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. )
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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. )
II
Revision: 9
⇑ Back To Top Date: 06/27/2009
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
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
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
⇑ Back To Top
SECTION ONE LRU / COMPONENT RELIEF ITEMS
DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
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
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
message) 24-3
Electrical Management System - Control Display Units (EMS CDU)
24-3
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
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
Compartments/ Closets 25-3
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
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
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
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
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
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
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
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
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
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:
BD-700-1A10 / 1A11 REVISION: 14 DATE: 08/26/2008
PAGE: 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:
BD-700-1A10 / 1A11 REVISION: 14 DATE: 08/26/2008
PAGE: 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:
BD-700-1A10 / 1A11 REVISION: 14 DATE: 08/26/2008
PAGE: 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:
BD-700-1A10 / 1A11 REVISION: 14 DATE: 08/26/2008
PAGE: 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:
BD-700-1A10 / 1A11 REVISION: 14 DATE: 08/26/2008
PAGE: 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:
BD-700-1A10 / 1A11 REVISION: 14 DATE: 08/26/2008
PAGE: 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:
BD-700-1A10 / 1A11 REVISION: 14 DATE: 08/26/2008
PAGE: 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:
BD-700-1A10 / 1A11 REVISION: 1 DATE: 07/05/1990
PAGE NO: 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:
BD-700-1A10 / 1A11 REVISION: 1 DATE: 07/05/1990
PAGE NO: 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
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) 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.
IIIIIIIII
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 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.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
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.
⇑
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.
I IIII I
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
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.
I III I
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.
I
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.
(cont’d)
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
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 (relief is limited to installation defined by Bombardier Modsum MS 700T01756)
D 1 0
60-04 ⇑
Hot Air Shut Off Valves (HASOV)
C 2 1 (M) One may be inoperative CLOSED provided the affected HASOV is secured CLOSED.
(cont’d)
C 2 1 One may be inoperative OPEN provided: a) The Trim Air Valves are operative, and b) Both air conditioning packs are
operative.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
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
considered inoperative.
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.
III
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
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 –
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
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
Humidifier System (relief limited to installation defined by Bombardier Modsum MS C700-09025, S/B 700-21-001 or S/B 700-21-020)
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.
IIIIIIIIIIIIIIIIIIIII
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
Integrated Comm Unit (ICU) Tray Mounted Cooling Fan
C - 1 (M) May be inoperative provided a minimum of one fan is verified to operate normally.
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 Communication System (SATCOM)
D - 0
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
NOTE: Passenger to attendant call system is considered a passenger convenience item.
40-03 ⇑
Crewmember Interphone System (Flight Compartment/ Cabin, Cabin/ Flight Compartment)
B -
1
(O) Any in excess of the requirement may be inoperative provided alternative communications procedures between the affected flight attendant station(s) are established and used.
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 Ground Service Interphone System (Nose and Avionic bay)
C 1 0 (O) May be inoperative provided alternate procedures are established and used.
51-01 ⇑
Flight Compartment Speakers
C 2 0 Both may be inoperative provided: 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 Microphones
C 2 1 One may be inoperative provided associated boom microphone is operative.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
C 2 0 (M) Vertical adjustments may be inoperative 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 (Including associated equipment)
A
-
-
May be inoperative provided: a) A passenger seat in the passenger
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
A 1 0 (M)(O) Flight attendant seat may be inoperative 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 Bin(s)/Cabin and Galley Storage Compartments/ Closets
C - - (M) May be inoperative provided: a) Procedures are established to secure
compartment CLOSED, b) Compartment is not used for storage of
emergency equipment, and c) Affected compartment is not used for
storage of any item(s) except for those permanently affixed.
50-01 ⇑
Cargo Restraint Systems
C - - May be inoperative, or missing such that the effect is that the item must be considered inoperative, provided cargo compartment remains empty.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
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.
- 0 May be inoperative, damaged or missing provided that the item(s) is deferred in 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 Receptacle Access Doors / Covers
C - - (M) May be inoperative provided the container is empty and the access is secured to prevent waste introduction into the compartment.
70-04 ⇑
Exterior Lavatory Entry Door Ashtrays
1) Airplanes with more than one exterior lavatory door ashtray
A - - One may be missing provided it is replaced within 10 calendar days
2) Airplanes with only one exterior lavatory door ashtray
A 1 0 May be missing provided it is replaced within 3 calendar days.
71-01 ⇑
Baggage Compartment Liners
C - - Liner panels may be missing or damaged 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
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
Horizontal Stabilizer Trim Actuator (RVDT Channels)
C
4
3
One RVDT channel may be inoperative 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 (Relief limited to p/n GT415-5900-13 & subs)
B 2 1 (M)(O) One Slat channel may be inoperative provided: a) Both Flap channels are operative, and b) Aircraft is operated in accordance with
AFM Supplement for SLATS HALFSPEED OR FLAPS HALFSPEED.
2)
⇑
Flap Channels (Relief limited to p/n GT415-5900-13 & subs)
B 2 1 (M)(O) One Flap channel may be inoperative provided:
a) Both Slat channels are operative, and 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 Proximity Switch Sensors (PSS)
C 8 6 (M) One or two on the same MFS pair may be inoperative provided visual check is made to verify that the surfaces operate normally prior to take-off.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
C 1 0 (M) May be inoperative provided: a) Aft tank SOVs are verified in the
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 Control Valves
C 3 0 (M) All may be inoperative CLOSED provided alternate refuelling procedures are established and used.
23-02 ⇑
Aft Refuel / Defuel SOV (GX only)
C 1 0 (M) May be inoperative provided the SOV is 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 Refuel SOV (GX only) (Relief applicable to post BA SB 700-28-040)
C 1 0 May be inoperative provided the SOV is CLOSED.
23-06 ⇑
External Refuel/Defuel Panel
C
1
0 (O)(M)
One or all functions may be inoperative provided alternate means are available to perform required operations (ie: Flight Compartment Refuel/Defuel Panel or gravity refuelling)
NOTE: For inoperative panel indications,
refer to MMEL Item 28-41-05, Refuel/Defuel Panel Indications, herein)
IIIIIIIIIII
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
One or all functions may be inoperative provided alternate means are available to perform required operations (ie: External Refuel/Defuel Panel or gravity refuelling)
NOTE: For inoperative panel indications,
refer to MMEL Item 28-41-05, Refuel/Defuel Panel Indications, herein)
IIIIIIIIIII
24-01 ⇑
Fuel Recirculation Systems (Including systems’ PBA indications & EICAS messages)
C 2 0 One or both may be inoperative OFF provided:
a) Both recirculation systems are OFF, and
b) Fuel tank temperature indication is operative on EICAS
40-01 ⇑
L-R AUX PUMPS “OFF” Switch lights (light function only)
C 2 0
40-02 ⇑
L-R PRI PUMPS “OFF” Switch lights (light function only)
C 2 0
40-03 ⇑
XFEED SOV “OPEN” Switch lights (light function only)
C 1 0
40-04 ⇑
XFEED SOV “FAIL” Switch lights (light function only)
C 1 0
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
C 3 0 All may be inoperative provided switch(es) are manually selected ON before take-off and landing.
12-01 (deleted)
(deleted, 07/02/07)
13-01 ⇑
AC Motor Pump (ACMP) (System #3)
B 2 1 (O) One may be inoperative provided: a) Affected pump is deactivated, b) Remaining system 3 AC Motor Pumps is
operated continuously during flight, and c) All other hydraulic pumps are operative.
13-02 ⇑
RAT Accumulator Pressure Gauge
C 1 0 (M) May be inoperative provided the accumulator pre-charge is verified using a calibrated ground equipment gauge prior to the first flight of each day.
30-01 ⇑
HYD SOV CLOSED Switch Lights (light function only)
C 2 0 One or both may be inoperative provided that the FWSOV indication on the HYDRAULC synoptic page is operative.
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 Off Valves (WAIV)
(deleted)
III
C 2 0 (M) One or both may be inoperative CLOSED 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.
I
11-03 ⇑
WING XBLEED Valve (CBW)
C 1 1 (M) May be inoperative provided: 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: SB#700-27-048 or SB#700-1A11-27-011)
(cont’d)
C 8 4 (M) Except for the sensors used by the stall protection system (outboard), sensors may be inoperative provided the L (R) WING ANTI-ICE FAIL Caution or WING A/ICE SENSOR Advisory message is not annunciated.
IIIII
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
Windshield and Side Window Anti-Ice Controller Channels
C 4 3 (O) One may be inoperative provided: a) Pilot's side window heating is
operative, and b) Operations are not conducted in known
or forecast icing conditions
I
C 4 2 (O) Two may be inoperative provided: 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.
I
81-01 ⇑
Ice Detection Systems
C 2 1 (M) One may be inoperative provided wing and 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
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 Monitoring System (BTMS)
B 1 0 May be inoperative provided operations are conducted in accordance with the AFM Supplement for DISPATCH WITH BRAKE TEMPERATURE MONITORING SYSTEM INOPERATIVE.
1)
⇑
Brake Temperature Sensors
C 4 - One temperature sensor may be inoperative provided operations are conducted in accordance with the AFM Supplement for DISPATCH WITH BRAKE TEMPERATURE MONITORING SYSTEM INOPERATIVE.
43-05 ⇑
Wheel Speed Transducer Coils
C 8 7 (M)
43-06 ⇑
Brake Accumulator Pressure Gauges
C 2 0 (M) Both may be inoperative provided accumulator pre-charge pressure is checked using a suitable pressure gauge before the first flight of each flight day.
50-01 ⇑
Nosewheel Steering System
C 1 0 (M) May be inoperative provided: 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
Cockpit/ Flight Deck/ Flight Compartment and Instrument Lighting Systems
C - - Individual lights may be inoperative provided remaining lights are:
a) Sufficient to clearly illuminate all 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 (Area Lights)
C 2 0
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 Lighting
D - -
21-03 ⇑
Stair Lighting Systems
D - 0 May be inoperative provided a flashlight is used to illuminate stairs for night operations.
22-01 ⇑
Passenger InformationSigns “Fasten Seat Belts / No Smoking”
C - - (M)(O) Passenger Seats, Flight Attendant Seats, or Lavatory from which a sign is not readily legible shall not be occupied and must be 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
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
(Upper and lower fuselage)
C
4
0
One or all may be inoperative provided aircraft is not operated at night.
IIII
1) Red Beacons
C 2 0 One or both may be inoperative provided adequate precautions are taken to clear danger areas before engine start and while engines are running.
IIIII
⇑ 2) White Beacons
C 2 0 One or both white beacons may be inoperative provided all wing & tail anti-collision strobe lights are operative and selected ON prior to flight.
IIIII
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
May be inoperative provided any combination 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 Systems
C 2 1 One may be inoperative provided approach procedures are not dependent on its use.
⇑
1) Flight Director Modes
C - - Except where enroute operations or approach minimums / procedures require their use, individual flight director modes may be inoperative provided Altitude Alerting System is operative.
NOTE 1: Flight director altitude hold
mode is required for RVSM Operations.
NOTE 2: Any flight director mode, which operates normally, may be used.
IIIIIIIIIIII
24-01 ⇑
Electronic Standby Instrument
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
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 (brightness)
B 2 0 Dim / Bright controls may be inoperative 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 Sensor Unit)
D
1
0
(M)
May be inoperative provided EVS fairing and 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
C - 0 (O) May be inoperative provided: 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 Systems
C 3 2 (M)(O) One may be inoperative provided: 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
C 1 0 (O) May be inoperative provided EICAS readout is operative and checked prior to each flight.
2) Bottle Pressure Gauges
C 4 0 (M) Any or all may be inoperative provided: 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 Switch
C 4 3 (M) One may be inoperative provided pressure on all bottle pressure gauges is operative and checked prior to each flight.
12-03 ⇑
Overboard Discharge Indicator
C 1 0 May be missing provided: 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 – Cruise Masks (incl. Mask mics)
C - - (M)(O) Any in excess of those required by regulation may be inoperative or missing provided the 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 Equipment (PBE)
D - - Any in excess of those required by Regulations may be inoperative.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
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
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 – (EPR Control Modes)
C
2
0
Both EPR Control modes may be inoperative 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 Readouts
B 2 1 One may be inoperative provided: 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 Readouts
C 2 0 Both may be inoperative provided: 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 Indications (on the FUEL Synoptic Page)
C
2
1
(M)
Except for Polar Ops, one may be inoperative provided icing inhibitor is added to the fuel.
I II
(deleted)
(deleted)
IIIIi
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
C 2 1 (M) One may be inoperative provided: 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
C 1 0 (M) Part or all of the system may be inoperative provided that the affected engine(s) oil level is/are checked and filled manually, prior to each flight.
30-01
⇑
Engine Oil Quantity Indication System
B 2 0 (M) Both may be inoperative provided: 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 Bypass Indication
A 2 1 (M) One may be inoperative provided: 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
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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: TOC – 1
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
⇑ Back To Top
SECTION TWO CAS MESSAGE RELIEF
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: TOC – 2
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
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 (Advisory)
C Aircraft may be dispatched provided: a) AFCS 2 FAIL Advisory message is not also
annunciated, and b) Approach procedures are not dependent on
its use.
⇑ AFCS 2 FAIL (Advisory)
C Aircraft may be dispatched provided: 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 3
1.CAS Indication
2. Dispatch Consideration
⇑ AP 1 FAIL (Advisory)
C Aircraft may be dispatched provided: 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 (Advisory)
C Aircraft may be dispatched provided: 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 (Caution)
B Aircraft may be dispatched provided: 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
(Caution)
C
(O) Aircraft may be dispatched provided: 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 (Caution)
C
Aircraft may be dispatched with APU inlet door fully - OPEN provided:
a) APU is operated continuously during flight, and
b) AFM performance corrections for APU ON are applied.
OR
⇑ (cont’d)
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.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 4
1.CAS Indication
2. Dispatch Consideration
⇑ C
(O)
Aircraft may be dispatched with APU inlet door fully CLOSED provided APU is considered inoperative.
⇑ APU FADEC FAIL (Advisory)
C
(O)
Aircraft may be dispatched provided the system remains switched OFF and the inlet door is CLOSED.
⇑ APU FAULT (Advisory)
C Aircraft may be dispatched provided: 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 (Caution)
C Aircraft may be dispatched provided the APU is considered inoperative and is NOT used.
⇑ APU FIRE FAULT (Advisory)
C
(O)
Aircraft may be dispatched provided the APU fire 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 (Caution)
C
(O)
Aircraft may be dispatched provided APU fuel valve is deactivated and visually confirmed CLOSED.
⇑ APU GEN FAIL (Advisory)
C Aircraft may be dispatched provided: 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 5
1.CAS Indication
2. Dispatch Consideration
⇑ APU NOT AVAILABLE (Advisory)
C
(O) Aircraft may be dispatched provided the system remains switched OFF and the inlet door is CLOSED.
⇑ APU OIL HI TEMP (Caution)
C (O) Aircraft may be dispatched provided the system remains switched OFF and the inlet door is CLOSED.
⇑ APU OIL LO PRESS (Caution)
C (O)
Aircraft may be dispatched provided the system remains switched OFF and the inlet door is CLOSED.
⇑ APU OIL LO QTY (Advisory)
C (O) Aircraft may be dispatched provided the system remains switched OFF and the inlet door is CLOSED.
⇑ APU SHUTDOWN (Advisory)
C (O) Aircraft may be dispatched provided the system remains switched OFF and the inlet door is CLOSED.
⇑ APU SQUIB 1 FAIL (Advisory)
C Aircraft may be dispatched provided the APU is considered inoperative and is not used.
⇑ APU SQUIB 2 FAIL (Advisory)
C Aircraft may be dispatched provided the APU is considered inoperative and is not used.
⇑ ASCB CTLR 1 FAIL (Advisory)
B Aircraft may be dispatched provided: a) None of the following CAS messages are
C Aircraft may be dispatched provided: a) Autobrake selector switch remains in the OFF
position, and b) BRAKE FAULT Advisory is not also
annunciated.
⇑ AVIONIC FAN FAIL (Advisory) (GX only)
C (O) Aircraft may be dispatched 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.
⇑ CHECK DU 4
(Caution)
B (O) Aircraft may be dispatched provided: a) Display unit #4 is considered inoperative, b) All remaining displays are operative, and c) Reversion switching system is verified
operative.
⇑ CHECKLIST MISMATCH (Advisory)
D Aircraft may be dispatched provided 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 7
1.CAS Indication
2. Dispatch Consideration
⇑ CPLT BRAKE FAULT (Caution)
A Aircraft may be dispatched for one flight day 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
(Caution) C
Aircraft may be dispatched provided the center tank remains empty.
⇑ C Aircraft may be dispatched provided remaining fuel in center tank is considered as unusable fuel.
⇑ CTR XFER FAULT (Advisory)
C
(O)
Aircraft may be dispatched provided: 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 8
1.CAS Indication
2. Dispatch Consideration
⇑ ELEC SYS FAULT (Advisory)
C Aircraft may be dispatched provided the ELEC SYS FAIL Caution message is not annunciated.
⇑ EVS DEFOG FAULT (Advisory)
C Aircraft may be dispatched providing the EVS 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 (Caution)
D
(O)
Aircraft may be dispatched provided: 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 (Caution)
C (O) Aircraft may be dispatched provided: 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 (Caution)
C (O) Aircraft may be dispatched provided: 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 9
1.CAS Indication
2. Dispatch Consideration
⇑ FDR ACCEL FAIL (Advisory)
A Aircraft may be dispatched provided: a) Cockpit Voice Recorder (CVR) operates
normally, and b) Repairs are made within twenty flight days
⇑ FDR FAIL (Advisory)
A (O) Aircraft may be dispatched provided: a) Cockpit Voice Recorder (CVR) is verified
operative, and b) Repairs are made within three flight days.
B (O) Aircraft may be dispatched provided SLAT HALFSPD Advisory or SLAT FAIL Caution messages are not also posted.
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 (Advisory)
C Aircraft may be dispatched provided that in combination with any other long-range navigation source failures, unit is not required to meet regulatory requirements.
⇑ FMS 3 FAIL (Advisory)
C Aircraft may be dispatched provided that in combination with any other long-range navigation source failures, unit is not required to meet regulatory requirements.
⇑ FUEL TEMP SENSOR (Caution)
C (O) Aircraft may be dispatched provided: 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 10
1.CAS Indication
2. Dispatch Consideration
⇑ GEAR SYS FAIL (Caution)
A (O) Aircraft may be dispatched for one flight day, 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:
d) If GEAR DISAGREE Caution is annunciated during flight, nosewheel steering is to be selected OFF for landing.
⇑ GEAR SYS FAULT (Advisory)
A Aircraft may be dispatched for one flight day, provided flights are conducted with gear locked down and in accordance with all provisos of GEAR SYS FAIL Caution relief.
⇑ GND PROX FAIL
(Advisory) A Aircraft may be dispatched provided:
a) Alternate procedures are established and used, and
b) Repairs are made within two flight days
⇑ GPWS SYSTEMS FAIL
(Advisory)
A Aircraft may be dispatched provided: 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 (Caution)
D Aircraft may be dispatched provided, a) Approach procedures are not dependent on
its use, and b) HUD is selected OFF and stowed.
⇑ HUD FAN FAIL (Advisory)
D (O) Aircraft may be dispatched provided: 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 11
1.CAS Indication
2. Dispatch Consideration
⇑ HUD MISALIGN (Advisory)
D Aircraft may be dispatched provided: 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 (Advisory)
C (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.
⇑ HYD PUMP 3A FAIL (Advisory)
B (O) Aircraft may be dispatched provided: 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
(Advisory)
B (O) Aircraft may be dispatched provided: 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 12
1.CAS Indication
2. Dispatch Consideration
⇑ IAC 3 INVALID (Advisory)
B (O) Aircraft may be dispatched provided: 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 (Caution)
B (O) Aircraft may be dispatched provided: 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 (Caution)
C Aircraft may be dispatched provided: 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 13
1.CAS Indication
2. Dispatch Consideration
⇑ ICE DETECTOR FAIL (Caution)
C (O) Aircraft may be dispatched provided operations are not conducted in known or forecast icing conditions.
⇑ ICE DETECTOR FAULT (Advisory)
C Aircraft may be dispatched provided wing and cowl anti-ice systems are turned ON when icing conditions as defined in the AFM exist or are anticipated.
⇑ INT CABIN DOOR (Caution)
C (O) Aircraft may be dispatched provided, prior to take off and landing, the door is physically verified fully open.
⇑ IRS 1 AUX FAIL (Advisory)
C Aircraft may be dispatched provided no other IRS AUX PWR, IRS AUX FAIL or IRS FAIL messages are posted.
⇑ IRS 1 AUX PWR (Advisory)
C Aircraft may be dispatched provided no other IRS AUX PWR, IRS AUX FAIL or IRS FAIL messages are posted.
⇑ IRS 1 FAIL (Advisory)
C
(O)
Aircraft may be dispatched provided: 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 14
1.CAS Indication
2. Dispatch Consideration
⇑ IRS 1 MISCMP (Caution)
C (O) Aircraft may be dispatched provided: a) None of the following CAS messages are
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 (Caution)
C (O) Aircraft may be dispatched provided: 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 (Advisory) (GX)
C
(O)
Aircraft may be dispatched provided: a) Left AUX pump is de-activated, 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 17
1.CAS Indication
2. Dispatch Consideration
⇑ L AUX FUEL PUMP (Advisory) (G5000 only)
C
(O)
Aircraft may be dispatched provided: a) Left AUX pump is de-activated, 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 (Advisory)
C (O) Aircraft may be dispatched provided, prior to each 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 (Advisory)
A Aircraft may be dispatched for one flight day 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 (Advisory)
A May be dispatched with FADEC faults provided 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 18
1.CAS Indication
2. Dispatch Consideration
⇑ L PACK AUTO FAIL (Caution) (GX)
C (O)
Aircraft may be dispatched provided: a) Left pack is selected OFF and the FCV is
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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 19
1.CAS Indication
2. Dispatch Consideration
⇑ L PACK AUTO FAIL (Caution) (Global 5000)
C (O)
Aircraft may be dispatched provided: a) Left pack is selected OFF and the FCV is
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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 20
1.CAS Indication
2. Dispatch Consideration
⇑ L PACK FAIL (Caution) (GX)
C (O)
Aircraft may be dispatched provided: a) Left pack is selected OFF, 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 21
1.CAS Indication
2. Dispatch Consideration
⇑ L PACK FAIL (Caution) (Global 5000)
C (O) Aircraft may be dispatched provided: a) Left pack is selected OFF, 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 22
1.CAS Indication
2. Dispatch Consideration
⇑ L PACK FAULT (Advisory)
C
Aircraft may be dispatched provided, prior to each 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 (Advisory)
C (O) Aircraft may be dispatched provided: 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 23
1.CAS Indication
2. Dispatch Consideration
⇑ L PROBE MON FAIL (Advisory)
B (O) 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, 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 24
1.CAS Indication
2. Dispatch Consideration
⇑ L WING A/ICE FAIL (Caution)
C Aircraft may be dispatched provided: 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
(Caution) C
(O) Aircraft may be dispatched provided: 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 (Caution)
C (O) Aircraft may be dispatched provided prior to each 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 (Advisory)
C Aircraft may be dispatched provided two FMSs are operative.
⇑ MAN PRESS FAULT (Advisory)
A (O) Aircraft may be dispatched for one flight day, 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 25
1.CAS Indication
2. Dispatch Consideration
⇑ MLG BAY OVHT FAIL (Caution)
B Aircraft may be dispatched provided: 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 (Advisory)
B Aircraft may be dispatched provided: 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 (Advisory)
C (O) Aircraft may be dispatched provided 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 (Advisory)
C (O) Aircraft may be dispatched provided 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 26
1.CAS Indication
2. Dispatch Consideration
⇑ OXYGEN LO QTY (Caution)
B (O) Aircraft may be dispatched provided: 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 (Caution)
B (O) Except where operations require its use, including RVSM, aircraft may be dispatched provided:
a) ADC # 2 is de-activated, b) None of the following CAS messages are
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, andd) Operations are conducted in day VMC
conditions only
⇑ PLT BRAKE FAULT (Caution)
A Aircraft may be dispatched for one flight day 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 28
1.CAS Indication
2. Dispatch Consideration
⇑ R AUX FUEL PUMP (Advisory) (GX)
C
(O)
Aircraft may be dispatched provided: a) Right AUX pump is de-activated, 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, andh) An extra 1,000 pounds of fuel is carried for the
planned flight.
⇑ R AUX FUEL PUMP (Advisory) (G5000 only)
C
(O)
Aircraft may be dispatched provided: a) Right AUX pump is de-activated, 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, andf) An extra 1,000 pounds of fuel is carried for the
planned flight.
⇑ R BLEED FAULT (Advisory)
C (O) Aircraft may be dispatched provided, prior to each 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
(Advisory)
A Aircraft may be dispatched for one flight day 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
(Advisory)
A May be dispatched with FADEC faults provided 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 – 29
1.CAS Indication
2. Dispatch Consideration
⇑ R PACK AUTO FAIL (Caution) (GX)
C (O)
Aircraft may be dispatched provided: a) Right pack is selected OFF and the FCV is
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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 - 30
1.CAS Indication
2. Dispatch Consideration
⇑ R PACK AUTO FAIL (Caution) (Global 5000)
C (O) Aircraft may be dispatched provided: a) Right pack is selected OFF and the FCV is
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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 - 31
1.CAS Indication
2. Dispatch Consideration
⇑ R PACK FAIL (Caution) (GX)
C (O)
Aircraft may be dispatched provided: a) Right pack is selected OFF, 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 - 32
1.CAS Indication
2. Dispatch Consideration
⇑ R PACK FAIL (Caution) (Global 5000)
C (O) Aircraft may be dispatched provided: a) Right pack is selected OFF, 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 - 33
1.CAS Indication
2. Dispatch Consideration
⇑ R PACK FAULT (Advisory)
C
Aircraft may be dispatched provided, prior to 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
(Advisory)
C (O) Aircraft may be dispatched provided: 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 - 34
1.CAS Indication
2. Dispatch Consideration
⇑ R PROBE MON FAIL (Advisory)
B (O) 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 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 - 35
1.CAS Indication
2. Dispatch Consideration
⇑ R WINDOW HEAT FAIL (Caution)
C
(O)
Aircraft may be dispatched provided: 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
(Caution)
C Aircraft may be dispatched provided: 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 - 36
1.CAS Indication
2. Dispatch Consideration
⇑ R WSHLD HEAT FAIL (Caution)
C
(O)
Aircraft may be dispatched provided: 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 (Advisory)
C (O) Aircraft may be dispatched provided neither, L PACK FAIL or R PACK FAIL Caution messages are posted.
⇑ SAFETY VALVE OPEN (Advisory)
C (O) Aircraft may be dispatched 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.
⇑ SG 3 FAIL (Caution)
C (O) Aircraft may be dispatched provided: 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
B (O) Aircraft may be dispatched provided FLAP HALFSPD Advisory and/or FLAP FAIL Caution messages are not also posted.
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 (Advisory)
C Aircraft may be dispatched.
⇑ SMALL SERV DOOR (Caution)
C (O) Aircraft may be dispatched provided prior to each flight, all small service doors are verified CLOSED, LATCHED and LOCKED.
⇑ SMOKE AFT LAV FAIL (Caution)
C (O) Aircraft may be dispatched provided: 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 - 38
1.CAS Indication
2. Dispatch Consideration
⇑ SMOKE AV RACK FAIL (Caution) (Global 5000)
B Aircraft may be dispatched provided: a) Following messages are not also posted- - 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 (Caution)
C Aircraft may be dispatched provided cargo is 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 (Caution)
C (O) Aircraft may be dispatched provided: 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 (Caution)
C (O) Aircraft may be dispatched provided: 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 - 39
1.CAS Indication
2. Dispatch Consideration
⇑ SMOKE FWD LAV FAIL (Caution)
C (O) Aircraft may be dispatched provided: 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 (Advisory)
[NOTE: Relief limited to aircraft serial numbers 9193 & subsequent, and previous serial numbers incorporating BA Service Bulletins as below. Model 700-1A10: Both S/Bs #700-27-053 and S/B #700-27-058. Model 700-1A11: Both S/Bs #700-1A11-27-009 and S/B #700-1A11-27-016]
C (O) Aircraft may be dispatched provided: a) All multi-function spoilers are operative in
roll assist mode, b) Visual check is made to verify that the MFS
surfaces operate normally prior to take-off, c) Ground Lift Dump is manually armed for
take-off, and d) All flight control modules are operative*.
(*All flight control modules are operative assumes MMEL relief has not already been undertaken for Item 27-61-02 - Flight Control Modules (FCM) Channels).
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 - 40
1.CAS Indication
2. Dispatch Consideration
⇑ TAT 2 FAIL (Advisory)
B (O) Except where enroute operations, including 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
(Advisory) B (O) Except where enroute operations, including
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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 - 41
1.CAS Indication
2. Dispatch Consideration
⇑ TAT HT 1 FAIL (Advisory)
B (O) Except where enroute operations require its 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 (Advisory)
B (O) Except where enroute operations require its 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 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 (Advisory)
B (O) Except where enroute operations require its 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 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 - 42
1.CAS Indication
2. Dispatch Consideration
⇑ TERR FAIL (Advisory)
C May be inoperative provided TERR is selected OFF.
⇑ TRU 1 FAIL (Advisory)
C (O) Aircraft may be dispatched provided: 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 (Advisory)
C (O) Aircraft may be dispatched provided: 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 (Advisory)
C Aircraft may be dispatched provided: 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 (Advisory)
C (O) Aircraft may be dispatched provided prior to 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
(Caution)
C
Aircraft may be dispatched provided: 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 - 43
1.CAS Indication
2. Dispatch Consideration
⇑ WING A/ICE LO HEAT (Caution)
C Aircraft may be dispatched in accordance with MMEL relief provisos for L WING A/ICE FAILor R WING A/ICE FAIL Caution message.
⇑ WING A/ICE SENSOR (Advisory)
C Aircraft may be dispatched in accordance with MMEL relief provisos for L WING A/ICE FAIL or R WING A/ICE FAIL Caution message.
⇑ WOW FAULT (Advisory)
C (O) Aircraft may be dispatched provided: 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 (Caution)
C (O) Except for ER operations, aircraft may be dispatched provided:
a) YD 2 FAIL message is not also displayed, and
b) Airplane is operated at or below FL 390.
⇑ YD 2 FAIL (Caution)
C (O) Except for ER operations, aircraft may be 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 (Advisory)
B (O) Aircraft may be dispatched provided: 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: BD--700-1A10 / -1A11
REVISION NO: 9 DATE: 06/27/2009
PAGE NO: 2 - 44
1.CAS Indication
2. Dispatch Consideration
⇑ YD HEAT 2 FAIL (Advisory)
B (O) Aircraft may be dispatched provided: 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.