FEDERAL AVIATION ADMINISTRATION

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

for

BOMBARDIER
Global Express BD-700-1A10
&
Global 5000 BD-700-1A11
Part 91 Operations only

Revision: Rev 9

This MMEL document has been developed with embedded hyper-links in the Table of Contents.
This methodology has been incorporated to save time and in keeping pace with industry changes,
will be particularly useful in the development and use of electronic media in the cockpit, such as
Electronic Flight Bags.

Dispatch relief provisos for inoperative equipment may be accessed by simply selectng the
Equipment List link, below, and then locating the respective item name from the ensuing list. The
facility to use conventional page scrolling remains unchanged.

MMEL – FRONT MATTER

SECTION ONE
LRU / COMPONENT RELIEF ITEMS

SECTION TWO
CAS MESSAGE RELIEF

(Note that while the FAA has approved the printed contents of this MMEL, it does not maintain
control of the hyper-links used herein. Control of hyper-links remains the sole responsibility of the
aircraft OEM and any errors or omissions experienced in use of these linked Table of Contents’
should be directed to the OEM for correction. )
 Back Revision: 9
⇑ To
Date: 06/27/2009
Top

DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

WASHINGTON, D.C.

MASTER MINIMUM EQUIPMENT LIST

BD-700-1A10 / 1A11

APPROVED BY :

___________________
__

GENE HARTMAN CHAIRMAN

FLIGHT OPERATIONS
EVALUATION BOARD

Federal Aviation Administration

Flight Standards Division
Aircraft Evaluation Group
3960 Paramount Blvd, Suite 100
Lakewood, CA 90712

Telephone: (562) 627-5317

FAX: (562) 627-5281
WWW.FAA.GOV/FSDO/LGBAEG

II
 DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / 1A11 DATE: 06/27/2009 III

TABLE OF CONTENTS

Back
⇑ To MMEL – FRONT MATTER
Top

Subject Page

COVER PAGE
TITLE PAGE
TABLE OF CONTENTS III THRU XIII
LOG OF REVISIONS XIV, XV,
CONTROL PAGE XVI, XVII, XVIII
HIGHLIGHTS OF CHANGE XIX THRU XXII,
DEFINITIONS XXIII THRU XXIX
PREAMBLE XXX, XXXI

Back SECTION ONE

⇑ To
Top LRU / COMPONENT RELIEF ITEMS
Subject Chapter/Page

Air Conditioning
Flow Control Valve 21-1
Recirculation Fans 21-1
Display Unit Cooling Fans 21-1
Cabin Pressurization Control 21-1
Outflow Valves 21-2
Safety Valves 21-2
Auxiliary Pressurization System 21-2
Pack Inlet Temperature Sensor (PITS) 21-3
Ram Air Valve 21-3
Pack Inlet Flow Sensor (PIFS) 21-3
Pack Flow Control Selection 21-3
Ozone Converters 21-3
Air Conditioning Packs 21-3
Pack AUTO Mode 21-4
Pack Inlet Pressure Sensor (PIPS) 21-5
Avionics Exhaust Fan 21-5
Av Rack Fan (Global 5000) 21-6
Gasper Assist Fan 21-6
Hot Air Shut Off Valves (HASOV) 21-6
Trim Air Valves (TAV) 21-7
 DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / 1A11 DATE: 06/27/2009 IV
TABLE OF CONTENTS (cont’d)

⇑ EQUIPMENT LIST (cont’d)

Subject Chapter/Page

Air Conditioning (cont’d)

Pack Discharge Temperature Indication 21-7
Cabin Temperature Control 21-7
Temperature Sensors 21-8
RECIRC “OFF” Switch light 21-9
L Pack “FAIL/OFF” Switch lights 21-9
R Pack “FAIL/OFF” Switch lights 21-9
TRIM AIR “OFF” Switch light 21-9
AUX PRESS “ON” Switch light 21-9
RAM AIR “ON” Switch light 21-9
DITCHING “ON” Switch light 21-9
OUTFLOW VLV 1 “CLOSED” Switch light 21-9
OUTFLOW VLV 2 “CLOSED” Switch light 21-9
Emer Depress “ON” Switch light 21-9
Pressurization AUTO/MAN “MAN” Switch light 21-9
Humidifier System 21-10

Autoflight
Autopilot System 22-1
A/P Quick DISC Buttons (Control Wheel) 22-1
Touch Control Steering Buttons (TCS) 22-1
Take-Off/Go-Around (TOGA) Buttons (on Thrust Levers) 22-1
Yaw Damper Systems 22-2
Autothrottle Systems 22-2
Autothrottle Engage / Disengage Switches (Thrust Lever Stem) 22-2
Autothrottle Quick Disconnect Buttons (on Thrust Lever Handles) 22-2

Communications
Integrated Comm Unit (ICU)Tray Mounted Cooling Fan 23-1
Communication Systems UHF, VHF, HF 23-1
Satellite Communication System (SATCOM) 23-1
Datalink System 23-1
Selective Call System (SELCAL) 23-2
Pre-recorded Announcement and Boarding Music System 23-2
Passenger Address System 23-2
 DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / 1A11 DATE: 06/27/2009 V
TABLE OF CONTENTS (cont’d)

⇑ EQUIPMENT LIST (cont’d)

Subject Chapter/Page

Communications (cont’d)
Alerting System (chime / light) 23-3
Crewmember Interphone System 23-4
Flight Compartment to Ground Service Interphone System 23-4
Flight Compartment Speakers 23-4
Boom Microphones 23-5
Hand Held Microphones 23-5
Headsets 23-5
Cockpit Voice Recorder (CVR) 23-5
Radio Management Units 23-5

Electrical Power
Transformer Rectifier Units (TRUs) 24-1
RAT Auto-deployment 24-1
Engine Generator Systems 24-1
GEN 1 FAIL/OFF Switch lights 24-2
GEN 2 FAIL/OFF Switch lights 24-2
GEN 3 FAIL/OFF Switch lights 24-2
GEN 4 FAIL/OFF Switch lights 24-2
APU Generator System 24-2
APU GEN FAIL/OFF Switch lights 24-2
RAT GEN FAIL/OFF Switch lights 24-2
Battery Temperature Control System 24-2
DC Power Center (DCPC) - Ground Cooling Fan (CAIMS 24-3
message)
Electrical Management System - Control Display Units (EMS 24-3
CDU)
AC External Power System 24-3
EXT AC ON Switch Light 24-3
Aft External Services Panel 24-3
EXT DC ON Switch Light 24-4
DC External Power System 24-4
 DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / 1A11 DATE: 06/27/2009 VI
TABLE OF CONTENTS (cont’d)

⇑ EQUIPMENT LIST (cont’d)

Subject Chapter/Page

Equipment / Furnishings
Pilot Seat(s) Adjustments 25-1
Chart Holders 25-1
Sun visors 25-1
Observer Seats (Including associated equipment) 25-1
Mid-Cabin Door Indication System (CABIN DOOR Caution Message) 25-2
Passenger Seat(s) 25-2
Flight Attendant Seat Assembly 25-3
Overhead Storage Bin(s)/Cabin and Galley Storage 25-3
Compartments/ Closets
Cargo Restraint Systems 25-3
Life Preservers and Survival Equipment 25-4
Emergency Locator Transmitter 25-4
First Aid Kits 25-4
Flight Attendant Flashlights / Flashlight Holder 25-4
Passenger Convenience / NEF Items 25-4
Office in the Sky 25-5
Galley waste Receptacle Access Doors / Covers 25-5
Exterior Lavatory Entry Door Ashtrays 25-5
Baggage Compartment Liners 25-5
Crew Rest Facilities - Bunk 25-6

Fire Protection
APU Fire Detection Systems 26-1
APU Fire Extinguishing System 26-1
Flight Crew Rest (FCR) Area Smoke Detection System 26-1
Baggage Compartment Smoke Detectors 26-1
Lavatory Smoke Detection System 26-2
Cabin Closet Smoke Detection Systems 26-2
Engine Fire Detection System 26-2
Portable Fire Extinguishers 26-2
Lavatory Fire Extinguishing System 26-3
 DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / 1A11 DATE: 06/27/2009 VII
TABLE OF CONTENTS (cont’d)

⇑ EQUIPMENT LIST (cont’d)

Subject Chapter/Page

Flight Controls
Aileron Control Surface Position Indications 27-1
Aileron Trim Indicator 27-1
Rudder Pedal Adjustments 27-1
Rudder Control Surface Position Indication 27-1
Elevator Surface Position Indications 27-1
STAB CH 1 “OFF” Switch Light 27-1
STAB CH 2 “OFF” Switch Light 27-1
Horizontal Stabilizer Trim Actuator (RVDT Channels) 27-2
Slat/Flap Control Unit (SFCU) 27-2
MFS Surface Proximity Switch Sensors (PSS) 27-2
Flight Control Modules (FCM) Channels 27-3
Multi-Function Spoilers (MFS) 27-3
Roll Control Input Modules (RCIM) (RVDT Channels) 27-3
Flight Spoiler Control Lever (RVDTs) 27-3
Throttle Lever RVDTs (Ground Spoiler Control) 27-4
Ground Spoilers (Inboard or Outboard) 27-4
Ground Spoilers Position Indication on EICAS 27-4

Fuel
Refuel/Defuel Adaptor Cap 28-1
Fwd AC Pumps (Boost Pumps) 28-1
APU Fuel SOV 28-1
DC Aux Pumps 28-2
Crossfeed SOV 28-2
Center Transfer Pumps 28-3
Wing Transfer SOV 28-3
Aft Tank Transfer Pumps 28-3
Aft Tank Transfer SOVs 28-4
Aft Tank Transfer System 28-4
Manifold Refuel/Defuel Control Valves 28-5
Aft Refuel / Defuel SOV 28-5
Defuel SOVs 28-5
Single Point Pressure Refuelling System 28-5
 DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / 1A11 DATE: 06/27/2009 VIII
TABLE OF CONTENTS (cont’d)

⇑ EQUIPMENT LIST (cont’d)

Subject Chapter/Page

Fuel (cont’d)
Forward Tank Refuel SOV 28-5
External Refuel/Defuel Panel 28-5
Flight Compartment Refuel/Defuel Panel 28-6
Fuel Recirculation Systems 28-6
L-R AUX PUMPS “OFF” Switch lights 28-6
L-R PRI PUMPS “OFF” Switch lights 28-6
XFEED SOV “OPEN” Switch lights 28-6
XFEED SOV “FAIL” Switch lights 28-6
Fuel Quantity Probes 28-6
EICAS Aft Fuel Tank and Total Fuel Quantity Readouts 28-7
Fuel System Indications on External Refuel/Defuel Control 28-7
Panel
Float Valve – Gravity Refuel - CTR TANK - 28-8

Hydraulic Power
Heat Exchanger Bypass Valve 29-1
HYDRAULIC Switches “AUTO” Function (ACMP) 29-1
AC Motor Pump (ACMP)(System #3) 29-1
RAT Accumulator Pressure Gauge 29-1
HYD SOV CLOSED Switch Lights 29-1
Hydraulic Firewall Shut-off Valve – EICAS Synoptic Page Indication 29-1
EICAS Hydraulic Pressure Readouts 29-1
Hydraulic Pump Low Pressure Switches 29-1
EICAS Hydraulic Reservoir Quantity Readouts(Systems 1, 2, and 3) 29-2
Hydraulic Reservoir Quantity Gauges (Systems 1, 2, and 3) 29-2

Ice and Rain Protection

Wing Anti-Ice System 30-1
Wing Anti-Ice Shut Off Valves (WAIV) 30-1
WING XBLEED Valve (CBW) 30-1
Wing Anti-Ice Temperature Sensors (WAITS) 30-1
WING XBLEED Switch 30-2
Cowl Anti-Ice System AUTO Mode (LH and RH) 30-2
 DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / 1A11 DATE: 06/27/2009 IX
TABLE OF CONTENTS (cont’d)
⇑ EQUIPMENT LIST (cont’d)

Subject Chapter/Page

Ice and Rain Protection (cont’d)

Cowl Anti-Ice Valves 30-3
Probe Heaters 30-3
Yaw Damper Heaters 30-4
Probe Heater monitor Channels (HBMU) 30-5
Enhanced Vision System - Ice Protection 30-5
Windshield and Side Window Anti-Ice Controller Channels 30-6
Ice Detection Systems 30-6

Indicating / Recording Systems

Clocks 31-1
Flight Data Recorder (FDR) 31-1
Quick Access Recorder 31-1
Pilot Event Marker 31-1
Cockpit Printer (Flight Deck) 31-1
Integrated Avionics Computer (IAC) #3 31-1
Lamp Dimmer Power Supplies (LDPS) 31-2
Display Units 31-2
Electronic Checklist System 31-2

Landing Gear
Landing Gear Retraction System 32-1
Landing Gear Selector Handle Anti-Retraction Mechanism 32-1
Nose and Main Gear Door Uplock Sensors 32-1
Brake Accumulator on Hydraulic System #2 32-1
EICAS Brake Pressure Readouts 32-2
Autobrake System 32-2
Brake Temperature Monitoring System (BTMS) 32-2
Wheel Speed Transducer Coils 32-2
Brake Accumulator Pressure Gauges 32-2
Nosewheel Steering System 32-2
 DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / 1A11 DATE: 06/27/2009 X
TABLE OF CONTENTS (cont’d)
⇑ EQUIPMENT LIST (cont’d)

Subject Chapter/Page

Lights
Cockpit/ Flight Deck/ Flight Compartment and Instrument 33-1
Lighting Systems
Cockpit Dome Light (Area Lights) 33-1
Cabin Interior Lights 33-1
Entrance Area Lighting 33-1
Stair Lighting Systems 33-1
Passenger InformationSigns “Fasten Seat Belts / No Smoking” 33-1
Nosewheel Compartment Light 33-2
Avionics Compartment Lights 33-2
APU Compartment Light 33-2
Aft Equipment Compartment Light 33-2
Aft Service Area Lights / Engine Pylon Lights 33-2
Main Gear Wheelwell Service Lights 33-2
Baggage Compartment Lights 33-2
Landing Lights 33-3
Taxi / Recognition Lights (Wing Outbd) 33-3
Wing-Tip Taxi Lights 33-3
Pulselite® Landing Lights System 33-3
Navigation Lights 33-3
Anti-Collision Strobe Lights (Wing and Tail) 33-4
Red / White Beacon Lights 33-4
Wing Inspection Lights 33-5
Logo Lights 33-5
Interior Emergency Lights 33-5
Floor Proximity Escape Path Lighting 33-5
Exterior Emergency Lights 33-5

Navigation
Air Data Computers (ADC) 34-1
Total Air Temperature Indications 34-1
Static Air Temperature Indication (SAT) 34-1
Altitude Alerting System 34-1
Standby Attitude Indicator 34-1
Non-stabilized Magnetic Compass (Standby Compass) 34-2
 DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / 1A11 DATE: 06/27/2009 XI
TABLE OF CONTENTS (cont’d)
⇑ EQUIPMENT LIST (cont’d)

Subject Chapter/Page

Navigation (cont’d)
Flight Director Systems 34-2
Electronic Standby Instrument 34-2
VHF Navigation Systems (VOR/ILS #1) 34-3
Head-up Guidance System 34-3
Enhanced Vision System (incl. Infrared Sensor Unit) 34-3
Weather Radar System 34-4
Weather Radar Controllers 34-4
Ground Proximity Warning System 34-4
Traffic Collision and Avoidance System (TCAS II) 34-5
Radio Altimeter 34-6
Inertial Reference Systems 34-6
Lasertrak NDU 34-6
IRS Mode Select Switches 34-7
Lightning Sensor Systems (LSS) 34-7
Integrated Nav Unit (INU) – Tray Mounted Cooling Fans 34-7
Marker Beacon Systems 34-7
Automatic Direction Finding System (ADF #1) 34-7
Distance Measuring Equipment Systems (DME) 34-7
ATC Transponders and Automatic Altitude Reporting Systems 34-7
Global Positioning Sensors 34-8
Flight Management Systems (FMS) 34-8
Data Loader 34-8

Oxygen
Flight Crew Oxygen Pressure 35-1
Oxygen Pressure Switch 35-1
Overboard Discharge Indicator 35-1
Crew Oxygen – Cruise Masks (incl. Mask mics) 35-1
Protective Breathing Equipment (PBE) 35-1
Passenger Oxygen System 35-2
Passenger Oxygen System – Automatic Presentation System 35-2
Passenger Service Units 35-2
Therapeutic Oxygen (First Aid) System 35-2
Portable Oxygen Dispensing Unit 35-3
 DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / 1A11 DATE: 06/27/2009 XII
TABLE OF CONTENTS (cont’d)

⇑ EQUIPMENT LIST (cont’d)

Subject Chapter/Page

Pneumatic
Bleed Pressure Transducer (BPT) 36-1
Fan Air Valve (FAV) 36-1
HP Ground Connection 36-1
Bleed Leak Detection Loops 36-1

Water & Waste

Potable Water Systems 38-1
Lavatory Waste System 38-1

Central Maintenance Systems

Central Aircraft Information/ Maintenance System (CAIMS) 45-1
Portable Maintenance Access Terminal (PMAT) 45-1

Information Systems
Electronic Flight Bags 46-1

Airborne Auxiliary Power

Auxiliary Power Unit (APU) 49-1
APU Air Intake Door linear actuator 49-1
APU Load Control Valve (LCV) 49-1
APU Subsystems 49-1
APU Oil Quantity Indication System 49-2

Doors
Passenger Door Power Assist System 52-1
Passenger Door - Folding Step Actuator 52-1
Passenger Door Indication System 52-1
Aft Equipment Bay Door Indication System 52-1
Overwing Emergency Exits Indication System 52-2
Baggage Compartment Door Indication System 52-2
Refuel/Defuel Door Indication System 52-2
Aft Hydraulic Door Indication System 52-2
 DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / 1A11 DATE: 06/27/2009 XIII
TABLE OF CONTENTS (cont’d)

⇑ EQUIPMENT LIST (cont’d)

Subject Chapter/Page

Engine Fuel & Control

Engine FADEC Faults 73-1
Engine Electronic Controller – (EPR Control Modes) 73-1
EICAS Fuel Flow Readouts 73-1
EICAS Fuel Used Readouts 73-1
Engine Fuel Temp Indications (on the FUEL Synoptic Page) 73-1

Ignition
Ignition Systems 74-1
Ignition “ON” Switch light 74-1

Engine Indicating
Engine Vibration Indication 77-1

Exhaust
Thrust Reverser Systems 78-1

Oil
Remote Oil Fill System 79-1
Engine Oil Quantity Indication System 79-1
Impending Oil Filter Bypass Indication 79-1

Starting
Starter Air Valve (SAV) 80-1
 FDEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION: 9 PAGE NO:
BD-700-1A10 / 1A11 DATE: 06/27/2009 XIV

⇑ Back LOG OF REVISIONS

Rev No. Date Page Numbers Initials

Original 08/17/98
1 11/02/2000 HIGHLIGHTS OF REV. DEFINITIONS
1 11/02/2000 21-1,21-2,21-3,21-4,22-1
1 11/02/2000 22-2,23-1,23-2,23-3,23-4
1 11/02/2000 23-5,24-1,24-2,25-1,25-2
1 11/02/2000 25-3,25-4,25-5,25-6,25-7
1 11/02/2000 25-8,25-9,26-1,26-2,26-3
1 11/02/2000 26-4,26-5,27-1,27-2,27-3
1 11/02/2000 27-4,28-1,28-2,28-3,28-4
1 11/02/2000 28-5,28-6,28-7,28-8,28-9
1 11/02/2000 28-10,28-11,29-1,29-2,30-1
1 11/02/2000 30-2,30-3,30-4,30-5,31-1
1 11/02/2000 31-2,32-1,32-2,32-3,33-1
1 11/02/2000 33-2,33-3,34-1,34-2,34-3
1 11/02/2000 34-4,34-5,34-6,34-7,35-1
1 11/02/2000 35-2,35-3,36-1,38-1,38-2
1 11/02/2000 45-1,49-1,49-2,52-1,52-2
1 11/02/2000 73-1,74-1,77-1,78-1,79-1
1 11/02/2000 80-1
2 06/04/2001 HIGHLIGHTS OF REV. DEFINITIONS
2 06/04/2001 25-2,25-3,25-4,25-5,25-6
2 06/04/2001 25-7,25-8,25-9,26-1,26-2
2 06/04/2001 27-2,27-3,27-4,30-2,32-1
2 06/04/2001 32-2,32-3,34-5,52-1,52-2
3 03/05/2002 HIGHLIGHTS OF REV. DEFINITIONS
3 03/05/2002 21-1,21-2,21-3,21-4,21-5
3 03/05/2002 21-6,21-7,21-8,21-9,21-10
3 03/05/2002 21-11,21-12,21-13,21-14,21-15
3 03/05/2002 21-16,21-17,22-1,22-2,22-3
3 03/05/2002 23-1,23-2,23-3,23-4,23-5
3 03/05/2002 23-6,23-7,24-1,24-2,24-3
3 03/05/2002 24-4,24-5,24-6,25-1,25-2
3 03/05/2002 25-3,25-4,25-5,25-6,25-7
3 03/05/2002 25-8,25-9,25-10,26-1,26-2
3 03/05/2002 26-3,26-4,26-5,27-1,27-2
3 03/05/2002 27-3,27-4,27-5,28-1,28-2
3 03/05/2002 28-3,28-4,28-5,28-6,28-7
3 03/05/2002 28-8,28-9,28-10,28-11,28-12
3 03/05/2002 28-13,28-14,29-1,29-2,30-1
3 03/05/2002 30-2,30-3,30-4,30-5,30-6
3 03/05/2002 30-7,30-8,32-1,32-2,32-3
3 03/05/2002 33-1, 33-2, 33-3, 33-4, 33-5
3 03/05/2002 33-6,34-1,34-2,34-3,34-4
3 03/05/2002 34-5,34-6,34-7,35-1,35-2
3 03/05/2002 35-3,35-4,36-1,36-2,38-1
FDEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION: 9 PAGE NO:
BD-700-1A10 / 1A11 DATE: 06/27/2009 XV
LOG OF REVISIONS (cont’d)
Rev No. Date Page Numbers Initials

3 03/05/2002 38-2,39-1,39-2,39-3,39-4
3 03/05/2002 39-5,39-6,39-7,39-8,39-9
3 03/05/2002 39-10,49-1,49-2,49-3,49-4
3 03/05/2002 52-1,52-2,52-3,52-4,73-1
3 03/05/2002 73-2,79-1
4 03/12/2002 HIGHLIGHTS OF REV., DEFINITIONS
4 03/12/2002 34-1,34-2,34-3,34-4,34-5
4 03/12/2002 34-6,34-7,34-8,34-9,34-10
4 03/12/2002 39-1,39-2,39-3,39-4,39-5
4 03/12/2002 39-6,39-7,39-8,39-9,39-10
5 10/18/2004 ALL PAGES REVISED
6 06/12/2006 29-1,34-3,34-4,34-5,34-11
6a 06/21/2006 HIGHLIGHTS OF CHG.
6a 06/21/2006 30-6,30-7,30-8,34-4
7 07/18/2007 21-1 THRU 21-9
7 07/18/2007 22-1, 22-2
7 07/18/2007 23-1 THRU 23-5
7 07/18/2007 24-1 THRU 24-4
7 07/18/2007 25-1 THRU 25-6
7 07/18/2007 26-1 THRU 26-3
7 07/18/2007 27-1 THRU 27-4
7 07/18/2007 28-1 THRU 28-7
7 07/18/2007 29-1, 29-2
7 07/18/2007 30-1 THRU 30-6
7 07/18/2007 31-1, 31-2
7 07/18/2007 32-1, 32-2
7 07/18/2007 33-1 THRU 33-5
7 07/18/2007 34-1 THRU 34-8
7 07/18/2007 35-1 THRU 35-3
7 07/18/2007 36-1
7 07/18/2007 38-1
7 07/18/2007 45-1
7 07/18/2007 49-1, 49-2
7 07/18/2007 52-1, 52-2
7 07/18/2007 73-1
7 07/18/2007 74-1
7 07/18/2007 77-1
7 07/18/2007 78-1
7 07/18/2007 79-1
7 07/18/2007 80-1
8 02/26/2008 HIGHLIGHTS OF REV., DEFINITIONS
8 02/26/2008 24-2
9 All Pages excepting DEFINITIONS and PREAMBLE
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / -1A11 DATE: 06/27/2009 XVI
CONTROL PAGE
System Page No. Rev. No. Current Date
⇑ Back CONTROL PAGE
System Page No. Rev. No. Current Date
COVER PAGE
TITLE PAGE 9 06/27/2009
TABLE OF CONTENTS III 9 06/27/2009
IV 9 06/27/2009
V 9 06/27/2009
VI 9 06/27/2009
VII 9 06/27/2009
VIII 9 06/27/2009
IX 9 06/27/2009
X 9 06/27/2009
XI 9 06/27/2009
XII 9 06/27/2009
XII 9 06/27/2009
LOG OF REVISIONS XIV 9 06/27/2009
XV 9 06/27/2009
CONTROL PAGE XVI 9 06/27/2009
XVII 9 06/27/2009
XVIII 9 06/27/2009
HIGHLIGHTS OF CHANGE XIX 9 06/27/2009
XX 9 06/27/2009
XXI 9 06/27/2009
XXII 9 06/27/2009
DEFINITIONS XXIII 14 08/26/2008
XXIV 14 08/26/2008
XXV 14 08/26/2008
XXVI 14 08/26/2008
XXVII 14 08/26/2008
XXVIII 14 08/26/2008
XXXIX 14 08/26/2008
PREAMBLE XXX 2 07/05/1990
XXXI 2 07/05/1990
Section One divider XXXII 9 06/27/2009
21 21-1 9 06/27/2009
21-2 9 06/27/2009
21-3 9 06/27/2009
21-4 9 06/27/2009
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / -1A11 DATE: 06/27/2009 XVII
CONTROL PAGE
System Page No. Rev. No. Current Date

21-5 9 06/27/2009
21-6 9 06/27/2009
21-7 9 06/27/2009
21-8 9 06/27/2009
21-9 9 06/27/2009
21-10 9 06/27/2009
22 22-1 9 06/27/2009
22-2 9 06/27/2009
23 23-1 9 06/27/2009
23-2 9 06/27/2009
23-3 9 06/27/2009
23-4 9 06/27/2009
23-5 9 06/27/2009
24 24-1 9 06/27/2009
24-2 9 06/27/2009
24-3 9 06/27/2009
24-4 9 06/27/2009
25 25-1 9 06/27/2009
25-2 9 06/27/2009
25-3 9 06/27/2009
25-4 9 06/27/2009
25-5 9 06/27/2009
25-6 9 06/27/2009
26 26-1 9 06/27/2009
26-2 9 06/27/2009
26-3 9 06/27/2009
27 27-1 9 06/27/2009
27-2 9 06/27/2009
27-3 9 06/27/2009
27-4 9 06/27/2009
28 28-1 9 06/27/2009
28-2 9 06/27/2009
28-3 9 06/27/2009
28-4 9 06/27/2009
28-5 9 06/27/2009
28-6 9 06/27/2009
28-7 9 06/27/2009
28-8 9 06/27/2009
29 29-1 9 06/27/2009
29-2 9 06/27/2009
30 30-1 9 06/27/2009
30-2 9 06/27/2009
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / -1A11 DATE: 06/27/2009 XVIII
CONTROL PAGE
System Page No. Rev. No. Current Date

30-3 9 06/27/2009
30-4 9 06/27/2009
30-5 9 06/27/2009
30-6 9 06/27/2009
31 31-1 9 06/27/2009
31-2 9 06/27/2009
32 32-1 9 06/27/2009
32-2 9 06/27/2009
33 33-1 9 06/27/2009
33-2 9 06/27/2009
33-3 9 06/27/2009
33-4 9 06/27/2009
33-5 9 06/27/2009
34 34-1 9 06/27/2009
34-2 9 06/27/2009
34-3 9 06/27/2009
34-4 9 06/27/2009
34-5 9 06/27/2009
34-6 9 06/27/2009
34-7 9 06/27/2009
34-8 9 06/27/2009
35 35-1 9 06/27/2009
35-2 9 06/27/2009
35-3 9 06/27/2009
36 36-1 9 06/27/2009
38 38-1 9 06/27/2009
45 45-1 9 06/27/2009
46 46-1 9 06/27/2009
49 49-1 9 06/27/2009
49-2 9 06/27/2009
52 52-1 9 06/27/2009
52-2 9 06/27/2009
73 73-1 9 06/27/2009
74 74-1 9 06/27/2009
77 77-1 9 06/27/2009
78 78-1 9 06/27/2009
79 79-1 9 06/27/2009
80 80-1 9 06/27/2009
Section Two divider 9 06/27/2009
Section Two Introduction INT-1 9 06/27/2009
Section 2 – Table Of Contents TOC-1, -2, -3 9 06/27/2009
CAS Messages 2-1 Thru 2-46 9 06/27/2009
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / -1A11 DATE: 06/27/2009 XIX
HIGHLIGHTS OF CHANGE (cont’d)

⇑ Back HIGHLIGHTS OF CHANGE

Effective the above date, the Bombardier BD-700-1A1O / -1A11 (Global Express) Master
Minimum Equipment List (MMEL) is revised. Revision 9 is a Standard revision.

Primarily, Revision 9 has re-instated Section 2, MMEL relief for CAS messages, following revision
and re-instatement of FAA Policy Letter PL 119. Rev 9 also removes references to respective
AFM Supplements from the provisos. Instead, these have been incorporated into the respective
(O) Procedures.

Also, Revision 9 is the first to incorporate document hyper-links in order to faciliatate moving
through the document. The Table Of Contents has been re-created to provide a line-item
description of each MMEL item herein, and each item provided a hyper-link directly to its
location. Return links back to the Table Of Contents are also provided on each page. As
hyper-links have been inserted throughout the document as a broad clerical change, all pages
have been re-dated to this revision. However, change bars have not been designated for this
purpose, continuing their main purpose for use in highlighting the technical changes.

Technical Changes
MMEL Seq. No. Item:

21-30-02 Outflow Valves – Provisos amended

21-52-01 1) Pack AUTO Mode – Identified as sub – item
21-52-02 Pack Inlet Pressure Sensor (PIPS) – (O) Procedure added
21-60-06 Pack Discharge Temperature Indication . – Note added.
21-71-01 Humidifier System - Modified proviso.
24-30-01 ELEC SYS FAULT Advisory message - Moved to Section 2.
27-61-02 Flight Control Modules (FCM) Channels -
Clerical change to AFM Supplement title
27-62-01 Multi-Function Spoilers (MFS) –
Clerical change to AFM Supplement title
27-63-01 Ground Spoilers (Inboard or Outboard) –
Clerical change to AFM Supplement title
27-63-02 Ground Spoilers Position Indication on EICAS –
Clerical change to AFM Supplement title
28-21-05 DC Aux Pumps - Added proviso to deactivate. Added relief for GL5000.
28-22-02 Wing Transfer SOV - Modify proviso
28-23-06 External Refuel/Defuel Panel - New item
28-23-07 Flight Compartment Refuel/Defuel Panel - New item
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / -1A11 DATE: 06/27/2009 XX
HIGHLIGHTS OF CHANGE (cont’d)

Technical Changes (cont’d)

30-11-02 Wing Anti-Ice Shut Off Valves (WAIV) - C/2/1 case deleted. C/2/0
amended
30-11-04 Wing Anti-Ice Temperature Sensors (WAITS) - Provisos amended.
30-30-01 1) Probe Heaters – Relief restricted for system one and standby P/S probes
30-30-01 3) Probe Heaters – Base Heater relief deleted. Redundant to P/S heaters.
30-41-01 Windshield and Side Window Anti-Ice Controller Channels -
(O) Procedure requirements added
31-31-03 Pilot Event Marker - New Item
32-30-01 Landing Gear Retraction System – Modified provisos
33-43-02 Red / White Beacon Lights- Provided W&T Strobes operative
34-14-01 Altitude Alerting System - Modified relief proviso
34-23-01 Flight Director Systems - Add relief for Flight Director Modes
35-21-01 1) Passenger Oxygen System; Test / Reset switch – Added note for
effectivity
36-12-01 1) Bleed Leak Detection Loops – Wing Anti-Ice - Sub-item 1) clarify: One or Both
46 -10-01 Electronic Flight Bags - New Item
49-14-01 APU Air Intake Door linear actuator – Added provisos for partially OPEN.
73-32-01 2) Engine Fuel Temp Indications (on the FUEL Synoptic Page) –
Caution message relief deleted.

Addition of Section Two

The following list summarizes the CAS Messages now provided MMEL relief, pursuant
to the re-instatement of FAA Policy Letter number 119, at Rev 2. The list of messages
are those that had been previously accepted in Rev 7 of this MMEL, and a number of
new CAS Message reliefs accepted through the last Global Express FOEB.

Dispatch relief for the following messages can be viewed in Section 2 of this MMEL.

(cont’d)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / -1A11 DATE: 06/27/2009 XXI
HIGHLIGHTS OF CHANGE (cont’d)

New and re-instated CAS Messages MMEL relief:

CAS MESSAGE CAS MESSAGE

A/T 1 FAIL EVS FAIL
A/T 2 FAIL EVS HEAT FAIL
ADC 2 DEGRADED EVS HEAT OVHT
ADC 3 DEGRADED FDR ACCEL FAIL
ADC 2 FAIL FDR FAIL
ADC 3 FAIL FLAP HALFSPD
AFCS 1 FAIL FMS 2 FAIL
AFCS 2 FAIL FMS 3 FAIL
AP 1 FAIL FUEL TEMP SENSOR
AP 2 FAIL GEAR SYS FAIL
AP PITCH TRIM FAIL GEAR SYS FAULT
APU BLEED SYS FAIL GND PROX FAIL
APU DOOR FAIL GPWS SYSTEMS FAIL
APU FADEC FAIL HUD FAIL
APU FAULT HUD FAN FAIL
APU FIRE FAIL HUD MISALIGN
APU FIRE FAULT HUMIDIFIER FAIL
APU FUEL SOV HYD PUMP 3A FAIL
APU GEN FAIL HYD PUMP 3B FAIL
APU NOT AVAILABLE IAC 3 INVALID
APU OIL HI TEMP IAC 3 OVHT
APU OIL LO PRESS ICE
APU OIL LO QTY ICE DETECTOR FAIL
APU SHUTDOWN ICE DETECTOR FAULT
APU SQUIB 1 FAIL INT CABIN DOOR
APU SQUIB 2 FAIL IRS 1 AUX FAIL
ASCB CTLR 1 FAIL IRS 1 AUX PWR
ASCB CTLR 2 FAIL IRS 1 FAIL
ASCB CTLR 3 FAIL IRS 1 MISCMP
AUTOBRAKE FAIL IRS 1 OVHT
AVIONIC FAN FAIL (GX ONLY) IRS 2 AUX FAIL
CHECK DU 4 IRS 2 AUX PWR
CHECKLIST MISMATCH IRS 2 FAIL
CPLT BRAKE FAULT IRS 2 MISCMP
CTR FUELXFER FAIL IRS 2 OVHT
CTR XFER FAULT IRS 3 AUX FAIL
ELEC SYS FAULT IRS 3 AUX PWR
EVS DEFOG FAULT IRS 3 FAIL
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO. 9 PAGE NO.
BD-700-1A10 / -1A11 DATE: 06/27/2009 XXII
HIGHLIGHTS OF CHANGE (cont’d)

New and re-instated CAS Messages MMEL relief: (cont’d)

IRS 3 MISCMP RECIRC FAN FAIL
IRS 3 OVHT SAFETY VALVE OPEN
L AUX FUEL PUMP SG 3 FAIL
L BLEED FAULT SLAT HALFSPD
L ENG FIRE FAULT SLAT-FLAP BIT
L FADEC FAULT SMALL SERV DOORS
L PACK AUTO FAIL SMOKE AFT LAV FAIL
L PACK FAIL SMOKE AV RACK FAIL
L PACK FAULT SMOKE BAGGAGE FAIL
L PRI FUEL PUMP SMOKE CLOSET AFT FAIL
L PROBE MON FAIL SMOKE CLOSET FWD FAIL
L WING A/ICE FAIL SMOKE FWD LAV FAIL
L WSHLD HEAT FAIL SPLRS/STAB BIT
LARGE SERV DOORS TAT 2 FAIL
LTRK FAIL TAT 3 FAIL
MAN PRESS FAULT TAT HT 1 FAIL
MLG BAY OVHT FAIL TAT HT 2 FAIL
MLG BAY OVHT FAULT TAT HT 3 FAIL
OUTFLOW VLV 1 FAIL TERR FAIL
OUTFLOW VLV 2 FAIL TRIM AIR FAIL
OXYGEN LO QTY TRIM AIR FAULT
PITOT 2 HT FAIL TRIM AIR LEAK
PITOT 3 HT FAIL TRU 1 FAIL
PLT BRAKE FAULT TRU 2 FAIL
R AUX FUEL PUMP WINDSHEAR FAIL
R BLEED FAULT WING A/ICE FAULT
R ENG FIRE FAULT WING A/ICE LEAK
R FADEC FAULT WING A/ICE LO HEAT
R PACK AUTO FAIL WING A/ICE SENSOR
R PACK FAIL WOW FAULT
R PACK FAULT YD 1 FAIL
R PRI FUEL PUMP YD 2 FAIL
R PROBE MON FAIL YD HEAT 1 FAIL
R WINDOW HEAT FAIL YD HEAT 2 FAIL
R WING A/ICE FAIL
R WSHLD HEAT FAIL
 U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION: 14 PAGE:
BD-700-1A10 / 1A11 DATE: 08/26/2008 XXIII

⇑ Back DEFINITIONS

1. System Definitions.
System numbers are based on the Air Transport Association (ATA) Specification and items
are numbered sequentially.
a. "Item" (Column 1) means the equipment, system, component, or function
listed in the "Item" column. Repair interval categories (A, B, C, and D) are listed on
right side of column 1. Repair intervals are described in definition 22.

b. "Number Installed" (Column 2) is the number (quantity) of items normally

installed in the aircraft. This number represents the aircraft configuration considered
in developing this MMEL. Should the number be a variable (e.g., passenger cabin
items) a number is not required.

c. "Number Required for Dispatch" (Column 3) is the minimum number (quantity)

of items required for operation provided the conditions specified in Column 4 are met.

NOTE: Where the MMEL shows a variable number required for dispatch, the MEL
must reflect the actual number required for dispatch or an alternate means of
configuration control approved by the Administrator.

d. "Remarks or Exceptions" (Column 4) in this column includes a statement

either prohibiting or permitting operation with a specific number of items inoperative,
provisos (conditions and limitations) for such operation, and appropriate notes.

e. A vertical bar (change bar) in the margin indicates a change, addition or

deletion in the adjacent text for the current revision of that page only. The change
bar is dropped at the next revision of that page.

2. "Airplane/Rotorcraft Flight Manual" (AFM/RFM) is the document required for type

certification and approved by the responsible FAA Aircraft Certification Office. The FAA
approved AFM/RFM for the specific aircraft is listed on the applicable Type Certificate Data
Sheet.

3. "As required by FAR" means that the listed item is subject to certain provisions
(restrictive or permissive) expressed in the Federal Aviation Regulations operating rules.
The number of items required by the FAR must be operative. When the listed item is not
required by FAR it may be inoperative for time specified by repair category. The term “14
CFR” may be substituted for “FAR” in MMELs or operator MELs.

4. Each inoperative item must be placarded to inform and remind the crewmembers and
maintenance personnel of the equipment condition.

NOTE: To the extent practical, placards should be located adjacent to the control or
indicator for the item affected; however, unless otherwise specified, placard wording and
location will be determined by the operator.

5. "-" symbol in Column 2 and/or Column 3 indicates a variable number (quantity) of the
item installed.
U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION: 14 PAGE:
BD-700-1A10 / 1A11 DATE: 08/26/2008 XXIV
DEFINITIONS (cont’d)

6. "Deleted" in the remarks column after a sequence item indicates that the item was
previously listed but is now required to be operative if installed in the aircraft.

7. As used in MMELs, "ER" refers to Extended Operations (ETOPS) of an airplane

with operational approval to conduct ETOPS in accordance with the applicable
regulations.

8. "Federal Aviation Regulations" (FAR) means the applicable portions of the Federal
Aviation Act and Federal Aviation Regulations.

9. "Flight Day" means a 24 hour period (from midnight to midnight) either Universal
Coordinated Time (UCT) or local time, as established by the operator, during which at least
one flight is initiated for the affected aircraft.

10. "Icing Conditions" means an atmospheric environment that may cause ice to form on the
aircraft (structural) or in the engine(s) (induction).

11. Alphabetical symbol in Column 4 indicates a proviso (condition or limitation) that must be
complied with for operation with the listed item inoperative.

12. "Inoperative" means a system and/or component malfunction to the extent that it does
not accomplish its intended purpose and/or is not consistently functioning normally within its
approved operating limit(s) or tolerance(s).

13. "Notes:" in Column 4 provides additional information for crewmember or maintenance

consideration. Notes are used to identify applicable material which is intended to assist with
compliance, but do not relieve the operator of the responsibility for compliance with all
applicable requirements. Notes are not a part of the provisos.

14. Inoperative components of an inoperative system: Inoperative items which are

components of a system which is inoperative are usually considered components directly
associated with and having no other function than to support that system. (Warning/caution
systems associated with the inoperative system must be operative unless relief is specifically
authorized per the MMEL).

15. "(M)" symbol indicates a requirement for a specific maintenance procedure which must
be accomplished prior to operation with the listed item inoperative. Normally these
procedures are accomplished by maintenance personnel; however, other personnel may be
qualified and authorized to perform certain functions. Procedures requiring specialized
knowledge or skill, or requiring the use of tools or test equipment should be accomplished by
maintenance personnel. The satisfactory accomplishment of all maintenance procedures,
regardless of who performs them, is the responsibility of the operator. Appropriate
procedures are required to be published as part of the operator's manual or MEL.

16. "(O)" symbol indicates a requirement for a specific operations procedure, which must be
accomplished in planning for and/or operating with the listed item inoperative. Normally these
procedures are accomplished by the flight crew; however, other personnel may be
U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION: 14 PAGE:
BD-700-1A10 / 1A11 DATE: 08/26/2008 XXV
DEFINITIONS (cont’d)

qualified and authorized to perform certain functions. The satisfactory accomplishment of

all procedures, regardless of who performs them, is the responsibility of the operator.
Appropriate procedures are required to be published as a part of the operator's manual or
MEL.
NOTE: The (M) and (O) symbols are required in the operator's MEL unless
otherwise authorized by the Administrator.

17. "Deactivated" and "Secured" means that the specified component must be put into an
acceptable condition for safe flight. An acceptable method of securing or deactivating will
be established by the operator.

18. "Visual Flight Rules" (VFR) is as defined in FAR Part 91. This precludes a pilot from
filing an Instrument Flight Rules (IFR) flight plan.

19. "Visual Meteorological Conditions" (VMC) means the atmospheric environment is such
that would allow a flight to proceed under the visual flight rules applicable to the flight. This
does not preclude operating under Instrument Flight Rules.

20. "Visible Moisture" means an atmospheric environment containing water in any form
that can be seen in natural or artificial light; for example, clouds, fog, rain, sleet, hail, or
snow.

21. "Passenger Convenience Items" means those items related to passenger

convenience, comfort or entertainment such as, but not limited to, galley equipment, movie
equipment, ash trays, stereo equipment, overhead reading lamps, etc.

22. Repair Intervals: All users of an MEL approved under FAR 121, 125, 129 and 135
must effect repairs of inoperative systems or components, deferred in accordance with the
MEL, at or prior to the repair times established by the following letter designators:

Category A. Items in this category shall be repaired within the time interval
specified in the remarks column of the operator's approved MEL. For time intervals
specified in "flight days," the day the malfunction was recorded in the aircraft
maintenance record/logbook is excluded. For all other time intervals (flights, flight
legs, cycles, hours, etc), repair tracking begins at the point when the malfunction is
deferred in accordance with the operator's approved MEL.

Category B. Items in this category shall be repaired within three (3) consecutive
calendar days (72 hours), excluding the day the malfunction was recorded in the
aircraft maintenance record/logbook. For example, if it were recorded at 10 a.m. on
January 26th, the three day interval would begin at midnight the 26th and end at
midnight the 29th.

Category C. Items in this category shall be repaired within ten (10) consecutive
calendar days (240 hours), excluding the day the malfunction was recorded in the
aircraft maintenance record/logbook. For example, if it were recorded at 10 a.m. on
January 26th, the 10 day interval would begin at midnight the 26th and end at
midnight February 5th.
U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION: 14 PAGE:
BD-700-1A10 / 1A11 DATE: 08/26/2008 XXVI
DEFINITIONS (cont’d)

Category D. Items in this category shall be repaired within one hundred and twenty
(120) consecutive calendar days (2880 hours), excluding the day the malfunction

was recorded in the aircraft maintenance log and/or record. The letter designators
are inserted adjacent to Column 2.

An operator who has the authorization to use an MEL also has the authority to
approve extensions to the maximum repair interval for category B and C items
provided the responsible Flight Standards District Office (FSDO) is notified within 24
hours of the MEL extension. The operator is not authorized to extend A and D items
in the MEL. Misuse of the MEL extension authority may result in the operators
OpSpecs/Mspecs being amended by removing the authority for the operator to use
the MEL extension authority and/or use an MEL.

23. Electronic fault alerting system – General New generation aircraft display system fault
indications to the flight crew by use of computerized display systems. Each aircraft
manufacturer has incorporated individual design philosophies in determining the data that
would be represented.

The following are customized definitions (specific to each manufacturer) to help determine
the level of messages affecting the aircraft's dispatch status. When preparing the MEL
document, operators are to select the proper Definition No. 23 for their aircraft, if
appropriate.

a. BOEING (747-400, 757, 767, 777, 787)

Boeing airplanes equipped with Engine Indicating and Crew Alerting Systems (EICAS),
provide different priority levels of system messages (WARNING, CAUTION, ADVISORY,
STATUS and MAINTENANCE). Any messages that affects airplane dispatch status will be
displayed at a STATUS message level or higher. The absence of an EICAS STATUS or
higher level (WARNING, CAUTION, ADVISORY) indicates that the system/component is
operating within its approved operating limits or tolerances. System conditions that result
only in a maintenance level
message, i.e. no correlation with a higher level EICAS message, do not affect dispatch and
do not require action other than as addressed within an operators standard maintenance
program.

b. BOEING (B-717, MD-10, MD-11)

These aircraft are equipped with an alerting function which is a subsystem within the
Electronic Instrument System (EIS). The alerting function provides various levels of system
condition alerts (WARNING, CAUTION, ADVISORY, MAINTENANCE and STATUS). Alerts
that affect aircraft dispatch will include WARNING, CAUTION, STATUS or MAINTENANCE
level. MAINTENANCE alerts are displayed on the status page of the EIS display panel
under the maintenance heading.
A MAINTENANCE alert on the EIS indicates the presence of a system fault which can be
identified by the Central Fault Display System (CFDS) interrogation. The systems are
designed to be fault tolerant, however, for any MAINTENANCE alert, the MEL must be
verified for dispatch purposes.
U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION: 14 PAGE:
BD-700-1A10 / 1A11 DATE: 08/26/2008 XXVII
DEFINITIONS (cont’d)

‘c. AIRBUS (A-300-600, A-310, A-318/319/320/321, A-330, A-340)

Airbus aircraft equipped with Electronic Centralized Aircraft Monitoring (ECAM) provide
different levels of system condition messages (WARNING, CAUTION, STATUS, and
ADVISORY). A-318/319/320/321, A-330, and A-340 also provide MAINTENANCE status
messages. Any message that effects airplane dispatchability will normally be at the
WARNING, CAUTION or STATUS level. MAINTENANCE messages (A-318/319/320/321,
A-330, and A-340 only) are also indicated on ECAM Status Page below the white
Maintenance label. A MAINTENANCE status (Class II) message on ECAM indicates the
presence of a system fault which can be identified by CFDS (A-318/319/320/321) or CMS
(A-330/A-340) interrogation. The systems are designed to be fault tolerant. For A-
318/319/320/321, MAINTNENACE status (Class II) do not affect dispatch but are listed in
the MMEL. Dispatch is allowed without specific conditions except for:
- BLUE RSVR MAINTENANCE status: If applicable, and
- AIR BLEED MAINTENANCE status: As applicable.
For the A-330 and A-340, MAINTENANCE status messages do not affect dispatch.

d. FOKKER (FK-100)
Fokker aircraft are equipped with Multi Function Display System (MFDS) which provides
electronic message referring to the different priority levels of system information (WARNING
(red), CAUTION (amber), AWARENESS (cyan) AND STATUS (white). Any
messages that affects aircraft dispatch will be at the WARNING, CAUTION or AWARENESS
level. In these cases the MEL must be verified for dispatch capability and maintenance may
be required. System conditions that only require maintenance are not presented on the
flight deck. These maintenance indications/messages may be presented on the
Maintenance & Test Panel (MAP) or the Centralized Fault Display Unit (CFDU) and by
dedicated Built In Test Evaluation (BITE) of systems.

e. CANADAIR (CL-65, CL-604)

Canadair aircraft equipped with Engine Indication and Crew Alerting Systems (EICAS)
provide four classes of messages (WARNING, CAUTION, ADVISORY, and STATUS). Any
message that affects aircraft dispatch will be at the WARNING, CAUTION, or STATUS level.
System conditions that only require maintenance are not visible to the flight crew. These
maintenance indications/messages are only activated by maintenance personnel using the
Maintenance Diagnostics Computer.

f. EMBRAER (EMB-135/145, ERJ-170/190 Series)

The EMB-135/145 and ERJ-170/190 are equipped with an Engine Indicating and Crew
Alerting System (EICAS) that provides three different message levels: WARNING,
CAUTION, and ADVISORY. The ERJ-170/190 Series add STATUS messages. Failures
that effect dispatchability are presented to the flight crew at one of these levels. Other
failures may be presented only to the maintenance personnel on the Multi Function Display
(MFD) maintenance pages or through the download of the Central Maintenance Computer
(CMC). System conditions that result only in a maintenance level message, i.e. no
correlation with a higher level EICAS message, do not affect dispatch and do not require
action other than as addressed within an operator's standard maintenance program.
U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION: 14 PAGE:
BD-700-1A10 / 1A11 DATE: 08/26/2008 XXVIII
DEFINITIONS (cont’d)

g. GULFSTREAM (G-IV, G-V, GV-SP, and GIV-X G-150 and G-200)

Gulfstream airplanes equipped with EICAS provide different priority levels of system
messages: WARNING (red), CAUTION (amber), ADVISORY, STATUS and MAINTENANCE
(cyan or blue). Any WARNING or CAUTION message affects airplane dispatch status and
requires that the Airplane Flight Manual or the MEL be used to determine dispatch capability.
STATUS messages which indicate a system failure (e.g., FMS 1 fail) require that the Airplane
Flight Manual or the MEL be used to determine dispatch capability. MAINTENANCE
messages do not affect airplane dispatch status. They indicate the presence of a system fault
which can be identified by Maintenance Data Acquisition Unit (MDAU on the G-V)
interrogation, Central Maintenance Computer (CMC on the GV-SP/GIV-X) interrogation or by
reference to the Airplane Flight Manual.

Gulfstream mid-cabin airplanes (G-150, G-200) equipped with EICAS provide different
priority levels of system messages: WARNING (red), CAUTION (amber), ADVISORY
(green), and STATUS (white). The Airplane Flight Manual prohibits take off with any
WARNING message displayed. CAUTION, ADVISORY and STATUS messages may
affect airplane dispatch status and requires the Airplane Flight Manual or the MEL be
used to determine dispatch capability. The airplane may dispatch with CAUTION,
ADVISORY and STATUS messages that indicate proper system operation and are not
illuminated due to a system failure (i.e. FUEL STBY PUMP ON when the pump is
selected ON, GND A/B OUT with LAND selected on the ground, or APU GEN OFF with
the switch OFF). MAINTENANCE and MAINTENANCE DATA STATUS messages do not
affect airplane dispatch status. They indicate the presence of a system fault which can
be retrieved from the Maintenance Diagnostics Computer. In all cases, the Airplane
Flight Manual must be referenced and procedures compiled with for the displayed
message prior to applying MEL dispatch relief.

h. De-HAVILLAND (DASH 8 SERIES 400)

Series 400 aircraft are equipped with a Caution/Warning Panel that annunciates all cautions
and warnings. Advisory messages are displayed by the Electronic Indication System (EIS) or
individual advisory lights supplied in the cockpit. "Class 1 failures" are failures that prevent
continued operation of a specific Line Replacement Unit or channel and are annunciated via
advisory messages: caution, warning or advisory lights in the flight compartment. Dispatch
with such posted failures are to be in accordance with the MMEL. "Class 2 failures" are
failures which do not prevent continued system function. These faults will not be annunciated
to the flight crew and the absence of the higher level alert (warning, caution, advisory)
indicates that the system/component is operating within its approved operating limits or
tolerances. Such faults would be evident during maintenance interrogation performed during
maintenance activities. Class 2 faults do not affect dispatch
and will be listed in the Fault Isolation Manual (FIM). Class 2 faults will be left to the discretion
of the operators when these faults are to be rectified.

24. "Administrative control item" means an item listed by the operator in the MEL for tracking
and informational purposes. It may be added to an operator's MEL by approval of the
Principal Operations Inspector provided no relief is granted, or provided conditions and
limitations are contained in an approved document (i.e. Structural Repair Manual,
airworthiness directive, etc.). If relief other than that granted by an approved document is
sought for an administrative control item, a request must be submitted to the Administrator.
U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION: 14 PAGE:
BD-700-1A10 / 1A11 DATE: 08/26/2008 XXIX
DEFINITIONS (cont’d)

If the request results in review and approval by the FOEB, the item becomes an MMEL item
rather than an administrative control item.

25. "***" symbol in Column 1 indicates an item which is not required by regulation but which
may have been installed on some models of aircraft covered by this MMEL. This item may
be included on the operator's MEL after the approving office has determined that the item has
been installed on one or more of the operator's aircraft. The symbol, however, shall not be
carried forward into the operator's MEL. It should be noted that neither this policy nor the use
of this symbol provide authority to install or remove an item from an aircraft.

26. "Excess Items" means those items that have been installed that are redundant to the
requirements of the FARs.

27. "Day of Discovery" is the calendar day an equipment/instrument malfunction was recorded
in the aircraft maintenance log and or record. This day is excluded from the calendar days or
flight days specified in the MMEL for the repair of an inoperative item of equipment. This
provision is applicable to all MMEL items, i.e., categories "A, B, C, and D."

28. “Considered Inoperative”, as used in the provisos means that item must be treated for
dispatch, taxi and flight purposes as though it were inoperative. The item shall not be used or
operated until the original deferred item is repaired. Additional actions include: documenting
the item on the dispatch release (if applicable), placarding, and complying with all remarks,
exceptions, and related MMEL provisions, including any (M) and (O) procedures and
observing the repair category.

29. “ Is not used” in the provisos, remarks or exceptions for an MMEL item may specify that
another item relieved in the MMEL “is not used.” In such cases, crewmembers should not
activate, actuate, or otherwise utilize that component or system under normal operations. It is
not necessary for the operators to accomplish the (M) procedures associated with the item.
However, operational requirements must be complied with, and an additional placard must be
affixed, to the extent practical, adjacent to the control or indicator for the item that is not used
to inform crewmembers that a component or system is not to be used under normal
operations.

30. Nonessential equipment and furnishings (NEF) are those items installed on the aircraft
as part of the original type certification, supplemental type certificate, or or other form of
alteration that have no effect on the safe operation of flight and would not be required by
the applicable certification rules or operational rules. They are those items that if
inoperative, damaged or missing have no effect on the aircraft’s ability to be operated
safely under all operational conditions. These nonessential items may be installed in areas
including, but not limited to, the passenger compartment, flight deck area, service areas,
cargo areas, crew rest areas, lavatories, and galley areas. NEF items are not items
already identified in the MEL or CDL of the applicable aircraft. They do not include items
that are functionally required to meet the certification rule or for compliance with any
operational rule. Operator’s NEF process shall not provide for deferral of items within
serviceable limits identified in the manufacture’s maintenance manual or operator’s
approved maintenance program such as wear limits, fuel/hydraulic leak rates, oil
consumption, etc. Cosmetic items that are fully serviceable but worn or soiled may be
deferred under an operator’s NEF process.
 U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION: 1 PAGE NO:
BD-700-1A10 / 1A11 DATE: 07/05/1990 XXX

⇑ Back PREAMBLE
(07/05/1990)

This preamble is applicable to, and will be included in, master minimum equipment lists
(MMEL) issued under the provisions of Section 91.30(a) ¢NEW Section 91.213(a)(2)|.
It is not applicable to MMELs issued under the provisions of Parts 121, 125, 129, and
135 of the FAR.
Except as provided in Section 91.30(d) ¢NEW Section 91.213(d)|, or under the
provisions of an approved MMEL, all equipment installed on an aircraft in compliance
with the airworthiness standards or operating rules must be operative. Experience has
shown that with the various levels of redundancy designed into aircraft, operation of
every system or component installed may not be necessary when the remaining
equipment can provide an acceptable level of safety.
An MMEL is developed by the FAA,, with participation by the aviation industry, to
improve aircraft utilization and thereby provide more convenient and economic air
transportation for the public. The FAA-approved MMEL includes only those items of
equipment, which the Administrator finds may be inoperative and yet maintain an
acceptable level of safety by appropriate conditions and limitations. The MMEL and
FAA-issued letter of authorization are used as an MEL by an operator and permit
operation of the aircraft with inoperative equipment.
The MMEL includes all items of installed equipment that are permitted to be
inoperative. Equipment required by the FAR, and optional equipment in excess of FAR
requirements, is included with appropriate conditions and limitations. For each listed
item, the installed equipment configuration considered to be normal for the aircraft is
specified. Items of equipment installed on aircraft (except for passenger convenience
items such as galley equipment and passenger entertainment devices), such as
"TCAS," windshear detection devices, and ground proximity warning systems (GPWS)
that are in excess of what is required, and are not listed on the MMEL, must be
operational for dispatch unless MMEL relief is sought through the FSDO having
jurisdiction for the operator. If MMEL relief is sought, the operator must notify the
FSDO who will make a request of the FOEB to convene and consider adding the
equipment to the MMEL. The operator may then dispatch with the equipment disabled,
or rendered inoperative, in accordance with all FAR. It is incumbent on the operator to
endeavor to determine if O and/or M procedures for that equipment must be developed.
If so, any procedures developed must comply with all FAR. Procedures developed to
use the MMEL must not conflict with either the aircraft flight manual limitations,
emergency procedures, or with airworthiness directives (AD), all of which take
precedence over the MMEL and those procedures.
Suitable conditions and limitations in the form of placards, maintenance procedures,
crew operating procedures, and other restrictions, as necessary, are required to be
accomplished by the operator to ensure that an acceptable level of safety is
maintained. Those procedures should be developed from guidance provided in the
manufacturer's aircraft flight and/or maintenance manuals, manufacturer's
recommendations, engineering specifications, and other appropriate sources.
Procedures must not be contrary to any FAR. Wherever the statement "as required by
FAR" appears in the MMEL, the operator must either list the specific FAR by part and
section and carry the FAR on board the aircraft or specify the requirements and/or
limitations to conduct the flight in accordance with the appropriate FAR.
U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION: 1 PAGE NO:
BD-700-1A10 / 1A11 DATE: 07/05/1990 XXXI
PREAMBLE
(07/05/1990)

The MMEL is intended to permit operations with inoperative items of equipment for the
minimum period of time necessary until repairs can be accomplished. It is important
that repairs be accomplished at the earliest opportunity in order to return the aircraft to
its design level of safety and reliability. Inoperative equipment in all cases must be
repaired, or inspected and deferred, by qualified maintenance personnel at the next
required inspection ¢Section 91.165(c), NEW Section 91.405(c)|. The repair intervals
indicated by the Letters A, B, and C inserted adjacent to column 2 are NOT applicable
to this MMEL.

The MMEL provides for release of the aircraft for flight with inoperative equipment.
When an item of equipment is discovered to be inoperative, it is reported by making an
entry in the aircraft maintenance records. The item is then either repaired or deferred
per the MMEL or other approved means acceptable to the Administrator prior to further
operation. In addition to the specific MMEL conditions and limitations, determination by
the operator that the aircraft is in condition for safe operations under anticipated flight
conditions must be made for all items of inoperative equipment. When these
requirements are met, the aircraft may be considered airworthy and returned to service.
Operators are responsible for exercising the necessary operational control to ensure
that an acceptable level of safety is maintained. When operating with multiple
inoperative items, the interrelationship between those items, and the effect on
operation and crew workload, must be considered. Operators are expected to establish
a controlled and sound repair program, including the parts, personnel, facilities,
procedures, and schedules to ensure timely repair.

WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE
PREAMBLE, DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED
IN THE MEL IS REQUIRED
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD-700-1A10 / 1A11 DATE: 06/27/2009 XXXII

⇑ Back
To
Top

SECTION ONE

LRU /
COMPONENT
ORIENTED
MMEL RELIEF
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD-700-1A10 / -1A11 DATE: 06/27/2009 21-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
20-01 Flow Control Valve
⇑ (FCV) C 2 1 (O)(M) One may be inoperative provided:
a) Affected valve is secured CLOSED,
b) Affected air conditioning pack is selected
OFF and considered inoperative,
c) Opposite air conditioning pack is operative,
d) AUX PRESS system is operative.

21-01 Recirculation Fans C 2 1 (M) One may be inoperative.

⇑ C 2 0 (M) Both may be inoperative provided both air

conditioning packs operate normally.

23-01 Display Unit Cooling C 12 6 (M) One per Display Unit may be inoperative
Fans provided the avionics fan is operative.
⇑

30-01 Cabin Pressurization

⇑ Control
1) AUTO Pressurization
Channels C 2 1 (M) One may be inoperative provided:
a) MAN control channels are verified
operative,
b) Safety valves are verified operative, and
c) Cabin RATE Indicator, Cabin ALT
Indicator, and Cabin DIFF Pressure
⇑ Indicator are verified operative.

C 2 0 (O)(M) Both may be inoperative provided:

a) MAN control channels are verified
operative,
b) Safety valves are verified operative,
c) Cabin RATE Indicator, Cabin ALT
Indicator, and Cabin DIFF Pressure
Indicator are verified operative, and
d) Flight is conducted at or below FL250.

2) MAN Pressurization C 2 1 (M) One MANUAL channel may be inoperative

Channels provided:
a) Both automatic cabin pressurization
⇑ control channels are operative, and
b) Both Outflow valves are verified
operative.
(cont’d)
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD-700-1A10 / -1A11 DATE: 06/27/2009 21-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING

A 2 0 (O) Both MANUAL channels may be inoperative

for one flight day, provided the flight is
conducted in accordance with AFM for
unpressurized flight configuration at or below
9,000 ft MSL.

30-02 Outflow Valves C 2 1 (O)(M) One may be inoperative OPEN provided: I

⇑ a) Affected outflow valve is verified open, I
b) AFM Buoyancy Limitations are I
observed with respect to take-offs and I
landings near bodies of water, and I
c) Flight is conducted in accordance with I
AFM for an unpressurized flight I
configuration at or below 9,000 ft MSL. I
I
31-01 Safety Valves C 2 0 (O) One or both may be inoperative OPEN
⇑ provided:
a) Both air conditioning packs operate
normally,
b) Operations are conducted unpressurized
at or below 9,000 ft MSL,
c) Take-offs and landings are not
conducted on runways near bodies of
water, and
d) Extended over-water operations are
prohibited.
31-02 Auxiliary C 1 0 May be inoperative provided both air
⇑ Pressurization conditioning packs are operative.
System

51-01 Pack Inlet C 2 0 One or both may be inoperative

⇑ Temperature Sensor
(PITS)

51-02 Ram Air Valve C 1 0 (M) Mmay be inoperative secured CLOSED

⇑

C 1 0 (O) May be inoperative OPEN provided:

a) RH air conditioning pack is selected
OFF and considered inoperative,
b) LH air conditioning pack is operative,
and
c) Pack NORM and MAN control modes
are operative.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD-700-1A10 / -1A11 DATE: 06/27/2009 21-3
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING

51-03 Pack Inlet Flow C 2 1 (M) One may be inoperative provided MANUAL
⇑ Sensor mode of both air conditioning packs is verified
(PIFS) operative.

C 2 0 (O)(M) Both may be inoperative provided:

a) One pack is selected OFF and
considered inoperative,
b) MANUAL mode of air conditioning is
selected for the remaining pack and
verified operative.

51-04 Pack Flow Control

⇑ Selection

1) HIGH C 1 0 May be inoperative failed in HIGH position.

2) LO, NORM C 1 0 LO or NORM positions may be inoperative

provided both packs are operative in the
HIGH position.

51-05 Ozone Converters C 2 0 Flights are conducted at FL 250 or below.

⇑

52-01 Air Conditioning C 2 1 (O)(M) One may be inoperative provided:

⇑ Packs a) The remaining pack is operated in
(GX) AUTO mode,
b) Affected air conditioning pack is
selected OFF,
c) Avionics fan is selected OFF,
d) Recirculation system is verified
operative,
e) AUX PRESS system is verified
operative, and
f) TRIM AIR is selected OFF, and
g) Operations are conducted at or below
FL 410.

Note: If dispatching with right pack operative,

ensure that RAM Air Valve is not failed in
OPEN position.

(cont’d)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD-700-1A10 / -1A11 DATE: 06/27/2009 21-4
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
Air Conditioning C 2 1 (O)(M) One may be inoperative provided:
Packs a) The remaining pack is operated in
⇑
(Global 5000) AUTO mode,
b) Affected air conditioning pack is
selected OFF,
c) Avionics fan is selected OFF,
d) Recirculation system is verified
operative,
e) AUX PRESS system is verified
operative,
f) TRIM AIR is selected OFF,
g) Operations are conducted at or below FL
410, and
h) Av Rack Fan is verified operative.

Note: If dispatching with right pack operative,

ensure that RAM Air Valve is not failed in
OPEN position.

1) Pack AUTO Mode C 2 1 (O)(M) One may be inoperative provided: I

(GX) a) MANUAL mode on the unaffected pack
⇑ is verified operative, I
b) Unaffected pack is operated in AUTO I
mode, I
c) Affected air conditioning pack is selected I
OFF,
d) Avionics Fan is selected OFF,
e) Recirculation system is verified operative,
f) AUX PRESS system is verified operative,
g) TRIM AIR is selected OFF, and
h) Operations are conducted at or below
FL410.
I
Note: If dispatching with right pack
operative, ensure that RAM Air
Valve is not failed OPEN.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD-700-1A10 / -1A11 DATE: 06/27/2009 21-5
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING

Pack AUTO Mode C 2 1 (O)(M) One may be inoperative provided: I

(Global 5000) a) MANUAL mode on unaffected pack is
verified operative, I
⇑ b) Unaffected pack is operated in AUTO I
mode, I
c) Affected air conditioning pack is selected
OFF,
d) Avionics Fan is selected OFF,
e) Recirculation system is verified operative,
f) AUX PRESS system is verified operative,
g) TRIM AIR is selected OFF,
h) Operations are conducted at or below
FL410, and
i) Av Rack fan is verified operative. I

Note: If dispatching with right pack

operative, ensure that RAM Air
Valve is not failed OPEN.

52-02 Pack Inlet Pressure C 2 0 (O) One or both may be inoperative provided I
⇑ Sensor (PIPS) MANUAL mode of both air conditioning packs
is verified operative.

53-01 Avionics Exhaust Fan C 1 0 May be inoperative provided one or both air
⇑ (GX) conditioning packs are operated during
ground operation.

NOTES:
Minimize utilization of equipment in the
avionics bay without air conditioning and
fans during engine start and shutdown.

If only one air conditioning pack is

operating, passenger door opening should
be minimized.

(cont’d)
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD-700-1A10 / -1A11 DATE: 06/27/2009 21-6
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
(Global 5000) C 1 0 (M) May be inoperative provided:
⇑ a) Air conditioning is operated during
ground operations, and
b) AV Rack Fan is confirmed operative.

NOTES:
Minimize utilization of equipment in the
avionics bay without air conditioning and
fans during engine start and shutdown.

If only one air conditioning pack is

operating, passenger door opening should
be minimized.

53-02 Av Rack Fan C 1 0 (M) May be inoperative provided:

(Global 5000) a) Air conditioning is operated during
ground operations, and
⇑
b) Avionics exhaust fan is confirmed
operative.

NOTES:
Minimize utilization of avionics equipment
without air conditioning and during engine
start and shutdown.

If only one air conditioning pack is

operating, passenger door opening
should be minimized.

53-03 Gasper Assist Fan D 1 0

***
⇑ (relief is limited to
installation defined by
Bombardier Modsum
MS 700T01756)

60-04 Hot Air Shut Off C 2 1 (M) One may be inoperative CLOSED provided
⇑ Valves (HASOV) the affected HASOV is secured CLOSED.

C 2 1 One may be inoperative OPEN provided:

a) The Trim Air Valves are operative, and
b) Both air conditioning packs are
operative.

(cont’d)
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD-700-1A10 / -1A11 DATE: 06/27/2009 21-7
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
C 2 0 (M) Both may be inoperative CLOSED provided:
a) Both HASOVs are secured CLOSED,
b) Trim Air system is selected to OFF,
c) Both air conditioning packs are
operative, and
d) AUX PRESS is selected OFF and is
considered inoperative.

60-05 Trim Air Valves C 3 0 (M) All may be inoperative CLOSED provided:
⇑ (TAV) a) Trim Air Switch is selected OFF,
b) Both air conditioning packs are
operative,
c) Both HASOVs are secured CLOSED,
and
d) AUX PRESS is selected OFF and
considered inoperative.

60-06 Pack Discharge C 2 0 (M) One or both may be inoperative provided:

⇑ Temperature a) Both associated automatic temperature
Indication controls are operative, and
b) Pack Control selection switch is set to
either LO, NORM, or HIGH.

NOTE: I
Associated with loss of PDT indications, I
pack MANUAL mode will be inoperative. I

61-01 Cabin Temperature

⇑ Control
1) AUTO mode
(NORM) C 1 0 (O)(M) AUTO Mode of temperature control may be
inoperative provided:
a) One pack is selected OFF and
considered inoperative,
b) MANUAL temp control is verified
operative, and
c) Operations are conducted at or below
FL350.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD-700-1A10 / -1A11 DATE: 06/27/2009 21-8
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING

2) MANUAL mode
(MAN) C 1 0 MAN Mode of temperature control may be
inoperative provided:
⇑ a) AUTO mode is operative, and
b) Both packs are operative.

(O) a) AUTO mode is operative,

b) One pack is selected OFF and
considered inoperative.

3) Temperature
Selectors – C 3 0 Any or all may be inoperative.
Cockpit,
⇑ FWD Cabin,
AFT Cabin

61-02 Temperature Sensors

⇑
1) Ventilated
Temperature
Sensors (VENTS)
- Sensors elements C 6 3 One element from each sensor may be
inoperative.

C 6 4 (M) Both elements of any one VENTS sensor

may be inoperative provided all duct
temperature indications are operative.

2) Duct Temperature
Sensors (DTS)
⇑ - Sensors elements C 6 3 (M) One element from each sensor may be
inoperative.

C 6 0 (M) Both elements of any or all DTS sensors may

be inoperative provided:
(a) Both HASOVs are secured CLOSED,
(b) TRIM air system is selected OFF,
(c) Both air conditioning packs are
operative, and
(d) AUX PRESS is selected OFF and is
considered inoperative.

3) Mix Manifold
Temperature Sensor
⇑ (MMTS)
- Sensors elements C 4 1 Three may be inoperative.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD-700-1A10 / -1A11 DATE: 06/27/2009 21-9
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING

62-01 RECIRC “OFF” C 1 0

⇑ Switch light
(Light function only)

62-02 L Pack “FAIL/OFF” C 2 0

⇑ Switch lights
(Light function only)

62-03 R Pack “FAIL/OFF” C 2 0

⇑ Switch lights
(Light function only)
62-04 TRIM AIR “OFF” C 1 0
⇑ Switch light
(light function only)

62-05 AUX PRESS “ON” C 1 0

Switch light
⇑
(light function only)

62-06 RAM AIR “ON” C 1 0

Switch light
⇑
(light function only)

62-07 DITCHING “ON” C 1 0

Switch light
⇑
(light function only)

62-08 OUTFLOW VLV 1 C 1 0

⇑ “CLOSED”
Switch light
(light function only)

62-09 OUTFLOW VLV 2 C 1 0

⇑ “CLOSED”
Switch light
(light function only)

62-10 Emer Depress C 1 0

⇑ “ON” Switch light
(light function only)

62-11 Pressurization C 1 0
⇑ AUTO/MAN
“MAN” Switch light
(light function only
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD-700-1A10 / -1A11 DATE: 06/27/2009 21-10
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING

71-01 Humidifier System D 1 0 (O) Aircraft may be dispatched provided I

*** a) System is deactivated, I
⇑ (relief limited to b) Neither L PACK FAIL or R PACK FAIL I
installation defined by Caution messages are also I
Bombardier Modsum annunciated, I
MS C700-09025, c) TRIM AIR switch is selected and I
S/B 700-21-001 or remains OFF, I
S/B 700-21-020) d) HASOVs are indicated closed on I
Synoptic Page, and I
e) Extended periods of aircraft in-operation I
or ground handling during freezing I
temperatures must be avoided to I
prevent system damage due to possible I
freezing of water trapped in the system. I
I
NOTE: Potential freezing is not of concern I
provided ECS is operating. I
NOTE: Overnight parking in hangar should I
be considered where freezing I
temperatures are forecast. I
I
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD-700-1A10 / -1A11 DATE: 06/27/2009 22-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTOFLIGHT

10-01 Autopilot System C 2 1 One may be inoperative provided approach

⇑ procedures are not dependent on its use.

C 2 0 Both may be inoperative provided:

a) Approach procedures are not
dependent on its use, and
b) Intended flights do not exceed two
hours.

11-01 A/P Quick DISC

⇑ Buttons
(Control Wheel)
1) Autopilot Disconnect
Function C 2 1 (O) One may be inoperative failed CLOSED
provided:
a) Associated stall protection system
pusher disconnect function is
operative;
b) Pilot flying has the operative A/P Quick
Disc button.
c) Autopilot is not used below 1500 feet
AGL, and
d) Approach minimums do not require the
use of autopilot.

2) Pitch Trim Disconnect

Function C 2 1 (O) One may be inoperative failed CLOSED
⇑ provided:
a) Associated Stall Protection System
pusher disconnect function is
operative, and
b) Pilot flying has the operative A/P
Quick Disc button.

11-02 Touch Control C 2 0

⇑ Steering Buttons
(TCS)

11-03 Take-Off/Go-Around C 2 1 One may be inoperative provided:

⇑ (TOGA) Buttons a) Approach procedures do not require
(on Thrust Levers) its use, and
b) Pilot flying has the operative switch.

(cont’d)
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD-700-1A10 / -1A11 DATE: 06/27/2009 22-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTOFLIGHT

Take-Off/Go-Around
(TOGA) Buttons C 2 0 Both may be inoperative provided:
⇑
(cont’d) a) Both thrust levers are operated manually
for take-off and go-around, and
b) Autopilot and flight director are not
used at less than 1500 feet AGL.

13-01 Yaw Damper Systems C 2 1 (O) One may be inoperative provided airplane is
⇑ operated at or below
FL 390.

30-01 Autothrottle Systems C 2 1

⇑
C 2 0 May be inoperative provided autothrottle is
confirmed disengaged.

30-02 Autothrottle Engage / C 2 0 (M) Both may be inoperative provided autothrottle

⇑ Disengage Switches system is rendered inoperative.
(on Thrust Lever
Stem)

30-03 Autothrottle Quick C 2 0 (M) One or both may be inoperative provided the
⇑ Disconnect Buttons autothrottle system is rendered inoperative.
(on Thrust Lever
Handles)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 23-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATION

10-01 Integrated Comm C - 1 (M) May be inoperative provided a minimum of

⇑ Unit (ICU) one fan is verified to operate normally.
Tray Mounted
Cooling Fan

11-01 Communication
⇑ Systems
1) VHF, UHF D - - Any in excess of those required by
regulations may be inoperative provided it is
not powered by the AC Essential Bus, DC
Emergency Bus, Battery Bus, Battery Direct
Buss, or the DC Essential Bus and not
required for emergency procedures.
2) HF D - 1 (O) One may be inoperative while conducting
operations that require two Long Range
Communication Systems provided:
⇑ a) SATCOM voice or Datalink system
operates normally,
b) Alternate procedures are established
and used.
c) SATCOM communication operates
normally over the intended route of
flight, and
d) If Inmarsat codes are not available while
using SATCOM voice, prior coordination
with the appropriate ATS facility is
required.

NOTE: SATCOM is to be used only as a

backup to normal HF
communications unless otherwise
authorized by the appropriate ATS
facilities.

13-01 Satellite D - 0
*** Communication
⇑ System (SATCOM)

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

*** procedures are established and used.
⇑
D 1 0 May be inoperative provided routine
procedures do not require its use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 23-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATION

22-01 Selective Call System C 1 0 (O) May be inoperative provided alternate

*** (SELCAL) procedures are established and used.
⇑
D 1 0 May be inoperative provided procedures do
not require its use.

1) Channels C 5 0 (O) May be inoperative provided alternate

procedures are established and used.
⇑

D 5 0 May be inoperative provided procedures do

not require its use.

32-01 Pre-recorded C 1 0 (O) May be inoperative provided alternate

*** Announcement and procedures are established and used.
⇑ Boarding Music
System

40-01 Passenger Address

⇑ System
1) Passenger B 1 0 (O) May be inoperative provided:
Configuration a) Alternate procedures are established
and used,
b) Flight deck / cabin interphone (two way)
with associated calls (e.g. chimes) is
operative, and
c) Required safety briefings are given to
passengers using a means that will
ensure the briefings are audible to each
passenger.

⇑ a) Lavatory Speaker C - 0 (O) May be inoperative provided alternate

procedures are established and used.

2) Non - Passenger A 1 0 (O) May be inoperative for non-passenger

Configuration carrying operations for one flight day,
provided:
⇑ a) Crewmembers are the only occupants of
the aircraft, and
b) Alternate procedures are established
and used.

(cont’d)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 23-3
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATION

3) All Cargo D 1 0 May be inoperative provided all crewmembers

Configuration are on flight deck.
⇑
4) Crew Rest Facility - C - 0 (O) May be inoperative provided:
Bunk a) Flight deck and Cabin/Crew Rest Facility
- bunk interphone (two-way) with
associated calls (e.g. Chimes) is
operative,
b) Crew rest facility - bunk drop down
oxygen system is operative,
c) Alternate procedures are established
and used, and
d) The Pilot-In-Command is advised that all
crew have been briefed.

⇑ D - 0 (O)(M) May be inoperative provided:

a) Associated Crew Rest Facility – bunk is
not occupied, and
b) Associated Crew Rest Facility – bunk is
placarded INOPERATIVE – DO NOT
USE.

40-02 Alerting System

⇑ (chime / light)
1) Flight Deck Call Light B 1 0 May be inoperative provided the flight deck
chime is operative.
NOTE: The flight deck chime must always
be operative.
2) Flight Attendant / B - 0 May be inoperative provided:
Cabin Call Light a) PA system operates normally, and
⇑ b) Affected chime is not used for lavatory
smoke detector alerting, and
c) Alternate procedures are established
and used.

NOTE: Passenger to attendant call System

is considered a convenience item.

3) Flight Attendant / B - 0 May be inoperative provided:

Cabin Chime a) PA system is operates normally,
⇑ b) Affected Chime is not used for lavatory
smoke detector alerting, and
c) Alternate procedures contacting flight
attendants are established and used.
(cont’d)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 23-4
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATION

NOTE: Passenger to attendant call system

is considered a passenger
convenience item.
40-03 Crewmember B - 1 (O) Any in excess of the requirement may be
⇑ Interphone inoperative provided alternative
System (Flight communications procedures between the
Compartment/ Cabin, affected flight attendant station(s) are
Cabin/ Flight established and used.
Compartment)
NOTE: Any station that operates normally
may be used.
A 1 0 (O) May be inoperative for non-passenger
carrying operations for one flight day
provided:
a) Crewmembers are the only occupants of
the aircraft, and
b) Alternate procedures are established
and used.

41-01 Flight Compartment to C 1 0 (O) May be inoperative provided alternate

Ground Service procedures are established and used.
⇑ Interphone System
(Nose and Avionic bay)

51-01 Flight Compartment C 2 0 Both may be inoperative provided:

⇑ Speakers a) Procedures are not dependent on their
use, and
b) Headsets are installed and used by
each person on flight deck duty.

51-02 Boom Microphones A - 0 May be inoperative provided:

⇑ a) Flight Data Recorder (FDR) operates
normally, and
b) Repairs are made within three flight days.

51-03 Hand Held C 2 1 One may be inoperative provided

*** Microphones associated boom microphone is operative.
⇑
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 23-5
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATION

51-04 Headsets D - - Any in excess of those required for each

⇑ person on flight compartment duty may be
inoperative.

71-01 Cockpit Voice A 1 0 May be inoperative provided repairs are

⇑ Recorder (CVR) made in accordance with applicable FARs.

81-01 Radio Management B 2 1 (O) One may be inoperative provided:

⇑ Units a) Cross-side tuning is verified operative,
and
b) Two FMSs are operative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 24-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
24 ELECTRICAL

20-01 Transformer Rectifier C 4 3 (M) One may be inoperative provided:

⇑ Units (TRUs) a) Affected unit is not ESS TRU 1 or ESS
TRU 2,
b) All indications for the remaining TRUs
operate normally, and
c) The affected unit is deactivated.

1) TRU Fan C 4 3 (M) One fan may be failed provided:

(amber TRU box icon) a) All other associated parameters are
⇑ normal,
b) The reason for the amber indication is
verified to be TRU fan failure, and
c) All four TRUs are powering the busses.

2) TRU Volts (V) C 4 3 One TRU VOLTS indication may be

Indication inoperative provided the affected TRU Load
⇑ (A) indication is operative.

3) TRU Load (A) C 4 3 One TRU Load indication may be inoperative

Indication provided the affected TRU volts (V)
⇑ indications is operative.

20-02 RAT Auto-deployment B 1 0 (M) May be inoperative provided the RAT manual
⇑ deployment is verified operative.

21-01 Engine Generator C 4 3 One may be inoperative provided:

⇑ Systems a) Associated Generator switch is
selected to OFF, and
b) APU Generator is operative.

B 4 2 One generator per engine may be inoperative

provided:
a) Associated Generator switches are
⇑ selected to OFF,
b) APU generator is operated
continuously throughout the flight

NOTE: Limitations surrounding APU

operations must be observed
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 24-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
24 ELECTRICAL

21-02 GEN 1 FAIL/OFF C 2 0

⇑ Switch lights
(light function only)

21-03 GEN 2 FAIL/OFF C 2 0

⇑ Switch lights
(light function only)

21-04 GEN 3 FAIL/OFF C 2 0

⇑ Switch lights
(light function only)

21-05 GEN 4 FAIL/OFF C 2 0

⇑ Switch lights
(light function only)

22-01 APU Generator C 1 0 May be inoperative.

⇑ System
NOTE: APU can be used as a pneumatic
source.
22-02 APU GEN C 2 0
⇑ FAIL/OFF
Switch lights
(light function only)

22-03 RAT GEN C 2 0

⇑ FAIL/OFF
Switch lights
(light function only)

30-01 (moved to Section 2) I

⇑

31-01 Battery Temperature

⇑ Control System
1) EICAS Indications
a) AV BATT °C B 1 0 (M) May be inoperative provided the AV BATT
caution and AV BATT CHGR advisory
messages are verified operative.

b) APU BATT °C B 1 0 (M) May be inoperative provided the APU BATT

caution and APU BATT CHGR advisory
messages are verified operative.

(cont’d)
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 24-3
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
24 ELECTRICAL

2) Battery Heaters D 2 0 May be inoperative provided the associated

(relief applicable only battery charger operates normally.
⇑ to Pre-mod
BA SB 700-24-056)

31-02 DC Power Center

⇑ (DCPC) -
Ground Cooling Fan C 1 0 (O) May be inoperative.
(CAIMS message)
NOTE:
Ground operations above 30 deg C
should be limited to 30 minutes if the
Environmental Control System is not
running.
31-03 Electrical Management
⇑ System -
Control Display Units
(EMS CDU)

1) DIM / BRT Control C 2 1 Dimming may be inoperative on one provided

display intensity is adequate.

2) EMS Maint Mode D 2 0 (M) Both may be inoperative provided alternate

maintenance procedures are established and
used.

41-01 AC External C 1 0
⇑ Power System
41-02 EXT AC ON C 1 0
⇑ Switch Light
(light function only)
41-03 Aft External Services
Panel
1) All panel functions
and indications
(excepting
⇑ APU SHUT-OFF) C - 0 (M) One or all may be inoperative provided
alternate procedures are established and
used.
D - 0 May be inoperative provided routine
procedures do not require its use.
(cont’d)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 24-4
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
24 ELECTRICAL

2) APU SHUT-OFF C 1 0 (M) May be inoperative provided the APU is

(Emergency) Switch monitored from the cockpit during operation.
⇑
D 1 0 May be inoperative provided the APU is not
used for ground maintenance

42-01 EXT DC ON C 1 0
Switch Light
⇑ (light function only)

42-02 DC External Power C 1 0

System
⇑
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 25-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 FURNISHINGS

10-01 Pilot Seat(s) C 2 0 (M) Vertical adjustments may be inoperative

⇑ Adjustments provided the seat is secured in a position,
which meets individual pilot requirements.
10-02 Chart Holders C 2 0 One or both may be inoperative

10-03 Sun visors C 2 0 Except where required for Head-Up

⇑ Guidance System viewing, one or both may
be inoperative

11-01 Observer Seats A - - May be inoperative provided:

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

OR
A - - c) The secondary observer's seat is
available to the FAA inspector for
performance of official duties, and
d) Repairs are made within two flight days.
OR
⇑ A - - e) The primary observer's seat is available
with the required minimum safety
equipment (safety belt and oxygen) and
acceptable to the FAA Inspector for the
performance of official duties, and
f) Repairs are made within two flight days.

NOTES:
1. These provisos are intended to provide
for occupancy of the above seats by an
FAA inspector when the minimum safety
equipment (oxygen and safety belt) is
functional and the inspector determines
the conditions to be acceptable.
2. The pilot-in-command will determine if
the minimum safety equipment is
functional for other persons authorized
to occupy any observer seat(s).
3. Associated equipment includes shoulder
harness, lap belt, Audio Control Unit,
RT/IC Switches, and Observer's oxygen
system.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 25-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 FURNISHINGS

20-01 Mid-Cabin Door C 1 0 (O) May be inoperative provided that prior to

*** Indication System each take-off and landing, the door is verified
⇑ (CABIN DOOR open.
Caution Message)

21-01 Passenger Seat(s) 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 aircraft aisle,
and
c) The affected seat(s) are blocked and
placarded "DO NOT OCCUPY".
NOTES:
1. A seat with an inoperative seat belt is
considered inoperative.
2. Inoperative seats do not affect the
required number of Flight Attendants.
3. Affected seat(s) may include the
seat(s) behind and/or adjacent
outboard seat(s).

1) Recline Mechanism D - - (M) May be inoperative provided the seat is

secured in the up-right position.
⇑

2) Underseat Baggage D - - (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.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 25-3
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 FURNISHINGS

22-01 Flight Attendant Seat A 1 0 (M)(O) Flight attendant seat may be inoperative
⇑ Assembly provided:
a) Affected seat or seat assembly is not
occupied,
b) Flight attendant displaced by inoperative
seat occupies the passenger seat most
accessible to the inoperative seat,
c) Alternate procedures are established
and used as published in crew member
manuals,
d) Folding type seat is stowed or secured
in the retracted position,
e) Passenger seat assigned to flight
attendant is placarded "FOR FLIGHT
ATTENDANT ONLY", and
f) Repairs are made within two flight days
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 automatically is
considered inoperative.
NOTE 3: The above provisos apply to flight
attendant seats. Individual operators,
when operating with inoperative seats, will
consider the locations and combinations of
seats to ensure the proximity to exits and
distribution requirements of the applicable
FAR are met.

30-01 Overhead Storage C - - (M) May be inoperative provided:

⇑ Bin(s)/Cabin and a) Procedures are established to secure
Galley Storage compartment CLOSED,
Compartments/ b) Compartment is not used for storage of
Closets emergency equipment, and
c) Affected compartment is not used for
storage of any item(s) except for those
permanently affixed.

50-01 Cargo Restraint C - - May be inoperative, or missing such that the

⇑ Systems effect is that the item must be considered
inoperative, provided cargo compartment
remains empty.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 25-4
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 FURNISHINGS

61-01 Life Preservers and D - - As required by Regulations.

*** Survival Equipment
⇑

61-02 Emergency Locator D 1 0 As required by Regulations.

⇑ Transmitter

61-03 First Aid Kits D - - Any in excess of those required by

⇑ regulations may be incomplete or missing
provided:
a) Required distribution is maintained, and
b) Procedures are established to alert
crewmembers of missing or incomplete
kits.

64-01 Flight Attendant

⇑ Flashlights / Flashlight
Holder
1) Flashlights C - 0 (O) May be inoperative or missing provided the
flight attendant assigned to the associated
seat has a flashlight of equivalent
characteristics (has a ruggedized, electrically
insulated exterior, uses two “D” size batteries,
and has a shatter-resistant lens and reflector)
readily available.

2) Holders C - 0 (M)(O) May be inoperative or missing provided

alternate stowage provisions are provided.

70-01 Passenger
⇑ Convenience / NEF
Items

1) Passenger
Convenience Items (Expired on December 31, 2007) I

2) Non-Essential
*** Equipment &
⇑ Furnishings (NEF)

(cont’d) (cont’d)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 25-5
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 FURNISHINGS

2) Non-Essential - 0 May be inoperative, damaged or missing

*** Equipment & provided that the item(s) is deferred in
⇑ Furnishings (NEF) accordance with the operator's NEF
deferral program.
The NEF program, procedures and
processes are outlined in the operator's
Manual.

(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 ashtrays

are not considered NEF items.

70-02 Office in the Sky D - 0

***
⇑
70-03 Galley waste C - - (M) May be inoperative provided the container is
Receptacle Access empty and the access is secured to prevent
⇑ Doors / Covers waste introduction into the compartment.

70-04 Exterior
⇑ Lavatory Entry Door
Ashtrays

1) Airplanes with more A - - One may be missing provided it is replaced

than one exterior within 10 calendar days
lavatory door ashtray

2) Airplanes with only A 1 0 May be missing provided it is replaced within

one exterior lavatory 3 calendar days.
door ashtray

71-01 Baggage C - - Liner panels may be missing or damaged

⇑ Compartment Liners provided baggage is not carried in the
associated compartment.
NOTE:
For ballast purposes, use of bags
(made of glass fibre or kevlar) of sand
or ingots of non-magnetic metals (such
as lead) is acceptable.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 25-6
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 FURNISHINGS

75-01 Crew Rest Facilities - D - 0 May be inoperative provided regulations do

*** Bunk not require its use.
⇑
1) Bunk Main Entry Door C 1 0 (O) May be inoperative provided:
a) Crew rest area is not used, and
b) Bunk entry door is locked closed and
placarded “INOPERATIVE DO NOT
ENTER”.
NOTE: These provisions are not intended
to prohibit crew rest Area inspections
by crewmembers.

C 1 0 (M) May be inoperative provided door is removed

and securely stowed inside the crew rest area
or removed from the aircraft.

2) Bunk Restraint C - - (O) One or more may be inoperative provided:

System a) Affected bunk is placarded
⇑ “INOPERATIVE DO NOT USE”, and
b) Procedures are established and used to
alert crewmembers that the bunk
restraint system cannot be used.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 26-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
26 FIRE PROTECTION

12-01 APU Fire Detection C 2 1 One detection loop may be inoperative,

⇑ Systems provided the fire test is performed before
each flight.

C 2 0 Both detection loops may be inoperative

provided the APU is considered inoperative.

12-02 APU Fire C 1 0 May be inoperative provided the APU is

⇑ Extinguishing System considered inoperative and is not used.

13-01
(deleted, 05/15/01)

14-01 Flight Crew C 1 0 May be inoperative provided:

*** Rest (FCR) Area a) FCR area is empty,
⇑ Smoke Detection b) FCR area door is locked and placarded,
System “INOPERATIVE - DO NOT ENTER”,
c) FCR area is not used for any purpose.

NOTE:
These provisions are not intended to
prohibit FCR inspections by
crewmembers.

15-01 Baggage C - 1 (M) One may be inoperative provided remaining

*** Compartment detector is verified operative prior to each
⇑ Smoke Detectors flight.

C - 0 (M) May be inoperative provided:

a) Cabin to baggage compartment door
remains secured OPEN, and
b) Baggage compartment remains empty.

NOTE:
Does not preclude the carriage of empty
cargo containers, pallets, ballast, etc.
Class E cargo compartments require
only the installation of smoke or fire
detection systems (not suppression).
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 26-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
26 FIRE PROTECTION

16-01 Lavatory Smoke

*** Detection System C - - (M)(O) For each lavatory, the lavatory smoke
⇑ detection system may be inoperative
provided:
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
crewmembers.
NOTES:
1. These provisos are not intended to
prohibit lavatory inspections by
crewmembers.
2. Lavatory smoke detection system is
not required for all-cargo operations.

16-02 Cabin Closet Smoke

*** Detection Systems C - - (O) May be inoperative provided:
⇑ a) Closet is empty, and
b) Cabin closet door is locked
CLOSED and placarded, “DO
NOT USE”.

21-01 Engine Fire Detection

⇑ System A 4 2 One loop per engine may be inoperative for
one flight day provided the Fire Test is
performed before each flight.

C 4 2 One loop per engine may be inoperative

provided:
a) Fire Test is performed before each
flight, and
b) Operations are conducted not more than
60 minutes from a suitable airport.

23-01 Portable Fire

⇑ Extinguishers D - - Any in excess of those required by FAR may
be inoperative or missing provided:
a) The inoperative fire extinguisher is
tagged inoperative, removed from the
installed 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 NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 26-3
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
26 FIRE PROTECTION

26-01 Lavatory Fire

*** Extinguishing System C - - For each lavatory, the fire extinguisher
⇑ system may be inoperative provided lavatory
smoke detection system operates normally.

C - - (M)(O) May be inoperative provided:

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
crewmembers.

NOTES:
1. These provisos are not intended to
prohibit lavatory inspections by
crewmembers.
2. A lavatory fire system is not required
for all-cargo operations.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 27-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS

11-01 Aileron Control C 2 0 (O) Both may be inoperative provided a visual

⇑ Surface Position check of the associated control surface
Indications movements is made prior to each flight.

12-01 Aileron Trim Indicator C 1 0 (M) May be inoperative provided, prior to each
⇑ flight:
a) Aileron trim is visually checked for full,
free and correct movement, and
b) Aileron trim is confirmed neutral.

20-01 Rudder Pedal C 2 0 (M) May be inoperative provided:

⇑ Adjustments a) The rudder pedal adjustment
mechanism is not free to
move, and
b) The mechanism has failed such that
the rudder pedals are in a position
which meets individual pilot
requirements.

21-01 Rudder Control C 1 0 (O) May be inoperative provided a visual check

⇑ Surface Position of the associated control surface
Indication movements is made prior to each flight.

31-01 Elevator Surface C 2 0 (O) Both may be inoperative provided:

⇑ Position Indications a) Visual inspection of affected control
surface for correct operation is made
before each departure, and
b) Aircraft speed is limited to 250 KIAS
throughout the flight.

41-01 STAB CH 1 “OFF” C 1 0

⇑ Switch Light
(Light function only)

41-02 STAB CH 2 “OFF” C 1 0

⇑ Switch Light
(Light function only)
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 27-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS

42-01 Horizontal Stabilizer

⇑ Trim Actuator C 4 3 One RVDT channel may be inoperative
(RVDT Channels) provided all flight control modules are
operative. *

OR
C 4 3 (M) One RVDT channel may be inoperative in
combination with a flight control module
provided it is associated with the same flight
control unit.

(* All flight control modules are operative

assumes MMEL relief has not already
been undertaken for Item 27-61-02 –
Flight Control Modules (FCM) Channels.)
51-01 Slat/Flap Control Unit
(SFCU)
1) Slat Channels B 2 1 (M)(O) One Slat channel may be inoperative
(Relief limited to p/n provided:
GT415-5900-13 & a) Both Flap channels are operative, and
⇑ subs) b) Aircraft is operated in accordance with
AFM Supplement for SLATS
HALFSPEED OR FLAPS HALFSPEED.

2) Flap Channels B 2 1 (M)(O) One Flap channel may be inoperative

(Relief limited to p/n provided:
GT415-5900-13 a) Both Slat channels are operative, and
⇑ & subs) b) Aircraft is operated in accordance with
AFM Supplement for SLATS
HALFSPEED OR FLAPS HALFSPEED.

NOTE:
Slat or Flap system will operate at
half speed and it will be shown as
an advisory message:
“ SLATS HALFSPD” or “FLAPS
HALFSPD” on EICAS.

61-01 MFS Surface C 8 6 (M) One or two on the same MFS pair may be
⇑ Proximity Switch inoperative provided visual check is made to
Sensors (PSS) verify that the surfaces operate normally
prior to take-off.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 27-3
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS

61-02 Flight Control

⇑ Modules (FCM) C 4 3 (M)(O) One channel may be inoperative provided:
Channels a) Affected MFS pair and ground spoilers
are verified retracted before each take
off,
b) Remaining MFS and ground spoilers are
verified operative prior to each flight,
c) Airplane is operated at or below FL410,
d) Both packs are operated in AUTO mode,
and
e) Aircraft is operated in accordance with
AFM Supplement for DISPATCH WITH
ONE PAIR OF MULTI-FUNCTION
FLIGHT AND/OR GROUND SPOILERS I
INOPERATIVE.

62-01 Multi-Function
⇑ Spoilers (MFS) C 8 6 (M)(O) One surface or one symmetrical pair may be
inoperative:
a) Affected MFS pair is verified retracted
before each take off,
b) Remaining MFS and ground spoilers are
verified operative prior to each flight,
c) Airplane is operated at or below FL410,
and
d) Both packs are operated in AUTO mode,
e) Aircraft is operated in accordance with
AFM Supplement for DISPATCH WITH
ONE PAIR OF MULTI-FUNCTION
FLIGHT AND/OR GROUND SPOILERS I
INOPERATIVE.

62-02 Roll Control Input

⇑ Modules (RCIM) C 4 3 One RVDT channel may be inoperative
(RVDT Channels) provided all multi-function spoilers are
operative in roll assist mode.

62-03 Flight Spoiler Control

⇑ Lever (RVDTs) C 4 3 One RVDT may be inoperative provided all
multi-function spoilers are operative in
proportional lift- dump mode.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 27-4
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS

62-04 Throttle Lever RVDTs C 4 3 One throttle lever RVDT may be inoperative.
⇑ (Ground Spoiler
Control)

63-01 Ground Spoilers C 4 2 (M)(O) One symmetrical pair of ground spoilers

⇑ (Inboard or Outboard) may be inoperative provided:
a) All remaining MFS and remaining GND
spoiler pair surfaces are operative in
the GLD modes,
b) Both surfaces of the inoperative pair
are verified fully retracted prior to each
flight,
c) Autobrakes are considered inoperative,
and
d) Aircraft is operated in accordance with
AFM Supplement for DISPATCH WITH
ONE PAIR OF MULTI-FUNCTION
FLIGHT AND/OR GROUND I
SPOILERS INOPERATIVE.

63-02 Ground Spoilers

⇑ Position Indication on
EICAS C 4 2 (M)(O)) Indication for one or for one symmetrical
pair may be inoperative provided:
a) Affected ground spoiler actuator
connections are inspected prior to
each flight,
b) Affected ground spoiler pair is
considered inoperative, and
c) Aircraft is operated in accordance with
AFM Supplement for DISPATCH WITH
ONE PAIR OF MULTI-FUNCTION
FLIGHT AND/OR GROUND I
SPOILERS INOPERATIVE.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 28-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL

21-01 Refuel/Defuel Adaptor C 1 0 (M) May be inoperative (missing) provided:

⇑ Cap a) Refuel/Defuel adaptor is visually
checked for contamination prior to
each refuelling,
b) No leakage can be detected after
refuelling is complete, and
c) Aft tank is defueled and remains
empty.

21-02 Fwd AC Pumps C 2 1 One may be inoperative provided:

⇑ (Boost Pumps) a) Aft AC pump on affected side is
operative,
b) DC Aux pump on affected side is
operative, and
c) All fuel quantity indications are
operative.

C 2 0 Both may be inoperative provided:

⇑ a) Both aft AC pumps are operative,
b) Both DC Aux pumps are operative,
c) All fuel quantity indications are
operative, and
d) Wing transfer system is operative.

OR
⇑ C 2 0 Both may be inoperative provided:
a) Both aft AC pumps are operative,
b) Both DC Aux pumps are operative,
c) All fuel quantity indications are
operative, and
d) Crossfeed SOV is operative.

21-03 (reserved)

21-04 APU Fuel SOV C 1 0 (M) May be inoperative provided:

⇑ a) Valve is deactivated CLOSED, and
b) APU is not used.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 28-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL

21-05 DC Aux Pumps C 2 1 (M) One may be inoperative provided: I

⇑ a) Prior to each dispatch, opposite
Center Transfer pump is verified I
operative, I
b) Opposite aft tank transfer pump is
operative,
c) Opposite aft tank transfer SOV is
operative,
d) Opposite wing transfer SOV is
operative,
e) Crossfeed SOV is operative,
f) Both associated AC pumps are
operative, and
g) Affected pump is de-activated, I

(Global 5000) C 2 1 (M) One may be inoperative provided: I

a) Prior to each dispatch, opposite I
⇑ Center Transfer pump is verified I
operative, I
b) Opposite Wing transfer SOV is I
operative, I
c) Crossfeed SOV is operative, I
d) Both associated AC Pumps are I
operative, and I
e) Affected pump is de-activated. i
. i
I

21-06 Crossfeed SOV C 1 0 (M) May be inoperative provided:

⇑ a) Valve is secured CLOSED,
b) Both DC Aux Pumps are operative,
and
c) Both wing Transfer SOVs are
operative.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 28-3
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL

22-01 Center Transfer C 2 1 (O) One pump may be inoperative provided:

⇑ Pumps a) Opposite DC AUX pump is operative,
b) Opposite Wing transfer SOV is
operative,
c) Fuel XFEED valve is verified
operative prior to each dispatch, and
d) Fuel quantity remaining in the main
wing tank is adequate to reach a
suitable or alternate destination if
remaining center pump fails at any
time.

⇑ C 2 0 One or both may be inoperative provided

the center wing tank remains empty.

OR
⇑ C 2 0 Both may be inoperative provided the
remaining fuel in center tank is considered
as unusable fuel.

22-02 Wing Transfer SOV C 2 0 (M) Both may be inoperative provided: I

⇑ a) Affected SOV is secured CLOSED,
b) Crossfeed SOV is operative,
c) Both AC pumps on the same side are
operative, and
d) Prior to each dispatch, opposite
CenterTransfer Pump is verified I
operative. I

22-03 Aft Tank Transfer

⇑ Pumps C 2 1 (M)(O) One may be inoperative provided:
(GX only) a) Affected pump is deactivated,
b) Associated aft tank transfer SOV is
deactivated CLOSED,
c) Opposite aft tank transfer SOV is
operative,
d) Opposite DC Aux pump is operative,
e) Opposite wing transfer SOV is
operative,
f) Both opposite fwd and aft AC pumps
are operative,
g) Aft tank fuel quantity readout is
operative, and
h) Planned flight considered the aft tank fuel
as unusable fuel.
(cont’d)
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 28-4
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL

Aft Tank Transfer C 2 0 (M) Both may be inoperative provided the Aft
Pumps Fuel Tank is empty.
(cont’d)
OR
⇑ C 2 0 (M) Both may be inoperative provided:
a) Remaining fuel in Aft tank is
considered as unusable fuel, and
b) AFM table from “AFT XFER FAIL” for
Aft tank unusable fuel is used to
determine fuel quantity for landing.

22-04 Aft Tank Transfer C 2 1 (M)(O) One may be inoperative provided:

⇑ SOVs a) Affected SOV is secured CLOSED,
(GX only) b) Associated aft tank transfer pump is
deactivated,
c) Opposite aft tank transfer pump is
operative,
d) Opposite DC Aux pump is operative,
e) Opposite wing transfer SOV is
operative,
f) Both opposite AC pumps are
operative,
g) Aft fuel tank quantity readout is
operative, and
h) Planned flight considered the aft tank
fuel as unusable fuel.

⇑ C 2 0 (M) Both may be inoperative provided the Aft

Fuel Tank is empty.

C 2 0 (M) Both may be inoperative provided:

a) Aft tank SOVs are verified in CLOSED
position,
b) Remaining fuel in Aft tank is
considered as unusable fuel, and
c) AFM table from “AFT XFER FAIL” for
Aft tank unusable fuel is used to
determine fuel quantity for landing.

22-05 Aft Tank Transfer

⇑ System C 1 0 (M) May be inoperative provided:
(GX only) a) Aft transfer SOVs are verified in the
CLOSED position, and
b) AFT fuel tank is empty.
(cont’d)
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 28-5
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL

⇑ Aft Tank Transfer C 1 0 (M) May be inoperative provided:

System a) Aft tank SOVs are verified in the
(cont’d) CLOSED position, and
b) AFM table from “AFT XFER FAIL” for
Aft tank unusable fuel is used to
determine fuel quantity for landing.

23-01 Manifold Refuel/Defuel C 3 0 (M) All may be inoperative CLOSED provided

⇑ Control Valves alternate refuelling procedures are
established and used.

23-02 Aft Refuel / Defuel SOV C 1 0 (M) May be inoperative provided the SOV is
⇑ (GX only) deactivated CLOSED.

23-03 Defuel SOVs C 2 0 (M) Both may be inoperative deactivated

⇑ CLOSED.

23-04 Single Point Pressure

⇑ Refuelling System
1) Automatic Mode C 1 0 May be inoperative provided Manual Mode is
operative.

2) Manual Mode C 1 0 May be inoperative provided Automatic Mode

is operative.

23-05 Forward Tank C 1 0 May be inoperative provided the SOV is

*** Refuel SOV CLOSED.
⇑ (GX only)
(Relief applicable to post
BA SB 700-28-040)

23-06 External Refuel/Defuel I

I
⇑ Panel C 1 0 (O)(M) One or all functions may be inoperative
I
provided alternate means are available to
I
perform required operations (ie: Flight
I
Compartment Refuel/Defuel Panel or gravity
I
refuelling)
I
I
NOTE: For inoperative panel indications, I
refer to MMEL Item 28-41-05, I
Refuel/Defuel Panel Indications, I
herein)
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 28-6
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL

23-07 Flight Compartment I

I
*** Refuel/Defuel Panel C 1 0 (O)(M) One or all functions may be inoperative
I
⇑ provided alternate means are available to
I
perform required operations (ie: External
I
Refuel/Defuel Panel or gravity refuelling)
I
I
NOTE: For inoperative panel indications, I
refer to MMEL Item 28-41-05, I
Refuel/Defuel Panel Indications, I
herein) I

24-01 Fuel Recirculation C 2 0 One or both may be inoperative OFF

⇑ Systems provided:
(Including systems’ a) Both recirculation systems are OFF,
PBA indications & and
EICAS messages) b) Fuel tank temperature indication is
operative on EICAS

40-01 L-R AUX PUMPS C 2 0

⇑ “OFF” Switch lights
(light function only)

40-02 L-R PRI PUMPS C 2 0

⇑ “OFF” Switch lights
(light function only)

40-03 XFEED SOV “OPEN” C 1 0

⇑ Switch lights
(light function only)

40-04 XFEED SOV “FAIL” C 1 0

⇑ Switch lights
(light function only)

41-01 Fuel Quantity Probes

⇑
1) Densitometer C 1 0 (O) May be inoperative provide alternate fuel
planning procedures are used.

2) Wing Tank Probes –

Probe / Compensators C 30 22 (M) One probe per fuel compartment may be
⇑ inoperative.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 28-7
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL

3) Center Tank Probes –

Probe / Compensators C 4 2 (M)

4) Reference
Compensator C 1 0 (O) May be inoperative provide alternate fuel
⇑ planning procedures are used.

5) Aft Tank Probe /

Compensators C 2 1 (M)
(GX only)

6) Forward Tank
*** Probe / Compensators C 2 1
⇑ (GX only)
C 2 0 (O) Both may be inoperative provided the
forward tank is not used.

NOTE:
With both probes failed, the FUEL
QTY DEGRADED advisory will
remain annunciated on EICAS as
long as any fuel remains in the tank.

41-03 EICAS Aft Fuel Tank C 2 0 (M)(O) Both may be inoperative provided:
⇑ and Total Fuel a) Aft tank remains empty, and
Quantity Readouts b) An in-flight log of fuel in all tanks is
(GX only) maintained.

41-04 (deleted)

41-05 Fuel System

⇑ Indications on External
Refuel/Defuel Control
Panel
1) Fuel Quantity Fields C 5 0 (M) One or all may be inoperative provide
alternate procedures are used to verify fuel
quantity.
2) PRESEL Field C 1 0 (M) May be inoperative provided that refuel
AUTO mode is considered inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 28-8
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL

41-06 Float Valve –

⇑ Gravity Refuel
- CTR TANK - C 1 0 May be inoperative provided:
a) Single point pressure refuelling is
(Global 5000) operative and used, in either AUTO or
MANUAL modes, and
b) Center Refuel/Defuel control valve is
operative.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 29-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
29 HYDRAULICS

10-01 Heat Exchanger C 3 2 One may be inoperative.

⇑ Bypass Valve

11-01 HYDRAULIC C 3 0 All may be inoperative provided switch(es)

⇑ Switches “AUTO” are manually selected ON before take-off and
Function (ACMP) landing.

12-01
(deleted) (deleted, 07/02/07)

13-01 AC Motor Pump B 2 1 (O) One may be inoperative provided:

(ACMP) a) Affected pump is deactivated,
⇑
(System #3) b) Remaining system 3 AC Motor Pumps is
operated continuously during flight, and
c) All other hydraulic pumps are operative.

13-02 RAT Accumulator C 1 0 (M) May be inoperative provided the accumulator

⇑ Pressure Gauge pre-charge is verified using a calibrated
ground equipment gauge prior to the first flight
of each day.

30-01 HYD SOV CLOSED C 2 0 One or both may be inoperative provided that
⇑ Switch Lights the FWSOV indication on the HYDRAULC
(light function only) synoptic page is operative.

30-02 Hydraulic Firewall C 2 0 (M) One or both EICAS Synoptic HYD SOV icons
⇑ Shut-off Valve – may be magenta, provided that prior to each
EICAS Synoptic Page dispatch:
Indication a) The associated valve is verified to
operate to fully OPEN and fully
CLOSED positions, and
b) The associated valve remains in the
OPEN position for take-off

31-01 EICAS Hydraulic C 3 0 (O) All may be inoperative provided the

⇑ Pressure Readouts associated pressure switches are operative.

31-02 Hydraulic Pump Low C 6 3 (M) Three may be inoperative provided:

⇑ Pressure Switches a) Associated AC hydraulic pump is
selected “ON”,
b) At least one low pressure switch is
operative for each hydraulic system,
and
c) All other hydraulic system components
are operative.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 29-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
29 HYDRAULICS

31-03 EICAS Hydraulic C 3 0 (M) All may be inoperative provided quantity in

⇑ Reservoir Quantity associated reservoir(s) is checked on
Readouts reservoir quantity gauges prior to each flight.
(Systems 1, 2, and 3)

31-04 Hydraulic Reservoir C 3 0 All may be inoperative provided reservoir

⇑ Quantity Gauges levels are verified on the EICAS Synoptic
(Systems 1, 2, and 3)
Page prior to each flight.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 30-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
30 ICE PROTECTION

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

⇑ a) Operations are not conducted in
known or forecast icing conditions, and
b) Both ice detection systems are
operative.

1) AUTO Mode C 1 0 (M)(O) May be inoperative provided:

a) MAN mode (ON) is verified operative,
and
b) Both ice detection systems are
operative.

11-02 Wing Anti-Ice Shut I

⇑ Off Valves (WAIV) (deleted) I
I
C 2 0 (M) One or both may be inoperative CLOSED I
provided:
a) Valves are secured CLOSED,
b) Wing ANTI-ICE switch is selected to
OFF,
c) Both ice detection systems are
operative, and
d) Operations are not conducted in
known or forecast icing conditions.

11-03 WING XBLEED Valve C 1 1 (M) May be inoperative provided:

⇑ (CBW) a) Affected valve is secured CLOSED,
b) Operations are not conducted in
known or forecast icing conditions, and
c) Both ice detection systems are
operative.

11-04 Wing Anti-Ice

⇑ Temperature Sensors
(WAITS)

(pre-mod # 700T02064: C 8 4 (M) Except for the sensors used by the stall
⇑ SB#700-27-048 or protection system (outboard), sensors I
SB#700-1A11-27-011) may be inoperative provided the L (R) I
WING ANTI-ICE FAIL Caution or WING I
A/ICE SENSOR Advisory message is not
I
(cont’d) annunciated.
I
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 30-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
30 ICE PROTECTION

⇑ Wing Anti-Ice
Temperature Sensors
(WAITS)
(cont’d)

(post-mod # 700T02064: C 8 - Any combination of sensors may be

SB#700-27-048 or inoperative provided the L (R) WING ANTI-
SB#700-1A11-27-011 )
ICE FAIL Caution or WING A/ICE SENSOR I
Advisory message is not annunciated. I
I

11-05 WING XBLEED

⇑ Switch
1) AUTO C 1 0 (M)(O) May be inoperative provided:
(mode unavailable) a) Wing anti-ice selector switch is
operative,
b) Wing anti-ice system is verified
⇑ operative,
c) Switch selections FROM L and FROM R
are verified operative.

2) FROM L C 1 0 (M)(O) May be inoperative provided:

(manual) a) Flight is not conducted in known or
forecast icing conditions,
b) Both ice detection systems are
⇑ operative, and
c) Wing cross bleed valve is CLOSED.

3) FROM R C 1 0 (M)(O) May be inoperative provided:

(manual) a) Flight is not conducted in known or
forecast icing conditions,
⇑ b) Both ice detection systems are
operative, and
c) Wing cross bleed valve is CLOSED.

21-01 Cowl Anti-Ice System

⇑ AUTO Mode C 2 0 (M) May be inoperative provided:
(LH and RH) a) Associated manual mode is operative,
and
b) Both ice detection systems are
operative.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 30-3
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
30 ICE PROTECTION

21-02 Cowl Anti-Ice Valves

⇑ Pre BA MODSUM
B700T63444 B 2 1 (M) One may be inoperative CLOSED provided:
(BRR SB # 30-101200 a) Affected valve is secured CLOSED,
Issue 01) b) Aircraft is not dispatched into known or
forecast icing, and
c) Both ice detection systems are
operative.

⇑ B 2 1 (M) One may be inoperative OPEN provided:

a) Affected valve is secured OPEN,
b) Both ice detection systems are
operative, and
c) Operations are conducted in
accordance with the AFM Supplement
for DISPATCH WITH COWL ANTI-ICE
FAILED OPEN.

⇑ Post BA MODSUM B 2 1 (M) One may be inoperative provided:

B700T63444 a) Affected valve is secured OPEN,
(BRR SB # 30-101200 b) Both ice detection systems are
Issue 01) operative, and
c) Operations are conducted in
accordance with the AFM Supplement
for DISPATCH WITH COWL ANTI-ICE
FAILED OPEN.

30-01 Probe Heaters

1) Pitot/Static Probes B 4 3 (M) Except where enroute operations require its
use, including RVSM, one may be I
inoperative provided:
⇑ a) ADC 1 and Standby system probes I
heating is operative, I
b) Associated ADC is considered I
inoperative, I
c) Operations are not conducted in visible
moisture in any form,
d) Operations are not conducted in known
or forecast icing conditions, and
e) Both ice detection systems are I
operative.
I
(deleted) I
I
(cont’d) I
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 30-4
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
30 ICE PROTECTION

2) TAT probe B 3 2 (M) Except where enroute operations, including

RVSM, require its use, one may be
inoperative provided:
a) Operations are not conducted in visible
⇑
moisture where TAT is 10 deg C or
lower,
b) Operations are not conducted in known
or forecast icing conditions,
c) Both Ice Detection systems are
operative, and
d) Operations are conducted in day VMC
conditions only.
I
(deleted) (deleted) I
I

31-01 Yaw Damper Heaters C 2 1 (O) One may be inoperative provided:

a) Yaw Damper with the inoperative
⇑ heater is selected ON, and
b) Both Yaw Dampers are verified
operative before dispatch.

C 2 0 (O) Both may be inoperative provided:

a) Operations are conducted at or below
FL410, and
b) Both Yaw Dampers are verified
operative before dispatch.

31-02 Probe Heater monitor

Channels (HBMU) B 2 0 (M) One or both may be inoperative provided:
a) Both ice detection systems are
⇑ operative,
b) Operations are not conducted in known
or forecast icing conditions,
c) Operations are conducted under day
VMC only,
d) Enroute operations, do not require its
use, and
e) Flights are conducted in accordance
with the AFM Supplement for
DISPATCH WITH BRAKE
TEMPERATURE MONITORING
SYSTEM INOPERATIVE.
NOTE: The associated BTMU (both inboard
and outboard) will be inoperative.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 30-5
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
30 ICE PROTECTION

40-02 Enhanced Vision

System - Ice Protection
1) EVS Fairing & IR C 2 0 One or both may be inoperative provided:
Window Heat DE-ICE a) Operations are not conducted in
/ ANTI-ICE Function known or forecast icing conditions, and
⇑ b) Ice detection system is operative.
NOTE:
With IR Window heat inoperative, the
EVS image may degrade in high
humidity conditions, to the point of
disappearance, as IR Window misting
increases
D 2 0 (M) One or both may be inoperative provided the
IR Window and EVS fairing are removed as
an assembly and replaced with an approved
blanking plate.
2) IR Window –
DE-MIST Function C 1 0 May be inoperative provided EVS image is
acceptable to the pilot.
⇑
NOTE:
With IR Window heat inoperative, the
EVS image may degrade in high
humidity conditions, to the point of
disappearance, as IR Window misting
increases.
OR
C 1 0 May be inoperative provided EVS IR Window
heat is considered inoperative.

3) EVS Fairing
Temperature Sensors D 2 1 One may be inoperative.
⇑
C 2 0 Both may be inoperative provided EVS fairing
heat is considered inoperative.

4) IR Window
Temperature Sensors D 2 1 One may be inoperative.
⇑

C 2 0 Both may be inoperative provided EVS fairing

heat is considered inoperative.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 30-6
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
30 ICE PROTECTION

41-01 Windshield and Side C 4 3 (O) One may be inoperative provided: I

⇑ Window Anti-Ice a) Pilot's side window heating is
Controller Channels operative, and
b) Operations are not conducted in known
or forecast icing conditions
C 4 2 (O) Two may be inoperative provided: I
a) Operations are not conducted in
known or forecast icing conditions,
b) Pilot's side window heating is
operative, and
c) Both ice detection systems are
operative.

81-01 Ice Detection C 2 1 (M) One may be inoperative provided wing and
⇑ Systems cowl anti- ice systems are turned ON when
icing conditions as defined in the AFM exist
or are anticipated.

C 2 0 (M) Both may be inoperative provided operations

are not conducted in known or forecast icing
forecast conditions.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 31-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
31 INDICATING &
RECORDING

21-01 Clocks C 2 1 As required by Regulations.

⇑ C 2 0 Both cockpit clocks may be inoperative

provided:
a) Correct time is displayed on the NAV /
IDENT Page of the FMS CDU(s), and
b) A reliable and functioning timepiece is
readily available to all flight deck
crewmembers.

31-01 Flight Data

⇑ Recorder (FDR) A - 0 May be inoperative provided repairs are
made in accordance with FARs.

31-02 Quick Access D 1 0

*** Recorder
⇑

31-03 Pilot Event Marker A 1 0 May be inoperative provided repairs are I

made before completion of the next heavy I
⇑
maintenance visit (C check). I

33-01 Cockpit Printer C 1 0 May be inoperative provided alternate

*** (Flight Deck) procedures are established and used.
⇑
D 1 0 May be inoperative provided routine
procedures do not require its use.

41-01 Integrated Avionics B 1 0 (O) May be inoperative provided:

⇑ Computer a) Reversion switching system is
(IAC) #3 operative,
b) All EICAS displays are operative, and
c) Both AP Quick DISC buttons, and both
A/T disengage switches are operative.
NOTE:
Loss of IAC #1 or #2 results in loss of
one autothrottle system, one yaw
damper system, one autopilot system,
one Flight Director and one FMS.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 31-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
31 INDICATING &
RECORDING

43-01 Lamp Dimmer Power C 3 2

⇑ Supplies (LDPS)

61-01 Display Units B 6 5 (M) Display Unit #4 may be inoperative provided

⇑ reversion-switching system is verified
operative.

61-02 Electronic Checklist D 1 0

*** System
⇑
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 32-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
32 LANDING GEAR

30-01 Landing Gear

⇑ Retraction System A 1 0 (M) Aircraft may be dispatched for one flight day, I
provided: I
a) All gear doors (not attached to gear leg) I
close normally, I
b) Approved ground lock-pins are installed I
(flags removed) for flight, I
c) All weight-on-wheels sensors are I
operative, I
d) Both ice detector probes are operative, I
e) Both packs are operative, I
f) Aircraft is operated in accordance with I
AFM Supplement for Dispatch With I
Landing Gear Retraction System I
Inoperative, and I
g) If GEAR DISAGREE Caution is I
annunciated during flight, nosewheel I
steering is to be selected OFF for I
landing. I
I
I
I

31-01 Landing Gear

⇑ Selector Handle
Anti-Retraction
Mechanism C 1 0 (M) May be inoperative in LOCKED position
(down) provided downlock release mechanism
is verified operative.

32-01 Nose and Main Gear

⇑ Door Uplock Sensors C 3 0 All may be inoperative provided the EICAS
gear door indications are operative.

43-01 Brake Accumulator on

⇑ Hydraulic System #2 A 1 0 (O) May be inoperative provided:
a) Both thrust reversers are operative,
b) Hydraulic electric pumps 3A, 3B & 2B
(ACMP) are operative,
c) Autobrake is selected to OFF, and
d) Repairs are made within three flight days.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 32-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
32 LANDING GEAR
43-02 EICAS Brake Pressure
⇑ Readouts C 2 0 (M) Both may be inoperative provided:
a) Brake accumulator(s) nitrogen pressure
is checked prior to the first flight of the
day,
b) Capability of brake accumulators to retain
adequate hydraulic fluid for brakes is
verified prior to the first flight of the day,
and
c) Hydraulic pressure indications are
operative.
43-03 Autobrake System C 1 0 May be inoperative provided autobrake
⇑ selector switch remains in the OFF position.

43-04 Brake Temperature B 1 0 May be inoperative provided operations are

⇑ Monitoring System conducted in accordance with the AFM
(BTMS) Supplement for DISPATCH WITH BRAKE
TEMPERATURE MONITORING SYSTEM
INOPERATIVE.
1) Brake Temperature C 4 - One temperature sensor may be inoperative
Sensors provided operations are conducted in
⇑ accordance with the AFM Supplement for
DISPATCH WITH BRAKE TEMPERATURE
MONITORING SYSTEM INOPERATIVE.

43-05 Wheel Speed C 8 7 (M)

⇑ Transducer Coils

43-06 Brake Accumulator C 2 0 (M) Both may be inoperative provided

⇑ Pressure Gauges accumulator pre-charge pressure is checked
using a suitable pressure gauge before the
first flight of each flight day.
50-01 Nosewheel Steering C 1 0 (M) May be inoperative provided:
⇑ System a) Solenoid selector valve is not failed
OPEN,
b) Nosewheel steering system is
selected off,
c) Auto brake system is selected to OFF,
d) Take-off and landing is not conducted
from a contaminated runway, and
e) Operations are conducted in accordance
with the AFM Supplement for
DISPATCH WITH NOSEWHEEL
STEERING SYSTEM INOPERATIVE.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 33-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
33 LIGHTS

11-01 Cockpit/ Flight Deck/ C - - Individual lights may be inoperative provided

⇑ Flight Compartment remaining lights are:
and Instrument a) Sufficient to clearly illuminate all
Lighting Systems required instruments, controls, and other
devices for which it is provided,
b) Positioned so that direct rays are
shielded from flight crew members eyes,
and
c) Lighting configuration and intensity is
acceptable to the flight crew.

13-01 Cockpit Dome Light C 2 0

⇑ (Area Lights)

21-01 Cabin Interior Lights C - - May be inoperative provided:

⇑ a) Cabin Emergency Lighting is operative
for cabin crew to perform required
duties, and
b) Sufficient lighting is operative for cabin
crew to perform required duties, and
c) Lighting configuration at dispatch is
acceptable to the flight crew.

21-02 Entrance Area D - -

⇑ Lighting

21-03 Stair Lighting D - 0 May be inoperative provided a flashlight is

⇑ Systems used to illuminate stairs for night operations.

22-01 Passenger C - - (M)(O) Passenger Seats, Flight Attendant Seats, or

⇑ InformationSigns Lavatory from which a sign is not readily
“Fasten Seat Belts / legible shall not be occupied and must be
No Smoking” blocked and placarded “DO NOT OCCUPY”.

C - - (O) The affected Seats or Lavatory may be

occupied provided procedures are developed
and used to alert flight attendants and notify
passengers when seat belts should be
fastened and smoking prohibited.

(cont’d)
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 33-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
33 LIGHTS

1) Non-Passenger
Carrying Operations A - - (O) May be inoperative for one flight day for non-
passenger carrying operations provided:
⇑ a) Crew members are the only occupants
of the aircraft, and
b) Alternate procedures are established
and used.

C - - (O) Aural tone function may be inoperative.

⇑ C - - (O) Automatic function may be inoperative

provided:
a) Manual control function is operative, and
b) Alternate procedures are established
and used.
2) All Cargo Operations D - - May be inoperative provided all crewmembers
are in the flight compartment.
⇑

31-01 Nosewheel
⇑ Compartment Light D 1 0

31-02 Avionics
⇑ Compartment Lights D 6 0

31-03 APU Compartment

⇑ Light D 1 0

31-04 Aft Equipment

⇑ Compartment Light D - 0

31-05 Aft Service Area

⇑ Lights / Engine Pylon
Lights D 2 0

31-06 Main Gear Wheelwell

*** Service Lights D 2 0
⇑
40-01 Baggage
⇑ Compartment Lights C - 0 (M) May be inoperative providing adequate
alternate lighting is available.

D - 0 May be inoperative for daylight operations.

 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 33-3
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
33 LIGHTS

41-01 Landing Lights C 4 0 All may be inoperative provided aircraft is not

⇑ operated at night.

1) Nose Gear C 2 1 One may be inoperative provided the same-

side wing landing light, and associated taxi
⇑ light are operative.

C 2 0 Both may be inoperative provided the wing

landing lights, and both taxi lights are
operative.

2) Wing Landing (Inbd)

Lights C 2 1 One may be inoperative provided both nose
⇑ gear mounted landing lights and the
associated taxi light and are operative.

C 2 0 Both may be inoperative provided nose gear

mounted landing lights, and both taxi lights
are operative

41-02 Taxi / Recognition

⇑ Lights (Wing Outbd) C 2 1 One may be inoperative provided the same-
side wing and same-side nose gear mounted
landing lights are operative.
C 2 0 Both may be inoperative provided both wing
and both gear mounted landing lights are
operative.

C 2 0 Both may be inoperative provided aircraft is

not operated at night.

41-03 Wing-Tip Taxi Lights D 2 0 One or both may be inoperative.

***
⇑
41-04 Pulselite® Landing
*** Lights System D 1 0
⇑
42-01 Navigation Lights
1) Wing Tip Position
Light Bulbs C 4 2 One bulb may be inoperative at each
position.
⇑
C 4 0 Any or all may be inoperative for day
operations.
(cont’d)
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 33-4
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
33 LIGHTS

42-01 Navigation Lights

(cont’d)
2) Aft Position Light
Bulbs C 2 1
⇑
C 2 0 Both may be inoperative provided aircraft is
not operated at night

⇑ C 2 0 Both may be inoperative provided both wing

and both gear mounted landing lights are
operative.

C 2 0 Both may be inoperative provided aircraft is

not operated at night.

43-01 Anti-Collision Strobe

⇑ Lights (Wing and Tail) C 3 0 Any or all may be inoperative provided
operations are not conducted at night.

C 3 0 Any or all may be inoperative provided upper

and lower fuselage anti-collision beacon
lights are operative with the BEACON switch
in the WHT position.

43-02 Red / White Beacon

⇑ Lights
C 4 0 One or all may be inoperative provided
I
(Upper and lower I
aircraft is not operated at night.
fuselage) I
I
1) Red Beacons C 2 0 One or both may be inoperative provided I
adequate precautions are taken to clear I
danger areas before engine start and while I
engines are running. I
I
⇑ 2) White Beacons C 2 0 One or both white beacons may be I
inoperative provided all wing & tail anti- I
collision strobe lights are operative and I
selected ON prior to flight. I
I
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 33-5
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
33 LIGHTS

45-01 Wing Inspection C 2 0 Both may be inoperative provided:

⇑ Lights a) Both Ice Detection Systems are
operative,
b) Ground de-icing procedures do not
require their use, and
c) A portable lamp/light, of adequate
capacity for wing and/or control surface
inspection is available for night
operations in icing conditions.

46-01 Logo Lights D 2 0

***
⇑
50-01 Interior Emergency
⇑ Lights 1 1 Must be operative.

1) Individual Lights C - - May be inoperative provided compliance to

certification requirements has been satisfied
with only the remaining lights.
2) Crew Rest Facility -
Bunk D - - (O) May be inoperative provided:
⇑ a) Crew Rest Facility – Bunk is not
occupied, and
b) Crew Rest Facility – Bunk is placarded
INOPERATIVE – DO NOT USE.
50-02 Floor Proximity
⇑ Escape Path Lighting C - - Individual sources may be inoperative
provided FAA approved minimum lighting
levels specified in one of the following
documents are complied with:
a) FAA engineering approval letter;
OR
b) FAA approved report of the Type
Design holder;
OR
c) Limitations and Conditions section of
the applicable Supplemental Type
Certificate (STC);
OR
d) The Master Drawing List of the
applicable STC.

51-01 Exterior Emergency

⇑ Lights C 3 0 May be inoperative provided aircraft is not
operated at night.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 34-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

10-01 Air Data Computers B 3 2 (O)(M) One may be inoperative provided:

⇑ (ADC) a) ADC #1 is operative,
b) Reversion Switching System is
operative,
c) The four pitot-static probes are
functional, including the probe heaters,
and
d) TAT probes of the unaffected ADCs
are operative.

NOTE:
Transponder and Flight
Director/Autopilot must use same
ADC data for RVSM.

11-01 Total Air Temperature

Indications

⇑ 1) TAT #1 and
TAT#2 Systems B 2 1 May be inoperative provided TAT #3 is
operative.

2) TAT #3 C 1 0 (O) May be inoperative provided SAT indication is

operative.

13-01 Static Air

⇑ Temperature
Indication (SAT) C 2 0 (O) May be inoperative provided TAT Indication is
operative.

14-01 Altitude Alerting A 1 0 As required by FAR. I

⇑ System I
I
I

21-01 Standby Attitude C 1 0 May be inoperative provided not required by

⇑ Indicator FAR.

B 1 0 (M) May be inoperative provided:

a) Operations are conducted in day VMC,
and
b) Operations are not conducted into
known or forecast over-the-top
conditions.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 34-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

22-01 Non-stabilized
⇑ Magnetic Compass B 1 0 (O) May be inoperative provided any combination
(Standby Compass) of three IRS stabilized compass systems are
operative.

OR
B 1 0 (O) May be inoperative provided:
⇑ a) Any combination of two IRS stabilized
compass systems operate normally, and
b) Aircraft is operated:
1) with dual independent navigation
capability, and
2) under positive radar control by ATC
on the enroute flight phase, or one
of the systems is a TSO’d GPS
which provides track information.
OR
B 1 0 (O) May be inoperative for flights that are entirely
⇑ within areas of magnetic unreliability provided
at least two IRS stabilized directional gyro
systems are installed, operative and used in
conjunction with approved Free gyro
Navigation Techniques.

23-01 Flight Director C 2 1 One may be inoperative provided approach

⇑ Systems procedures are not dependent on its use.

1) Flight Director C - - Except where enroute operations or I

⇑ Modes approach minimums / procedures require I
their use, individual flight director modes I
may be inoperative provided Altitude I
Alerting System is operative. I
I
NOTE 1: Flight director altitude hold I
mode is required for RVSM I
Operations. I
NOTE 2: Any flight director mode, which I
operates normally, may be used. I
I

24-01 Electronic Standby

⇑ Instrument
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 34-3
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

1) Attitude / Slip Skid

Function A 1 0 (O) May be inoperative for two flight days
provided:
⇑ a) Operations are conducted in day VMC,
b) Operations are not conducted into
known or forecast over-the-top
conditions, and.
c) Each primary flight display is fed from
independent IRSs.

2) STD (Standard)
⇑ Button C 1 0
3) + / - Buttons B 2 0 Dim / Bright controls may be inoperative
(brightness) provided the display intensity is adequate.

4) ILS / LOC / GS D - 0
⇑
31-01 VHF Navigation
⇑ Systems (VOR/ILS #1) C 1 0

32-01 Head-up Guidance

*** System D 1 0
May be inoperative provided approach
⇑ minimums are not dependent on its use.

32-02 Enhanced Vision

*** System (incl. Infrared D 1 0 (M) May be inoperative provided EVS fairing and
⇑ Sensor Unit) IR Window heater functions are operative.
NOTE:
For loss of IR Window heat functions,
see MMEL Item 30-40-02.

1) Infrared Window D 1 0 (M) May be scratched or crazed provided

damage limits are not exceeded.

⇑ NOTE: Where the EVS image is

adversely affected, the system is to be
considered inoperative.

D 1 0 (M) May be removed with fairing assembly and

replaced with an approved blanking plate.
NOTE: For loss of IR Window heat
functions, see MMEL Item 30-40-02.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 34-4
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

2) CLEAR Switch D 1 0 (M) May be inoperative provided the EVS is

considered inoperative and is not used.

3) FMS CDU –
Infrared Image D 1 0 May be inoperative provided the EVS is not
⇑ used in lieu of natural vision below minimums
and is only used for enhanced situational
awareness.
32-03 (deleted)

41-01 Weather Radar

⇑ System C 1 0 As required by Regulations.

41-02 Weather Radar C 2 1

⇑ Controllers

42-01 Ground Proximity A - 0 (O) May be inoperative provided:

⇑ Warning System a) Alternate procedures are established
and used,
b) Repairs are made within two flight days.

1) Terrain Avoidance A 4 0 (O) May be inoperative provided:

(Modes 1 - 4) a) Alternate procedures are established
⇑ and used, and
b) Repairs are made within two flight days.

2) Test Mode A 1 0 May be inoperative provided:

a) GPWS is considered inoperative, and
⇑ b) Repairs are made within two flight days.

3) Glideslope Deviation B 1 0
(Mode 5)
⇑

4) Advisory Callouts B 1 0 (O) May be inoperative provided alternate

*** (Mode 6) procedures are established and used.
(Ten or more
passenger seats)
C 1 0 (O) May be inoperative provided:
(Six to nine a) Advisory callouts not required by FAR,
⇑ passenger seats) 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 NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 34-5
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

5) Windshear Mode B 1 0 (O) May be inoperative provided alternate

(Mode 7) procedures are established and used

NOTE:
⇑ Alternate procedures should include
reviewing windshear avoidance and
recovery procedures.

6) TERRAIN function B 1 0 May be inoperative provided system is

selected OFF.

43-01 Traffic Collision and B - 0 (M) May be inoperative provided:

⇑ Avoidance System a) System is deactivated and secured,
(TCAS II) and
b) Enroute or approach procedures do
not require its use.

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

a) Not required by FAR,
b) System is deactivated and secured,
and
c) Enroute or approach procedures do not
require its use.

1) Combined Traffic C 2 1 (M) May be inoperative on the non-flying pilot

Alert (TA) and side provided:
Resolution Advisory a) TA and RA visual display is operative
⇑ (RA) Dual Displays on the flying pilot side, and
b) TA and RA audio function is operative
on flying pilot side.

2) Resolution Advisory C 2 1 May be inoperative on non-flying pilot side.

(RA) Display
⇑ System(s)
C - 0 (O) May be inoperative provided:
a) Traffic Alert (TA) visual display and
audio functions are operative,
b) TA ONLY mode is selected by the
crew, and
c) Enroute or approach procedures do
not require its use.
(cont’d)
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 34-6
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

3) Traffic Alert C - 0 (O) May be inoperative provided:

Display System(s) a) RA visual display and audio functions
⇑ are operative, and
b) Enroute or approach procedures do
not require its use.

4) Audio Functions B 1 0 May be inoperative provided enroute or

approach procedures do not require use of
TCAS.

44-01 Radio Altimeter C 2 1 (M) (O) One may be inoperative provided approach
⇑ minimums are not dependent on its use.

NOTE:
The flight director must be coupled to the
PFD with the operative Radio Altimeter
for landing with autothrottle engaged.

⇑ B 2 0 (M)(O) Both may be inoperative provided:

a) GPWS is considered inoperative,
b) TCAS is considered inoperative, and
c) Landings are conducted in accordance
with the Non-Normal Procedures for
Dual Radio Altimeter Failure.

45-01 Inertial Reference C 3 2 (M)(O) One may be inoperative provided:

⇑ Systems a) Independent attitude indication is
available at each pilot’s station,
b) Independent directional compass
indication is available at each pilot’s
station, and
c) Standby Attitude Indicator is operative.

45-02 Lasertrak NDU C 1 0 May be inoperative provided two FMS are

⇑ operative.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 34-7
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

45-03 IRS Mode Select

⇑ Switches C 3 2 (M)(O) One may be inoperative provided:
a) Affected switch is selected to OFF,
b) Associated IRS is considered
inoperative,
c) Independent attitude indication is
available at each pilot’s station,
d) Independent directional compass
indication is available at each pilot’s
station, and
e) Standby attitude indicator is operative.

47-01 Lightning Sensor

*** Systems (LSS) C - -
⇑

50-01 Integrated Nav Unit

⇑ (INU) – Tray Mounted
Cooling Fans C 2 1 (M) May be inoperative provided the remaining
fan is verified to operate normally.
51-01 Marker Beacon
⇑ Systems C - - May be inoperative provided approach
procedures do not require its use.

52-01 Automatic Direction

⇑ Finding System C 1 0
(ADF #1)

53-01 Distance Measuring D - - Any in excess of those required by

⇑ Equipment Systems Regulations may be inoperative.
(DME)

54-01 ATC Transponders B - 0 May be inoperative provided:

⇑ and Automatic a) Enroute operations do not require its
Altitude Reporting use, and
Systems b) Prior to flight, approval is obtained from
ATC facilities having jurisdiction over
the planned route of flight.
NOTE: This item is RVSM critical.
(cont’d)
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 34-8
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

D - 1 Any in excess of those required by FAR may

⇑ be inoperative.
NOTE:
Transponder and Flight Director/
Autopilot must use same side ADC
data for RVSM operations.

1) 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
Required by FAR of next heavy maintenance visit.

55-01 Global Positioning C - 0 May be inoperative provided operations do

⇑ Sensors not require their use.

61-01 Flight Management

⇑ Systems (FMS) C - 1 FMS 2 and/or FMS 3 may be inoperative
provided operating procedures do not require
their use.

1) Navigation Databases C - - (O) May be out of currency provided:

a) Current aeronautical charts are used to
verify navigation fixes prior to dispatch,
b) Procedures are established and used to
⇑ verify status and suitability of navigation
facilities used to define route of flight,
c) Navigation radios are manually tuned and
identified, and
d) FMS approaches are not conducted.

61-02 Data Loader C 1 0

⇑
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 35-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
35 OXYGEN

12-01 Flight Crew Oxygen

⇑ Pressure
1) Ground Service C 1 0 (O) May be inoperative provided EICAS readout is
Panel Pressure Gauge operative and checked prior to each flight.

2) Bottle Pressure C 4 0 (M) Any or all may be inoperative provided:

Gauges a) EICAS readout is verified normal, and
b) Bottle SOV levers are verified OPEN.

3) EICAS Readout B 1 0 (O) May be inoperative provided:

a) Ground service panel pressure gauge or
all bottle pressure gauges are operative
and checked prior to each flight, and
b) Minimum enroute altitude does not
exceed 10,000 ft above MSL.

12-02 Oxygen Pressure C 4 3 (M) One may be inoperative provided pressure on

⇑ Switch all bottle pressure gauges is operative and
checked prior to each flight.

12-03 Overboard Discharge C 1 0 May be missing provided:

⇑ Indicator a) EICAS Oxygen readouts are
serviceable,
b) Oxygen pressure switch is operative,
and
c) Ground service panel pressure gauge is
operative.

12-04 Crew Oxygen – C - - (M)(O) Any in excess of those required by regulation

*** Cruise Masks may be inoperative or missing provided the
⇑ (incl. Mask mics) inoperative unit is removed from the installed
location, secured out of sight and the unit and
its installed location are placarded
INOPERATIVE.

20-01 Protective Breathing D - - Any in excess of those required by

⇑ Equipment (PBE) Regulations may be inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 35-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
35 OXYGEN

21-01 Passenger Oxygen

*** System B 1 0 (O) May be inoperative provided:
⇑ a) All components of cabin pressurization
system are operative,
b) Minimum enroute altitude does not
exceed 14,000 ft above MSL,
c) Operations are conducted at or below
FL 250,
d) Portable oxygen units capable of
delivering two liters per minute for 30
minutes are available for 10 % of the
passengers, and
e) Operations procedures are established
to ensure that passengers are
appropriately briefed to accommodate
revised equipment.

1) System TEST / C 1 0 (M) May be inoperative provided alternate

RESET Switch procedures are established and used to verify I
⇑ (relief limited to system operation. I
Bombardier I
Completions Centre I
Installations) I
OR
B 1 0 May be inoperative provided passenger I
oxygen is considered inoperative

21-02 Passenger Oxygen B - 0 May be inoperative provided:

⇑ System – a) Manual deployment system is operative,
Automatic and
Presentation System b) Flight remains at or below FL 300.

21-03 Passenger Service D - 0 (M)(O) Individual PSUs may be inoperative with no

⇑ Units flight altitude restriction provided:
a) Affected seats, banks of seats and
lavatories are blocked and placarded
to prevent occupancy,
b) No more than two consecutive banks
of seats have an inoperative PSU, and
c) Units at assigned flight attendant
locations are operative.

21-04 Therapeutic Oxygen

*** (First Aid) System D 1 0 Any in excess of those required by Regulations
⇑ may be inoperative or missing.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 35-3
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
35 OXYGEN

30-01 Portable Oxygen

⇑ Dispensing Unit D - - (M)(O) Any in excess of those required by Regulation
may be inoperative or missing provided:
a) Required distribution of operative units
is maintained throughout the aircraft,
b) Inoperative unit is removed from the
aircraft, or removed from the installed
location, placarded “INOPERATIVE”,
and secured out of sight so it cannot be
mistaken for an operative unit, and
c) Procedures are established to alert
crew members of inoperative or missing
equipment.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 36-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
36 PNEUMATICS

11-01 Bleed Pressure C 2 0 (M)

⇑ Transducer (BPT)

11-02 Fan Air Valve C 2 1 (M)(O) One may be inoperative failed in OPEN
⇑ (FAV) position provided:
a) Associated air conditioning pack is
selected OFF and considered
inoperative,
b) Opposite air conditioning pack is
operative,
c) Opposite bleed system is operative, and
d) Cross bleed valve is verified operative.

11-03 HP Ground C 1 0 (M) May be inoperative failed in CLOSED

⇑ Connection position.

12-01 Bleed Leak Detection C 18 9 Either loop A or loop B may be inoperative

⇑ Loops provided redundant loop in the same zone is
operative.

1) Wing Anti-Ice Leak C 12 6 (M) One loop in each section may be inoperative I
provided: I
a) Power-up BIT test is performed on I
system prior to each dispatch into icing, I
and I
⇑ b) Cause of WING ANTI-ICE FAULT I
Advisory message is confirmed by I
maintenance. I
I
C 12 0 Both loops on each section may be
inoperative provided:
a) Aircraft is not operated in known or
forecast icing conditions, and
b) Both ice detection systems are
operative.

2) Trim Air Leak C 2 1 One loop may be inoperative.

⇑
C 2 0 (M) Both loops may be inoperative provided:
a) Trim air switch is selected OFF, and
b) Both HASOVs are secured CLOSED
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 38-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
38 WATER & WASTE

10-01 Potable Water C - - (M) Individual components may be inoperative

⇑ Systems 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.

⇑ C - - (M) May be inoperative provided:

a) System is drained, and
b) Procedures are established to ensure
that system is not serviced.

10-02 Lavatory Waste C - - (M) Individual component may be inoperative

⇑ System 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.

C - - (M) Associated lavatory system(s) may be

⇑ inoperative provided:
a) Associated components are deactivated
or isolated to prevent leak, and
b) Associated lavatory door(s) is secured
closed and placarded inoperative.

NOTE:
These provisions are not intended to
prohibit inspections by crewmembers.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 45-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
45 CENTRAL
MAINTENANCE
SYSTEMS

45-01 Central Aircraft

⇑ Information/
Maintenance System C 1 0
(CAIMS)
1) Cockpit Printer-
CAIMS Function D 1 0 NOTE: Refer to ATA 23, Item 21-01 for
Datalink (ACARS) printer function.

45-02 Portable Maintenance C 1 0

⇑ Access Terminal
(PMAT)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 46-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
46 INFORMATION
SYSTEMS

10-01 Electronic Flight Bags I

I
⇑
*** 1) Class 3 EFB C - - (O) May be inoperative provided alternate I
procedures are established and used. I
I
NOTE: Any function, program or I
⇑ document, which operates normally, I
may be used. I
D - 0 May be inoperative provided procedures do I
not require its use. I
I
*** 2) Data Connectivity C - - (O) May be inoperative provided alternate I
(Class 2) procedures are established and used. I
I
NOTE: Any function, program or I
⇑ document, which operates normally, I
may be used. I
D - 0 May be inoperative provided procedures do I
not require its use. I
I
*** 3) Power C - - (O) May be inoperative provided alternate I
Connection procedures are established and used. I
(Class 1& 2) I
NOTE: Any function, program or I
⇑ document, which operates normally, I
may be used. I
D - 0 May be inoperative provided procedures do I
not require its use. I
I
*** 4) Mounting C - - (O)(M) May be inoperative provided: I
Devices a) Associated EFB and hardware is I
(Class 2) secured by an alternate means or I
removed from the aircraft, and I
⇑ b) Alternate procedures are established I
and used. I
D - 0 (M) May be inoperative provided: I
a) Associated EFB and hardware is I
secured by an alternate means or I
removed from the aircraft, and I
b) Procedures do not require its use. I
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 49-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
49 AUXILIARY POWER

10-01 Auxiliary Power Unit C 1 0 (M) May be inoperative provided the inlet door is
⇑ (APU) secured CLOSED.

14-01 APU Air Intake C 1 0 (M) May be inoperative CLOSED provided:

⇑ Door linear actuator a) APU intake door is secured CLOSED,
and
b) APU is considered inoperative.

A 1 0 Aircraft may be dispatched for one flight day, I

with APU inlet door partially - OPEN I
provided: I
a) APU wind-milling RPM is monitored per I
AFM Non-Normal Procedure for APU I
DOOR FAIL Caution, and I
b) AFM performance corrections for APU
ON are applied.

⇑ C 1 0 (M) May be inoperative fully OPEN provided: I

a) APU is operated continuously during
flight, and
b) AFM performance corrections for APU
ON are applied.

52-01 APU Load Control C 1 0 (M) May be inoperative provided it is secured

⇑ Valve (LCV) CLOSED.

NOTE:
The APU is still available as a source of
electrical power, if required.

61-01 APU Subsystems Any or all may be inoperative as indicated by

“APU FAULT” advisory message on ground
⇑ provided the APU is operative (start and
shutdown normally).

1) EGT Thermocouples C 2 1

2) Speed Sensors C 2 1
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 49-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
49 AUXILIARY POWER
3) Fuel Filter C 1 0

4) Oil Filter C 1 0 APU may be operated with impending oil filter

bypass indicated provided:
a) Engines are started by an external
power source, and
b) APU is used only where required by
AFM Emergency Procedures
.
5) APU Generator
Oil Filter C 1 0
6) Hour Meter C 1 0

7) Start Counter C 1 0

8) Sump Oil Heater C 1 0 May be inoperative provided a minimum of

three engine generators, are operative.

9) Dual Ignition Box C 2 1 One channel may be inoperative.

Channels
NOTE:
With one channel inoperative, delayed
APU light-off may be observed.

90-01 APU Oil Quantity C 1 0 (M) May be inoperative provided oil quantity is
⇑ Indication System visually verified before each departure.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 52-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
52 DOORS

11-01 Passenger Door Power

⇑ Assist System C 1 0 (M) May be inoperative provided door is verified
manually operative (OPEN and CLOSED)
without any interference.

11-02 Passenger Door -

Folding Step Actuator
⇑ (Post MODSUM
V700T-804023)
C 1 0 May be inoperative provided folding step
travels to full deploy and stow positions using
assistance of door internal spring.

⇑ C 1 0 (O)(M) May be inoperative in the stowed position

provided alternate procedures are used for
embarking and disembarking.

70-01 Passenger Door C 1 0 (M)(O) May be inoperative provided prior to each

⇑ Indication System flight:
a) Door is CLOSED and all 10 door stops
are visually verified to be properly
aligned,
b) Inner handle is verified STOWED,
c) Flag indicator indicates SAFE,
d) External handle is verified STOWED,
and
e) External pressure vent flap is verified
FLUSH.
f) AUTO mode of cabin pressurization is
considered inoperative,
g) Cabin pressure MAN control channels
are verified operative,
h) Safety valves are verified operative,
j) Cabin RATE Indicator, Cabin ALT
indicator, and Cabin DIFF Pressure
Indicator are verified operative, and
k) Flights are conducted at or below
FL250.

70-02 Aft Equipment Bay C 1 0 (O) May be inoperative provided prior to each
⇑ Door Indication System flight affected door is verified CLOSED,
LATCHED and LOCKED.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 52-2
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
52 DOORS

70-03 Overwing Emergency

⇑ Exits Indication
System C 1 0 (M)(O) May be inoperative provided prior to each
flight:
a) Affected door is verified CLOSED,
LATCHED and LOCKED,
b) External push plate is verified FLUSH,
c) AUTO mode of cabin pressurization is
considered inoperative,
d) Cabin pressure MAN control channels
are verified operative,
e) Safety valves are verified operative,
f) Cabin RATE Indicator, Cabin ALT
indicator, and Cabin DIFF Pressure
Indicator are verified operative, and
g) Flights are conducted at or below
FL250.

70-04 Baggage
⇑ Compartment Door
Indication System C 1 0 (M)(O) May be inoperative provided prior to each
flight:
a) Affected door is verified CLOSED,
LATCHED and LOCKED,
b) External push plate is verified FLUSH
c) AUTO mode of cabin pressurization is
considered inoperative,
d) Cabin pressure MAN control channels
are verified operative,
e) Safety valves are verified operative,
f) Cabin RATE Indicator, Cabin ALT
indicator, and Cabin DIFF Pressure
Indicator are verified operative, and
g) Flights are conducted at or below
FL250.

70-05 Refuel/Defuel Door

⇑ Indication System C 1 0 (O) May be inoperative provided prior to each
flight, affected door is verified CLOSED,
LATCHED and LOCKED.
70-06 Aft Hydraulic Door
⇑ Indication System C 1 0 (O) May be inoperative provided prior to each
flight, affected door is verified CLOSED,
LATCHED and LOCKED.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 73-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
73 ENGINE FUEL &
CONTROL

21-01 Engine FADEC Faults A 2 0 May be dispatched with FADEC faults

⇑ provided repairs are made in accordance with
times established by engine manufacturer.
No extensions are allowed.
21-02 Engine Electronic
⇑ Controller – C 2 0 Both EPR Control modes may be inoperative
(EPR Control Modes) provided:
a) Both L ENGINE and R ENGINE
N1/EPR switches are selected to N1,
and
b) Flights are conducted in accordance
with the AFM Supplement for
DISPATCH IN ALTERNATE
CONTROL (N1) MODE.

NOTE: Autothrottle system will be

inoperative.
31-01 EICAS Fuel Flow B 2 1 One may be inoperative provided:
⇑ Readouts a) EICAS aft fuel tank and total fuel
quantity readouts are operative,
b) FMS fuel remaining indication system
is considered inoperative and not
used, and
c) EICAS fuel used readouts are
considered inoperative and not used.
31-02 EICAS Fuel Used C 2 0 Both may be inoperative provided:
⇑ Readouts a) EICAS aft fuel tank and total fuel
quantity readouts are operative, and
b) EICAS fuel flow readouts are
operative.

32-01 Engine Fuel Temp I

⇑ Indications (on the
FUEL Synoptic Page) C 2 1 (M) Except for Polar Ops, one may be inoperative I
provided icing inhibitor is added to the fuel. I

I
(deleted) (deleted) I
I
I
i
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 74-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
74 IGNITION

10-01 Ignition Systems B 4 3 (O) One may be inoperative provided cowl anti-ice
⇑ system operates normally on the associated
engine.

30-01 Ignition “ON”

⇑ Switch light C 1 0 (M) May be inoperative provided no fault
(light function only) messages are displayed for both FADEC
systems and the stall protection computer.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 77-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
77 ENGINE INDICATING

31-01 Engine Vibration C 2 0 Both may be inoperative provided:

Indication a) Both ice detection systems are
⇑ operative,
b) Operations are not conducted in known
or forecast icing conditions,
c) Operations are not conducted more than
60 minutes from a suitable airport, and
d) No deteriorating engine vibration trend
had been observed on the affected
channel(s) immediately prior to failure.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 78-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
78 EXHAUST

31-01 Thrust Reverser C 2 1 (M) One may be inoperative provided:

Systems a) Inoperative thrust reverser is
⇑ deactivated, stowed and locked in the
forward thrust position, and
b) Operations are conducted in accordance
with AFM performance data and AFM
Supplement for OPERATION ON
CONTAMINATED RUNWAYS.

NOTE:
Under conditions of one thrust reverse
rinoperative, where AFM Non-Normal
Procedures reference values With or
Without Thrust Reversers, the values
Without Thrust Reversers are to be
used.

C 2 0 (M) Both may be inoperative provided:

a) Inoperative thrust reversers are
⇑ deactivated, stowed and locked in the
forward thrust position, and
b) Operations are conducted in
accordance with AFM performance
data and AFM Supplement for
OPERATION ON CONTAMINATED
RUNWAYS.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 79-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
79 OIL

12-01 Remote Oil Fill C 1 0 (M) Part or all of the system may be inoperative
⇑ System provided that the affected engine(s) oil level
is/are checked and filled manually, prior to
each flight.

30-01 Engine Oil Quantity B 2 0 (M) Both may be inoperative provided:

Indication System a) The engine oil quantity is verified on the
⇑ engine oil quantity gauge prior to each
engine start, and
b) Operations are not conducted more
than 120 minutes from a suitable
airport.

NOTE:
After dispatch (10 min.) the caution
message “L-R OIL LO QTY” will
appear on EICAS.

34-01 Impending Oil Filter A 2 1 (M) One may be inoperative provided:

⇑ Bypass Indication a) A daily check of the oil filter pop-up
indicator is made, and
b) Repairs are made within three flight
days.
 U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/2009 80-1
1. SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & 2. NUMBER INSTALLED
ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
80 STARTING

11-01 Starter Air Valve C 2 1 (M)(O) One may be inoperative CLOSED provided:
⇑ (SAV) a) Alternate starting procedures are
established and used, and
b) APU Is operative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
BD--700-1A10 / -1A11 DATE: 06/27/20091

SECTION TWO

CAS
MESSAGE
ORIENTED
MMEL RELIEF
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
INT - 1
BD--700-1A10 / -1A11 DATE: 06/27/2009

INTRODUCTION

Two-section MMELs are authorized by FAA Policy Letter 119, Revision 2. Policy Letter 119, Revision 2
allows the flight crews of CFR 14 Part 91 operated aircraft to accomplish certain operational procedures that
allows the dispatch of the aircraft. The Master Minimum Equipment List (MMEL) is used in conjunction with
the respective dispatch procedures manual [ie.: Operations and Maintenance Procedures (OMP); Dispatch
Deviation Guide (DDG); etc], to accomplish the tasks required by the MMEL for dispatch.

Section Two of two-section MMELs may grant relief for failure indications presented as CAS messages
on Engine Indicating and Crew Alerting Systems (EICAS), or Electronic Centralized Aircraft Monitoring
(ECAM), rather than the traditional relief (Section One) for failed equipment.

Section Two of the MMEL will list only Crew Alerting system (CAS) messages meeting the following
requirements:
1) Equipment failure indications(s) that can be used to determine the airworthiness status of the
airplane,
2) Messages that the crew can act upon with simple troubleshooting procedures without the assistance
of a mechanic, and
3) Messages using the new self-diagnostic technology (virtual) actions.

CAS message relief items not meeting these requirements will be listed in Section One of the MMEL.

Section Two CAS message relief items may require flight crews to accomplish one or more steps to
deactivate/re-configure the affected system prior to flight. The “(O)” indicates the need for these tasks,
the details of which can be found in the respective dispatch procedures manual.

Tasks associated with candidate relief items are subject to verification by FOEB. They may include, but
are not necessarily limited to the following duties:
a) Procedures accomplished using cockpit (or cabin) system controls.
b) Deactivation of affected systems (by pulling system breaker or use of remote electronic system
isolation),
c) Visual confirmation of remote gauge indications, or valve positions as provided by integral
external indicators.
d) Visual inspection behind panels (internal or external) which are accessible without tools via
quick-release latches and which clearly indicate their unlocked or unsafe state; (ie.: red/green
safe window; flush fit latches; etc.)
.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
TOC – 1
BD--700-1A10 / -1A11 DATE: 06/27/2009

Back SECTION TWO

⇑ To
Top CAS MESSAGE RELIEF

SECTION 2 Cover…………………………………………………………………………………………..
INTRODUCTION………………………………………………………………………………………………INT1
TABLE of CONTENTS………………………………………………………………………………………TOC-1
MESSAGES……………………………………………………………………………………………………..2-1

CAS MESSAGE CAS MESSAGE

A/T 1 FAIL CHECK DU 4
A/T 2 FAIL CHECKLIST MISMATCH
ADC 2 DEGRADED CPLT BRAKE FAULT
ADC 3 DEGRADED CTR FUELXFER FAIL
ADC 2 FAIL CTR XFER FAULT
ADC 3 FAIL ELEC SYS FAULT
AFCS 1 FAIL EVS DEFOG FAULT
AFCS 2 FAIL EVS FAIL
AP 1 FAIL EVS HEAT FAIL
AP 2 FAIL EVS HEAT OVHT
AP PITCH TRIM FAIL FDR ACCEL FAIL
APU BLEED SYS FAIL FDR FAIL
APU DOOR FAIL FLAP HALFSPD
APU FADEC FAIL FMS 2 FAIL
APU FAULT FMS 3 FAIL
APU FIRE FAIL FUEL TEMP SENSOR
APU FIRE FAULT GEAR SYS FAIL
APU FUEL SOV GEAR SYS FAULT
APU GEN FAIL GND PROX FAIL
APU NOT AVAILABLE GPWS SYSTEMS FAIL
APU OIL HI TEMP HUD FAIL
APU OIL LO PRESS HUD FAN FAIL
APU OIL LO QTY HUD MISALIGN
APU SHUTDOWN HUMIDIFIER FAIL
APU SQUIB 1 FAIL HYD PUMP 3A FAIL
APU SQUIB 2 FAIL HYD PUMP 3B FAIL
ASCB CTLR 1 FAIL IAC 3 INVALID
ASCB CTLR 2 FAIL IAC 3 OVHT
ASCB CTLR 3 FAIL ICE
AUTOBRAKE FAIL ICE DETECTOR FAIL
AVIONIC FAN FAIL (GX ONLY) ICE DETECTOR FAULT
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
TOC – 2
BD--700-1A10 / -1A11 DATE: 06/27/2009

TABLE OF CONTENTS
(cont’d)

INT CABIN DOOR PLT BRAKE FAULT

IRS 1 AUX FAIL R AUX FUEL PUMP
IRS 1 AUX PWR R BLEED FAULT
IRS 1 FAIL R ENG FIRE FAULT
IRS 1 MISCMP R FADEC FAULT
IRS 1 OVHT R PACK AUTO FAIL
IRS 2 AUX FAIL R PACK FAIL
IRS 2 AUX PWR R PACK FAULT
IRS 2 FAIL R PRI FUEL PUMP
IRS 2 MISCMP R PROBE MON FAIL
IRS 2 OVHT R WINDOW HEAT FAIL
IRS 3 AUX FAIL R WING A/ICE FAIL
IRS 3 AUX PWR R WSHLD HEAT FAIL
IRS 3 FAIL RECIRC FAN FAIL
IRS 3 MISCMP SAFETY VALVE OPEN
IRS 3 OVHT SG 3 FAIL
L AUX FUEL PUMP SLAT HALFSPD
L BLEED FAULT SLAT-FLAP BIT
L ENG FIRE FAULT SMALL SERV DOORS
L FADEC FAULT SMOKE AFT LAV FAIL
L PACK AUTO FAIL SMOKE AV RACK FAIL
L PACK FAIL SMOKE BAGGAGE FAIL
L PACK FAULT SMOKE CLOSET AFT FAIL
L PRI FUEL PUMP SMOKE CLOSET FWD FAIL
L PROBE MON FAIL SMOKE FWD LAV FAIL
L WING A/ICE FAIL SPLRS/STAB BIT
L WSHLD HEAT FAIL TAT 2 FAIL
LARGE SERV DOORS TAT 3 FAIL
LTRK FAIL TAT HT 1 FAIL
MAN PRESS FAULT TAT HT 2 FAIL
MLG BAY OVHT FAIL TAT HT 3 FAIL
MLG BAY OVHT FAULT TERR FAIL
OUTFLOW VLV 1 FAIL TRU 1 FAIL
OUTFLOW VLV 2 FAIL TRU 2 FAIL
OXYGEN LO QTY WINDSHEAR FAIL
PITOT 2 HT FAIL WING A/ICE FAULT
PITOT 3 HT FAIL WING A/ICE LEAK
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
TOC – 3
BD--700-1A10 / -1A11 DATE: 06/27/2009

TABLE OF CONTENTS
(cont’d)

WING A/ICE LO HEAT YD 1 FAIL

WING A/ICE SENSOR YD 2 FAIL
WOW FAULT YD HEAT 1 FAIL
YD HEAT 2 FAIL
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2–1
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ A/T 1 FAIL C Aircraft may be dispatched provided affected A/T

(Advisory) is confirmed disengaged.

⇑ A/T 2 FAIL C Aircraft may be dispatched provided affected A/T

(Advisory) is confirmed disengaged.

⇑ ADC 2 DEGRADED B (O) Aircraft may be dispatched provided:

(Advisory) a) ADC 2 is de-activated,
b) None of the following CAS messages are
also posted:
ADC 1 FAIL Advisory;
ADC 3 FAIL Advisory;
ADC 1 DEGRADED Advisory;
ADC 3 DEGRADED Advisory;
c) Reversion Switching System is operative;
d) The four pitot-static probes are functional,
including the probe heaters, and
e) TAT probes of the unaffected ADCs are
operative.
NOTE: Transponder and Flight Director/Autopilot
must use same ADC data for RVSM.

⇑ ADC 3 DEGRADED B (O) Aircraft may be dispatched provided:

(Advisory) a) ADC 3 is de-activated,
b) None of the following CAS messages are also
posted:
ADC 1 FAIL Advisory;
ADC 2 FAIL Advisory;
ADC 1 DEGRADED Advisory;
ADC 2 DEGRADED Advisory;
c) Reversion Switching System is operative,
d) The four pitot-static probes are functional,
including the probe heaters, and
e) TAT probes of the unaffected ADCs are
operative.
NOTE: Transponder and Flight Director/Autopilot
must use same ADC data for RVSM.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2–2
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ ADC 2 FAIL B (O) Aircraft may be dispatched provided:

(Advisory) a) None of the following CAS messages are
also posted:
ADC 1 FAIL Advisory;
ADC 3 FAIL Advisory;
ADC 1 DEGRADED Advisory;
ADC 3 DEGRADED Advisory;
b) Reversion Switching System is operative;
c) The four pitot-static probes are functional,
including the probe heaters, and
d) TAT probes of the unaffected ADCs are
operative.

NOTE: Transponder and Flight Director /

Autopilot must use same ADC data for RVSM.
⇑ ADC 3 FAIL B (O) Aircraft may be dispatched provided:
(Advisory)
a) None of the following CAS messages are
also posted:
ADC 1 FAIL Advisory;
ADC 2 FAIL Advisory;
ADC 1 DEGRADED Advisory;
ADC 2 DEGRADED Advisory;
b) Reversion Switching System is operative;
c) The four pitot-static probes are functional,
including the probe heaters, and
d) TAT probes of the unaffected ADCs are
operative.

NOTE: Transponder and Flight Director /

Autopilot must use same ADC data for RVSM.

⇑ AFCS 1 FAIL C Aircraft may be dispatched provided:

(Advisory) a) AFCS 2 FAIL Advisory message is not also
annunciated, and
b) Approach procedures are not dependent on
its use.

⇑ AFCS 2 FAIL C Aircraft may be dispatched provided:

(Advisory) a) AFCS 1 FAIL Advisory message is not also
annunciated, and
b) Approach procedures are not dependent on
its use.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2–3
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ AP 1 FAIL C Aircraft may be dispatched provided:

(Advisory) a) Approach procedures are not dependent on
its use, and
b) In combination with AP 2 FAIL, intended
flights do not exceed two hours.

⇑ AP 2 FAIL C Aircraft may be dispatched provided:

(Advisory) a) Approach procedures are not dependent on
its use, and
b) In combination with AP 1 FAIL, intended
flights do not exceed two hours.

⇑ AP PITCH TRIM FAIL B Aircraft may be dispatched provided:

(Caution) a) Flight operations do not require the use of
the autopilot,
b) Autopilots are not used, and
c) Provisos associated with AP 1 FAIL and AP
2 FAIL Advisory messages are followed.
NOTE: Use of yaw damper is not affected by
this restriction.
⇑ APU BLEED SYS FAIL C (O) Aircraft may be dispatched provided:
(Caution) a) APU BLEED remains selected OFF,
b) Load control valve is confirmed closed,
c) Following Caution messages are not also
illuminated:
- L BLEED SYS FAIL, and
- R BLEED SYS FAIL

NOTE: All ground engine starts will require

ground air source.
NOTE: APU is still available as a source of
electrical power if required.

⇑ APU DOOR FAIL C Aircraft may be dispatched with APU inlet door
(Caution) fully - OPEN provided:
a) APU is operated continuously during flight,
and
b) AFM performance corrections for APU ON
are applied.
OR
⇑ A Aircraft may be dispatched for one flight day with
APU inlet door partially- OPEN provided APU
wind-milling RPM is monitored per AFM Non-
Normal Procedure for APU DOOR FAIL Caution.
(cont’d)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2–4
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ C (O) Aircraft may be dispatched with APU inlet door

fully CLOSED provided APU is considered
inoperative.

⇑ APU FADEC FAIL C (O) Aircraft may be dispatched provided the system
(Advisory) remains switched OFF and the inlet door is
CLOSED.

⇑ APU FAULT C Aircraft may be dispatched provided:

(Advisory) a) APU allows normal start and shutdown,
b) APU is only used for in-flight emergency,
c) A minimum of three engine electrical
generators are operative,
d) Engines are started by an external power
source.

NOTE: Where APU fault does not allow normal

start and shutdown, APU is to be
considered inoperative.
OR
⇑
C Aircraft may be dispatched provided APU is
considered inoperative and not used.

⇑ APU FIRE FAIL C Aircraft may be dispatched provided the APU is

(Caution) considered inoperative and is NOT used.

⇑ APU FIRE FAULT C (O) Aircraft may be dispatched provided the APU fire
(Advisory) test is conducted prior to each use of the APU.

⇑ C Aircraft may be dispatched provided the APU is

considered inoperative and is not used.

⇑ APU FUEL SOV C (O) Aircraft may be dispatched provided APU fuel
(Caution) valve is deactivated and visually confirmed
CLOSED.

⇑ APU GEN FAIL C Aircraft may be dispatched provided:

(Advisory) a) GEN #1, #2, #3 and #4 are operative, and
b) APU GEN SW is selected OFF.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2–5
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ APU NOT AVAILABLE C (O) Aircraft may be dispatched provided the system
(Advisory) remains switched OFF and the inlet door is
CLOSED.

⇑ APU OIL HI TEMP C (O) Aircraft may be dispatched provided the system
(Caution) remains switched OFF and the inlet door is
CLOSED.

⇑ APU OIL LO PRESS C (O) Aircraft may be dispatched provided the system
(Caution) remains switched OFF and the inlet door is
CLOSED.

⇑ APU OIL LO QTY C (O) Aircraft may be dispatched provided the system
(Advisory) remains switched OFF and the inlet door is
CLOSED.

⇑ APU SHUTDOWN C (O) Aircraft may be dispatched provided the system

(Advisory) remains switched OFF and the inlet door is
CLOSED.

⇑ APU SQUIB 1 FAIL C Aircraft may be dispatched provided the APU is

(Advisory) considered inoperative and is not used.
⇑ APU SQUIB 2 FAIL C Aircraft may be dispatched provided the APU is
(Advisory) considered inoperative and is not used.

⇑ ASCB CTLR 1 FAIL B Aircraft may be dispatched provided:

(Advisory) a) None of the following CAS messages are
also displayed:
- ASCB CTLR 2 FAIL Advisory;
- ASCB CTLR 3 FAIL, Advisory;
and
b) IAC 3 is operative.

⇑ ASCB CTLR 2 FAIL B Aircraft may be dispatched provided:

(Advisory) a) None of the following CAS messages are
also displayed:
- ASCB CTLR 1 FAIL Advisory;
- ASCB CTLR 3 FAIL Advisory,
and
b) IAC 3 is operative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2–6
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ ASCB CTLR 3 FAIL B Aircraft may be dispatched provided none of the

(Advisory) following CAS messages are also displayed:
- ASCB CTLR 1 FAIL Advisory; and
- ASCB CTLR 2 FAIL Advisory.

⇑
AUTOBRAKE FAIL C Aircraft may be dispatched provided:
(Caution) a) Autobrake selector switch remains in the OFF
position, and
b) BRAKE FAULT Advisory is not also
annunciated.

⇑ AVIONIC FAN FAIL C (O) Aircraft may be dispatched provided one or both
(Advisory) air conditioning packs are operated during ground
(GX only) operation.
NOTES:
Minimize utilization of equipment in the
avionics bay without air conditioning and fans
during engine start and shutdown.
If only one air conditioning pack is operating,
passenger door opening should be minimized.

⇑ CHECK DU 4 B (O) Aircraft may be dispatched provided:

(Caution) a) Display unit #4 is considered inoperative,
b) All remaining displays are operative, and
c) Reversion switching system is verified
operative.

⇑ CHECKLIST MISMATCH D Aircraft may be dispatched provided

(Advisory) a) Electronic checklist 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 NO:
2–7
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ CPLT BRAKE FAULT A Aircraft may be dispatched for one flight day
(Caution) provided:
a) None of the following CAS messages are also
displayed:
- PLT BRAKE FAULT Caution;
- L (R) REV LOCK FAIL Caution;
- L (R) REVERSER FAIL Caution;
- NOSE STEER FAIL Caution,
- BRAKE FAULT Advisory;
- L (R) REV LOCK FAULT Advisory;
- L (R) REVERSER FAULT Advisory;
- FLT SPOILERS FAULT Advisory; and
- GND LIFT DUMP Advisory;
b) Takeoff and landing limited to dry runway
operations only,
c) Multiply normal T/O field length by 2.1,
d) Takeoff and landing tailwind component
limited to no more than 3 knots,
e) Maximum cross-winds limited to 10 kts for
both T/O and landing, and
f) Multiply landing field length by 2.2.

⇑ CTR FUELXFER FAIL C Aircraft may be dispatched provided the center

(Caution) tank remains empty.

⇑ C Aircraft may be dispatched provided remaining

fuel in center tank is considered as unusable fuel.

⇑ CTR XFER FAULT C (O) Aircraft may be dispatched provided:

(Advisory) a) Opposite DC AUX pump is operative,
b) Opposite wing transfer SOV is operative,
c) Cross-feed valve is verified operative prior to
each dispatch,
d) Any failure causing continuous center
transfer pump operation is de-activated via
EMS CDU power to the affected transfer
pump, and
e) Where mission requirements utilize fuel in the
center tank, fuel planning considers that the
quantity in the wing tanks is adequate to
reach a suitable or alternate destination if the
remaining center pump fails at any time.

⇑ C Aircraft may be dispatched provided the center

wing tank remains empty.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2–8
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ ELEC SYS FAULT C Aircraft may be dispatched provided the ELEC

(Advisory) SYS FAIL Caution message is not annunciated.

⇑ EVS DEFOG FAULT C Aircraft may be dispatched providing the EVS

(Advisory) image is acceptable to the pilot.

NOTE: The EVS image may degrade in high humidity

condition, to the point of disappearance, as the
IR Window misting increases.
OR
⇑ C Aircraft may be dispatched provided provisos
associated with EVS HEAT FAIL are observed.

⇑ EVS FAIL D (O) Aircraft may be dispatched provided:

(Caution) a) EVS is considered inoperative and is not
used, and
b) EVS HEAT FAIL and EVS HEAT OVHT
Caution messages are not annunciated.

⇑ EVS HEAT FAIL C (O) Aircraft may be dispatched provided:

(Caution)
a) EVS ice protection is deactivated.
b) Operations are not conducted in known or
forecast icing conditions, and
c) Ice detection system is operative.

NOTE: With IR Window heat inoperative, the EVS

image may degrade in high humidity conditions, to the
point of disappearance, as IR Window misting
increases.
⇑ EVS HEAT OVHT C (O) Aircraft may be dispatched provided:
(Caution) a) EVS ice protection is deactivated.
b) Operations are not conducted in known or
forecast icing conditions, and
c) Ice detection system is operative.
NOTE: With IR Window heat inoperative, the EVS
image may degrade in high humidity conditions,
to the point of disappearance, as IR Window
misting increases.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2–9
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ FDR ACCEL FAIL A Aircraft may be dispatched provided:

(Advisory) a) Cockpit Voice Recorder (CVR) operates
normally, and
b) Repairs are made within twenty flight days

⇑ FDR FAIL A (O) Aircraft may be dispatched provided:

(Advisory) a) Cockpit Voice Recorder (CVR) is verified
operative, and
b) Repairs are made within three flight days.

⇑ FLAP HALFSPD B (O) Aircraft may be dispatched provided SLAT

(Advisory) HALFSPD Advisory or SLAT FAIL Caution
messages are not also posted.
(relief limited to SFCU
p/n GT415-5900-13 & sub)
NOTE: If NO TAKEOFF Advisory message is
posted when aircraft is correctly configured
for take-off and throttles are advanced,
dispatch is not permitted.
NOTE: Flap system will operate at half speed

⇑ FMS 2 FAIL C Aircraft may be dispatched provided that in

(Advisory) combination with any other long-range navigation
source failures, unit is not required to meet
regulatory requirements.

⇑ FMS 3 FAIL C Aircraft may be dispatched provided that in

(Advisory) combination with any other long-range navigation
source failures, unit is not required to meet
regulatory requirements.

⇑ FUEL TEMP SENSOR C (O) Aircraft may be dispatched provided:

(Caution) a) Only one bulk fuel temperature indication on
the FUEL Synoptic page is affected, and
b) AFM Non-Normal procedures are followed for
the respective conditions of amber or dashed
temperature indication, when the FUEL
TEMP SENSOR message is present during
flight.
NOTE: WING FUEL LO TEMP and WING FUEL
HI TEMP caution messages will not operate
for the affected system.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 10
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ GEAR SYS FAIL A (O) Aircraft may be dispatched for one flight day,
(Caution) provided:
a) All gear doors (not attached to gear leg) close
normally,
b) Approved ground lock-pins are installed (flags
removed) for flight, and
c) None of the following CAS messages are
also displayed:
- WOW FAULT Advisory;
- ICE DETECTOR FAULT Advisory;
- ICE DETECTOR FAIL Caution;
- L PACK FAIL Caution;
- R PACK FAIL Caution;
d) If GEAR DISAGREE Caution is annunciated
during flight, nosewheel steering is to be
selected OFF for landing.

⇑ GEAR SYS FAULT A Aircraft may be dispatched for one flight day,
(Advisory) provided flights are conducted with gear locked
down and in accordance with all provisos of
GEAR SYS FAIL Caution relief.

⇑ GND PROX FAIL A Aircraft may be dispatched provided:

(Advisory) a) Alternate procedures are established and
used, and
b) Repairs are made within two flight days

⇑ GPWS SYSTEMS FAIL A Aircraft may be dispatched provided:

(Advisory) a) Alternate procedures are established and
used,
b) Repairs are made within two flight days, and
c) Takeoffs and landings are not conducted in
known or forecast windshear conditions.

⇑ HUD FAIL D Aircraft may be dispatched provided,

(Caution) a) Approach procedures are not dependent on
its use, and
b) HUD is selected OFF and stowed.

⇑
HUD FAN FAIL D (O) Aircraft may be dispatched provided:
(Advisory) a) Approach procedures are not dependent on
its use, and
b) HUD is selected OFF, deactivated and
stowed.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 11
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ HUD MISALIGN D Aircraft may be dispatched provided:

(Advisory) a) Approach procedures are not dependent on
use of HUD,
b) HUD is considered unuseable and not used,
and
c) HUD is selected OFF and stowed.

⇑ HUMIDIFER FAIL C (O) Aircraft may be dispatched provided

(Advisory) a) System is deactivated,
b) Neither L PACK FAIL or R PACK FAIL
Caution messages are also annunciated,
c) TRIM AIR switch is selected and remains
OFF,
d) HASOVs are indicated closed on Synoptic
Page, and
e) Extended periods of aircraft in-operation or
ground handling during freezing temperatures
must be avoided to prevent system damage
due to possible freezing of water trapped in
the system.

NOTE: Potential freezing is not of concern

provided ECS is operating.

NOTE: Overnight parking in hangar should be

considered where freezing temperatures
are forecast.

⇑ HYD PUMP 3A FAIL B (O) Aircraft may be dispatched provided:

(Advisory) a) Affected pump is switched OFF,
b) Remaining system 3B AC motor pump is
operated continuously during flight, and
c) All other hydraulic pumps are operative.

⇑ HYD PUMP 3B FAIL B (O) Aircraft may be dispatched provided:

(Advisory) a) Affected pump is switched OFF,
b) Remaining system 3A AC motor pump is
operated continuously during flight, and
c) All other hydraulic pumps are operative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 12
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ IAC 3 INVALID B (O) Aircraft may be dispatched provided:

(Advisory) a) IAC #3 is deactivated,
b) SG 3 switch on reversion control panel
remains selected to ALTN,
c) Reversion switching system is verified
operative,
d) All EICAS displays are operative, and
e) Both AP Quick DISC buttons, and both A/T
Disengage switches are operative.
NOTE: Subsequent loss of IAC #1 or #2 results
in loss of three display units, one
Autothrottle system, one Yaw Damper
system, one Autopilot system, one Flight
Director, and one FMS.

⇑ IAC 3 OVHT B (O) Aircraft may be dispatched provided:

(Caution) a) IAC #3 remains deactivated,
b) Operations are conducted with SG 3 switch
in the ALTN position,
c) Reversion switching system is verified
operative,
d) All EICAS displays are operative, and
e) Both AP Quick DISC buttons, and both A/T
Disengage switches are operative.

NOTE: Subsequent loss of IAC #1 or #2

results in loss of three display units, one
Autothrottle system, one Yaw Damper
system, one Autopilot system, one Flight
Director, and one FMS.

⇑ ICE C Aircraft may be dispatched provided:

(Caution) a) When WING ANTI-CE knob is selected to
ON, none of the following messages are
displayed;
- L WING A/I FAIL Caution;
- R WING A/I FAIL Caution;
- L COWL A/I FAIL Caution;
- R COWL A/I FAIL Caution;
- L COWL A/I FAULT Advisory,
- R COWL A/I FAULT Advisory;
and
b) Aircraft is not dispatched into known or
forecast icing conditions.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 13
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ ICE DETECTOR FAIL C (O) Aircraft may be dispatched provided operations

(Caution) are not conducted in known or forecast icing
conditions.

⇑ ICE DETECTOR FAULT C Aircraft may be dispatched provided wing and

(Advisory) cowl anti-ice systems are turned ON when icing
conditions as defined in the AFM exist or are
anticipated.

⇑ INT CABIN DOOR C (O) Aircraft may be dispatched provided, prior to take
(Caution) off and landing, the door is physically verified fully
open.

⇑ IRS 1 AUX FAIL C Aircraft may be dispatched provided no other IRS

(Advisory) AUX PWR, IRS AUX FAIL or IRS FAIL messages
are posted.

⇑ IRS 1 AUX PWR C Aircraft may be dispatched provided no other IRS

(Advisory) AUX PWR, IRS AUX FAIL or IRS FAIL messages
are posted.

⇑ IRS 1 FAIL C (O) Aircraft may be dispatched provided:

(Advisory) a) Independent attitude indication is available at
each pilot’s station,
b) Independent directional compass indication is
available at each pilot’s station,
c) Standby Attitude Indicator is operative, and
d) IRS 2 FAIL and IRS 3 FAIL are not
annunciated.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 14
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ IRS 1 MISCMP C (O) Aircraft may be dispatched provided:

(Caution) a) None of the following CAS messages are
also posted:
- IRS 2 MISCMP Caution,
- IRS 3 MISCMP Caution;
- IRS 2 FAIL Caution;
- IRS 3 FAIL Caution;
b) Independent attitude indication is available
at each pilot’s station,
c) Independent directional compass indication
is available at each pilot’s station,
d) Standby Attitude Indicator is operative.

NOTE: If miscompare cannot be cleared

through re-alignment, the IRS should be de-
activated.

⇑ IRS 1 OVHT C (O) Aircraft may be dispatched provided:

(Caution) a) IRS 1 remains deactivated,
b) Independent attitude indication is available
at each pilot’s station,
c) Independent directional compass indication
is available at each pilot’s station,
d) Standby Attitude Indicator is operative, and
e) IRS 2 and IRS 3 are operative.

⇑ IRS 2 AUX FAIL C Aircraft may be dispatched provided no other IRS

(Advisory) AUX PWR, IRS AUX FAIL or IRS FAIL messages
are posted.

⇑
IRS 2 AUX PWR C Aircraft may be dispatched provided no other IRS
(Advisory) AUX PWR, IRS AUX FAIL or IRS FAIL messages
are posted.

⇑ IRS 2 FAIL C (O) Aircraft may be dispatched provided:

(Advisory) a) Independent attitude indication is available
at each pilot’s station,
b) Independent directional compass indication
is available at each pilot’s station,
c) Standby Attitude Indicator is operative, and
d) IRS 1 FAIL and IRS 3 FAIL are not
annunciated.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 15
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ IRS 2 MISCMP C (O) Aircraft may be dispatched provided:

(Caution) a) None of the following CAS messages are
also posted:
- IRS 1 MISCMP Caution,
- IRS 3 MISCMP Caution;
- IRS 1 FAIL Caution;
- IRS 3 FAIL Caution;
b) Independent attitude indication is available
at each pilot’s station,
c) Independent directional compass indication
is available at each pilot’s station,
d) Standby Attitude Indicator is operative.

NOTE: If miscompare cannot be cleared

through re-alignment, the IRS should be de-
activated.

⇑ IRS 2 OVHT C (O) Aircraft may be dispatched provided:

(Caution) a) IRS 2 remains deactivated,
b) Independent attitude indication is available
at each pilot’s station,
c) Independent directional compass indication
is available at each pilot’s station,
d) Standby Attitude Indicator is operative, and
e) IRS 1 and IRS 3 are operative.

⇑ IRS 3 AUX FAIL C Aircraft may be dispatched provided no other IRS

(Advisory) AUX PWR, IRS AUX FAIL or IRS FAIL messages
are posted.

⇑ IRS 3 AUX PWR

(Advisory)
C Aircraft may be dispatched provided no other IRS
AUX PWR, IRS AUX FAIL or IRS FAIL messages
are posted.

⇑ IRS 3 FAIL C (O) Aircraft may be dispatched provided:

(Advisory) a) Independent attitude indication is available
at each pilot’s station,
b) Independent directional compass indication
is available at each pilot’s station,
c) Standby Attitude Indicator is operative, and
d) IRS 1 FAIL and IRS 2 FAIL are not
annunciated.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 16
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ IRS 3 MISCMP C (O) Aircraft may be dispatched provided:

(Caution) a) None of the following CAS messages are
also posted:
- IRS 1 MISCMP Caution,
- IRS 2 MISCMP Caution;
- IRS 1 FAIL Caution;
- IRS 2 FAIL Caution;
b) Independent attitude indication is available
at each pilot’s station,
c) Independent directional compass indication
is available at each pilot’s station,
d) Standby Attitude Indicator is operative.

NOTE: If miscompare cannot be cleared

through re-alignment, the IRS should be de-
activated.

⇑ IRS 3 OVHT C (O) Aircraft may be dispatched provided:

(Caution) a) IRS 3 remains deactivated,
b) Independent attitude indication is available
at each pilot’s station,
c) Independent directional compass indication
is available at each pilot’s station, and
d) Standby Attitude Indicator is operative, and
e) IRS 1 and IRS 2 are operative.

⇑ L AUX FUEL PUMP C (O) Aircraft may be dispatched provided:

(Advisory) a) Left AUX pump is de-activated,
(GX) b) Right centre transfer pump is operative,
c) Right aft tank transfer pump is operative,
d) Right aft tank transfer SOV is operative,
e) Right wing transfer SOV is operative,
f) XFEED FAIL Caution is not posted,
g) L PRI FUEL PUMP Advisory is not posted,
and
h) An extra 1,000 pounds of fuel is carried for
the planned flight.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 17
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ L AUX FUEL PUMP C (O) Aircraft may be dispatched provided:

(Advisory) a) Left AUX pump is de-activated,
(G5000 only) b) Right centre transfer pump is operative,
c) Right wing transfer SOV is operative,
d) XFEED FAIL Caution is not posted,
e) L PRI FUEL PUMP Advisory is not posted,
and
f) An extra 1,000 pounds of fuel is carried for
the planned flight.

⇑ L BLEED FAULT C (O) Aircraft may be dispatched provided, prior to each

(Advisory) flight:
a) None of the following messages are also
posted:
- R BLEED SYS FAIL Caution;
- R WING ANTI-ICE FAIL Caution;
- XBLEED FAIL Caution;
- R BLEED FAULT Advisory;
- WING ANTI-ICE FAULT Advisory;
b) Left PRV and HP SOV open and close
correctly in response to L BLEED OFF switch
selection, as indicated on Synoptic Page, and
c) Left HP valve is open at engine idle and
closed at high thrust settings, as indicated on
Synoptic Page.

⇑ L ENG FIRE FAULT A Aircraft may be dispatched for one flight day
(Advisory) provided the Fire Test is conducted before each
flight.

⇑ C Aircraft may be dispatched provided:

a) Fire test is conducted before each flight, and
b) Operations are conducted not more than 60
minutes from a suitable airport.

⇑ L FADEC FAULT A May be dispatched with FADEC faults provided

(Advisory) repairs are made in accordance with times
established by engine manufacturer.
No extensions are allowed.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 18
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ L PACK AUTO FAIL C (O) Aircraft may be dispatched provided:

(Caution) a) Left pack is selected OFF and the FCV is
(GX) verified closed on Synoptic Page,
b) Right pack discharge temperature
indications on Synoptic Page are operative,
c) Right pack is verified operative in MAN
mode,
d) Right pack is operated in AUTO mode,
e) Avionics Bay fan is selected OFF,
f) Recirculation system is verified operative,
g) AUX PRESS system is verified operative,
h) TRIM AIR is selected OFF,
i) RAM Air valve is verified operative,
j) None of the following CAS messages are
also posted:
i) L BLEED SYS FAIL Caution;
ii) R BLEED SYS FAIL Caution;
iii) L BLEED LEAK Caution;
iv) R BLEED LEAK Caution;
v) R PACK TEMP Caution;
vi) X BLEED FAIL Caution;
vii) R BLEED FAULT Advisory;
viii) R PACK FAULT Advisory;
and
k) Operations are conducted at or below
FL410.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 19
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ L PACK AUTO FAIL C (O) Aircraft may be dispatched provided:

(Caution) a) Left pack is selected OFF and the FCV is
(Global 5000) verified closed on Synoptic Page,
b) Right pack discharge temperature
indications on Synoptic Page are operative,
c) Right pack is verified operative in MAN mode,
d) Right pack is operated in AUTO mode,
e) Avionics Bay fan is selected OFF,
f) Recirculation system is verified operative,
g) AUX PRESS system is verified operative,
h) TRIM AIR is selected OFF,
i) RAM Air valve is verified operative,
j) None of the following CAS messages are
also posted:
i) L BLEED SYS FAIL Caution;
ii) R BLEED SYS FAIL Caution;
iii) L BLEED LEAK Caution;
iv) R BLEED LEAK Caution;
v) R PACK TEMP Caution;
vi) X BLEED FAIL Caution;
vii) R BLEED FAULT Advisory;
viii) R PACK FAULT Advisory;
ix) AV RACK FAN FAIL Advisory;
and
k) Operations are conducted at or below FL 410.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 20
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ L PACK FAIL C (O) Aircraft may be dispatched provided:

(Caution) a) Left pack is selected OFF,
(GX) b) Left FCV is visually verified closed in aft
equipment bay,
c) Right pack discharge temperature
indications on Synoptic Page are operative,
d) Right pack is verified operative in MAN
mode,
e) Right pack FCV opens and closes correctly in
response to PACK OFF switch,
f) Right pack is operated in AUTO mode,
g) Avionics Bay fan is selected OFF,
h) Recirculation system is verified operative,
i) AUX PRESS system is verified operative,
j) TRIM AIR is selected OFF,
k) RAM Air valve is verified operative,
l) None of the following CAS messages are
also posted:
i) R BLEED FAULT Advisory;
ii) R PACK FAULT Advisory;
iii) L BLEED SYS FAIL Caution;
iv) R BLEED SYS FAIL Caution;
v) L BLEED LEAK Caution;
vi) R BLEED LEAK Caution;
vii) R PACK TEMP Caution;
viii) R PACK AUTO FAIL Caution;
ix) XBLEED FAIL Caution;
and
m) Operations are conducted at or below FL410.

Note: If pack closure cannot be confirmed on

synoptic, then manual closure and lock-out
is required prior to dispatch.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 21
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ L PACK FAIL C (O) Aircraft may be dispatched provided:

(Caution) a) Left pack is selected OFF,
(Global 5000) b) Left FCV is visually verified closed in aft
equipment bay,
c) Right pack discharge temperature
indications on Synoptic Page are operative,
d) Right pack is verified operative in MAN
mode,
e) Right pack FCV opens and closes correctly
in response to PACK OFF switch,
f) Right pack is operated in AUTO mode,
g) Avionics Bay fan is selected OFF,
h) Recirculation system is verified operative,
i) AUX PRESS system is verified operative,
j) TRIM AIR is selected OFF,
k) RAM Air valve is verified operative,
l) None of the following CAS messages are
also posted:
i) L BLEED SYS FAIL Caution;
ii) R BLEED SYS FAIL Caution;
iii) L BLEED LEAK Caution;
iv) R BLEED LEAK Caution;
v) R PACK TEMP Caution;
vi) R PACK AUTO FAIL Caution;
vii) XBLEED FAIL Caution;
viii) R BLEED FAULT Advisory;
ix) R PACK FAULT Advisory;
x) AV RACK FAN FAIL Advisory,
and
m) Operations are conducted at or below FL 410.

Note: If pack closure cannot be confirmed on

synoptic, then manual closure and lock-out
is required prior to dispatch.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 22
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ L PACK FAULT C Aircraft may be dispatched provided, prior to each

(Advisory) dispatch:
a) The following messages are not also posted:
i) R PACK FAULT Advisory,
ii) L BLEED FAULT Advisory,
iii) L BLEED FAIL Caution,
iv) R PACK AUTO FAIL Caution,
v) R PACK FAIL Caution,
and
b) With bleed air on, left flow control valve
correctly closes and re-opens in response to
pack OFF / ON selection, as confirmed on the
Synoptic Page.

⇑ L PRI FUEL PUMP C (O) Aircraft may be dispatched provided:

(Advisory) a) None of the fllowing CAS messages are also
posted:
- L AUX FUEL PUMP Advisory;
- R AUX FUEL PUMP Advisory;
- R PRI FUEL PUMP Advisory;
b) Aft position L PRI pump is operative as
indicated on FUEL Synoptic Page,
c) All fuel quantity indications are operative, and
d) XFEED SOV is verified operative prior to
each dispatch.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 23
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ L PROBE MON FAIL B (O) Aircraft may be dispatched provided:

(Advisory) a) Neither ICE DETECTOR FAULT Advisory or
ICE DETECTOR FAIL Caution messages
are displayed,
b) Operations are not conducted in known or
forecast icing conditions,
c) Operations are conducted under day VMC
only,
d) Dispatch provisos and procedures
associated with YD HEAT1 FAIL, herein,
are carried out, and
e) Enroute operations do not require its use.

NOTE: Both inboard and outboard left brake

temperature indications on the EICAS
STATUS Page will be inoperative.

OR

⇑ B (O) In combination with R PROBE MON FAIL

message, aircraft may be dispatched provided:
a) Neither ICE DETECTOR FAULT Advisory
or ICE DETECTOR FAIL Caution messages
are displayed,
b) Operations are not conducted in known or
forecast icing conditions,
c) Operations are conducted under day VMC
only,
d) Dispatch provisos and procedures
associated with YD HEAT1 FAIL and YD
HEAT 2 FAIL, herein, are carried out, and
e) Enroute operations do not require its use.

NOTE: With both messages posted, all brake

temperature indications on the EICAS
STATUS Page will be inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 24
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ L WING A/ICE FAIL C Aircraft may be dispatched provided:

(Caution) a) Anti-Ice “WING” rotary switch is selected to
the OFF position and the valves confirmed
closed on the Synoptic Page,
b) ICE DETECTOR FAULT Advisory and/or
ICE DETECTOR FAIL Caution messages
are not also posted, and
c) Operations are not conducted in known or
forecast icing conditions.

⇑ L WSHLD HEAT FAIL C (O) Aircraft may be dispatched provided:

(Caution) a) Remaining channels are verified operative
by selecting both WINDSHIELD HEAT
switches to ON, and confirming none of the
following messages are annunciated by the
CAS:
- R WSHLD HEAT FAIL Caution;
- R WINDOW HEAT FAIL Caution;
- L WINDOW HEAT FAIL Caution;
and
b) Operations are not conducted in known or
forecast icing
OR
⇑ C (O) In conjunction with other window heat channel
failures, the aircraft may be dispatched provided:
a) Only one of the following messages are
annunciated,
- R WSHLD HEAT FAIL Caution;
- R WINDOW HEAT FAIL Caution;
b) Operations are not conducted in known or
forecast icing, and
c) Both ice detection systems are operative.
.
⇑ LARGE SERV DOOR C (O) Aircraft may be dispatched provided prior to each
(Caution) flight, Aft Equipment Bay Door, Refuel/Defuel
Station door, and Rear Hydraulic System Access
door, (and Optional Belly Fairing door) are verified
CLOSED, LATCHED and LOCKED.

⇑ LTRK FAIL C Aircraft may be dispatched provided two FMSs are

(Advisory) operative.

⇑ MAN PRESS FAULT A (O) Aircraft may be dispatched for one flight day,
(Advisory) provided flight is conducted in accordance with
AFM for unpressurized flight configuration, at or
below 9,000 ft MSL.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 25
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ MLG BAY OVHT FAIL B Aircraft may be dispatched provided:

(Caution) a) Landing gear is left extended for ten
minutes following take-off unless there is an
engine failure,
b) Brake Temperature Monitoring System is
fully functional, and
c) BTMS indications are monitored after take-
off and gear is not retracted until indications
show 09 or below and decreasing, and
d) Operations are conducted in accordance
with AFM Supplement for Dispatch With
Landing Gear Inoperative while gear
remains extended.

⇑ MLG BAY OVHT FAULT B Aircraft may be dispatched provided:

(Advisory) a) Landing gear is left extended for ten
minutes following take-off unless there is an
engine failure,
b) Brake Temperature Monitoring System is
fully functional, and
c) BTMS indications are monitored after take-
off and gear is not retracted until indications
show 09 or below and decreasing, and
d) Operations are conducted in accordance
with AFM Supplement for Dispatch With
Landing Gear Inoperative while gear
remains extended.

⇑ OUTFLOW VLV 1 FAIL C (O) Aircraft may be dispatched provided

(Advisory) a) Forward outflow valve is verified fully OPEN,
b) AFM Buoyancy Limitations are observed
with respect to take-offs and landings near
bodies of water, and
c) Flight is conducted in accordance with AFM
for an unpressurized flight configuration at
or below 9,000 ft MSL

⇑ OUTFLOW VLV 2 FAIL C (O) Aircraft may be dispatched provided

(Advisory) f) Aft outflow valve is verified OPEN,
g) AFM Buoyancy Limitations are observed
with respect to take-offs and landings near
bodies of water, and
h) Flight is conducted in accordance with AFM
for an unpressurized flight configuration at
or below 9,000 ft MSL
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 26
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ OXYGEN LO QTY B (O) Aircraft may be dispatched provided:

(Caution) a) Minimum oxygen quantity prior to dispatch
is greater than 50 %,
b) Minimum Enroute Altitude (MEA) shall not
exceed 10, 000 ft MSL, and
c) Quantity for dispatch is in accordance with
applicable operating rules and the
Bombardier Completions Center Oxygen
System Supplement in the FCOM
Supplementary Procedures.

⇑ PITOT 2 HT FAIL B (O) Except where operations require its use, including
(Caution) RVSM, aircraft may be dispatched provided:
a) ADC # 2 is de-activated,
b) None of the following CAS messages are
also displayed:
- PITOT 1 HT FAIL Caution;
- PITOT 3 HT FAIL Caution;
- STBY PITOT HT FAIL Caution;
- TAT HT 1 FAIL Caution;
- TAT HT 3 FAIL Caution;
- ICE DETECTOR FAIL Caution;
- ADC 1 FAIL Advisory;
- ADC 1 DEGRADED Advisory;
- ADC 3 FAIL Advisory;
- ADC 3 DEGRADED Advisory;
- ICE DETECTOR FAULT Advisory;
c) Operations are not conducted in known or
forecast icing conditions,
d) Operations are not conducted in visible
moisture in any form,
e) Reversion Switching System is operative, and
f) Operations are conducted in day VMC
conditions only.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 27
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ PITOT 3 HT FAIL B (O) Except where operations require its use, including
(Caution) RVSM, aircraft may be dispatched provided:
a) ADC # 3 is de-activated,
b) None of the following CAS messages are
also displayed:
- PITOT 1 HT FAIL Caution;
- PITOT 2 HT FAIL Caution;
- STBY PITOT HT FAIL Caution;
- TAT HT 1 FAIL Caution;
- TAT HT 2 FAIL Caution;
- ICE DETECTOR FAIL Caution;
- ADC 1 FAIL Advisory;
- ADC 1 DEGRADED Advisory;
- ADC 2 FAIL Advisory;
- ADC 2 DEGRADED Advisory;
- ICE DETECTOR FAULT Advisory;
a) Operations are not conducted in known or
forecast icing conditions,
b) Operations are not conducted in visible
moisture in any form,
c) Reversion Switching System is operative, and
d) Operations are conducted in day VMC
conditions only

⇑ PLT BRAKE FAULT A Aircraft may be dispatched for one flight day
(Caution) provided:
a) None of the following CAS messages are also
posted:
- CPLT BRAKE FAULT Caution;
- L (R) REV LOCK FAIL Caution;
- L (R) REVERSER FAIL;
- NOSE STEER FAIL Caution;
- BRAKE FAULT Advisory;
- L (R) REV LOCK FAULT Advisory;
- L (R) REVERSER FAULT advisory;
- FLT SPOILERS FAULT Advisory;
- GND LIFT DUMP Advisory;
b) Takeoff and landing limited to dry runway
operations only,
c) Multiply normal T/O field length by 2.1,
d) Takeoff and landing tailwind component
limited to no more than 3 knots,
e) Maximum cross-winds limited to 10 kts for
both T/O and landing, and
f) Multiply landing field length by 2.2.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 28
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ R AUX FUEL PUMP C (O) Aircraft may be dispatched provided:

(Advisory) a) Right AUX pump is de-activated,
(GX) b) Left centre transfer pump is operative,
c) Left aft tank transfer pump is operative,
d) Left aft tank transfer SOV is operative,
e) Left wing transfer SOV is operative,
f) XFEED FAIL Caution is not posted,
g) R PRI FUEL PUMP Advisory is not posted, and
h) An extra 1,000 pounds of fuel is carried for the
planned flight.
⇑ R AUX FUEL PUMP Aircraft may be dispatched provided:
C (O)
(Advisory) a) Right AUX pump is de-activated,
(G5000 only) b) Left centre transfer pump is operative,
c) Left wing transfer SOV is operative,
d) XFEED FAIL Caution is not posted,
e) R PRI FUEL PUMP Advisory is not posted, and
f) An extra 1,000 pounds of fuel is carried for the
planned flight.

⇑ R BLEED FAULT C (O) Aircraft may be dispatched provided, prior to each

(Advisory) flight:
a) None of the following messages are also
posted:
- L BLEED SYS FAIL Caution;
- L WING ANTI-ICE FAIL Caution;
- XBLEED FAIL Caution;
- L BLEED FAULT Advisory;
- WING ANTI-ICE FAULT Advisory;
b) Right PRV and HP SOV open and close
correctly in response to L BLEED OFF switch
selection, as indicated on Synoptic Page, and
c) Right HP valve is open at engine idle and
closed at high thrust settings, as indicated on
Synoptic Page.

⇑ R ENG FIRE FAULT A Aircraft may be dispatched for one flight day
(Advisory) provided the Fire Test is conducted before each
flight.

C Aircraft may be dispatched provided:

a) Fire test is conducted before each flight, and
b) Operations are conducted not more than 60
minutes from a suitable airport.
⇑ R FADEC FAULT A May be dispatched with FADEC faults provided
(Advisory) repairs are made in accordance with times
established by engine manufacturer.
No extensions are allowed.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 – 29
BD--700-1A10 / -1A11 DATE: 06/27/2009

1. 2.
CAS Indication Dispatch Consideration

⇑ R PACK AUTO FAIL C (O) Aircraft may be dispatched provided:

(Caution) a) Right pack is selected OFF and the FCV is
(GX) verified closed on Synoptic Page,
b) Left pack discharge temperature indications
on Synoptic Page are operative,
c) Left pack is verified operative in MAN mode,
d) Left pack is operated in AUTO mode,
e) Avionics Bay fan is selected OFF,
f) Recirculation system is verified operative,
g) AUX PRESS system is verified operative,
h) TRIM AIR is selected OFF,
i) RAM Air valve is verified operative,
j) None of the following CAS messages are
also posted:
i) L BLEED SYS FAIL Caution;
ii) R BLEED SYS FAIL Caution;
iii) L BLEED LEAK Caution;
iv) R BLEED LEAK Caution;
v) L PACK TEMP Caution;
vi) X BLEED FAIL Caution;
vii) L BLEED FAULT Advisory;
viii) L PACK FAULT Advisory;
and
k) Operations are conducted at or below FL410.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 - 30
BD--700-1A10 / -1A11 DATE: 06/27/2009
1. 2.
CAS Indication Dispatch Consideration

⇑ R PACK AUTO FAIL C (O) Aircraft may be dispatched provided:

(Caution) a) Right pack is selected OFF and the FCV is
(Global 5000) verified closed on Synoptic Page,
b) Left pack discharge temperature
indications on Synoptic Page are
operative,
c) Left pack is verified operative in MAN
mode,
d) Left pack is operated in AUTO mode,
e) Avionics Bay fan is selected OFF,
f) Recirculation system is verified operative,
g) AUX PRESS system is verified operative,
h) TRIM AIR is selected OFF,
i) RAM Air valve is verified operative,
j) None of the following CAS messages are
also posted:
i) L BLEED SYS FAIL Caution;
ii) R BLEED SYS FAIL Caution;
iii) L BLEED LEAK Caution;
iv) R BLEED LEAK Caution;
v) L PACK TEMP Caution;
vi) X BLEED FAIL Caution;
vii) L BLEED FAULT Advisory;
viii) L PACK FAULT Advisory;
ix) AV RACK FAN FAIL Advisory;
and
k) Operations are conducted at or below FL410.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 - 31
BD--700-1A10 / -1A11 DATE: 06/27/2009
1. 2.
CAS Indication Dispatch Consideration

⇑ R PACK FAIL C (O) Aircraft may be dispatched provided:

(Caution) a) Right pack is selected OFF,
(GX) b) Right FCV is visually verified closed in Aft
Equipment Bay,
c) Left pack discharge temperature
indications on Synoptic Page are
operative,
d) Left pack is verified operative in MAN
mode,
e) Left pack FCV opens and closes correctly
in response to PACK OFF switch,
f) Left pack is operated in AUTO mode,
g) Avionics Bay fan is selected OFF,
h) Recirculation system is verified operative,
i) AUX PRESS system is verified operative,
j) TRIM AIR is selected OFF,
k) RAM Air valve is verified operative,
l) None of the following messages are also
posted:
i) L BLEED SYS FAIL Caution:
ii) R BLEED SYS FAIL Caution:
iii) L BLEED LEAK Caution:
iv) R BLEED LEAK Caution:
v) L PACK TEMP Caution:
vi) L PACK AUTO FAIL Caution:
vii) X BLEED FAIL Caution:
viii) L BLEED FAULT Advisory:
ix) L PACK FAULT Advisory;
and
m) Operations are conducted at or below
FL 410.

Note: If pack closure cannot be confirmed on

synoptic, then manual closure and lock-
out is required prior to dispatch.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 - 32
BD--700-1A10 / -1A11 DATE: 06/27/2009
1. 2.
CAS Indication Dispatch Consideration

⇑ R PACK FAIL C (O) Aircraft may be dispatched provided:

(Caution) a) Right pack is selected OFF,
(Global 5000) b) Right FCV is visually verified closed in aft
equipment bay,
c) Left pack discharge temperature
indications on Synoptic Page are
operative,
d) Left pack is verified operative in MAN
mode,
e) Left pack FCV opens and closes correctly
in response to PACK OFF switch,
f) Left pack is operated in AUTO mode,
g) Avionics Bay fan is selected OFF,
h) Recirculation system is verified operative,
i) AUX PRESS system is verified operative,
j) TRIM AIR is selected OFF,
k) RAM Air valve is verified operative,
l) None of the following CAS messages are
also posted:
i) L BLEED SYS FAIL Caution;
ii) R BLEED SYS FAIL Caution;
iii) L BLEED LEAK Caution;
iv) R BLEED LEAK Caution;
v) L PACK TEMP Caution;
vi) L PACK AUTO FAIL Caution;
vii) X BLEED FAIL Caution;
viii) L BLEED FAULT Advisory;
ix) L PACK FAULT Advisory;
x) AV RACK FAN FAIL Advisory;
and
m) Operations are conducted at or below
FL 410.

Note: If pack closure cannot be confirmed on

synoptic then manual closure and lock-
out is required prior to dispatch.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 - 33
BD--700-1A10 / -1A11 DATE: 06/27/2009
1. 2.
CAS Indication Dispatch Consideration

⇑ R PACK FAULT C Aircraft may be dispatched provided, prior to

(Advisory) each dispatch:
a) The following messages are not also posted:
i) L PACK FAULT Advisory,
ii) R BLEED FAULT Advisory,
iii) R BLEED FAIL Caution,
iv) L PACK AUTO FAIL Caution,
v) L PACK FAIL Caution,
and
b) With bleed air on, right flow control valve
correctly closes and re-opens in response to
pack OFF / ON selection, as confirmed on
the Synoptic Page.

⇑ R PRI FUEL PUMP C (O) Aircraft may be dispatched provided:

(Advisory) a) None of the following CAS messages are
also posted:
- R AUX FUEL PUMP Advisory;
- L AUX FUEL PUMP Advisory;
- L PRI FUEL PUMP Advisory;
b) Aft position R PRI pump is operative as
indicated on FUEL Synoptic Page,
c) All fuel quantity indications are operative,
and
d) XFEED SOV is verified operative prior to
each dispatch.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 - 34
BD--700-1A10 / -1A11 DATE: 06/27/2009
1. 2.
CAS Indication Dispatch Consideration

⇑ R PROBE MON FAIL B (O) Aircraft may be dispatched provided:

(Advisory) a) Neither ICE DETECTOR FAULT Advisory
or ICE DETECTOR FAIL Caution
messages are displayed,
b) Operations are not conducted in known or
forecast icing conditions,
c) Operations are conducted under day VMC
only,
d) Dispatch provisos and procedures
associated with YD HEAT 2 FAIL, herein,
are carried out, and
e) Enroute operations do not require its use.

NOTE: Both inboard and outboard right brake

temperature indications on the EICAS
STATUS Page will be inoperative.

OR

⇑ B (O) In combination with L PROBE MON FAIL

message, aircraft may be dispatched provided:
a) Neither ICE DETECTOR FAULT Advisory
or ICE DETECTOR FAIL Caution
messages are displayed,
b) Operations are not conducted in known or
forecast icing conditions,
c) Operations are conducted under day VMC
only,
d) Dispatch provisos and procedures
associated with YD HEAT1 FAIL and YD
HEAT 2 FAIL, herein, are carried out, and
e) Enroute operations do not require its use.

NOTE: With both messages posted, all brake

temperature indications on the EICAS
STATUS Page will be inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 - 35
BD--700-1A10 / -1A11 DATE: 06/27/2009
1. 2.
CAS Indication Dispatch Consideration

⇑ R WINDOW HEAT FAIL C (O) Aircraft may be dispatched provided:

(Caution) a) Remaining channels are verified operative
by selecting both WINDSHIELD HEAT
switches to ON, and confirming none of
the following messages are annunciated
by the CAS:
- L WSHLD HEAT FAIL Caution;
- L WINDOW HEAT FAIL Caution;
- R WSHLD HEAT FAIL Caution;
and
b) Operations are not conducted in known or
forecast icing

⇑ C (O) In conjunction with other windshield failures, the

aircraft may be dispatched provided:
a) Only one of the following messages are
annunciated,
- L WSHLD HEAT FAIL Caution;
- R WSHLD HEAT FAIL Caution;
and
b) Operations are not conducted in known or
forecast icing, and
c) Both ice detection systems are operative

⇑ R WING A/ICE FAIL C Aircraft may be dispatched provided:

(Caution) a) Anti-Ice “WING” rotary switch is selected to
the OFF position and the valves confirmed
closed on the Synoptic Page,
b) ICE DETECTOR FAULT Advisory and/or
ICE DETECTOR FAIL Caution messages
are not also posted, and
c) Operations are not conducted in known or
forecast icing conditions.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 - 36
BD--700-1A10 / -1A11 DATE: 06/27/2009
1. 2.
CAS Indication Dispatch Consideration

⇑ R WSHLD HEAT FAIL C (O) Aircraft may be dispatched provided:

(Caution)
a) Remaining channels are verified operative
by selecting both WINDSHIELD HEAT
switches to ON, and confirming none of the
following messages are annunciated by the
CAS:
- L WSHLD HEAT FAIL Caution;
- L WINDOW HEAT FAIL Caution;
- R WINDOW HEAT FAIL Caution;
and
b) Operations are not conducted in known or
forecast icing

⇑ C (O) In conjunction with other windshield failures, the

aircraft may be dispatched provided:
a) Only one of the following messages are
annunciated,
- L WSHLD HEAT FAIL Caution;
- R WINDOW HEAT FAIL Caution;
and
b) Operations are not conducted in known or
forecast icing, and
c) Both ice detection systems are operative

⇑ RECIRC FAN FAIL C (O) Aircraft may be dispatched provided neither, L

(Advisory) PACK FAIL or R PACK FAIL Caution messages
are posted.

⇑ SAFETY VALVE OPEN C (O) Aircraft may be dispatched provided:

(Advisory) a) Both air conditioning packs operate
normally,
b) Operations are conducted unpressurized
at or below 9,000 ft MSL,
c) Take-offs and landings are not conducted
on runways near bodies of water, and
d) Extended over-water operations are
prohibited.

⇑ SG 3 FAIL C (O) Aircraft may be dispatched provided:

(Caution) a) SG 3 switch on reversion control panel
remains selected to ALTN,
b) All cockpit displays are operative with the
EFIS and EICAS in normal, and
c) Reversion switching system is verified
operative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 - 37
BD--700-1A10 / -1A11 DATE: 06/27/2009
1. 2.
CAS Indication Dispatch Consideration

⇑ SLAT HALFSPD B (O) Aircraft may be dispatched provided FLAP

(Advisory) HALFSPD Advisory and/or FLAP FAIL Caution
messages are not also posted.
(relief limited to SFCU
p/n GT415-5900-13 & sub)
NOTE: If NO TAKEOFF Advisory message is
posted when aircraft is correctly
configured for take-off and throttles are
advanced, dispatch is not permitted.

NOTE: Slat system will operate at half speed

⇑ SLAT – FLAP BIT C Aircraft may be dispatched.

(Advisory)

⇑ SMALL SERV DOOR C (O) Aircraft may be dispatched provided prior to

(Caution) each flight, all small service doors are verified
CLOSED, LATCHED and LOCKED.

⇑ SMOKE AFT LAV FAIL C (O) Aircraft may be dispatched provided:

(Caution) a) Lavatory is not used by passengers for any
purpose,
b) Lavatory waste receptacle is empty,
c) Lavatory door is locked closed and
placarded, “INOPERATIVE DO NOT
ENTER”,
d) Access to waste receptacle from outside
lavatory must be secured closed and
placarded, “INOPERATIVE - DO NOT USE”,
e) Lavatory is used only by crew members,
and
f) Lavatory is inspected periodically.

⇑ B (O) May be inoperative for non-passenger carrying

operations provided crew members are the only
occupants of the aircraft and are briefed as to
which smoke detection system(s) is/are
inoperative.

NOTE: These provisos are not intended to

prohibit lavatory use or inspections by
crewmembers.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 - 38
BD--700-1A10 / -1A11 DATE: 06/27/2009
1. 2.
CAS Indication Dispatch Consideration

⇑ SMOKE AV RACK FAIL B Aircraft may be dispatched provided:

(Caution) a) Following messages are not also posted-
(Global 5000) - AVFANS FAIL Caution,
- AVIONIC FAN FAIL Advisory,
- AV RACK FAN FAIL Advisory,
- RECIRC FAN FAIL Advisory,
and
b) Aircraft is not dispatched in unpressurized
configuration.

⇑ SMOKE BAGGAGE FAIL C Aircraft may be dispatched provided cargo is

(Caution) not carried in the associated compartment.

NOTE:
Where fitted for carriage, Unit Load Devices
(ULDs - terminology used by the air transport
industry for containers and loading units that are
used for the carriage of cargo) may be carried in
the associated compartment provided no cargo
is carried on or in these devices. For ballast
purposes, use of bags (made of glass fibre or
kevlar) of sand or ingots of non-magnetic metals
(such as lead) is acceptable.

⇑ SMOKE CLO AFT FAIL C (O) Aircraft may be dispatched provided:

(Caution) a) Closet is empty,
b) Cabin closet door is locked CLOSED and
placarded, “DO NOT USE”, and
c) Closet is inspected periodically.

⇑ SMOKE CLO FWD FAIL C (O) Aircraft may be dispatched provided:

(Caution) a) Closet is empty,
b) Cabin closet door is locked CLOSED and
placarded, “DO NOT USE”, and
c) Closet is inspected periodically.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 - 39
BD--700-1A10 / -1A11 DATE: 06/27/2009
1. 2.
CAS Indication Dispatch Consideration

⇑ SMOKE FWD LAV FAIL C (O) Aircraft may be dispatched provided:

(Caution) a) Lavatory is not used by passengers for any
purpose,
b) Lavatory waste receptacle is empty,
c) Lavatory door is locked closed and
placarded “INOPERATIVE DO NOT
ENTER”,
d) Access to waste receptacle from outside
lavatory must be secured closed and
placarded, “INOPERATIVE - DO NOT
USE”,
e) Lavatory is used only by crew members,
and
f) Lavatory is inspected periodically.

⇑
B (O) May be inoperative for non-passenger carrying
operations provided crew members are the only
occupants of the aircraft and are briefed as to
which smoke detection system(s) is/are
inoperative.

NOTE: These provisos are not intended to

prohibit lavatory use or inspections by
crewmembers.

⇑ SPLRS/STAB BIT C (O) Aircraft may be dispatched provided:

(Advisory) a) All multi-function spoilers are operative in
roll assist mode,
[NOTE: Relief limited to aircraft b) Visual check is made to verify that the MFS
serial numbers 9193 & surfaces operate normally prior to take-off,
subsequent, and previous serial c) Ground Lift Dump is manually armed for
numbers incorporating BA take-off, and
Service Bulletins as below. d) All flight control modules are operative*.
Model 700-1A10: Both S/Bs
#700-27-053 and S/B #700-27- (*All flight control modules are operative
058. assumes MMEL relief has not already been
undertaken for Item 27-61-02 - Flight Control
Model 700-1A11: Both S/Bs Modules (FCM) Channels).
#700-1A11-27-009 and
S/B #700-1A11-27-016]
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 - 40
BD--700-1A10 / -1A11 DATE: 06/27/2009
1. 2.
CAS Indication Dispatch Consideration

⇑ TAT 2 FAIL B (O) Except where enroute operations, including

(Advisory) RVSM, require its use, aircraft may be
dispatched provided:
a) ADC 2 is de-activated,
b) None of the following CAS messages are
posted:
- ADC 1 DEGRADED Advisory;
- ADC 1 FAIL Advisory;
- ADC 3 DEGRADED Advisory;
- ADC 3 FAIL Advisory;
- TAT 1 FAIL Advisory;
- TAT 3 FAIL Advisory;
- TAT HT 1 FAIL Advisory;
- TAT HT 2 FAIL Advisory,
- TAT HT 3 FAIL Advisory;
c) Reversion switching is operative, and
d) The four pitot-static probes are
functional.

NOTE 1: R FADEC FAULT Advisory may

also post with TAT 2 FAIL annunciated.

NOTE 2: Transponder and Flight Director /

autopilot must use same ADC data for
RVSM.

⇑ TAT 3 FAIL B (O) Except where enroute operations, including

(Advisory) RVSM, require its use, aircraft may be
dispatched provided:
a) ADC 3 is de-activated,
b) None of the following CAS messages are
posted:
- ADC 1 DEGRADED Advisory;
- ADC 1 FAIL Advisory;
- ADC 2 DEGRADED Advisory;
- ADC 2 FAIL Advisory;
- TAT 1 FAIL Advisory;
- TAT 2 FAIL Advisory;
- TAT HT 1 FAIL Advisory;
- TAT HT 2 FAIL Advisory,
- TAT HT 3 FAIL Advisory;
and
c) The four pitot-static probes are functional.

NOTE 1: Transponder and Flight Director /

autopilot must use same ADC data for
RVSM.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 - 41
BD--700-1A10 / -1A11 DATE: 06/27/2009
1. 2.
CAS Indication Dispatch Consideration

⇑ TAT HT 1 FAIL B (O) Except where enroute operations require its

(Advisory) use, aircraft may be dispatched provided:
a) None of the following CAS messages are
also posted:
- ICE DETECTOR FAIL Caution;
- ICE DETECTOR FAULT Advisory,
- TAT HT 2 FAIL Advisory;
- TAT HT 3 FAIL Advisory;
b) Operations are not conducted in visible
moisture where TAT is 10 deg C or lower,
c) Operations are not conducted in known or
forecast icing conditions, and
d) Operations are conducted in day VMC
conditions only.

⇑ TAT HT 2 FAIL B (O) Except where enroute operations require its use,
(Advisory) aircraft may be dispatched provided:
a) None of the following CAS messages are
also posted:
- ICE DETECTOR FAIL Caution;
- ICE DETECTOR FAULT Advisory,
- TAT HT 1 FAIL Advisory;
- TAT HT 3 FAIL Advisory;
b) Operations are not conducted in visible
moisture where TAT is 10 deg C or lower,
c) Operations are not conducted in known or
forecast icing conditions, and
d) Operations are conducted in day VMC
conditions only.

⇑ TAT HT 3 FAIL B (O) Except where enroute operations require its use,
(Advisory) aircraft may be dispatched provided:
a) None of the following CAS messages are
also posted:
- ICE DETECTOR FAIL Caution;
- ICE DETECTOR FAULT Advisory,
- TAT HT 1 FAIL Advisory;
- TAT HT 2 FAIL Advisory;
b) Operations are not conducted in visible
moisture where TAT is 10 deg C or lower,
c) Operations are not conducted in known or
forecast icing conditions, and
d) Operations are conducted in day VMC
conditions only.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 - 42
BD--700-1A10 / -1A11 DATE: 06/27/2009
1. 2.
CAS Indication Dispatch Consideration

⇑
TERR FAIL C May be inoperative provided TERR is selected
(Advisory) OFF.
⇑
TRU 1 FAIL C (O) Aircraft may be dispatched provided:
(Advisory) a) TRU 2 FAIL advisory message is not
displayed,
b) All indications for the remaining TRUs
operate normally, and
c) Affected unit is de-activated.

⇑ TRU 2 FAIL C (O) Aircraft may be dispatched provided:

(Advisory) a) TRU 1 FAIL advisory message is not
displayed,
b) All indications for the remaining TRUs
operate normally, and
c) Affected unit is de-activated.

⇑ WINDSHEAR FAIL C Aircraft may be dispatched provided:

(Advisory) a) Alternate procedures are established and
used, and
b) Takeoffs and landings are not conducted
in known or forecast windshear conditions.
⇑ WING A/ICE FAULT C (O) Aircraft may be dispatched provided prior to
(Advisory) each departure:
a) Flight is not conducted in known or
forecast icing conditions,
b) A power-up test is performed by cycling
WING A/ICE switch form OFF to ON, and.
c) None of the following CAS messages are
also posted:
- ICE DETECT FAIL Caution;
- L BLEED SYS FAIL Caution;
- R BLEED SYS FAIL Caution;
- ICE DETECT FAULT Advisory;
- L BLEED SYS FAULT Advisory;
- R BLEED SYS FAULT Advisory

⇑ WING A/ICE LEAK C Aircraft may be dispatched provided:

(Caution) a) Selecting wing anti-ice system OFF
extinguishes the WING A/ICE LEAK
Caution message,
b) Wing Anti-Ice remains selected OFF,
c) Neither ICE DETECTOR FAULT Advisory
nor ICE DETECTOR FAIL Caution
messages are also posted, and
d) Operations are not conducted in known or
forecast icing conditions.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 - 43
BD--700-1A10 / -1A11 DATE: 06/27/2009
1. 2.
CAS Indication Dispatch Consideration

⇑ WING A/ICE LO HEAT C Aircraft may be dispatched in accordance with

(Caution) MMEL relief provisos for L WING A/ICE FAILor
R WING A/ICE FAIL Caution message.

⇑ WING A/ICE SENSOR C Aircraft may be dispatched in accordance with

(Advisory) MMEL relief provisos for L WING A/ICE FAIL or
R WING A/ICE FAIL Caution message.

⇑ WOW FAULT C (O) Aircraft may be dispatched provided:

(Advisory) a) Prior to each departure, refuel / defuel
panel(s) is/are verified selected OFF,
b) MANUAL mode of cabin pressure control
is verified operative.
NOTE: Subsequent in-flight WOW system
failure will impact continued operation of some
systems, as described in AFM Non-Normal
Procedures for WOW FAIL Caution.

⇑ YD 1 FAIL C (O) Except for ER operations, aircraft may be

(Caution) dispatched provided:
a) YD 2 FAIL message is not also displayed,
and
b) Airplane is operated at or below FL 390.

⇑ YD 2 FAIL C (O) Except for ER operations, aircraft may be

(Caution) dispatched provided:
a) YD 1 FAIL message is not also displayed,
and
b) Airplane is operated at or below FL 390.

⇑ YD HEAT 1 FAIL B (O) Aircraft may be dispatched provided:

(Advisory) a) Yaw damper 1 is selected and used as
primary throughout the flight, and
b) Both yaw dampers are verified operative
before dispatch.
OR
⇑ B (O) Aircraft may be dispatched with both YD HEAT 1
FAIL and YD HEAT 2 FAIL messages provided:
a) Operations are conducted at or below
FL410, and
b) Both yaw dampers are verified operative
before dispatch.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: REVISION NO: 9 PAGE NO:
2 - 44
BD--700-1A10 / -1A11 DATE: 06/27/2009
1. 2.
CAS Indication Dispatch Consideration

⇑ YD HEAT 2 FAIL B (O) Aircraft may be dispatched provided:

(Advisory) a) Yaw damper 2 is selected and used as
primary throughout the flight, and
b) Both yaw dampers are verified operative
before dispatch.
OR
⇑
B (O) Aircraft may be dispatched with both YD HEAT 1
FAIL and YD HEAT 2 FAIL messages provided:
a) Operations are conducted at or below
FL410, and
b) Both yaw dampers are verified operative
before dispatch.