Mmel Bd700 Rev12 Pt 91

(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. )

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

Date: 03/16/2012 Revision: 12

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

Revision: 12 Back To

Top Date: 03/16/2012 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

DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION AIRCRAFT:

BD-700-1A10 / 1A11 REVISION NO.12 DATE: 03/16/2012

PAGE NO. III

TABLE OF CONTENTS (contd)

Back To Top

MMEL FRONT MATTER

Subject Page

COVER PAGE TITLE PAGE TABLE OF CONTENTS III THRU XIV LOG OF REVISIONS XV THRU XVII, CONTROL PAGE XVIII THRU XXI HIGHLIGHTS OF CHANGE XXII THRU XXV, DEFINITIONS XXVI THRU XXXIII PREAMBLE XXXIV THRU XXXV

Subject Chapter/Page

Air Conditioning Flow Control Valve 21-1 Recirculation Fans 21-1 Display Unit Cooling Fans 21-1 AFD Display Fans - Filters 21-1 Supplemental Cooling Fans 21-1 Cabin Pressurization Control 21-1 Outflow Valves 21-2 Safety Valves 21-2 Auxiliary Pressurization System 21-3 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 21-4 Pack AUTO Mode 21-5 Pack Inlet Pressure Sensor (PIPS) 21-5 Avionics Exhaust Fan 21-6 Av Rack Fan (Global 5000) 21-6 Gasper Assist Fan 21-6 Hot Air Shut Off Valves (HASOV) 21-7

Back To Top

SECTION ONE LRU / COMPONENT RELIEF ITEMS




PAGE NO. IV


EQUIPMENT LIST (contd) Subject Chapter/Page

Air Conditioning (contd) Trim Air Valves (TAV) 21-7 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 Remote Electronics Unit (REU) Channels 22-1 A/P Quick DISC Buttons (Control Wheel) 22-1 Touch Control Steering Buttons (TCS) 22-2 Take-Off/Go-Around (TOGA) Buttons (on Thrust Levers) 22-2 Yaw Damper Systems 22-2 Autothrottle Systems 22-2 Autothrottle Engage / Disengage Switches (Thrust Lever Stem) 22-3 Autothrottle Quick Disconnect Buttons (on Thrust Lever Handles) 22-3

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 23-2 Selective Call System (SELCAL) 23-2




PAGE NO. V


EQUIPMENT LIST (contd)


Communications (contd) Pre-recorded Announcement and Boarding Music System 23-2 Passenger Address System 23-2 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 Radio Tuning System 23-6 Radio Interface Units Channels (RIU) 23-7

Electrical Power Transformer Rectifier Units (TRUs) 24-1 RAT Auto-deployment 24-1 RAT Gen Heater 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 message) 24-3 Electrical Management System - Control Display Units (EMS CDU) 24-3 AC External Power System 24-4 EXT AC ON Switch Light 24-4 Aft External Services Panel 24-4 EXT DC ON Switch Light 24-4 DC External Power System 24-4



BD-700-1A10 / 1A11 REVISION NO. 12 DATE: 03/16/2012

PAGE NO. VI



Equipment / Furnishings Pilot Seat(s) Adjustments 25-1 Chart Holders 25-1 Sun visors 25-1 Observer Seat (not required by FAR) 25-1 Mid-Cabin Door Indication System (CABIN DOOR Caution Message) 25-1 Passenger Seat(s) 25-1 Flight Attendant Seat Assembly 25-2 Overhead Storage Bin(s)/Cabin and Galley Storage

Compartments/ Closets 25-3

Cargo Restraint Systems 25-3 Life Preservers and Survival Equipment 25-3 Emergency Locator Transmitter 25-3 First Aid Kits 25-3 Emergency Vision Assurance Systems (EVAS) 25-3 Flight Attendant Flashlights / Flashlight Holder 25-4 Passenger Convenience / NEF Items 25-4 Office in the Sky 25-4 Galley waste Receptacle Access Doors / Covers 25-4 Exterior Lavatory Entry Door Ashtrays 25-5 Baggage Compartment Liners 25-5 Crew Rest Facilities - Bunk 25-5

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




PAGE NO. VII



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 28-2 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




PAGE NO. VIII



Fuel (contd) 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

Panel 28-7

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) 30-2 WING XBLEED Switch 30-2 Cowl Anti-Ice System AUTO Mode (LH and RH) 30-2




PAGE NO. IX



Ice and Rain Protection (contd) Cowl Anti-Ice Valves 30-3 Probe Heaters 30-3 Yaw Damper Heaters 30-4 Probe Heater monitor Channels (HBMU) 30-4 Enhanced Vision System - Ice Protection 30-5 Windshield and Side Window Anti-Ice Controller Channels 30-6 Ice Detection Systems 30-7

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 IAC Battery 31-2 Lamp Dimmer Power Supplies (LDPS) 31-2 Lamp Driver Unit (LDU) - Channels 31-2 Display Units 31-2 Electronic Checklist System 31-3 Control Tuning Panels (CTPs) 31-3 Multifunction Keyboard Panel (MKP) 31-4 Cursor Control Panel (CCP) 31-5 Reversion Switch Panel (RSP) 31-6

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




PAGE NO. X



Landing Gear (contd) Wheel Speed Transducer Coils 32-2 Brake Accumulator Pressure Gauges 32-2 Nosewheel Steering System 32-2

Lights

Cockpit/ Flight Deck/ Flight Compartment and Instrument Lighting Systems

33-1

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




PAGE NO. XI



Navigation

Air Data Computers (ADC) 34-1 Total Air Temperature Systems 34-1 Standby Attitude Indicator 34-1 Non-stabilized Magnetic Compass (Standby Compass) 34-2 Flight Director Systems 34-2 Electronic Standby Instrument 34-3 VHF Navigation Systems (VOR/ILS #1) 34-4 Head-up Guidance System 34-4 Enhanced Vision System (incl. Infrared Sensor Unit) 34-4 Synthetic Vision System (SVS) 34-5 Weather Radar System 34-5 Weather Radar Controllers 34-5 Ground Proximity Warning System / TAWS 34-5 Surface Management System (SMS) 34-6 Traffic Collision and Avoidance System (TCAS II) 34-7

Radio Altimeter 34-8 Inertial Reference Systems 34-8 Lasertrak NDU 34-8 IRS Mode Select Switches 34-9 Lightning Sensor Systems (LSS) 34-9 Integrated Nav Unit (INU) Tray Mounted Cooling Fans 34-9 Marker Beacon Systems 34-9 Automatic Direction Finding System (ADF #1) 34-9 Distance Measuring Equipment Systems (DME) 34-9 ATC Transponders and Automatic Altitude Reporting Systems 34-9 Automatic Dependent Surveillance Broadcast System 34-10 Global Positioning Sensors 34-10 Flight Management Systems (FMS) 34-10 Data Loader 34-11




PAGE NO. XII


EQUIPMENT LIST (contd)


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

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 Centralized Maintenance Systems 45-1 Portable Maintenance Access Terminal (PMAT) 45-1

Information Systems Electronic Flight Bags 46-1 Integrated Flight Information System (IFIS) 46-2 () 46-3




PAGE NO. XIII



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 52-2 Aft Equipment Bay Door Indication System 52-2 Overwing Emergency Exits Indication System 52-2 Baggage Compartment Door Indication System 52-3 Refuel/Defuel Door Indication System 52-3 Aft Hydraulic Door Indication System 52-3

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




PAGE NO. XIV



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


BD-700-1A10 / 1A11 REVISION: 9 DATE: 06/27/2009

PAGE NO: XV

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




PAGE NO: XVI

LOG OF REVISIONS (contd) 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 06/27/2009 All Pages excepting DEFINITIONS and PREAMBLE 10 09/21/2010 TABLE OF CONTENTS III, 10 09/21/2010 HIGHLIGHTS OF REV., 10 09/21/2010 32-1

Section Two 10 09/21/2010 2-10, 2-42




PAGE NO: XVII

LOG OF REVISIONS (contd) Rev No. Date Page Numbers Initials

11 04/20/2011 Section One 11 04/20/2011 TABLE OF CONTENTS - III, V, IX, X 11 04/20/2011 HIGHLIGHTS OF CHANGE 17 01/20/2011 DEFINTIONS 11 04/20/2011 21-2, 21-6, 21-10 11 04/20/2011 24-1 thru 24-4 11 04/20/2011 25-1, thru 25-5 11 04/20/2011 26-2 11 04/20/2011 28-1 11 04/20/2011 30-1 thru 30-6 11 04/20/2011 31-2 11 04/20/2011 34-1 thru 34-8 11 04/20/2011 49-1, 49-2 11 04/20/2011 52-1, 52-2, 52-3

04/20/2011 Section Two 11 04/20/2011 TOC-1, -2, -3 11 04/20/2011 2-9 thru 2-44 12 03/16/2012 Section One 12 03/16/2012 TABLE OF CONTENTS - 12 03/16/2012 HIGHLIGHTS OF CHANGE 12 03/16/2012 21-1, 21-2, 21-3, 21-6 THRU 21-10 12 03/16/2012 22-1,22-2, 22-3 12 03/16/2012 23-1 THRU 23-7 12 03/16/2012 25-3, 25-4, 25-5 12 03/16/2012 27-2, 12 03/16/2012 31-1 THRU 31-6 12 03/16/2012 34-1 THRU 34-11 12 03/16/2012 45-1 12 03/16/2012 46-1, 46-2, 46-3 12 03/16/2012 Section Two 12 03/16/2012 INT-1, INT-2 12 03/16/2012 TOC-1, -2, -3 12 03/16/2012 2-1 thru 2-49

U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST


BD-700-1A10 / -1A11 REVISION NO. 12 DATE: 03/16/2012

PAGE NO. XVIII

CONTROL PAGE System Page No. Rev. No. Current Date

Back CONTROL PAGE

System Page No. Rev. No. Current Date COVER PAGE TITLE PAGE 12 03/16/2012 TABLE OF CONTENTS III 12 03/16/2012 IV 12 03/16/2012 V 12 03/16/2012 VI 12 03/16/2012 VII 9 06/27/2009 VIII 9 06/27/2009 IX 12 03/16/2012 X 12 03/16/2012 XI 12 03/16/2012 XII 12 03/16/2012 XIII 12 03/16/2012 XIV 12 03/16/2012 LOG OF REVISIONS XV 9 06/27/2009 XVI 10 09/21/2010 XVII 12 03/16/2012

CONTROL PAGE XVIII 12 03/16/2012

XIX 12 03/16/2012

XX 12 03/16/2012

XXI 12 03/16/2012

HIGHLIGHTS OF CHANGE XXII 12 03/16/2012

XXIII 12 03/16/2012

XXIV 12 03/16/2012

XXV 12 03/16/2012

DEFINITIONS XXVI 17 01/20/2011

XXVII 17 01/20/2011 XXVIII 17 01/20/2011

XXIX 17 01/20/2011 XXX 17 01/20/2011

XXXI 17 01/20/2011

XXXII 17 01/20/2011

PREAMBLE XXXIII 1 07/05/1990

XXXIV 1 07/05/1990

Section One divider XXXV 9 06/27/2009

21 21-1 12 03/16/2012




PAGE NO. XIX


21-2 12 03/16/2012

21-3 12 03/16/2012 21-4 9 06/27/2009

21-5 9 06/27/2009 21-6 12 03/16/2012 21-7 12 03/16/2012 21-8 12 03/16/2012 21-9 12 03/16/2012 21-10 12 03/16/2012 22 22-1 12 03/16/2012 22-2 12 03/16/2012 22-3 12 03/16/2012 23 23-1 12 03/16/2012 23-2 12 03/16/2012 23-3 12 03/16/2012 23-4 12 03/16/2012 23-5 12 03/16/2012 23-6 12 03/16/2012 23-7 12 03/16/2012 24 24-1 11 04/20/2011 24-2 11 04/2//2011 24-3 11 04/20/2011 24-4 11 04/20/2011 25 25-1 11 04/20/2011 25-2 9 06/27/2009 25-3 12 03/16/2012 25-4 12 03/16/2012 25-5 12 03/16/2012 26 26-1 11 04/20/2011 26-2 11 04/20/2011 26-3 11 04/20/2011 27 27-1 9 06/27/2009 27-2 12 03/16/2012 27-3 9 06/27/2009 27-4 9 06/27/2009 28 28-1 11 04/20/2011 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




PAGE NO. XX


28-8 9 06/27/2009 29 29-1 9 06/27/2009 29-2 9 06/27/2009 30 30-1 11 04/20/2011 30-2 11 04/20/2011 30-3 11 04/20/2011 30-4 11 04/20/2011 30-5 11 04/20/2011 30-6 11 04/20/2011 30-7 11 04/20/2011 31 31-1 12 03/16/2012 31-2 12 03/16/2012 31-3 12 03/16/2012 31-4 12 03/16/2012 31-5 12 03/16/2012 31-6 12 03/16/2012 32 32-1 10 09/21/2010 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 12 03/16/2012 34-2 12 03/16/2012 34-3 12 03/16/2012 34-4 12 03/16/2012 34-5 12 03/16/2012 34-6 12 03/16/2012 34-7 12 03/16/2012 34-8 12 03/16/2012 34-9 12 03/16/2012 34-10 12 03/16/2012 34-11 12 03/16/2012 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 12 03/16/2012 46 46-1 12 03/16/2012 46-2 12 03/16/2012 46-3 12 03/16/2012




PAGE NO. XXI


49 49-1 11 04/20/2011 49-2 11 04/20/2011 52 52-1 11 04/20/2011 52-2 11 04/20/2011 52-3 11 04/20/2011 73 73-1 11 04/20/2011 74 74-1 9 06/27/2009 77 77-1 9 06/27/2009 78 78-1 9 06/27/2009 79 79-1 11 04/20/2011 80 80-1 9 06/27/2009 Section Two divider 9 06/27/2009 Section Two Introduction INT-1 12 03/16/2012 Section 2 Table Of Contents TOC-1, -2, -3 12 03/16/2012 CAS Messages 2-1 Thru 2-49 12 03/16/2012




PAGE NO. XXII

HIGHLIGHTS OF CHANGE

Back

Effective the above date, the Bombardier BD-700-1A10 / -1A11 (Global Express) Master Minimum Equipment List (MMEL) is revised. Revision 12 is a Standard revision.

Following certification of the new Global Vision Flight Deck (GVFD), the new avionics suite manufactured by Rockwell-Collins, it is now incorporated on newly manufactured Global Express and Global 5000 aircraft. This Revision 12 incorporates new and revised relief cases, primarily intended to introduce dispatch relief associated with the introduction of these new avionics. Unless annotated as being specific to the Global Vision (Global Vision only), or as not applicable to the Global Vision (except Global Vision), MMEL relief cases and provisos throughout this revision are considered applicable to aircraft equipped with either suite of avionics. Associated with Revision 12, Section One introduces 16 new LRU/Component Oriented MMEL relief cases, and modifies 29 existing cases, adding sub-items to cover each of the avionics dispatch proviso differences. Another 12 existing relief cases have been amended simply to add the exclusion(except Global Vision), as above.

Among the amended items, minor correction have been applied to a few items wherein, provisos previously stating, as required by regulations have been amended to read, as required by FAR, in order to better reflect MMEL Policy Letter convention.

This revision also introduces 23 new Section Two CAS Message relief cases, and modifies 15 existing messages. Another 17 existing CAS relief cases have been amended simply to add the exclusion, as above. The WOW FAULT Advisory CAS message has been amended, to now require filight unpressurized.

Section One Technical Changes MMEL Seq. No. Item:

21-23-02 Display Units Fan Filters (new item)

21-23-02 Supplementary Cooling Fans (new item)

21-51-05 Ozone Converters (clerical amendment)

21-53-03 Gasper Fan (clerical amendment)

21-61-02 3) Cabin Temperature Control (clerical amendment)

22-10-01 Autopilot (amendment)

22-10-02 Remote Electronics Unit (REU) (new item)

22-11-02 Touch Control Steering Buttons (TCS) (amendment)

23-13-01 Satellite Communication System (SATCOM) (amendment)

23-22-01 Selective Call System (SELCAL) Channels (amendment)

23-40-01 Passenger Address System (amendment)

23-40-03 Crewmember Interphone System (amendment)

23-51-01 Flight Compartment Speakers (amendment)

23-51-02 Boom Microphones (amendment)




PAGE NO. XXIII


23-71-01 Cockpit Voice Recorder (CVR) (amendment)

23-81-01 Radio Management Units (amendment)

23-81-02 Radio Tuning System (new item)

23-81-03 Radio Interface Units Channels (RIU) (new item)

25-61-02 Emergency Locator Transmitter (amendment)

25-61-04 Emergency Vision Assurance Systems (EVAS) (new item)

27-42-01 Horizontal Stabilizer Trim Actuator (clerical amendment) 31-21-01 Clocks (amendment)

31-43-02 Lamp Driver Unit (LDU) - Channels (new item)

31-61-01 Display Units (amendment)

31-61-03 Control Tuning Panels (CTPs) (new item)

31-61-04 Multifunction Keyboard Panel (MKP) (new item)

31-61-05 Cursor Control Panel (CCP) (new item) 31-61-05 Reversion Switch Panel (RSP) (new item)

34-11-01 Total Air Temperature Systems (amendment)

34-14-01 Altitude Alerting System (amendment)

34-22-01 Non-stabilized Magnetic Compass (Standby Compass) (amendment)

34-23-01 Flight Director (amendment)

34-24-01 IESI (amendment)

34-34-01 Synthetic Vision Sytem (SVS) (new item)

34-41-01 Weather Radar System (amendment)

34-42-01 GPWS / TAWS (amendment)

34-42-02 Surface Management System (SMS) (new item)

34-43-01 Traffic Alert and Collision Avoidance System (TCAS) (amendment)

34-44-01 Radio Altimeter (amendment)

34-47-01 Lightning Detection / Sensor Systems (amendment)

34-54-01 ATC Transponders and Automatic Altitude Reporting Systems (amendt.)

34-54-02 Automatic Dependent Surveillance Broadcast System (ADS-B Out) (new)

34-55-01 Global Positioning Systems / Sensors (amendment)

34-61-01 Flight Management System (FMS) (amendment)

34-61-01 1) FMS Navigation Databases (amendment)

45-45-01 Centralized Maintenance Systems (amendment)




PAGE NO. XXIV


46-20-01 Integrated Flight Information System (IFIS) (new item)

46-30-01 Information Management System (IMS) (new item)

Items re-identified by (except Global Vision)

21-23-01 Display Unit Cooling Fans

23-10-01 Integrated Comm Unit (ICU) Tray Mounted Cooling Fans 31-41-02 Integrated Avionics Computer (IAC) #3

31-41-02 IAC Battery

31-43-01 Lamp Dimmer Power Supplies (LDPS)

31-61-02 Electronic Checklist System

34-32-01 Enhanced Vision System (EVS)

34-45-01 Lasertrak NDU

34-45-03 IRS Mode Select Switches

34-50-01 Integrated Nav Unit (INU) Tray Mounted Cooling Fans

45-45-01 1) Central Aircraft Information/ Maintenance System (CAIMS) 45-45-02 Portable Maintenance Access Terminal (PMAT)

CAS messages re-identified by (except Global Vision)

A/T 1 FAIL FMS 3 FAIL

A/T 2 FAIL GND PROX FAIL

AFCS 1 FAIL GPWS SYSTEMS FAIL

AFCS 2 FAIL HUD MISALIGN

AP PITCH TRIM FAIL IAC 3 INVALID

ASCB CTLR 1 FAIL IAC 3 OVHT

ASCB CTLR 2 FAIL IRS 1 OVHT

ASCB CTLR 3 FAIL IRS 2 OVHT

CHECK DU 4 IRS 3 OVHT

CHECKLIST MISMATCH LTRK FAIL

EVS DEFOG FAULT TERR FAIL

EVS FAIL WINDSHEAR FAIL




PAGE NO. XXV


Section Two Technical Changes

CAS MESSAGE

AT 1 FAIL (new item) IRS 1, 2, 3 MISCMP (amendment) AT 2 FAIL (new item)) SMS NOT AVAILABLE (new item) AT 12 FAIL (new item) SUPP FAN 1 FAIL (new item) ADC 2 DEGRADED (amendment) SUPP FAN 2 FAIL (new item) ADC 2 FAIL (amendment) SVS FAIL (new item) ADC 3 FAIL (amendment) SVS OBSTACLE FAIL (new item) AP 1 FAIL (amendment) SVS RUNWAYS FAIL (new item) AP 2 FAIL (amendment) SVS TAWS ALERT FAIL (new item) CVR FAULT (new item) SVS FAULT (new item) FDR FAIL (amendment) TAT 2 FAIL (amendment) FD 1 FAIL (new item) TAWS SYSTEM FAIL (new item) FD 2 FAIL (new item) TAWS GPWS FAIL (new item) FMS 1 FAIL (new item) TAWS MAP FAIL (new item) FMS 2 FAIL (amendment) TAWS TERRAIN FAIL (new item) FMS 3 FAIL (amendment) TAWS WINDSHEAR FAIL (new item) HUD FAIL (amendment) TCAS FAIL (new item) HUD FAN FAIL (amendment) WOW FAULT (amendment) HUD MISALIGN (amendment) YD 1 FAIL(amendment) IFIS 1 (2) (3) FAIL (new item) YD 2 FAIL (amendment) ISI FAULT (amendment) YD 1 FAIL (new item) YD 2 FAIL (new item)

U. S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST


BD-700-1A10 / 1A11 REVISION: 17 DATE: 01/2003/16/2012

PAGE: XXVI

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.




PAGE: XXVII

DEFINITIONS (contd)

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




PAGE: XXVIII

DEFINITIONS (contd)

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.




PAGE: XXIX

DEFINITIONS (contd)

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.



BD-700-1A10 / 1A11 REVISION: 17 DATE: 01/2003/16/2012

PAGE: XXX

DEFINITIONS (contd)

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.




PAGE: XXXI

DEFINITIONS (contd)

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.




PAGE: XXXII

DEFINITIONS (contd)

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 aircrafts 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. Operators NEF process shall not provide for deferral of items within serviceable limits identified in the manufactures maintenance manual or operators 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 operators NEF process.




PAGE NO: XXXIII

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.




PAGE NO: XXXIV

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



BD-700-1A10 / 1A11 REVISION NO: 9 DATE: 06/27/2009

PAGE NO: XXXV

Back To Top

SECTION ONE

LRU / COMPONENT

ORIENTED MMEL RELIEF



BD-700-1A10 / -1A11 REVISION NO: 12 DATE: 03/16/2012

PAGE NO: 21-1

REPAIR CATEGORY 2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

1. SYSTEM, SEQUENCE NUMBERS & ITEM

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 Fans (except Global Vision)

C 12 6 (M) One per Display Unit may be inoperative provided the avionics fan is operative.

II

23-02 AFD Display Fans - Filters (Global Vision only)

C

8

0

(M)

One or all fan filters may be damaged or missing.

IIII

23-03

Supplemental Cooling Fans (AFD Displays) (Global Vision only)

C

2

0

(M)

One or both display supplemental cooling fans may be inoperative, provided all AFD display fans are operative for AFD # 1, AFD #2 and AFD #3.

IIIII

30-01

Cabin Pressurization Control

1) AUTO Pressurization Channels

(contd)

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.




PAGE NO: 21-2





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 Channels

C

2

1

(M) One MANUAL channel may be inoperative provided: a) Both automatic cabin pressurization

control channels are operative, and b) Both Outflow valves are verified

operative.

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: a) Affected outflow valve is verified open, b) Flight is conducted in accordance with

AFM for an unpressurized flight configuration at or below 9,000 ft MS, and

c) AFM Buoyancy Limitations are observed with respect to take-offs and landings near bodies of water and extended over-water operations.

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.




PAGE NO: 21-3





31-02

Auxiliary Pressurization System

C 1 0 May be inoperative provided both air conditioning packs are operative.

51-01

Pack Inlet Temperature Sensor (PITS)

C 2 0 One or both may be inoperative

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.

51-03

Pack Inlet Flow Sensor (PIFS)

C

2

1

(M) One may be inoperative provided MANUAL mode of both air conditioning packs is verified 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

One or both may be inoperative provided flights are conducted at FL 250 or below.

II




PAGE NO: 21-4





52-01

Air Conditioning Packs (GX)

C

2

1

(O)(M)

One may be inoperative provided: a) The remaining pack is operated in

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.

(Global 5000)

C 2 1 (O)(M) One may be inoperative provided: a) The remaining pack is operated in

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.

(contd)




PAGE NO: 21-5





1) Pack AUTO Mode (GX)

C 2 1 (O)(M) One may be inoperative provided: a) MANUAL mode on the unaffected pack

is verified operative, b) Unaffected pack is operated in AUTO

mode, 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, and h) Operations are conducted at or below

FL410.

Note: If dispatching with right pack operative, ensure that RAM Air Valve is not failed OPEN.

(Global 5000) C 2 1 (O)(M) One may be inoperative provided: a) MANUAL mode on unaffected pack is

verified operative, b) Unaffected pack is operated in AUTO

mode, 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.

Note: If dispatching with right pack

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

52-02

Pack Inlet Pressure Sensor (PIPS)

C

2

0

(O) One or both may be inoperative provided MANUAL mode of both air conditioning packs is verified operative.




PAGE NO: 21-6





53-01

Avionics Exhaust Fan (GX)

C 1 0 May be inoperative provided one or both air 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.

(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 (Global 5000)

C 1 0 (M) May be inoperative provided: 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 (All aircraft 9127 & sub) (Pre-9127- if installed)

D 1 0 (M) May be inoperative provided unit is de-activated.

II




PAGE NO: 21-7





60-04

Hot Air Shut Off Valves (HASOV)

C 2 1 (M) One may be inoperative CLOSED provided 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.

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 (TAV)

C 3 0 (M) All may be inoperative CLOSED provided: 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


60-06

Pack Discharge Temperature Indication

C 2 0 (M) One or both may be inoperative provided: a) Both associated automatic temperature

controls are operative, and b) Pack Control selection switch is set to

either LO, NORM, or HIGH.

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

61-01

Cabin Temperature Control

1) AUTO mode (NORM)

(contd)

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.




PAGE NO: 21-8





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.

C 1 0 (O) MAN Mode of temperature control may be inoperative provided: a) AUTO mode is operative, and b) One pack is selected OFF and


III

3)

Temperature Selectors

Cockpit, FWD Cabin, AFT Cabin

C

3

0

Any or all may be inoperative.

61-02

1)

Temperature Sensors 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


3)

Mix Manifold Temperature Sensor (MMTS) - Sensors elements

C

4

1

II




PAGE NO: 21-9





62-01

RECIRC OFF Switch light (Light function only)

C 1 0

62-02

L Pack FAIL/OFF Switch lights (Light function only)

C 2 0

62-03

R Pack FAIL/OFF Switch lights (Light function only)

C 2 0

62-04

TRIM AIR OFF Switch light (light function only)

C 1 0

62-05

AUX PRESS ON Switch light (light function only)

C 1 0

62-06

RAM AIR ON Switch light (light function only)

C 1 0

62-07

DITCHING ON Switch light (light function only)

C 1 0

62-08

OUTFLOW VLV 1 CLOSED Switch light (light function only)

C 1 0

62-09

OUTFLOW VLV 2 CLOSED Switch light (light function only)

C 1 0

62-10

Emer Depress ON Switch light (light function only)

C 1 0

62-11

Pressurization AUTO/MAN MAN Switch light (light function only

C 1 0




PAGE NO: 21-10





71-01

***

Humidifier System (relief limited to installation defined by Bombardier Service Bulletins S/B 700-21-001, 700-21-020, 700-21-031, 700-21-039, 700-21-050, 700-21-051, or S/B 700-1A11-21-09, 700-1A11-21-24 )

D

1

0

(O) Aircraft may be dispatched provided 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.




PAGE NO: 22-1




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.

1) (except Global Vision)

C 2 0 Both may be inoperative provided: a) Approach procedures are not dependent

on its use, and b) Intended flights do not exceed three

hours.

NOTE: Automatic Emergency Descent Mode (EDM) is inoperative.

IIIIIII

2) (Global Vision only)

C 2 0 (M) Both may be inoperative provided: a) Procedures are not dependent on its use, b) Intended flights do not exceed three

hours, and c) EDM button is placarded INOP on flight

control panel.

NOTE: Automatic Emergency Descent Mode (EDM) is inoperative.

IIIIIIIII

10-02

Remote Electronics Unit (REU) Channels (Global Vision only)

C

4

2

One or both channels of one REU may be inoperative provided dispatch is in accordance with relief for the affected autopilot. (ref Item 22-10-01).

IIIIII

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.




PAGE NO: 22-2





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

1) Touch Control Steering Buttons (TCS)

(except Global Vision)

C 2 0 IIII

2) Touch Control Switch (TCS) (Global Vision Only)

C 2 0 IIII

11-03

Take-Off/Go-Around (TOGA) Buttons (on Thrust Levers)

C 2 1 One may be inoperative provided: a) Approach procedures do not require

its use, and b) Pilot flying has the operative switch.

C 2 0 Both may be inoperative provided: 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.




PAGE NO: 22-3





30-02

Autothrottle Engage / Disengage Switches (on Thrust Lever Stem)

C

2

1

C 2 0 (M) Both may be inoperative provided autothrottle system is rendered inoperative.

30-03

Autothrottle Quick Disconnect Buttons (on Thrust Lever Handles)

C

2

1

C 2 0 (M) Both may be inoperative provided the autothrottle system is rendered inoperative.



BD--700-1A10 / -1A11 REVISION NO: 12 DATE: 03/16/2012

PAGE NO: 23-1




4. REMARKS AND EXCEPTIONS 23 COMMUNICATION

10-01

Integrated Comm Unit (ICU) Tray Mounted Cooling Fan (except Global Vision)

C - 1 (M) May be inoperative provided a minimum of one fan is verified to operate normally.

II

11-01

Communication Systems

1) VHF, UHF

D

-

-

Any in excess of those required by FAR 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.

II

2) HF C - 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 fa

Documents

Mmel Bd700 Rev12 Pt 91