For inboard refuel valve inoperative,
crossfeed valve is verified to operate
normally, and
c) For inboard refuel valve inoperative,
alternate procedures are used for fuel
balancing.

-21-01-02
Center Tank Refuel C 2 0 (M) May be inoperative locked closed.
Valves

-21-01-03
Refuel Valve Lights C 6 0 (M) May be inoperative provided:
a) Associated valve is verified closed after
each refueling, and
b) Overfill light operates normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 28-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
28 FUEL

-21-01 Pressure Refueling

System
(Cont’d)

-21-01-04
Refuel Control Panel C 3 0 (M) May be inoperative provided alternate
Fuel Quantity procedures are used for refueling.
Indicators

-21-01-05
Load Select System C 1 0 (M) May be inoperative provided alternate
procedures are used for refueling.

NOTE: Any function which operates normally

may be used.

-21-01-06
Overfill Light C 1 0 (M) May be inoperative provided:
a) Refuel valves are verified to close when
appropriate during refueling, and
b) Refuel valve lights operate normally.

-21-01-07
Power Switch C 1 0

-21-01-08
Defuel Switch C 1 0

-21-01-09
Test Features (Panel C 2 0
and System)

-22-01 Main Tank Fuel C 4 3 (M) One may be inoperative provided:

Pumps a) Inoperative pump is deactivated, and
b) Main tank quantity indications operate
normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 28-3
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
28 FUEL

-22-02 Center Tank Fuel

Override/Jettison
Pump Systems

-22-02A C 2 1 (M)(O) One may be inoperative provided:

a) Inoperative pump is deactivated,
b) Fuel scavenge system operates
normally,
c) Crossfeed valve operates normally, and
d) Center tank quantity indication operates
normally.

-22-02B C 2 0 (M)(O) May be inoperative provided:

a) Pumps are deactivated,
b) Fuel scavenge system operates
normally,
c) Center tank quantity indication operates
normally,
d) For center tank fuel, fuel quantity
remaining in main tanks is adequate to
reach a suitable airport if scavenge
system fails at any time, and
e) Center tank fuel is accounted for in the
airplane weight and balance in the event
center tank fuel cannot be used.

-22-02C C 2 1 (M)(O) One may be inoperative provided:

a) Inoperative pump is deactivated,
b) Crossfeed valve operates normally,
c) Center tank quantity indication operates
normally,
d) For center tank fuel, fuel quantity in main
tanks is adequate to reach a suitable
airport if remaining center pump fails at
any time, and
e) Center tank fuel is accounted for in the
airplane weight and balance in the event
center tank fuel cannot be used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 28-4
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
28 FUEL

-22-02 Center Tank Fuel

Override/Jettison
Pump Systems
(Cont’d)

-22-02D C 2 0 (M)(O) May be inoperative provided:

a) Pumps are deactivated,
b) Center tank quantity indication operates
normally, and
c) Center tank fuel is considered unusable
and is accounted for in the airplane
weight and balance.

NOTE: AFM fuel loading and usage limitations

are for usable fuel.

-22-03 Crossfeed Valve

-22-03A C 1 0 (M) May be inoperative provided:

a) Valve is locked closed,
b) Fuel balance switch operates normally,
c) Main tank inboard refuel valves operate
normally, and
d) Both center tank pumps operate
normally.

-22-03B C 1 0 (M) May be inoperative provided:

a) Valve is locked closed,
b) Fuel balance switch operates normally,
c) Main tank inboard refuel valves operate
normally, and
d) Both center tank pumps are inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 28-5
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
28 FUEL

-22-04 Fuel Scavenge

System

-22-04-01
Scavenge Pumps C 2 0 (O) May be inoperative provided:
a) Center tank quantity indication operates
normally, and
b) Appropriate amount of center tank fuel is
considered unusable and is accounted
for in the airplane weight and balance.

NOTE: AFM fuel loading and usage limitations

are for usable fuel.

-22-04-02
Scavenge Valves C 2 0 (M)(O) May be inoperative provided:
a) Inoperative valve is locked closed,
b) Center tank quantity indication operates
normally, and
c) Appropriate amount of center tank fuel is
considered unusable and is accounted
for in the airplane weight and balance.

NOTE: AFM fuel loading and usage limitations

are for usable fuel.

-22-05 Crossfeed VALVE C 1 0

Light

-22-06 Fuel Balance Switch C 1 0 (M)(O) May be inoperative provided:

a) Crossfeed valve is verified to operate
normally, and
b) Alternate procedures are used for fuel
balancing.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 28-6
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
28 FUEL

-22-07 Deleted ATA number reserved for future use. |

-22-08 Deleted ATA number reserved for future use. |

-22-09 Deleted ATA number reserved for future use. |

-25-01 APU DC Fuel Pump C 1 0 (M) May be inoperative deactivated.

-25-02 APU Fuel Shutoff C 1 0 (M)(O) May be inoperative provided:

Valve a) Valve is locked closed,
b) Left AGCU operates normally, |
c) VFSG systems operate normally, and
d) Flight remains within 180 minutes of
landing at a suitable airport.

-26-01 Defuel/Isolation C 2 0 (M)(O) May be inoperative provided:

Valves a) Inoperative valve is locked closed,
b) Crossfeed valve is verified to operate
normally,
c) Alternate procedures are used for fuel
balancing, and
d) For both valves inoperative, appropriate
performance adjustments are applied.

-31-01 Fuel Jettison System C 1 0 (M)(O) May be inoperative provided:

a) Jettison system is deactivated,
b) Jettison nozzle valves are locked closed,
and
c) Appropriate performance adjustments
are applied.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 28-7
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
28 FUEL

-31-02 Center Tank Jettison

Isolation Valves

-31-02A C 2 1 (M) One may be inoperative locked closed.

-31-02B C 2 0 (M)(O) May be inoperative provided:

a) Jettison system is deactivated,
b) Both jettison isolation valves are locked
closed, and
c) Appropriate performance adjustments
are applied.

-31-03 Fuel Jettison Nozzle

Valves

-31-03A C 2 1 (M) One may be inoperative locked closed.

-31-03B C 2 0 (M)(O) May be inoperative provided:

a) Jettison system is deactivated,
b) Both jettison nozzle valves are locked
closed, and
c) Appropriate performance adjustments
are applied.

-40-01 Fuel Synoptic Display C 1 0 May be inoperative provided individual fuel

quantity indications required for dispatch operate
normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 28-8
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
28 FUEL

-41-01 Fuel Quantity

Indication Systems

-41-01-01
Main Tanks B 2 1 (M)(O) One may be inoperative provided:
a) Fuel quantity in associated tank is
verified by an alternate procedure,
b) Crossfeed valve is verified to operate
normally,
c) Both fuel pumps for the associated main
tank operate normally,
d) Center tank fuel quantity indication
operates normally,
e) Fuel flow indications operate normally,
f) FMC FUEL is initialized with the known
total fuel quantity,
g) Alternate procedures are used for fuel
balancing,
h) Appropriate amount of center tank fuel is
considered unusable and is accounted
for in the airplane weight and balance,
i) Appropriate performance adjustments
are applied, and
j) Flight remains within 180 minutes of
landing at a suitable airport.

NOTE: AFM fuel loading and usage limitations

are for usable fuel.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 28-9
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
28 FUEL

-41-01 Fuel Quantity

Indication Systems
(Cont’d)

-41-01-02
Center Tank B 1 0 (M)(O) May be inoperative provided:
a) Fuel quantity in center tank is verified by
an alternate procedure,
b) Both main tank fuel quantity indication
systems operate normally,
c) Both center tank fuel pumps operate
normally,
d) Fuel flow indications operate normally,
e) Fuel scavenge system operates
normally,
f) FMC FUEL is initialized with the known
total fuel quantity, and
g) Flight remains within 180 minutes of
landing at a suitable airport.

-41-02 Fuel Quantity Data C 6 3 (M) One channel for each tank may be
Concentrator (FQDC) inoperative deactivated.
Channels

-41-03 Fuel Quantity Sensor C 3 0 May be dispatched with FUEL QTY SENSORS
Systems faults.

-42-01 Fuel Pump Low C 6 3

PRESS Lights
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 28-10
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
28 FUEL

-43-01 Fuel Temperature

Indicating Systems

-43-01-01
Center Tank C 1 0

-43-01-02
Main Tank C 2 1
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 29-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER

-11-01 Engine Driven C 2 1

Pumps (EDP)
Depressurization
Function

-11-02 Center System C 2 1 (M)(O) One may be inoperative provided:

Electric Motor-Driven a) Inoperative EMP is deactivated,
Pumps (EMP) b) Slat secondary mode is verified to
operate normally once each flight day,
c) Flap secondary mode is verified to
operate normally once each flight day,
d) Main landing gear priority valve is |
verified to operate normally once each
flight day, and
e) Appropriate performance adjustments
are applied.

-11-03 Electric Motor-Driven

Pump (EMP)
Selectors

-11-03-01
Center System
AUTO Position

-11-03-01A C 2 1 (O) One may be inoperative provided:

a) Associated pump selector ON and OFF
positions operate normally,
b) Opposite center system EMP operates
normally, and
c) Associated pump selector is ON for all
operations.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 29-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER

-11-03 Electric Motor-Driven

Pump (EMP)
Selectors (Cont’d)

-11-03-01
Center System
AUTO Position
(Cont’d)

-11-03-01B C 2 0 (O) May be inoperative provided:

a) Both center system pump selector ON
and OFF positions operate normally,
b) Left and right system EMP selector
AUTO positions operate normally, and
c) Both center system pump selectors are
ON for takeoff and landing.

-11-03-02
Left System AUTO A 1 0 (O) May be inoperative provided:
Position a) Left pump selector ON and OFF
positions operate normally,
b) Center system EMP selector AUTO
positions operate normally,
c) Nitrogen generation system is
considered inoperative,
d) Left pump selector is ON for takeoff and
landing, and
e) Repairs are made within 10 flight days.

-11-03-03
Right System AUTO C 1 0 (O) May be inoperative provided:
Position a) Right pump selector ON and OFF
positions operate normally,
b) Center system EMP selector AUTO
positions operate normally, and
c) Right pump selector is ON for takeoff
and landing.

-11-03-04
ON Position C 4 0 May be inoperative provided the AUTO and OFF
positions for associated pump operate normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 29-3
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER

-11-04 Reserve Steering C 1 0 (M) May be inoperative provided reserve steering

Isolation System isolation valve is deactivated open.

-11-05 Nose Gear Isolation C 1 0 (M) May be inoperative provided:

System a) Nose gear isolation valve is deactivated
open, and
b) Center hydraulic system pressure
transducer operates normally.

-11-06 Alternate Gear C 1 0 (M)(O) May be inoperative provided:

Extension Isolation a) Landing gear is secured in the down
System position, and
b) Airplane is dispatched in accordance
with the AFM Landing Gear Extended
appendix.

-11-07 Hydraulic Pump C 6 0 May be dispatched with HYD FILTER CASE

Case Drain Filter faults provided associated hydraulic pump
Monitoring Systems temperature indication operates normally.

-18-01 Hydraulic Reservoir C 3 0

Accumulators

-18-01-01
Charging Valves C 3 0

-18-01-02
Charging Gauges C 3 0

-18-02 Hydraulic Reservoir C 3 0

Pressure Indication
Systems

-18-03 Reservoir Quantity C 1 0

Gauge (Remote)

-18-04 Hydraulic Reservoir C 3 0 May be inoperative provided associated pump

Temperature temperature indications operate normally.
Indication Systems
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 29-4
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER

-21-02 Ram Air Turbine C 1 0 M) May be inoperative provided: |

(RAT) Position a) RAT is verified to deploy normally, and |
Indication System b) RAT is verified to be stowed prior to each |
flight. |

-21-02-01
UNLKD Light C 1 0

-21-03 Ram Air Turbine C 2 1 One may be inoperative provided OAT at

(RAT) Heaters departure airport is not less than -35 degrees C.

-30-01 Hydraulic Pump C 6 0

FAULT Lights

-30-02 Hydraulic Synoptic C 1 0

Display

-31-01 Hydraulic System

Pressure Transducers

-31-01-01
Left and Right System C 2 0 (M) May be inoperative provided:
Pressure Transducers a) Inoperative system pressure transducer
is deactivated, and
b) Associated system pump pressure
indications operate normally.

-31-01-02
Center System C 1 0 (M) May be inoperative provided:
Pressure Transducer a) Center system pressure transducer is
deactivated,
b) Center system pump pressure
indications operate normally, and
c) Nose gear isolation system operates
normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 29-5
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER

-31-02 Hydraulic Pump C 6 3 (M) One in each system may be inoperative

Pressure Indication provided:
Systems a) Inoperative pump pressure transducer is
deactivated,
b) Associated pump is verified to operate
normally before each departure,
c) Associated pump temperature
indications operate normally, and
d) Associated hydraulic system pressure
transducer operates normally.

-31-03 Hydraulic Reservoir |

Auto-Bleed Valves |

-31-03A C 3 0 (M) May be inoperative provided bleed valve is |

verified to operate normally. |

-31-03B C 3 0 (M) May be inoperative provided: |

a) Associated hydraulic system reservoir is
verified to be free of trapped air, and
b) Inoperative auto-bleed valve is
deactivated closed.

-32-01 Hydraulic Pump C 6 3 One in each system may be inoperative

Temperature provided:
Indications a) Associated pump pressure indications
operate normally, and
b) Associated reservoir temperature
indications operate normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 29-6
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER

-33-01 Hydraulic Fluid

Quantity Indications
(Flight Deck)

-33-01-01
Left and Right System C 2 0 (M) May be inoperative provided:
Quantity Indications a) Associated reservoir level is verified
normal before each departure, and
b) Associated system pressure indication
operates normally.

-33-01-02
Center System B 1 0 (M) May be inoperative provided:
Quantity Indication a) Center system reservoir level is verified
normal before each departure,
b) Center system pressure indication
operates normally,
c) Reserve steering isolation system is
considered inoperative,
d) Nose gear isolation system is considered
inoperative, and
e) Alternate gear extension isolation system
is considered inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 6 PAGE:
BOEING B-787
DATE: 11/21/2012 30-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION

-11-01 Wing Ice Protection C 1 0 May be inoperative provided:

System (WIPS) a) Airplane is not operated in known or
forecast icing conditions, and
b) Flight remains within 120 minutes of
landing at a suitable airport.

-11-01-01
Wing Ice Protection C 48 46 One heat zone pair in symmetrical slats may be
Heat Zones inoperative.

-11-01-02
Wing Ice Protection C 3 2
Channels

-11-02 Wing Anti-Ice (WAI) C 2 0

Indications

-21-01 Engine Anti-Ice (EAI) C 2 1 (M) One may be inoperative provided:

Systems a) Associated PRSOV is locked closed,
b) Associated engine ignition systems
operate normally,
c) Associated engine anti-ice control switch
remains OFF,
d) Airplane is not operated in known or
forecast icing conditions, and
e) Flight remains within 120 minutes of
landing at a suitable airport.

-21-01-01
Engine Anti-ice C 2 1 (M) One may be inoperative provided:
Pressure Regulating a) Associated PRSOV is locked closed,
and Shutoff Valves b) Associated engine ignition systems
(PRSOV) operate normally,
c) Associated engine anti-ice control switch
remains OFF,
d) Airplane is not operated in known or
forecast icing conditions, and
e) Flight remains within 120 minutes of
landing at a suitable airport.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 6 PAGE:
BOEING B-787
DATE: 11/21/2012 30-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION

-21-01 Engine Anti-Ice (EAI)

Systems
(Cont’d)

-21-01-02
Engine Anti-Ice C 2 1 (M)(O) One may be inoperative provided:
Pressure Regulating a) Inoperative valve is locked in mid
and Shutoff Valves position,
(PRSOV) (RR CN- b) Associated PRV operates normally,
AA25656 c) Operations are limited to OAT 38
Incorporated) degrees C or below, and
d) Appropriate performance adjustments
are applied.

-21-01-03
Engine Anti-Ice C 2 1 (M) One may be inoperative provided:
Pressure Regulating a) Associated PRSOV is locked closed,
Valves (PRV) b) Associated engine ignition systems
operate normally,
c) Associated engine anti-ice control switch
remains OFF,
d) Airplane is not operated in known or
forecast icing conditions, and
e) Flight remains within 120 minutes of
landing at a suitable airport.

-21-01-04
Engine Anti-Ice C 2 1 (M)(O) One may be inoperative provided:
Pressure Regulating a) Inoperative valve is locked in mid
Valves (PRV) (RR position,
CN-AA25656 b) Associated PRSOV operates normally,
Incorporated) c) Associated main engine data
concentrator (MEDC) channel A
operates normally,
d) Associated EAI PRSOV controller
operates normally,
e) At least one associated pressure sensor
operates normally, and
f) Operations are limited to OAT 38
degrees C or below.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 6 PAGE:
BOEING B-787
DATE: 11/21/2012 30-3
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION

-21-01 Engine Anti-Ice (EAI)

Systems
(Cont’d)

-21-01-05
Engine Anti-Ice C 2 1 (M)(O) One may be inoperative provided:
Pressure Regulating a) Inoperative valve is locked in mid
Valves (PRV) (GE) position,
b) Associated PRSOV operates normally,
c) Associated main engine data
concentrator (MEDC) channel A
operates normally,
d) Associated EAI PRSOV controller
operates normally,
e) At least one associated pressure sensor
operates normally, and
f) Operations are limited to OAT 38
degrees C or below.

-21-01-06
Pressure Sensors C 4 2 (M) May be inoperative on one engine provided:
a) Associated PRSOV is locked closed,
b) Associated engine ignition systems
operate normally,
c) Associated engine anti-ice control switch
remains OFF,
d) Airplane is not operated in known or
forecast icing conditions, and
e) Flight remains within 120 minutes of
landing at a suitable airport.

-21-01-06-01
Pressure Sensor C 2 0 May be inoperative provided associated pressure
Number 1 sensor number 2 operates normally.

-21-01-06-02
Pressure Sensor C 2 0 May be inoperative provided associated pressure
Number 2 sensor number 1 operates normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 6 PAGE:
BOEING B-787
DATE: 11/21/2012 30-4
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION

-21-01 Engine Anti-Ice (EAI)

Systems
(Cont’d)

-21-01-07
Pressure Sensors C 4 2 (M)(O) May be inoperative on one engine
(RR CN-AA25656 provided:
Incorporated) a) Associated PRSOV is locked in mid
position,
b) Associated PRV operates normally,
c) Operations are limited to OAT 38
degrees C or below, and
d) Appropriate performance adjustments
are applied.

-21-02 Engine Anti-Ice (EAI) C 2 0

Indications

-22-01 Cabin Air Compressor

Inlet Ice Protection
Systems (CIPS)

-22-01A C 2 1 (M) One may be inoperative provided:

a) Inoperative system is deactivated,
b) Opposite air conditioning pack operates
normally, and
c) EICAS TAT indication operates normally.

-22-01B C 2 1 (M) One may be inoperative provided:

a) Inoperative system is deactivated,
b) Opposite air conditioning pack operates
normally, and
c) Airport OAT remains at or above 2
degrees C since last landing.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 6 PAGE:
BOEING B-787
DATE: 11/21/2012 30-5
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION

-22-01 Cabin Air Compressor

Inlet Ice Protection
Systems (CIPS)
(Cont’d)

-22-01C C 2 1 (M) One may be inoperative provided:

a) Inoperative system is deactivated,
b) EICAS TAT indication operates normally,
c) Airplane is not operated in known or
forecast icing, and
d) Flight remains within 120 minutes of
landing at a suitable airport.

-22-01D C 2 1 (M) One may be inoperative provided:

a) Inoperative system is deactivated,
b) Airplane is not operated in known or
forecast icing,
c) Airport OAT remains at or above 2
degrees C since last landing and
d) Flight remains within 120 minutes of
landing at a suitable airport.

-22-01E C 2 0 (M) May be inoperative provided:

a) Inoperative system is deactivated,
b) Air conditioning packs operate normally,
and
c) EICAS TAT indication operates normally.

-22-01F C 2 0 (M) May be inoperative provided:

a) Inoperative system is deactivated,
b) Air conditioning packs operate normally,
and
c) Airport OAT remains at or above 2
degrees C since last landing.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 6 PAGE:
BOEING B-787
DATE: 11/21/2012 30-6
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION

-31-01 Pitot Probe Heater

Systems

-31-01-01
Right Pitot Heater B 1 0 (M) May be inoperative provided:
a) Left and center pitot probes are
inspected before each departure,
b) Left and center pitot probe heater
systems operate normally,
c) Left and center pitot air data modules
operate normally,
d) Static air data modules operate normally,
e) AIR DATA/ATT instrument source
switches operate normally, and
f) Approach minimums do not require its
use.

-31-01-02
Left Pitot Heater B 1 0 (M) May be inoperative provided:
a) Right and center pitot probes are
inspected before each departure,
b) Right and center pitot probe heater
systems operate normally,
c) Right and center pitot air data modules
operate normally,
d) Static air data modules operate normally,
e) AIR DATA/ATT instrument source
switches operate normally, and
f) Approach minimums do not require its
use.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 6 PAGE:
BOEING B-787
DATE: 11/21/2012 30-7
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION

-31-01 Pitot Probe Heater

Systems
(Cont’d)

-31-01-03
Center Pitot Heater B 1 0 (M) May be inoperative provided:
a) Left and right pitot probes are inspected
before each departure,
b) Left and right pitot probe heater systems
operate normally,
c) Left and right pitot air data modules
operate normally,
d) Static air data modules operate normally,
e) AIR DATA/ATT instrument source
switches operate normally,
f) Airplane is not operated in visible
moisture,
g) Airplane is not operated in known or
forecast icing conditions,
h) Approach minimums do not require its
use, and
i) Flight remains within 120 minutes of
landing at a suitable airport.

-32-01 Angle of Attack (AOA) B 2 1

Anti-Ice System

-41-01 Flight Deck Forward C 2 1 One may be inoperative provided:

Window Primary Heat a) Associated switch remains off,
Channels b) Associated forward window backup heat
channel operates normally,
c) Side window heat channels operate
normally,
d) Airplane is not operated in known or
forecast icing conditions, and
e) Flight remains within 120 minutes of
landing at a suitable airport.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 6 PAGE:
BOEING B-787
DATE: 11/21/2012 30-8
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION

-41-02 Flight Deck Side C 2 1 One may be inoperative provided:

Window Heat a) Associated switch remains off, and
Channels b) Forward window primary heat channels
operate normally.

-41-03 Flight Deck Forward C 2 1 One may be inoperative provided:

Window Backup Heat a) Associated switch remains off,
Channels b) Forward window primary heat channels
operate normally, and
c) Side window heat channels operate
normally.

-41-04 Window Heat INOP C 4 0

Lights

-41-05 Window Heat C 3 2

Software

-42-01 Windshield Wiper C 2 0 May be inoperative provided:

System a) Airplane is not operated in precipitation
within five statute miles of airport of
departure or intended landing, and
b) Approach minimums do not require its
use.

-42-01-01
Low Speed Functions C 2 0 (M) May be inoperative provided associated high
speed function is verified to operate normally.

-42-01 Windshield Wiper

System (Cont’d)

-42-01-02
High Speed Functions

-42-01-02A C 2 1 (M) One may be inoperative provided associated

low speed function is verified to operate normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 6 PAGE:
BOEING B-787
DATE: 11/21/2012 30-9
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION

-42-01 Windshield Wiper

System (Cont’d)

-42-01-02
High Speed Functions
(Cont’d)

-42-01-02B C 2 0 (M) May be inoperative provided:

a) Both low speed functions are verified to
operate normally, and
b) Airplane is not operated in known or
forecast precipitation of moderate or
greater intensity within 5 statute miles of
the airport of departure or intended
landing.

-42-01-03
Intermittent Functions C 2 0

-44-01 Windshield Washer D 1 0

System

-71-01 Water Supply In-line C - 0 (M) May be inoperative deactivated.

Heaters

-81-01 Ice Detectors

-81-01A C 2 1

-81-01B C 2 0 (O) May be inoperative provided alternate

procedures are established and used.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 2 PAGE:
BOEING B-787
DATE: 01/25/2012 31-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING
SYSTEMS

-31-01 Digital Voice-Data

Recorder Systems

-31-01-01
Cockpit Voice
Recorder (CVR)
Functions

-31-01-01A C 2 1

-31-01-01B A 2 0 May be inoperative provided:

a) At least one flight data recorder (FDR)
function operates normally, and
b) Repairs are made within three flight
days.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
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AIRCRAFT: REVISION NO: 2 PAGE:
BOEING B-787
DATE: 01/25/2012 31-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING
SYSTEMS

-31-01 Digital Voice-Data

Recorder Systems
(Cont’d)

-31-01-02
Flight Data Recorder
(FDR) Functions

-31-01-02A C 2 1

-31-01-02B A 2 0 May be inoperative provided:

a) At least one cockpit voice recorder
(CVR) function operates normally,
b) At least one datalink recorder (DLR)
function operates normally,
c) Airplane is not dispatched from a
designated airport as listed in the
operator’s MEL unless:
1) The FDR failure occurs after pushback
but prior to takeoff, or
2) The FDR repair was attempted but
was not successful,
d) In those cases where repair is attempted
but not successful, the airplane may be
dispatched on a flight or a series of
flights until the next designated airport
where repair must be accomplished prior
to dispatch, and
e) Repairs are made within three flight
days.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
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AIRCRAFT: REVISION NO: 2 PAGE:
BOEING B-787
DATE: 01/25/2012 31-3
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING
SYSTEMS

-31-01 Digital Voice-Data

Recorder Systems
(Cont’d)

-31-01-02
Flight Data Recorder
(FDR) Functions
(Cont’d)

-31-01-02-01
FDR Recording A - - Up to three (3) recording parameters may be
Parameters Required inoperative provided:
by FAR a) At least one cockpit voice recorder
(CVR) function operates normally,
b) At least one datalink recorder (DLR)
function operates normally, and
c) Repairs are made within 20 calendar
days.

-31-01-02-02
FDR Recording A - - May be inoperative provided repairs are made
Parameters Not prior to the completion of the next heavy
Required by FAR maintenance visit.

-31-01-03
Datalink Recorder
(DLR) Functions

-31-01-03A C 2 1

-31-01-03B A 2 0 May be inoperative provided:

a) At least one flight data recorder (FDR)
function operates normally, and
b) Repairs are made within three flight
days.

-31-01-04
Recorder C 1 0
Independent Power
Supply
U.S. DEPARTMENT OF TRANSPORTATION
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SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING
SYSTEMS

-33-01 Flight Deck Printer

-33-01A C 1 0 (O) May be inoperative provided alternate

procedures are established and used.

-33-01B D 1 0 May be inoperative provided procedures do not

require its use.

-33-01-01
Miscellaneous D - -
Features

-51-01 Master WARNING C 2 1 One may be inoperative provided both flight deck
Lights speaker systems operate normally.

-51-02 Master CAUTION C 2 1 One may be inoperative provided both flight deck
Lights speaker systems operate normally.

-51-03 Autopilot Disconnect B 1 0 (O) May be inoperative provided:

Warning Function a) Autopilot is not used,
b) Approach minimums do not require use
of the autopilot,
c) Number of flight segments and segment
duration is acceptable to flight crew, and
d) Enroute operations do not require use of
the autopilot.

-51-04 Nose Gear Pressure C 1 0 (O) May be inoperative provided stabilizer trim
Transducer System position is verified to be properly set before each
departure.
U.S. DEPARTMENT OF TRANSPORTATION
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SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING
SYSTEMS

-61-01 Display Units (DU)

-61-01-01
Lower DU C 1 0 May be inoperative provided:
a) EFIS/DSP panels operate normally, and
b) Remaining display units operate
normally.

-61-01-02
Left Inboard DU B 1 0 (M) May be inoperative provided:
a) Right PFD/MFD selector is verified to
operate normally,
b) ISFD operates normally,
c) Touchpad cursor control devices (CCDs)
operate normally,
d) EFIS/DSP panels operate normally,
e) Multifunction keypads (MFKs) operate
normally, and
f) Remaining display units operate
normally.

-61-01-03
Left Outboard DU B 1 0 (M) May be inoperative provided:
a) Right PFD/MFD selector is verified to
operate normally,
b) ISFD operates normally,
c) Touchpad cursor control devices (CCDs)
operate normally,
d) EFIS/DSP panels operate normally,
e) Multifunction keypads (MFKs) operate
normally, and
f) Remaining display units operate
normally.

-61-01-04
Display Unit C 5 0 May be inoperative provided master brightness
Brightness/Contrast control system operates normally.
Controls
U.S. DEPARTMENT OF TRANSPORTATION
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1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING
SYSTEMS

-61-02 Graphics Generator

Systems

-61-02-01
Graphics Generator C 4 3
Modules (GGMs)

-61-02-02
Display Unit Interface C 1 0 (M) May be dispatched with DISPLAY UNIT
INTERFACE faults provided:
a) Both PFD/MFD selector switches are
verified to operate normally,
b) Display units operate normally, and
c) Graphics generator modules operate
normally.

-61-03 Touchpad Cursor C 2 1 One may be inoperative provided:

Control Devices a) EFIS/DSP panels operate normally, and
(CCD) b) Multifunction keypads (MFKs) operate
normally.

-61-04 Multifunction Keypads A 2 1 (O) One may be inoperative provided:

(MFKs) a) Display units operate normally,
b) Touchpad cursor control devices (CCDs)
operate normally,
c) EFIS/DSP panels operate normally,
d) HDG-TRK SEL switch operates normally,
e) Tuning and control panels (TCPs)
operate normally,
f) All switches on remaining keypad
operate normally, and
g) Repairs are made within two flight days.

-61-04-01
SYS, CDU, INFO, C 12 6 May be inoperative provided all switches on
CHKL, COMM, ND opposite keypad operate normally.
Switches

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
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AIRCRAFT: REVISION NO: 2 PAGE:
BOEING B-787
DATE: 01/25/2012 31-7
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING
SYSTEMS

-61-04 Multifunction Keypads

(MFKs)
(Cont’d)

-61-04-02
PREV PAGE, NEXT C 6 3 May be inoperative provided all switches on
PAGE, EXEC opposite keypad operate normally.
Switches

-61-04-03
Rotary CURSOR C 2 1 One may be inoperative provided:
CONTROL Selector a) All switches on opposite keypad operate
normally, and
b) Associated touchpad cursor control
device (CCD) operates normally.

-61-05 EFIS/DSP Panels C 2 1 (O) One may be inoperative provided:

a) Touchpad cursor control devices (CCDs)
operate normally,
b) Multifunction keypads (MFKs) operate
normally, and
c) Display units operate normally.

-61-06 PFD/MFD Selector

Switches

-61-06-01
OUTBD Position C 2 1 (M) One may be inoperative provided:
a) Opposite switch is verified to operate
normally,
b) Associated selector switch remains in
NORM position, and
c) Display units operate normally.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 2 PAGE:
BOEING B-787
DATE: 01/25/2012 31-8
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING
SYSTEMS

-61-06 PFD/MFD Selector

Switches
(Cont’d)

-61-06-02
INBD Position C 2 1 (M) One may be inoperative provided:
a) Opposite switch is verified to operate
normally,
b) Associated selector switch remains in
NORM position, and
c) Display units operate normally.

-61-06-03
Left NORM Position

-61-06-03A B 1 0 May be inoperative with associated selector

switch in OUTBD position provided left inboard
display unit is considered inoperative.

-61-06-03B B 1 0 May be inoperative with associated selector

switch in INBD position provided left outboard
display unit is considered inoperative.

-61-07 Instrument Source

(AIR DATA/ATT)
Selector Switches

-61-07-01
ALTN Position C 2 1 (M) One may be inoperative provided:
a) Opposite AIR DATA/ATT switch is
verified to operate normally, and
b) Associated selector switch remains in
AUTO position.

-61-08 Clock Switches C 2 1

U.S. DEPARTMENT OF TRANSPORTATION
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AIRCRAFT: REVISION NO: 2 PAGE:
BOEING B-787
DATE: 01/25/2012 31-9
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING
SYSTEMS

-61-09 Heading Reference C 1 0 (O) May be inoperative provided enroute

(HDG REF) Switch procedures do not require its use.
TRUE Function

-61-10 Remote Light Sensor C 1 0

(RLS) System

-61-11 Electronic Checklist C 1 0 (M)(O) May be inoperative provided:

(ECL) System a) Electronic checklist is deactivated, and
b) Established paper checklist procedures
are used.

-61-11-01
ECL Closed Loop C - 0 (O) May be inoperative provided ECL line item
Switch Indications override procedures are used when required to
complete checklists.

-61-12 EICAS Status

Messages

-61-12A C - 0 (M) May be inoperative provided associated

equipment is verified to operate normally before
each departure.

-61-12B C - 0 May be inoperative provided associated

equipment is considered inoperative.

-61-13 Airport Map Function

***

-61-13A C 1 0 (O) May be inoperative or database may be out

of currency provided alternate procedures are
established and used.

-61-13B D 1 0 May be inoperative or database may be out of

currency provided procedures do not require its
use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 2 PAGE:
BOEING B-787
DATE: 01/25/2012 31-10
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING
SYSTEMS

-61-14 Head-Up Display

(HUD) Systems

-61-14A C 2 0 (O) May be inoperative provided alternate

procedures are established and used.

NOTE: Any mode which operates normally may

be used.

-61-14B D 2 0 May be inoperative provided procedures do not

require its use.

-61-14-01
***
Low Visibility Takeoff
Function

-61-14-01A C 1 0 May be inoperative provided takeoff minima do

not require its use.

-61-14-01B D 1 0 May be inoperative provided procedures do not

require its use.

-61-14-02
De-Clutter Switches C 2 0

-61-14-03
Brightness (BRT) C 2 0 May be inoperative and associated HUD used if
Controls acceptable to affected crew member.

-61-15 Display Panel C 1 0 May be dispatched with DISPLAY PANEL

Interface INTERFACE faults.

-61-16 Displays Airplane C 1 0 May be dispatched with DISPLAYS AP SEQ

Sequence Number DISAGREE faults.
Monitor
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 32-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR

-00-01 Landing Gear C 1 0

Synoptic Display

-08-01 Proximity Sensing

System

-08-01-01
Proximity Sensor C 1 0 May be inoperative or have faults provided
Data Concentrator associated equipment is considered inoperative.
(PSDC) 1

-08-01-02
Proximity Sensor C 1 0 May be inoperative or have faults provided
Data Concentrator associated equipment is considered inoperative.
(PSDC) 6

-08-01-03
PSDC 2, 3, 4, 5 C 8 4 One power source for each PSDC may be
Power Sources inoperative.

-08-01-04
PSDC 1, 6 Databuses C 4 2 One databus for each PSDC may be inoperative.

-08-01-05
PSDC 2, 3, 4, 5 C 8 4 (M) One databus for each PSDC may be
Databuses inoperative provided each inoperative databus is
verified to be connected to the remote data
concentrator (RDC) in position 19.

-09-01 Air/Ground Sensors C 8 4 (M) One tilt sensor on each main landing gear
and one strut compression sensor on each main
landing gear may be inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 32-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR

-30-01 Landing Gear C 1 0 (M)(O) May be inoperative provided:

Actuation System a) Landing gear is secured in the down
position, and
b) Airplane is dispatched in accordance
with the AFM Landing Gear Extended
Appendix.

-31-01 Landing Gear Lever C 1 0 (O) May be inoperative provided solenoid is in

Lock Solenoid the locked position.

-31-02 Landing Gear Control

Relays

-31-02-01
Landing Gear Control C 2 1 (M) One may be inoperative provided:
Reset Relays a) Inoperative relay is deactivated, and
b) Opposite system channel is verified to
operate normally.

-31-02-02
Main Landing Gear C 6 3 (M) May be inoperative on one system channel
Inhibit Relays provided:
a) Inoperative relay is deactivated, and
b) Opposite system channel is verified to
operate normally.

-31-02-03
Nose Landing Gear C 6 3 (M) May be inoperative on one system channel
Inhibit Relays provided:
a) Inoperative relay is deactivated, and
b) Opposite system channel is verified to
operate normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 32-3
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR

-31-03 Landing Gear Control

Solenoids

-31-03-01
Main Landing Gear C 18 9 (M) May be inoperative on one system channel
Control Solenoids provided:
a) Inoperative solenoid is deactivated, and
b) Opposite system channel is verified to
operate normally.

-31-03-02
Nose Landing Gear C 12 6 (M) May be inoperative on one system channel
Control Solenoids provided:
a) Inoperative solenoid is deactivated, and
b) Opposite system channel is verified to
operate normally.

-31-04 Landing Gear Control

Sensors

-31-04-01
Main Landing Gear C 16 15 (M) One may be inoperative deactivated.
Control Sensors

-31-04-02
Nose Landing Gear C 6 5 (M) One may be inoperative deactivated.
Control Sensors

-31-05 Landing Gear Control C 6 5 (M) One may be inoperative provided remaining
Lever Switches landing gear control lever switches are verified to
operate normally.

-31-06 Landing Gear Door C 3 0 (M) May be inoperative provided:

Safety Valve a) Associated landing gear door is verified
Indication Systems to open and close normally, and
b) Associated landing gear door safety
valve is verified to be in the STOW
position before each departure.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 32-4
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR

-31-07 Landing Gear

Bypass/Auto-Off
Valve System

-31-07-01
Nose Landing Gear C 1 0 (M)(O) May be inoperative provided:
a) Landing gear is secured in the down
position, and
b) Airplane is dispatched in accordance
with the AFM Landing Gear Extended
Appendix.

-31-07-01-01
Pressure Transducer C 1 0 (M) May be inoperative provided:
a) Nose landing gear bypass/auto-off valve
pressure transducer is deactivated, and
b) Nose landing gear bypass/auto-off valve
is verified to operate normally.

-31-07-02
Main Landing Gear C 1 0 (M)(O) May be inoperative provided:
a) Landing gear is secured in the down
position, and
b) Airplane is dispatched in accordance
with the AFM Landing Gear Extended
Appendix.

-31-07-02-01
Pressure Transducer C 1 0 (M) May be inoperative provided:
a) Main landing gear bypass/auto-off valve
pressure transducer is deactivated, and
b) Main landing gear bypass/auto-off valve
is verified to operate normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 32-5
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR

-32-01 Main Gear Door B 4 3 (M)(O) One spring on one main gear door uplock
Uplock Springs mechanism may be missing provided the gear
(CN-AA26494 Not extend speed placard is not exceeded.
Incorporated)

-32-02 Main Gear Uplock B 4 3 (M)(O) One spring on one main gear uplock
Springs mechanism may be missing provided the gear
extend speed placard is not exceeded.

-35-01 Landing Gear

Alternate Extend
System

-35-01A C 1 0 (M) May be inoperative provided:

a) Landing gear doors are verified to open
using the alternate extend system,
b) Landing gear control relays operate
normally,
c) Landing gear control solenoids operate
normally,
d) Landing gear control sensors operate
normally, and
e) Landing gear control lever switches
operate normally.

-35-01B C 1 0 (M)(O) May be inoperative provided:

a) Landing gear is secured in the down
position,
b) Alternate extend system is deactivated,
and
c) Airplane is dispatched in accordance
with the AFM Landing Gear Extended
Appendix.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 32-6
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR

-35-02 Ground Door Release

Control System

-35-02A C 1 0 (M) May be inoperative provided:

a) Both door open control switches are
verified to be open,
b) Landing gear doors are verified to open
using the alternate extend system, and
c) Landing gear doors are verified to close
using the ground door release closing
function.

-35-02B C 1 0 (M)(O) May be inoperative provided:

a) Landing gear is secured in the down
position,
b) Landing gear alternate extend system is
deactivated, and
c) Airplane is dispatched in accordance
with the AFM Landing Gear Extended
Appendix.

-42-01 Autobrake System C 1 0 May be inoperative provided autobrake selector

remains in the OFF position.

-42-02 Antiskid Control C 8 6 (M)(O) May be inoperative on one main landing

Systems gear wheel per truck provided:
a) Associated wheel brake is deactivated,
b) Brakes on remaining wheels on
associated truck operate normally,
c) Electric brake actuators on remaining
wheels on associated truck operate
normally,
d) Appropriate performance adjustments for
brake deactivated are applied, and
e) After takeoff, gear remains down for two
minutes before retraction.

NOTE: In the event of engine failure after V1,

retract landing gear after takeoff.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 32-7
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR

-44-01 Brake Status Lights

(On Nose Gear)

-44-01A C 3 0 (O) May be inoperative provided alternate

procedures are established and used.

-44-01B D 3 0 May be inoperative provided procedures do not

require their use.

-45-01 Wheel Brake Systems C 8 6 (M)(O) May be inoperative on one main landing
gear wheel per truck provided:
a) Inoperative wheel brake is deactivated,
b) Electric brake actuator systems on
remaining wheels on associated truck
operate normally,
c) Appropriate performance adjustments for
brake deactivated are applied, and
d) After takeoff, gear remains down for two
minutes before retraction.

NOTE: In the event of engine failure after V1,

retract landing gear after takeoff.

-45-01-01
Electric Brake C 32 24 (M)(O) One per wheel may be inoperative
Actuator Systems provided:
a) Inoperative electric brake actuator is
deactivated,
b) Remaining wheel brake systems on
associated truck have not been
deactivated, and
c) Appropriate performance adjustments for
electric brake actuator deactivated are
applied.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 32-8
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR

-45-02 Wheel Tie Bolts A - - (M) One per wheel may be broken or missing
provided:
a) Affected wheel is checked for broken
parts or damage, and replaced if broken
parts or damage is found,
b) Associated brake is checked for broken
parts or damage, and is replaced or
deactivated if broken parts or damage is
found,
c) Before each departure, wheel is
inspected for additional broken or
missing tie bolts, and
d) Operations are limited to 5 flights before
repairs are made.

-45-03 Nose Gear Spin C 2 0 (O) May be inoperative or missing provided gear
Brake remains down for two minutes before retraction
after takeoff.

NOTE: In the event of engine failure after V1,

retract landing gear after takeoff.

-46-01 Brake Temperature C 1 0 May be inoperative provided AFM Maximum

Monitor System Quick Turnaround Weight limitations are
(BTMS) observed.

NOTE: Any portion of the system which operates

normally may be used.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 32-9
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR

-49-01 Tire Pressure

Indication System
(TPIS)

-49-01-01 |
Nose Wheel TPIS |

-49-01-01A C 1 0 (M) May be inoperative provided: |

a) Nose wheel TPIS is deactivated, and |
b) Alternate procedures are established and |
used. |

-49-01-01B D 1 0 (M) May be inoperative provided: |

a) Nose wheel TPIS is deactivated, and |
b) Procedures do not require its use. |

-49-01-02 |
Main Wheel TPIS |

-49-01-02A C 1 0 (M) May be inoperative provided alternate |

procedures are established and used. |
|
NOTE: Any portion of the system that operates |
normally may be used. |

-49-01-02B D 1 0 May be inoperative provided procedures do not |

require its use. |
U.S. DEPARTMENT OF TRANSPORTATION
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AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
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1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR

-51-01 Nose Wheel Steering

-51-01-01
Nose Wheel Steering C 2 1 (M) One may be inoperative deactivated.
Channels

-51-01-02
Rudder Pedal C 3 2
Steering Channels

-51-02 Nose Wheel Tillers

-51-02-01
Left Tiller C 1 0 (O) May be inoperative provided:
a) Right tiller operates normally, and
b) Alternate procedures are established and
used.

-51-02-02
Right Tiller

-51-02-02A C 1 0 (O) May be inoperative provided:

a) Left tiller operates normally, and
b) Alternate procedures are established and
used.

-51-02-0B D 1 0 May be inoperative provided:

a) Left tiller operates normally, and
b) Procedures do not require its use.

-51-02-03
Nose Wheel Tiller C 6 4 One channel in each tiller may be inoperative.
Channels
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ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR

-51-03 Nose Wheel Steering

Rudder Pedal
Disconnect
Switches

-51-03A C 2 0 May be inoperative in disconnected position.

-51-03B C 2 1 One may be inoperative in connected position

provided remaining switch is used to disconnect
nose wheel steering for rudder sweeps.

-61-01 Landing Gear C 2 0 (M)(O) May be inoperative provided:

Position Indication a) Landing gear is secured in the down
System position, and
b) Airplane is dispatched in accordance
with the AFM Landing Gear Extended
Appendix.

-61-02 Landing Gear Door C 6 3 (M) One on each landing gear may be
Close Position inoperative deactivated.
Indication Sensors

-61-03 Main Landing Gear C 4 2 (M) One on each main landing gear may be
Uplock Position inoperative provided:
Indication Sensors a) Inoperative sensor is deactivated, and
b) Associated landing gear door close
position indication sensors operate
normally.

-71-01 Tail Strike Detector C 2 1

Channels
U.S. DEPARTMENT OF TRANSPORTATION
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SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
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4. REMARKS OR EXCEPTIONS
33 LIGHTS

-11-01 Flight Compartment C - - Individual lights may be inoperative provided:

Illumination System a) Remaining lighting system lights are
sufficient to clearly illuminate all required
instruments, controls and other devices
for which they are provided,
b) Remaining lighting system lights are
positioned so that direct rays are
shielded from flight crewmembers eyes,
and
c) Lighting configuration and intensity is
acceptable to the flight crew.

Note: Individual button/switch lights and/or

annunciations/indications are excluded
from this relief.

-13-01 Master Brightness C 1 0 May be inoperative provided:

Control System a) Master brightness control switch remains
off, and
b) Display unit brightness/contrast controls
operate normally.

-16-01 Master Auto and Test B 1 0 AUTO function may be inoperative provided:
System a) TEST and BRT functions operate
normally, and
b) Light intensity and configuration is
acceptable to the flight crew.

-21-01 Passenger C - - Individual lights may be inoperative provided

Compartment sufficient lighting remains for crew members to
Illumination System perform their duties.
U.S. DEPARTMENT OF TRANSPORTATION
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SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
33 LIGHTS

-24-01 Passenger
Information Signs

-24-01A C - - (O) May be inoperative provided:

a) PA system operates normally and can be
clearly heard throughout the cabin during
flight, and
b) PA system is used to alert passengers
when associated passenger lighted
information sign is inoperative.

-24-01B C - - (M) May be inoperative provided:

a) Passenger seats from which a
passenger lighted information sign is not
readily legible are blocked and placarded
DO NOT OCCUPY, and
b) Lavatory with passenger lighted
information sign not readily legible has
entrance door locked closed and
placarded, INOPERATIVE – DO NOT
ENTER.

NOTE: These provisions are not intended to

prohibit lavatory use or inspections by
crew members.

-24-01C C - 0 (O) May be inoperative provided:

a) No passengers are carried,
b) A maximum of 19 persons authorized by
14 CFR for non-passenger carrying
operations are carried, and
c) Alternate procedures are established and
used.

-24-01-01
Flight Deck Automatic C - 0 (O) May be inoperative provided alternate
Function procedures are established and used.
U.S. DEPARTMENT OF TRANSPORTATION
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SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
33 LIGHTS

-31-01 Main Wheel Well and

Nose Wheel Well
Service Area Lights

-31-01A C 6 0

-31-01B D 6 0 Individual lights may be inoperative provided

procedures do not require use of service lights

-37-01 Interior Cargo Lights D - - Individual lights may be inoperative provided

sufficient lighting remains for ground personnel to
perform their duties.

-37-02 Exterior Cargo Lights D 4 0

-41-01 Wing Illumination C 2 0 (O) May be inoperative provided ground de-icing

Lights procedures do not require their use.

-42-01 Landing and Taxi

Lights

-42-01A C 8 6 May be inoperative provided:

a) Inoperative lights are not on same side,
and
b) At least one light in each symmetrical
pair of lights (left to right) operates
normally.

-42-01B C 8 0 May be inoperative for day operations.

-42-02 Runway Turnoff C 2 0

Lights
U.S. DEPARTMENT OF TRANSPORTATION
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SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
33 LIGHTS

-43-01 Position Lights

-43-01A C 8 4 May be inoperative provided:

a) One red wingtip light operates normally, |
b) One green wingtip light operates |
normally, |
c) For one or both white tailcone lights |
inoperative, both white wingtip lights |
operate normally, and |
d) For one or both white wingtip lights |
inoperative, both stationary white |
tailcone lights operate normally. |

-43-01B C 8 0 May be inoperative for day operations.

-44-01 Anti-Collision Light C 2 0 May be inoperative for day operations.

Systems (Red
Strobes/White
Strobes)

-44-01-01
Red Strobe Light C 1 0 May be inoperative provided wingtip and tail
System white strobe light system operates normally.

-44-01-02
White Strobe Light C 1 0 May be inoperative provided upper and lower red
System fuselage strobe light system operates normally.

-45-01 Logo Lights D 2 0

-49-01 Exterior Passenger C 8 4 May be inoperative provided:

*** Door Viewing Lights a) At least one light at door 1L or 2L
operates normally,
b) At least one light at door 1R or 2R
operates normally,
c) At least one light at door 3L or 4L
operates normally, and
d) At least one light at door 3R or 4R
operates normally.
U.S. DEPARTMENT OF TRANSPORTATION
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SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
33 LIGHTS

-51-01 Emergency Lights C - 0 (O) May be inoperative provided:

a) No passengers are carried,
b) A maximum of 19 persons authorized by
14 CFR for non-passenger carrying
operations are carried, and
c) Alternate procedures are established and
used.

-51-01-01
Main-Aisle Overhead C - - Two main-aisle overhead emergency lights may
Emergency Lights be inoperative between each pair of fore and aft
adjacent passenger entry doors provided:
a) Inoperative lights are not located over
same aisle, and
b) Overhead emergency lights integrated
into exit signs at associated passenger
entry doors operate normally.

-51-01-02
Cross-Aisle Overhead C - - One cross-aisle overhead emergency light may
Emergency Lights be inoperative at each passenger entry door.

-51-02 Floor Proximity C - 0 (O) May be inoperative provided:

Lighting Systems a) No passengers are carried,
b) A maximum of 19 persons authorized by
14 CFR for non-passenger carrying
operations are carried, and
c) Alternate procedures are established and
used.

-51-02-01
Seat-Mounted C - - Every other seat-mounted light may be
Proximity Lights inoperative provided floor proximity lights
adjacent to each passenger entry door operate
normally.

(Continued)
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SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
33 LIGHTS

-51-02 Floor Proximity

Lighting Systems
(Cont’d)

-51-02-02
Main-Aisle Monument C - - One main-aisle light may be inoperative per aisle
Mounted Proximity side on a monument where two main-aisle lights
Lights per aisle side are installed.

-51-02-03
Cross-Aisle C - - One cross-aisle light may be inoperative on a
Monument Mounted monument where two cross-aisle lights are
Proximity Lights installed provided light is not adjacent to
attendant seat.

-51-02-04
Exit Identifiers

-51-02-04-01
Door 1 C 4 2 Aft exit identifier (back-light and/or flood-light) at
each door may be inoperative.

-51-02-04-02
Door 2 and Door 3 C 8 4 One exit identifier flood-light at each door may be
inoperative.

-51-02-04-03
Door 4 C 4 2 Forward exit identifier (back-light and/or flood-
light) at each door may be inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
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SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
34 NAVIGATION

-12-01 Pitot Air Data

Modules

-12-01-01
Right Pitot Air Data B 1 0 (M) May be inoperative provided:
Module a) Left and center pitot probes are
inspected before each departure,
b) Left and center pitot probe heater
systems operate normally,
c) Left and center pitot air data modules
operate normally,
d) Static air data modules operate normally,
e) AIR DATA/ATT instrument source
switches operate normally, and
f) Approach minimums do not require its
use.

-12-01-02
Left Pitot Air Data B 1 0 (M) May be inoperative provided:
Module a) Right and center pitot probes are
inspected before each departure,
b) Right and center pitot probe heater
systems operate normally,
c) Right and center pitot air data modules
operate normally,
d) Static air data modules operate normally,
e) AIR DATA/ATT instrument source
switches operate normally, and
f) Approach minimums do not require its
use.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
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AIRCRAFT: REVISION NO: 9 PAGE:
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1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
34 NAVIGATION

-12-01 Pitot Air Data

Modules
(Cont’d)

-12-01-03
Center Pitot Air Data B 1 0 (M) May be inoperative provided:
Module a) Left and right pitot probes are inspected
before each departure,
b) Left and right pitot probe heater systems
operate normally,
c) Left and right pitot air data modules
operate normally,
d) Static air data modules operate normally,
e) AIR DATA/ATT instrument source
switches operate normally, and
f) Approach minimums do not require its
use.

-12-02 Static Air Data

Modules

-12-02-01
Right Static Air Data B 1 0 May be inoperative provided:
Module a) Left static air data module operates
normally.
b) Pitot air data modules operate normally,
c) Pitot probe heater systems operate
normally,
d) AIR DATA/ATT instrument source
switches operate normally,
e) At least one GPS operates normally, and
f) Approach minimums do not require its
use.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
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AIRCRAFT: REVISION NO: 9 PAGE:
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DATE: 01/24/2014 34-3
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
34 NAVIGATION

-12-02 Static Air Data

Modules
(Cont’d)

-12-02-02
Left Static Air Data B 1 0 May be inoperative provided:
Module a) Right static air data module operates
normally,
b) Pitot air data modules operate normally,
c) Pitot probe heater systems operate
normally,
d) AIR DATA/ATT instrument source
switches operate normally,
e) At least one GPS operates normally, and
f) Approach minimums do not require its
use.

-12-03 Angle of Attack (AOA) B 4 2

Resolvers

-16-01 Altitude Alerting A 1 0 (O) May be inoperative provided:

System a) Autopilot with altitude hold and altitude
capture operates normally,
b) Enroute operations do not require its
use,
c) Airplane does not depart from an airport
(as listed in the operator’s MEL) where
repair or replacement can be made, and
d) Repairs are made within three flight
days.

-21-01 Earth Reference

System (ERS)

-21-01-01
Inertial Reference C 2 1 (M) One may be inoperative provided:
Units (IRUs) a) Inoperative IRU is deactivated,
b) AHRUs operate normally, and
c) At least one GPS operates normally.
U.S. DEPARTMENT OF TRANSPORTATION
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1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
34 NAVIGATION

-21-01-02
Attitude/Heading C 2 1 (M) One may be inoperative provided:
Reference Units a) Inoperative AHRU is deactivated, and
(AHRUs) b) IRUs operate normally.

-23-01 Non-Stabilized B 1 0 May be inoperative provided ISFD heading

Magnetic Compass display operates normally.
(Standby)

-24-01 Integrated Standby

Flight Display (ISFD)

-24-01-01
Attitude Indication B 1 0 May be inoperative provided:
a) Operations are conducted in day VMC
only, and
b) Operations are not conducted into known
or forecast over-the-top conditions.

-24-01-02
Airspeed Indication B 1 0 May be inoperative provided:
a) Left and right pitot air data modules
operate normally,
b) Left and right pitot probe heater systems
operate normally,
c) Left and right static air data modules
operate normally, and
d) AIR DATA/ATT instrument source
switches operate normally.

-24-01-03
Approach Mode C 1 0

-24-01-04
Heading Display B 1 0 May be inoperative provided non-stabilized
magnetic compass (standby) operates normally.

-31-01 Instrument Landing C 2 - Any in excess of those required by FAR may be

Systems (ILS) inoperative provided approach minimums do not
require their use.
U.S. DEPARTMENT OF TRANSPORTATION
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1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
34 NAVIGATION

-31-02 GPS Landing C 2 0 May be inoperative provided approach minimums

Systems (GLS) do not require their use.

-31-03 Marker Beacon C 1 0 May be inoperative provided approach minimums

System do not require its use.

-31-04 VOR Navigation D 2 - Any in excess of those required by FAR may be

Systems inoperative.

-31-05 Global Positioning

Systems (GPS)

-31-05A C 2 1 One may be inoperative provided enroute

operations do not require its use.

-31-05B C 2 0 May be inoperative provided:

a) Enroute operations do not require their
use, and
b) IRUs operate normally.

-33-01 Radio Altimeter |

Systems |

-33-01-01 |
CN AA-29854 (Part A B 2 1 (O) One may be inoperative provided: |
or B) Not a) NO AUTOLAND advisory message is |
Incorporated displayed, |
b) Approach minimums do not require its
use,
c) Operating procedures do not require its
use, and
d) LNAV is not armed for takeoff.

-33-01-02 |
CN AA-29854 (Part A B 2 1 (O) One may be inoperative provided: |
or B) Incorporated a) NO AUTOLAND advisory message is |
displayed, |
b) Approach minimums do not require its |
use, |
c) Operating procedures do not require its |
use. |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 34-6
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
34 NAVIGATION

-42-01 Weather Radar

System

-42-01A D 2 1

-42-01B C 2 0 (O) May be inoperative provided:

a) Weather radar is not required by FAR,
b) Reactive windshear alert (GPWS mode
7) operates normally, and
c) Alternate procedures are established and
used.

-42-01C B 2 0 (O) May be inoperative provided:

a) Weather radar is not required by FAR,
and
b) Alternate procedures are established and
used.

NOTE: Operator’s alternate procedures should

include reviewing windshear avoidance
and windshear recovery procedures.

-42-01-01
Predictive Windshear
Alert Mode

-42-01-01A D 2 1

-42-01-01B C 2 0 (O) May be inoperative provided:

a) Reactive windshear alert (GPWS mode
7) operates normally, and
b) Alternate procedures are established and
used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
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1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
34 NAVIGATION

-42-01 Weather Radar

System
(Cont’d)

-42-01-01
Predictive Windshear
Alert Mode
(Cont’d)

-42-01-01C B 2 0 (O) May be inoperative provided alternate

procedures are established and used.

NOTE: Operator’s alternate procedures should

include reviewing windshear avoidance
and windshear recovery procedures.

-42-01-02
Auto Tilt Function C 1 0

-42-02 Traffic Collision and

Avoidance System
(TCAS)

-42-02A C 2 1

-42-02B B 2 0 May be inoperative provided enroute or approach

procedures do not require its use.
U.S. DEPARTMENT OF TRANSPORTATION
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1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
34 NAVIGATION

-42-03 ATC Transponder/

Automatic Altitude
Reporting Systems

-42-03A D 2 1 Any in excess of those required by 14 CFR may |

be inoperative.

-42-03B B 2 0 May be inoperative provided:

a) Enroute operations do not require its |
use, and
b) Prior to flight, approval is obtained from
ATC facilities having jurisdiction over the
planned route of flight.

-42-03-01 |
Elementary and A - 0 May be inoperative provided: |
Enhanced Downlink a) Enroute operations do not require its |
Aircraft Reportable use, and |
Parameters Not b) Repairs are made prior to completion of |
Required By 14 CFR next heavy maintenance visit. |

-42-03-02 |
ADS-B Squitter |
Transmissions |

-42-03-02A C 2 0 (O) May be inoperative provided alternate |

procedures are established and used. |
|
NOTE: Any ADS-B Out function that operates |
normally may be used. |

-42-03-02B D 2 0 May be inoperative provided enroute operations |

do not require its use. |
U.S. DEPARTMENT OF TRANSPORTATION
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DATE: 01/24/2014 34-9
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
34 NAVIGATION

-42-04 Alerting and C 1 0 (O) May be inoperative provided tuning and

Transponder Control control panels operate normally.
Panel

-42-05 Ground Proximity

Warning System
(GPWS)

-42-05A D 2 1

-42-05B A 2 0 (O) May be inoperative provided:

a) Predictive windshear alert mode
operates normally,
b) Alternate procedures are established and
used, and
c) Repairs are made within two flight days.

-42-05C A 2 0 (O) May be inoperative provided:

a) Alternate procedures are established and
used, and
b) Repairs are made within two flight days.

NOTE: Operator’s alternate procedures should

include reviewing windshear avoidance
and windshear recovery procedures.

-42-05-01
Advisory Callouts C 2 0 (O) May be inoperative provided alternate
(Mode 6) procedures are established and used.

(Continued)
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SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
34 NAVIGATION

-42-05 Ground Proximity

Warning System
(GPWS) (Cont’d)

-42-05-02
Windshear Alert
Mode (Reactive)
(Mode 7)

-42-05-02A D 2 1

-42-05-02B C 2 0 (O) May be inoperative provided:

a) Alternate procedures are established and
used, and
b) Predictive windshear alert mode
operates normally.

-42-05-02C B 2 0 (O) May be inoperative provided alternate

procedures are established and used.

NOTE: Operator’s alternate procedures should

include reviewing windshear avoidance
and windshear recovery procedures.

-42-05-03
Terrain Awareness
Function

-42-05-03A D 2 1

-42-05-03B B 2 0 (O) May be inoperative provided alternate

procedures are established and used.
U.S. DEPARTMENT OF TRANSPORTATION
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1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
34 NAVIGATION

-55-01 Distance Measuring D 2 - Any in excess of those required by FAR may be

Equipment (DME) inoperative.

-57-01 ADF Systems D 2 - Any in excess of those required by FAR may be

*** inoperative.

-61-01 Flight Management C 3 2

Function

-61-01-01
Navigation Databases C 3 0 (O) May be out of currency provided:
a) Current aeronautical charts are used to
verify navigation fixes before dispatch,
b) Procedures are established and used to
verify status and suitability of navigation
facilities used to define route of flight,
and
c) Approach navigation radios are verified
to be properly tuned and identified.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 35-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
35 OXYGEN

-11-01 Crew Oxygen C 1 0 (M) May be inoperative provided:

Pressure Indication a) Crew oxygen supply is verified to be
System above minimum required before each
departure, and
b) Crew oxygen shutoff valve(s) is verified
open.

-11-01-01
Overboard Discharge C 1 0 May be damaged or missing.
Indicator Disc

-21-01 Passenger Oxygen B 1 0 (O) May be inoperative provided: |

System a) Appropriate portable oxygen supplies are |
available, |
b) Both air conditioning packs operate |
normally, |
c) Pressurization system operates normally, |
d) Appropriate altitude adjustments are |
applied, and |
e) Passengers are appropriately briefed. |

-21-01-01 |
Power Channels C 18 9 One for each PSU zone may be inoperative. |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 35-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
35 OXYGEN

-21-02 Passenger Oxygen

Controllers

-21-02A B - 0 (M) May be inoperative provided associated

seats are blocked and placarded to prevent
occupancy.

-21-02B B - 0 (O) May be inoperative provided:

a) Appropriate portable oxygen supplies are
available,
b) Both air conditioning packs operate
normally,
c) Pressurization system operates normally,
d) Appropriate altitude adjustments are
applied, and
e) Passengers are appropriately briefed.

-21-02-01
Lavatory Oxygen B - 0 (M) May be inoperative provided associated
Controllers lavatory door is locked closed and placarded
INOPERATIVE – DO NOT ENTER.

-21-03 Passenger Oxygen B 1 0 May be inoperative provided flight remains at or

Automatic below FL 300.
Presentation System

-21-04 Passenger Oxygen C 1 0

ON Light
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 35-3
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
35 OXYGEN

-21-05 OFCR/OFAR Oxygen

*** Controllers

-21-05-01
Seat/Bunk Controllers

-21-05-01A C - 0 (M) May be inoperative provided associated

seat/bunk is blocked and placarded to prevent
occupancy.

-21-05-01B C - 0 (O) May be inoperative provided:

a) Appropriate portable oxygen supplies are
available,
b) Both air conditioning packs operate
normally,
c) Pressurization system operates normally,
d) Appropriate altitude adjustments are
applied, and
e) Crew are appropriately briefed.

-31-01 Portable Oxygen D - - (M) Any in excess of those required by FAR may
Dispensing Units be inoperative or missing provided:
(Bottle and Mask) a) Required distribution of bottles is
maintained, and
b) Bottles not properly serviced are
replaced, serviced or removed at the
next available maintenance facility.

-31-02 Protective Breathing D - - Any in excess of those required by FAR may be

Equipment (PBE) inoperative or removed provided location
placarding is removed or obscured.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 7 PAGE:
BOEING B-787
DATE: 03/22/2013 38-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
38 WATER/WASTE

-10-01 Potable Water

Systems

-10-01A C - - (M) Individual components may be inoperative

provided:
a) Associated components are deactivated
or isolated, and
b) Associated system components are
verified not to have leaks.

NOTE: Any portion of system which operates

normally may be used.

-10-01B C 1 0 (M) May be inoperative provided:

a) System is drained, and
b) Procedures are established to ensure
that system is not serviced.

-10-01-01
Potable Water D - -
Indication System
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 7 PAGE:
BOEING B-787
DATE: 03/22/2013 38-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
38 WATER/WASTE

-30-01 Waste Water

Systems

-30-01A C - 0 (M) Individual components may be inoperative

provided:
a) Associated components are deactivated
or isolated, and
b) Associated system components are
verified not to have leaks.

NOTE: Any portion of system which operates

normally may be used.

-30-01B C - 0 (M) Associated lavatory may be inoperative

provided:
a) Associated components are deactivated
or isolated to prevent leaks, and
b) Associated lavatory door is locked closed
and placarded, INOPERATIVE - DO
NOT ENTER.

NOTE: These provisions are not intended to

prohibit inspections by crew members.

-30-01-01
Vacuum Blowers C 2 0 (M)(O) May be inoperative provided:
a) Associated vacuum blower is
deactivated, and
b) Galley sinks and lavatories affected by
inoperative vacuum blower are not used
on the ground or at flight altitudes below
16,000 feet.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 6 PAGE:
BOEING B-787
DATE: 11/21/2012 42-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
42 INTEGRATED MODULAR
AVIONICS

-21-01 Common Computing

Resource General
Processing
Modules (GPMs)

-21-01A C 16 15 One may be inoperative in position 8L provided

one High Frequency (HF) Communication
System is considered inoperative.

-21-01B C 16 15 One may be inoperative in position 8R.

-21-02 Remote Data

Concentrators
(RDCs)

-21-02-01
RDCs 1 and 3

-21-02-01A C 2 1 May be dispatched with CCS RDC FAULT

provided:
a) Remaining RDCs operate normally, and
b) Left thrust reverser locking actuator
proximity sensors operate normally.

-21-02-01B C 2 1 May be dispatched with CCS RDC FAULT

provided:
a) Remaining RDCs operate normally, and
b) Left thrust reverser is considered
inoperative.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 6 PAGE:
BOEING B-787
DATE: 11/21/2012 42-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
42 INTEGRATED MODULAR
AVIONICS

-21-02 Remote Data

Concentrators
(RDCs)
(Cont’d)

-21-02-02
RDCs 2 and 4

-21-02-02A C 2 1 May be dispatched with CCS RDC FAULT

provided:
a) Remaining RDCs operate normally, and
b) Right thrust reverser locking actuator
proximity sensors operate normally.

-21-02-02B C 2 1 May be dispatched with CCS RDC FAULT

provided:
a) Remaining RDCs operate normally, and
b) Right thrust reverser is considered
inoperative.

-21-02-03
RDCs 5-18, 21, 23 C 16 15 May be dispatched with CCS RDC FAULT
provided remaining RDCs operate normally.

-21-02-04
RDC 19

-21-02-04A C 1 0 May be dispatched with CCS RDC FAULT

provided remaining RDCs operate normally.

-21-02-04B C 1 0 (M)(O) May be inoperative deactivated provided

remaining RDCs operate normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 44-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
44 CABIN SYSTEMS

-11-01 Cabin Attendant C - 1 (M) May be inoperative deactivated.

Panels (CAP)

-12-01 Passenger Address B 1 0 (O) May be inoperative provided:

System a) Flight attendant call lights operate |
normally, and |
b) Alternate, normal and emergency
procedures, and/or operating restrictions
are established and used.

NOTE: Any function that operates normally may

be used.

-12-01-01
Lavatory Speakers C - - (O) May be inoperative provided alternate
procedures are established and used.

-12-01-02
Cabin Speakers C - - May be inoperative provided no adjacent cabin
speaker pairs (forward to aft) are inoperative.

-12-02 Prerecorded
*** Passenger
Announcement
System

-12-02A C 1 0 (O) May be inoperative provided alternate

procedures are established and used.

-12-02B D 1 0 May be inoperative provided procedures do not

require its use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 44-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
44 CABIN SYSTEMS

-14-01 Cabin Interphone

Systems

-14-01-01
Flight Deck to Cabin, B 8 4 (O) May be inoperative provided:
Cabin to Flight Deck a) Flight deck to cabin and cabin to flight
Functions deck interphone functions operate
normally on at least fifty percent of the
cabin handsets,
b) Flight deck to cabin and cabin to flight
deck interphone functions operate
normally on at least one handset at each
pair of exit doors, and
c) Alternate communications procedures
between affected flight attendant’s
station(s) and flight deck are established
and used.

NOTE: Any function that operates normally may

be used.

-14-01-02
Cabin to Cabin B 8 4 (O) May be inoperative provided:
Functions a) Cabin to cabin interphone functions
operate normally on at least fifty percent
of the cabin handsets,
b) Cabin to cabin interphone functions
operate normally on at least one handset
at each pair of exit doors, and
c) Alternate communications procedures
between affected flight attendant’s
station(s) are established and used.

NOTE: Any function that operates normally may

be used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 44-3
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
44 CABIN SYSTEMS

-14-01 Cabin Interphone

Systems
(Cont’d)

-14-01-03
Flight Deck to
Ground/Ground to
Flight Deck
Function (Includes
Nose Gear Flight
Interphone Jack)

-14-01-03A C 1 0 (O) May be inoperative provided:

a) Nose gear service interphone jack
operates normally, and
b) Alternate procedures are established and
used.

-14-01-03B B 1 0 (O) May be inoperative provided alternate

procedures are established and used.

-14-02 Cabin Interphone

Alerting Systems

-14-02-01
Flight Deck Call B - 0 May be inoperative provided the flight deck audio |
Visual Alerting alerting system operates normally. |
System |

-14-02-02
Flight Deck Call Audio B - 0 May be inoperative provided the flight deck visual |
Alerting System alerting system operates normally. |

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 44-4
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
44 CABIN SYSTEMS

-14-02 Cabin Interphone

Alerting Systems
(Cont’d)

-14-02-03 |
Flight Attendant Call B - 0 (O) May be inoperative provided:
Lights a) PA system operates normally, and
b) Alternate procedures for contacting flight
attendants are established and used.

NOTE 1: Passenger to attendant call system is

considered Nonessential Equipment
and Furnishings (NEF).

NOTE 2: Any visual alerting system function(s)

that operates normally may be used.

-14-02-04 |
Flight Attendant B 1 0 (O) May be inoperative provided:
Chime a) Flight attendant visual alerting system |
operates normally, and |
b) Alternate procedures for contacting flight
attendants are established and used.

NOTE 1: Passenger to attendant call system is

considered Nonessential Equipment
and Furnishings (NEF).

NOTE 2: Any audio alerting system function(s)

that operates normally may be used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 44-5
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
44 CABIN SYSTEMS

-14-02 Cabin Interphone

Alerting Systems
(Cont’d)

-14-02-05 |
***
OFCR/OFAR Call B - 0 (O) May be inoperative provided:
Light/Chime Systems a) Associated OFCR or OFAR cabin
interphone handset system operates
normally, and
b) Alternate procedures for contacting
crew/attendant rest occupants are
established and used.

NOTE: Any alerting system function that

operates normally may be used.

-14-03 Cabin Interphone

Handset Systems

-14-03-01
Flight Deck

-14-03-01A C 1 0 (O) May be inoperative provided:

a) Flight deck to cabin communication
operates normally, and
b) Alternate procedures are established and
used.

-14-03-01B D 1 0 May be inoperative provided procedures do not

require its use.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 44-6
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
44 CABIN SYSTEMS

-14-03 Cabin Interphone

Handset Systems
(Cont’d)

-14-03-02
Cabin B 8 4 (O) May be inoperative provided:
a) At least fifty percent of cabin handsets
operate normally,
b) One handset must operate normally at
each pair of exit doors, and
c) Alternate communications procedures
between the affected flight attendant’s
station(s) are established and used.

NOTE 1: An operative handset at an inoperative

flight attendant seat shall not be
counted to satisfy the fifty percent
requirement.

NOTE 2: Any handset functions that operate

normally may be used.
-14-03-03
***
OFCR/OFAR C - 0 (O) May be inoperative provided alternate
procedures are established and used.

-43-01 Ground Crew Call C 1 0 (O) May be inoperative provided alternate

System procedures are established and used.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: Original PAGE:
BOEING B-787
DATE: 09/01/2011 45-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
45 CENTRAL MAINTENANCE
SYSTEM

-11-01 Central Maintenance C 2 0

Computing Functions
(CMCF)

-12-01 Airplane Condition D 1 0

Monitoring Function
(ACMF)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: Original PAGE:
BOEING B-787
DATE: 09/01/2011 46-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
46 INFORMATION SYSTEMS

-11-01 Electronic Flight Bag

(EFB) Systems
(Class 3)

-11-01A C 2 1 NOTE: Any function, program or document which

operates normally may be used.

-11-01B C 2 0 (O) May be inoperative provided alternate

procedures are established and used.

NOTE: Any function, program or document which

operates normally may be used.

-11-01C D 2 0 May be inoperative provided procedures do not

require its use.

-12-01 Core Network System C 1 0 NOTE: Any function that operates normally may
be used.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: Original PAGE:
BOEING B-787
DATE: 09/01/2011 47-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
47 INERT GAS SYSTEM

-11-01 Nitrogen Generation

System (NGS)

-11-01-01
Nitrogen Generation A 1 0 May be inoperative provided repairs are made
Performance within 10 flight days.

-11-01-02
Ground Cooling Valve A 1 0 (M) May be inoperative provided:
a) Ground cooling valve is deactivated
closed, and
b) Repairs are made within 10 flight days.

-11-01-03
Cabin Shutoff Valve A 1 0 (M) May be inoperative provided:
a) NGS cabin shutoff valve is deactivated
closed, and
b) Repairs are made within 10 flight days.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 49-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
49 AIRBORNE AUXILIARY
POWER

-11-01 Auxiliary Power Unit C 1 0 (O) May be inoperative provided:

(APU) a) Left AGCU operates normally,
b) VFSG systems operate normally, and
c) Flight remains within 180 minutes of
landing at a suitable airport.

-15-01 APU Air Inlet Door

Actuation System

-15-01A C 1 0 (O) May be inoperative with door in any position

provided:
a) Left AGCU operates normally, |
b) VFSG systems operate normally, and
c) Flight remains within 180 minutes of
landing at a suitable airport.

-15-01B C 1 0 (M)(O) May be inoperative provided door is

deactivated in the inflight open position.

-15-01-01
APU Air Inlet Door C 1 0 (M) May be inoperative provided APU inlet door
Actuator Position is verified to operate normally before each
Indication Switch departure.

-41-01 APU Starting System

-41-01A C 1 0 (O) May be dispatched with APU START faults

provided APU is started before departure and
operated continuously throughout the flight.

-41-01B C 1 0 May be dispatched with APU START SYS faults

provided:
a) Left AGCU operates normally, |
b) VFSG systems operate normally, and
c) Flight remains within 180 minutes of
landing at a suitable airport.

-61-01 APU Controller C 1 0 May be dispatched with APU CONTROL faults.

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 49-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
49 AIRBORNE AUXILIARY
POWER

-61-02 APU Ground Control C 1 0 NOTE: Any function that operates normally may
Panel be used.

-70-01 APU FAULT Light C 1 0

-71-01 APU EGT Indication C 1 0

-73-01 APU RPM Indication C 1 0

-94-01 APU Oil Quantity

Indication System

-94-01A C 1 0 (M) May be inoperative provided APU oil quantity

is verified adequate once each flight day.

-94-01B C 1 0 May be inoperative provided:

a) Left AGCU operates normally, |
b) VFSG systems operate normally,
c) APU is not used, and
d) Flight remains within 180 minutes of
landing at a suitable airport.

-94-02 APU Oil Pressure C 1 0

Indication
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: Original PAGE:
BOEING B-787
DATE: 09/01/2011 50-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
50 CARGO & ACCESSORY
COMPARTMENTS

-11-01 Lower Cargo C - - (O) May be damaged or missing provided

Compartment Linings procedures are established and used to verify the
associated cargo compartment remains empty or
contains only ballast, empty cargo handling
equipment (ballast may be loaded in ULDs), or fly
away kits.

NOTE: Operator MELs must define which items

are approved for inclusion in the fly away
kits and which materials can be used as
ballast.

-20-01 Cargo Handling D 2 0 May be inoperative or portions of the system may

Systems be missing

NOTE: Any portion of the system which operates

normally may be used.

-21-01 Cargo Restraint

Systems

-21-01A A - - (M) May be inoperative or missing provided:

a) Acceptable cargo loading limits from an
approved source, i.e., an approved
Weight and Balance Control and Loading
Manual, are observed, and
b) Repairs are made prior to the completion
of the next heavy maintenance visit.

-21-01B C - - May be inoperative or missing provided

associated cargo compartment remains empty.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 52-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
52 DOORS

-00-01 Door Synoptic Display C 1 0

-11-01 Passenger Entry

Doors/Slides

-11-01A A 8 7 (M)(O) One may be inoperative or slide missing

provided:
a) A conspicuous barrier strap or rope and
a placard stating that the door is
inoperative shall be placed across the
inoperative door,
b) Emergency exit sign and floor proximity
lights associated with the inoperative exit
must be covered to obscure the sign and
lights,
c) Conspicuous signs and placards shall be
placed in appropriate locations to
indicate seats are not to be occupied by
passengers,
d) All other passenger entry doors are fully
operational,
e) All passenger seats halfway to the next
exit in each direction from the inoperative
door/slide, across the entire width of the
airplane, shall be blocked off with
conspicuous tapes or ropes that contrast
with the airplane interior before loading
passengers. Only the seats in these
areas shall be blocked; main passenger
aisles, cross aisles and exit areas must
not be blocked. (For an inoperative
forward door/side, the blocked seating
area shall extend from the forward cabin
end, rearward to a line halfway between
the inoperative forward door and the next
set of doors aft of the inoperative one.
For an inoperative rear door/slide, the
blocked seating area shall extend
forward from the aft cabin end to a line
halfway between the inoperative door
and the next set of doors forward of the
inoperative one),
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 52-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
52 DOORS

-11-01 Passenger Entry

Doors/Slides
(Cont’d)

-11-01A (Cont’d) f) Seated capacity must not exceed rated

capacity of remaining pairs of exits,
g) For extended overwater operations,
occupancy shall not exceed the normal
rated capacity of the slide/rafts, or the
remaining slide/rafts, or the rated
overload capacity of the slide/rafts
remaining after loss of one additional
slide/raft of greatest capacity, whichever
is least,
h) Blocked seating layouts and evacuation
procedures must be developed and
approved by the FAA certificate holding
office for inclusion in the operator’s
manual,
i) Affected door is not used for passenger
loading,
j) Passengers must be advised to not use
affected door, and
k) Repairs are made within one flight day.

NOTE 1: Flight attendants may be stationed in

the vicinity of each door within blocked
areas.

NOTE 2: Weight and Balance Manifest must be

revised as necessary to ensure proper
loading limits are observed.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 52-3
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
52 DOORS

-11-01 Passenger Entry

Doors/Slides
(Cont’d)

-11-01B C 8 4 (M)(O) May be inoperative or slide missing

provided:
a) No passengers are carried,
b) A maximum of 19 persons authorized by
14 CFR for non-passenger carrying
operations are carried,
c) A conspicuous barrier strap or rope and
a placard stating that the door is
inoperative shall be placed across each
inoperative door,
d) Emergency exit sign and floor proximity
lights associated with each inoperative
door must be covered to obscure the
sign and lights,
e) Inoperative doors are not used for
loading,
f) Each person carried has unobstructed
access from their seat to an operative
door,
g) Safety briefing includes location of
inoperative doors and instructions not to
use them, and
h) Alternate procedures are established and
used.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 52-4
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
52 DOORS

-11-02 Passenger Entry

Doors Pressure Stop
Assemblies

-11-02-01
Door Stops 1, 2, 5 C 64 - (M)(O) One pressure stop per door may be
and 6 missing or inoperative provided:
a) There are no visible defects on
remaining stops for the associated door,
b) Smoke detection systems in all |
centerline lavatories and in lavatories aft |
of door 4 are considered inoperative, and |
c) Flight is conducted unpressurized.

-11-02-02
Door Stops 3 and 4 C 32 - (M)(O) One pressure stop per door may be
missing or inoperative provided:
a) There are no visible defects on
remaining stops for the associated door,
b) All automatic cabin pressure control
channels operate normally, and
c) Airplane pressure altitude does not
exceed 12,000 feet.

-11-03 Passenger Entry C 8 7

Doors Hold-Open
Mechanisms

-11-04 Passenger Entry C 8 4

Doors Hold-Open
Release Handles

-11-05 Passenger Entry Door C 8 0 (M)(O) May be inoperative provided:

Flight Lock Systems a) Associated door is verified to be capable
of being opened before each departure,
and
b) A person employed by the operator is
designated to monitor the affected door
handle when cabin differential pressure
is less than 1.5 psi.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 52-5
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
52 DOORS

-11-06 EPAS Power C 16 8 One power channel per door may be inoperative.
Channels

-11-07 EPAS Disarmed C 8 0

Sensors

-11-07-01
Passenger Door C 9 0
Manual Mode
Indicators
(Including Door 1L |
Attendant Switch |
Panel Indicator) |

-11-08 Passenger Door C 9 0 May be inoperative provided flight deck

Automatic Mode indications for passenger door slide automatic
Indicators mode operate normally.
(Including Door 1L |
Attendant Switch |
Panel Indicator) |

-34-01 Forward Cargo Door C 2 1 (M) One may be inoperative provided:

Lift/Latch System a) There is no damage to the lift
(Electric and Manual mechanism,
Modes) b) There is no damage to the latch
mechanism, and
c) Door is operated using the maintenance
manual procedure.

-34-02 Forward Cargo Door C 3 0 (M) May be inoperative provided alternate

Control Panel Lights procedures are established and used.
(FULL OPEN,
READY TO LOCK,
CLOSED & LOCKED)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 52-6
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
52 DOORS

-35-01 Aft Cargo Door C 2 1 (M) One may be inoperative provided:

Lift/Latch System a) There is no damage to the lift
(Electric and Manual mechanism,
Modes) b) There is no damage to the latch
mechanism, and
c) Door is operated using the maintenance
manual procedure.

-35-02 Aft Cargo Door C 3 0 (M) May be inoperative provided alternate

Control Panel Lights procedures are established and used.
(FULL OPEN,
READY TO LOCK,
CLOSED & LOCKED)

-36-01 Bulk Cargo Door Gas C 1 0 (M) May be inoperative provided:

Spring a) Bulk cargo door damper operates
normally, and
b) Safety hold open device is used when
door is in the open position.

-36-02 Bulk Cargo Door C 1 0 May be inoperative provided the bulk cargo door
Damper gas spring operates normally.

-51-01 Flight Deck Door

Automatic Locking
System

-51-01-01
CN-AA33339 Not C 1 0 (M)(O) May be inoperative provided:
Incorporated a) Automatic locking system is deactivated,
b) No passengers are carried,
c) A maximum of 19 persons authorized by
14 CFR for non-passenger carrying
operations are carried, and
d) Alternate procedures are established and
used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 52-7
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
52 DOORS

-51-01 Flight Deck Door

Automatic Locking
System
(Cont’d)

-51-01-01
CN-AA33339 Not
Incorporated
(Cont’d)

-51-01-01-01
Flight Deck Access C 1 0 (M)(O) May be inoperative provided:
System a) Keypad is deactivated, and
b) Alternate procedures are established and
used.

-51-01-01-01-01
LEDs C 3 0 (O) May be inoperative provided alternate
procedures are established and used.

-51-01-01-01-02
***
Door Bell Mode C 1 0 (O) May be inoperative provided alternate
procedures are established and used.

-51-01-01-01-03
Keypad Channels C 2 1

-51-01-01-02
Flight Deck Door C 1 0 (M)(O) May be inoperative provided:
Access Selector a) Keypad is deactivated,
b) Electric lock is verified to operate
normally, and
c) Alternate procedures are established and
used.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 52-8
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
52 DOORS

-51-01 Flight Deck Door

Automatic Locking
System
(Cont’d)

-51-01-01
CN-AA33339 Not
Incorporated
(Cont’d)

-51-01-01-03
FD DOOR LOCK C 1 0 (M) May be inoperative provided automatic
FAIL Indication locking controls are verified to operate normally.

-51-01-01-04
FD DOOR AUTO C 1 0 (M) May be inoperative provided:
UNLK Indication a) Automatic lock controls are verified to
operate normally, and
b) Door chime is verified to operate
normally.

-51-01-01-05
FD DOOR OPEN C 1 0 (M) May be inoperative provided electric lock is
Indication verified to operate normally.

-51-01-02
CN-AA33339
Incorporated

-51-01-02A A 1 0 (M)(O) May be inoperative provided:

a) Automatic locking system is deactivated,
b) Door dead bolt operates normally and is
used to lock the door,
c) Alternate procedures are established and
used for locking and unlocking the door
using the dead bolt, and
d) Repairs are made within two flight days.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 52-9
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
52 DOORS

-51-01 Flight Deck Door

Automatic Locking
System
(Cont’d)

-51-01-02
CN-AA33339
Incorporated
(Cont’d)

-51-01-02B C 1 0 (M)(O) May be inoperative provided:

a) Automatic locking system is deactivated,
b) No passengers are carried,
c) A maximum of 19 persons authorized by
14 CFR for non-passenger carrying
operations are carried, and
d) Alternate procedures are established and
used.

-51-01-02-01
Flight Deck Access C 1 0 (M)(O) May be inoperative provided:
System a) Keypad is deactivated, and
b) Alternate procedures are established and
used.

-51-01-02-01-01
LEDs C 3 0 (O) May be inoperative provided alternate
procedures are established and used.

-51-01-02-01-02
***
Door Bell Mode C 1 0 (O) May be inoperative provided alternate
procedures are established and used.

-51-01-02-01-03
Keypad Channels C 2 1

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 52-10
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
52 DOORS

-51-01 Flight Deck Door

Automatic Locking
System
(Cont’d)

-51-01-02
CN-AA33339
Incorporated
(Cont’d)

-51-01-02-02
Flight Deck Door C 1 0 (M)(O) May be inoperative provided:
Access Selector d) Keypad is deactivated,
e) Electric lock is verified to operate
normally, and
f) Alternate procedures are established and
used.

-51-01-02-03
FD DOOR LOCK C 1 0 (M) May be inoperative provided automatic
FAIL Indication locking controls are verified to operate normally.

-51-01-02-04
FD DOOR AUTO C 1 0 (M) May be inoperative provided:
UNLK Indication a) Automatic lock controls are verified to
operate normally, and
b) Door chime is verified to operate
normally.

-51-01-02-05
FD DOOR OPEN C 1 0 (M) May be inoperative provided electric lock is
Indication verified to operate normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 52-11
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
52 DOORS

-51-02 Flight Deck Door C 1 0 May be inoperative provided flight deck door
Dead Bolt automatic locking system operates normally.

-51-03 Flight Deck Door A 1 0 May be inoperative provided:

Decompression Panel a) Decompression panel is in the latched
Latch position, and
b) Repairs are made within two flight days.

-71-01 Door Indication C 15 0 (M) May be inoperative provided associated door

Systems is verified closed, latched and, if applicable,
locked before each departure.

-71-01-01
Passenger Door C 8 0 May be inoperative provided associated
Locked Indication passenger entry door indication system operates
Light normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 73-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
73 ENGINE FUEL AND CONTROL

-11-01 Engine Main Fuel C 2 1

Pump Strainer
Sensors
(GE)

-11-02 Engine Fuel/Oil Heat C 2 1 One may be inoperative provided associated

*** Exchanger (FOHE) engine fuel filter bypass warning system operates
Sensors normally.

-21-01 Electronic Engine

Controls (EEC)
Normal Mode

-21-01-01
RR CN-AA32375 C 2 0 (O) Normal (NORM) mode may be inoperative
Incorporated provided:
a) Autothrottle system operates normally, |
b) Both engines are operated in the
alternate (ALTN) mode, and
c) Appropriate performance adjustments
are applied.

-21-01-02
GE CN-AA34291 C 2 0 (O) Normal (NORM) mode may be inoperative
Incorporated provided:
a) Autothrottle system operates normally,
b) Turbine case cooling air flow systems
operate normally,
c) Both engines are operated in the
alternate (ALTN) mode, and
d) Appropriate performance adjustments
are applied.

-21-02 Electronic Engine C 2 0 (M) May be inoperative provided associated

Controls (EEC) switches are verified to operate normally.
NORM/ALTN Mode
Lights

-21-03 EEC C1 Faults A 2 0 May be dispatched with C1 faults provided

repairs are made in accordance with times
established by engine manufacturer.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE:
BOEING B-787
DATE: 01/24/2014 73-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
73 ENGINE FUEL AND CONTROL

-21-04 Turbine Overspeed C 2 1

Systems
(RR)

-21-05 Engine Fuel Shutoff C 2 1 (M) One may be inoperative provided the
Valve Indication associated engine fuel shutoff valve is verified to
Systems operate normally once each flight day.
(GE)

-21-06 Engine Thrust Control C 2 1

Malfunction
Accommodation
(TCMA) Functions
(RR)

-31-01 Fuel Flow Indications C 2 1 One may be inoperative provided:

a) All fuel tank quantity indications operate
normally, and
b) Flight remains within 180 minutes of
landing at a suitable airport.

-34-01 Engine Fuel Filter

Bypass Warning
Systems

-34-01-01
Without Engine C 2 1
Fuel/Oil Heat
Exchanger Sensors
Installed

-34-01-02
With Engine Fuel/Oil C 2 1 One may be inoperative provided the associated
Heat Exchanger engine fuel/oil heat exchanger (FOHE) sensor
Sensors Installed operates normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: Original PAGE:
BOEING B-787
DATE: 09/01/2011 74-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
74 IGNITION

-00-01 Ignition Systems

-00-01-01
RR B 4 3 One may be inoperative provided:
a) Associated engine anti-ice system
operates normally, and
b) Associated engine ESS valve operates
normally.

-00-01-02
GE B 4 3 One may be inoperative provided:
a) Associated engine anti-ice system
operates normally, and
b) Associated engine BAI valve operates
normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 1 PAGE:
BOEING B-787
DATE: 10/24/2011 75-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
75 BLEED AIR

-11-01 Engine Section Stator

(ESS) Anti-Ice Valves
(RR)

-11-01A C 2 1 One may be inoperative closed provided:

a) Associated engine ignition systems
operate normally,
b) Airplane is not operated in known or
forecast icing conditions, and
c) Flight remains within 120 minutes of
landing at a suitable airport.

-11-01B B 2 0 (O) May be inoperative open provided

appropriate performance adjustments are
applied.

-11-02 Booster Anti-Ice (BAI) C 2 1 (M) One may be inoperative provided:

Valves a) Inoperative valve is locked closed,
(GE) b) Associated engine ignition systems
operate normally,
c) Airplane is not operated in known or
forecast icing conditions, and
d) Flight remains within 120 minutes of
landing at a suitable airport.

-23-01 Core Compartment C 2 0 (M) May be inoperative locked open.

Cooling (CCC) Valves
(GE)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 1 PAGE:
BOEING B-787
DATE: 10/24/2011 75-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
75 BLEED AIR

-24-01 Turbine Case Cooling

Air Flow Systems
(GE)

-24-01-01
HPTACC Valves C 2 0 (M)(O) May be inoperative provided:
a) Inoperative HPTACC valve is locked in
the closed position,
b) Associated engine CCC valve is locked
in the open position,
c) Associated engine LPTACC valve
operates normally,
d) Both EECs operate in the normal mode,
and
e) Appropriate takeoff thrust settings are
applied.

-24-01-02
LPTACC Valves C 2 0 (M)(O) May be inoperative provided:
a) Inoperative LPTACC valve is locked in
the closed position,
b) Associated engine CCC valve is locked
in the open position,
c) Associated engine HPTACC valve
operates normally,
d) Both EECs operate in the normal mode,
and
e) Appropriate takeoff thrust settings are
applied.

-33-01 Engine Intermediate B 6 4 (O) One may be inoperative on each engine

Pressure (IP) Bleed provided appropriate performance adjustments
Valves are applied.
(RR)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: Original PAGE:
BOEING B-787
DATE: 09/01/2011 77-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
77 ENGINE INDICATING

-22-01 Engine Turbine C 4 2 One per engine may be inoperative.

Overheat Sensors
(RR)

-31-01 Engine Vibration C 2 1

Monitoring Functions
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 6 PAGE:
BOEING B-787
DATE: 11/21/2012 78-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
78 ENGINE EXHAUST

-31-01 Thrust Reversers C 2 1 (M)(O) One may be inoperative provided:

a) Inoperative reverser is secured in the
forward thrust position, and
b) Appropriate performance adjustments
are applied.

-34-01 Reverse Thrust Lever

Interlocks

-34-01A C 2 1 One may be inoperative released.

-34-01B C 2 1 (O) One may be inoperative not released

provided appropriate performance adjustments
are applied.

-36-01 Thrust Reverser

Locking Actuator
Proximity Sensors

-36-01-01
Left Thrust Reverser

-36-01-01A C 4 3 One may be inoperative provided:

a) Remote data concentrator 1 operates
normally, and
b) Remote data concentrator 3 operates
normally.

-36-01-01B C 4 3 One may be inoperative provided left thrust

reverser is considered inoperative.

(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 6 PAGE:
BOEING B-787
DATE: 11/21/2012 78-2
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
78 ENGINE EXHAUST

-36-01 Thrust Reverser

Locking Actuator
Proximity Sensors
(Cont’d)

-36-01-02
Right Thrust Reverser

-36-01-02A C 4 3 One may be inoperative provided:

a) Remote data concentrator 2 operates
normally, and
b) Remote data concentrator 4 operates
normally.

-36-01-02B C 4 3 One may be inoperative provided right thrust

reverser is considered inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 2 PAGE:
BOEING B-787
DATE: 01/25/2012 79-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
79 ENGINE OIL

-21-01 Engine Oil Cooler C 2 0 (O) May be inoperative open provided fuel
Bypass Valves temperature and OAT are below the appropriate
(RR) limits before takeoff.

-21-02 Engine Oil Debris C 2 1 (M) One may be inoperative provided:

Monitoring System a) Inoperative DMS sensor is checked for
(DMS) Sensor contaminants, and
(GE) b) Associated engine oil filter bypass
warning system operates normally.

-22-01 Engine Oil Debris C 2 1 (M) One may be inoperative provided:

Sensor (ODS) a) Inoperative ODS is checked for
(RR) contaminants, and
b) Associated engine oil filter differential
pressure systems operate normally.

-31-01 Engine Oil Quantity A 2 1 (M) One may be inoperative provided:

Indicating Systems a) Before each departure, verify the
associated engine oil tank is filled to the
recommended capacity,
b) Oil consumption is within limits, and
c) Repairs are made within three flight
days.

-35-01 Engine Oil Filter

Differential Pressure
Systems (RR)

-35-01-01
***
Pressure Oil Filter C 2 0

-35-01-02
Scavenge Oil Filter C 2 1 One may be inoperative provided associated
engine oil debris sensor (ODS) operates
normally.

-35-02 Engine Oil Filter C 2 1 One may be inoperative provided the associated
Bypass Warning engine oil debris monitoring system (DMS)
Systems (GE) sensor operates normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: Original PAGE:
BOEING B-787
DATE: 09/01/2011 80-1
1. 2. NUMBER INSTALLED
SYSTEM &
ITEM
SEQUENCE 3. NUMBER REQUIRED FOR DISPATCH
NUMBERS
4. REMARKS OR EXCEPTIONS
80 STARTING

-11-01 Start Selector C 2 0 (O) May be inoperative provided alternate start

Holding/Cutout procedures are used.
Systems