Master Minimum Equipment List (MMEL)

Revision 5. Renumbered CVR items per PL 29 and renumbered subsequent items. Item 23-9, Static Discharge Wick: Deleted, Revision 2. 23-4 Item 23-10, Crewmember Interphone System: Revised per Policy Letter 9, Revision 12 as appropriate for G150. 23-5 Item 23-12, Emergency Locator Transmitter: Revised per Policy Letter 120, Revision 3. 23-6 Item 23-15, Flight Deck Hand Microphone: Revised per Policy Letter 58, Revision 4 and renumbered subsequent items. 23-7 thru 8 Item 23-16, Flight Deck Headsets Earphones/Headphones and Boom Microphones: Revised per Policy Letter 58, Revision 4 and renumbered subsequent items. 23-8 Item 23-17, High Frequency (HF) Communication System: Removed second set of relief because it does not apply to G150. Item 23-18, Headset: Relief combined with ATA 23-16, Flight Deck Headsets Earphones/Headphones and Boom Microphones, Revision 2. 23-9 Item 23-19, Alerting System (Audio/Visual): Removed Flight Attendant Visual and Audio Alerting System that was deleted in Revision 1. 23-10 Item 23-26, Flight Deck Hot Microphone: Added new relief. ATA 24 Electrical Power 24-2 Item 24-8, 60Hz AC Electrical Power System: Updated Repair Category from C to D. 24-3 Item 24-10, 50Hz AC Electrical Power System: Updated Repair Category from C to D. ATA 25 Equipment/Furnishings 25-1 thru 2 Item 25-1, Passenger Seats: Revised per Policy Letter 79, Revision 9. 25-3 thru 5 Item 25-2, Emergency Medical Equipment: Revised per Policy Letter 132, Revision 0. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. V AIRCRAFT: G150 HIGHLIGHTS OF CHANGE PAGE NO. EXPLANATION OF CHANGE 25-7 Item 25-6, Cargo Restrain Systems, Revised per Policy Letter 100, Revision 3. 25-8 Previous Item 25-8, Rudder Pedal Adjustment: Removed item. Relief was moved to 27-15 in Revision 1. Renumbered subsequent items. 25-9 thru 10 Item 25-9, Storage Bins/Cabin, Galley and Lavatory Storage Compartments/Closets: Revised per Policy Letter 104, Revision 7. 25-11 Item 25-10, Galley/Cabin/Waste Receptacles Access Doors/Covers: Revised per Policy Letter 96, Revision 2. Item 25-12, Cockpit Smoke Vision System: Revised per Policy Letter 129, Revision 0. Previous Item 25-14., Cockpit Convenience Items: Removed item. Relief was deleted in Revision 1. Renumbered subsequent items. Item 25-13, Portable Flashlight/Flashlight Holder: Revised per Policy Letter 132, Revision 0. ATA 26 Fire Protection 26-1 Previous Item 26-1, APU Bleed Leak Detector: Removed item. Relief was deleted in Revision 1. Renumbered subsequent items. Item 26-1, Portable Fire Extinguisher: Revised per Policy Letter 132, Revision 0. 26-2 Item 26-4, APU Fire Extinguisher System: Added additional proviso. Item 26-7, Lavatory Smoke Detection System: Revised per Policy Letter 24, Revision 5. 26-3 Item 26-8, Cargo Compartment Smoke Detection System: Revised per Policy Letter 102, Revision 2. ATA 27 Flight Controls 27-3 Item 27-8, Flight Airbrakes Warning System: Removed item. Relief was deleted in Revision 1. Renumbered subsequent items. ATA 28 Fuel 28-3 Item 28-9, Standby Fuel Pumps: Removed item. Relief was deleted in Revision 1. Renumbered subsequent items. 28-4 Item 28-13, Pressure Defueling System: Removed item. Relief was deleted in Revision 1. Renumbered subsequent items. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. VI AIRCRAFT: G150 HIGHLIGHTS OF CHANGE PAGE NO. EXPLANATION OF CHANGE ATA 31 Indicating/Recording Systems 31-1 thru 2 Item 31-2, Flight Data Recorder (FDR): Revised per Policy Letter 87, Revision 10. ATA 32 Landing Gear 32-1 Item 32-1, Anti-Skid System: Deleted in Revision 2. Item 32-3, Nose Wheel Steering System: Deleted in Revision 2 per Policy Letter 114, Revision 1. ATA 33 Lights 33-1 Item 33-1, Cockpit/Flight Deck/Flight Compartment and Instrument Lighting System: Revised per Policy Letter 77, Revision 4. 33-2 Item 33-3, Passenger Lighted Information Signs: Revised per Policy Letter 123, Revision 1. 33-3 Item 33-5, Navigation Light System: revised Remarks and Exceptions. Item 33-8, Wing Icing Detection Light: Revised per Policy Letter 72, Revision 4. 33-4 Item 33-12, Floor Proximity Emergency Escape Path Marking System Lights: Deleted, Revision 2. Item 33-16, Strobe Light (Tail Position Only): Added new relief and renumbered subsequent items. 33-5 Item 33-23, Flashlight: Relief moved to ATA 25-13, Revision 2. ATA 34 Navigation 34-1 Item 34-3, Flight Information System: Removed item. Relief was moved to Section 23 (Communications) and renamed “Airborne Flight Information System” in Revision 1. Renumbered subsequent items. 34-2 Item 34-3, Altitude Alerting System: Revised per Policy Letter 39, Revision 5. 34-3 Item 34-9, Radio Altimeter System: Revised Remarks or Exceptions. 34-4 Item 34-10, ATC Transponders and Automatic Altitude Reporting System: Combined ADS-B Squitter Transmissions with Item 34-16, Automatic Dependent Surveillance- Broadcast System, per Policy Letter 76, revision 7 and Policy Letter 105, Revision 4. 34-5 Item 34-13, Adaptive Flight Displays, 4) Accel/Decel Indication: Removed item. Relief was deleted in Revision 1. Renumbered subsequent items. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. VII AIRCRAFT: G150 HIGHLIGHTS OF CHANGE PAGE NO. EXPLANATION OF CHANGE 34-6 Item 34-13, Sub-items Vertical Speed Indications (PFD) and Multi-Function Display (MFD): Removed items. Reliefs were deleted in Revision 1. 34-12 thru 13 Item 34-16, Automatic Dependent Surveillance Broadcast (ADS-B) System: Revised per Policy Letter 105, Revision 4. 34-14 Item 34-18, Altitude Heading and Reference System (AHRS): Changed operable to operative in NOTE. 34-15 Item 34-20, Flight Management Systems (FMS) (CDU and Nav Computer only), 1) Navigation Database: Revised per Policy Letter 98, Revision 1. Replaced MNPS with NAT HLA. 34-16 Item 34-27, Lightning Sensor System: Added new relief. ATA 35 Oxygen 35-2 Item 35-6, Portable Protective Breathing Equipment (PBE): Revised per MMEL Policy Letter 132, Revision 0. ATA 46 Information Systems 46-1 Item 46-1, Electronic Flight Bag (EFB) System: Deleted, Revision 2. ATA 52 Doors 52-1 Item 52-1, Cabin Door Warning System: Revised Remarks or Exceptions. 52-2 Item 52-10, Lavatory Door: Added new relief. ATA 79 Engine Oil 79-1 Previous item 79-1, Engine Oil Level Low Warning System: Removed item. Relief was deleted in Revision 1. Renumbered subsequent item. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. VIII AIRCRAFT: G150 DEFINITIONS Refer to the current FAA MMEL Policy Letter 25, MMEL and MEL Definitions, found on the FAA Flight Standards Information Management System (FSIMS) website. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. IX AIRCRAFT: G150 PREAMBLE For operations under 14 CFR parts 91 subpart K (part 91K), 121, 125, 125 LODA, 129, and 135, refer to the current FAA MMEL Policy Letter PL-34, MMEL and MEL Preamble. For operations under 14 CFR part 91, refer to current FAA MMEL Policy Letter PL-36, 14 CFR Part 91 MEL Approval and Preamble. Both Policy Letters are found on the FAA Flight Standards Information Management System (FSIMS) website. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. X AIRCRAFT: G150 GUIDELINES FOR (M) AND (O) PROCEDURES The FOEB has identified a need for certain procedures to provide an adequate level of safety while providing relief for some items. These procedures must be established by the operator and may be based on the aircraft manufacturer’s recommended procedures, Supplemental Type Certificate modifier’s recommended procedures, or equivalent operator procedures. When recommended procedures are published, the operator should comply with these procedures. If recommended procedures are not published, the following guidelines delineate the aspects to be considered by the operator in the development of required procedures: Guidelines for (M) & (O) Procedures should be based on the Maintenance and Operational Procedures Manual for the Minimum Equipment List, published by Gulfstream Aerospace. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 21-1 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 21. Air Conditioning Sequence No. Item 1 2 3 4 Change Bar 1. Bleed Switching Valve C 2 1 (M) One may be inoperative provided airplane is operated at or below FL 250. | | C 2 0 (M) May be inoperative provided: a) Affected valves are closed, and b) Environmental Control System (ECS) Selector is in RAM. NOTE: Cabin pressurization and Temperature control are not available with Environmental Control System (ECS) Selector in RAM. 2. HP Bleed Air Duct Blow Out Disc C 2 0 (M) One or both discs may be missing provided no airflow from respective port(s) is verified with respective engine(s) running before each takeoff. | | 3. Ram Air Check Valve C 1 0 (O) May be inoperative in OPEN position provided airplane is operated unpressurized. 4. Automatic Cabin Temperature Control C 1 0 May be inoperative provided Manual Cabin Temperature Control is operative. | | C 1 0 (O) May be inoperative provided airplane is operated unpressurized. NOTE: When operating without either automatic or manual cabin temperature control, it is possible to heat cabin/cockpit using emergency bleed air from right engine. Place ECS Selector in EMERG and modulate right engine thrust to control temperature. If DUCT TEMP HI message comes on, reduce right engine thrust. | | | | | | (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 21-2 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 21. Air Conditioning Sequence No. Item 1 2 3 4 Change Bar 4. Automatic Cabin Temperature Control (Cont’d) C 1 0 CAUTION: Application of takeoff thrust to right engine below 10000 ft. with ECS Selector in EMERG may cause damage to ECS ducting. Do not take off with ECS Selector in EMERG. | | | | | | | | 5. Manual Cabin Temperature Control C 1 0 May be inoperative provided Automatic Cabin Temperature Control is operative. | | | C 1 0 (O) May be inoperative provided airplane is operated unpressurized. NOTE: When operating without either automatic or manual cabin temperature control, it is possible to heat cabin/cockpit using emergency bleed air from right engine. Place ECS Selector in EMERG and modulate right engine thrust to control temperature. If DUCT TEMP HI message comes on, reduce right engine thrust. CAUTION: Application of takeoff thrust to right engine below 10000 ft. with ECS Selector in EMERG may cause damage to ECS ducting. Do not take off with ECS Selector in EMERG. | | | | | | | | | | | | | | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 21-3 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 21. Air Conditioning Sequence No. Item 1 2 3 4 Change Bar 6. Air Conditioning Unit C 1 0 May be inoperative provided airplane is operated with Environment Control System (ECS) Selector in RAM. NOTE: Cabin pressurization and Temperature control are not available with Environmental Control System (ECS) Selector in RAM. 7. Cabin Pressurization Control System 1) Automatic Mode B 1 0 May be inoperative provided: a) Manual Mode is operative, and b) CABIN DOOR UNLOCK message is operative. B 1 0 May be inoperative provided airplane is operated with Environment Control System (ECS) Selector in RAM. NOTE: Cabin pressurization and Temperature control are not available with Environmental Control System (ECS) Selector in RAM. 2) Manual Mode B 1 0 May be inoperative provided Automatic Mode is operative. B 1 0 May be inoperative provided airplane is operated with Environment Control System (ECS) Selector in RAM. NOTE: Cabin pressurization and Temperature control are not available with Environmental Control System (ECS) Selector in RAM. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 21-4 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 21. Air Conditioning Sequence No. Item 1 2 3 4 Change Bar 8. Valves 1) Outflow Valve C 1 0 (M) May be inoperative provided: a) Extended overwater operations are not conducted, b) Outflow valve is secured OPEN, and c) Airplane is operated unpressurized. 2) Safety Valve C 1 0 (O) May be inoperative provided airplane is operated unpressurized. 9. Cabin Altitude Rate of Climb Indicator C 1 0 May be inoperative provided: a) Cabin Altitude Indicator is operative, and b) Automatic and Manual Mode of Cabin Pressurization Control System (CPCS) is operative. C 1 0 May be inoperative provided: a) Cabin Differential Pressure Indication is operative, b) A chart to convert cabin differential pressure to cabin altitude is provided to crew, and c) Automatic and Manual Mode of Cabin Pressurization Control System (CPCS) is operative. C 1 0 (O) May be inoperative provided airplane is operated unpressurized. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 21-5 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 21. Air Conditioning Sequence No. Item 1 2 3 4 Change Bar 10. Cabin Altitude Indicator C 1 0 May be inoperative provided: a) Cabin Differential Pressure Indicator is operative, b) A chart to convert cabin differential pressure to cabin altitude is provided to crew, and c) Cabin Altitude is monitored during flight by crewmember. C 1 0 (O) May be inoperative provided airplane is operated unpressurized. 11. Cabin Differential Pressure Indicator C 1 0 May be inoperative provided: a) Cabin Altitude Indicator is operative, b) A chart to convert cabin altitude to cabin differential pressure is provided to crew, and c) Cabin Altitude is monitored during flight by crewmembers. C 1 0 (O) May be inoperative provided airplane is operated unpressurized. 12. Nose Cooling Fan C 2 1 One may be inoperative provided AFM procedures are followed for each flight | 13. Bleed Pressure/ Temperature HI Warning System C 1 0 May be inoperative provided airplane is operated with Environment Control System (ECS) Selector in RAM. NOTE: Cabin pressurization and Temperature control are not available with Environmental Control System (ECS) Selector in RAM. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 21-6 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 21. Air Conditioning Sequence No. Item 1 2 3 4 Change Bar 14. Duct Temp HI Warning System C 1 0 May be inoperative provided airplane is operated with Environment Control System (ECS) Selector in RAM. NOTE: Cabin pressurization and Temperature control are not available with Environmental Control System (ECS) Selector in RAM. 15. Overhead Airflow Vent (Wemac/Gasper) D - - | | 16. Cabin Altitude High Warning System C 1 0 (O) May be inoperative provided airplane is operated unpressurized. | 17. Cabin Pressurization System C 1 0 (O) May be inoperative provided airplane is operated unpressurized. | 18. Cabin Temperature Indicator C 1 0 May be inoperative provided Automatic or Manual Temperature Control System is operative. | 19. Windshield Defog System C 1 0 May be inoperative provided windshield heating system is operative. | 20. APU Airflow HI Flow Pushbutton D 1 0 | 21. Cabin Temperature Remote Controller D - - | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 21-7 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 21. Air Conditioning Sequence No. Item 1 2 3 4 Change Bar 22. Emergency Pressurization System C 1 0 (O) May be inoperative provided airplane is operated unpressurized. | 23. Ditch Pushbutton C 1 0 May be inoperative provided outflow valve can be controlled by Manual Cabin Pressure operation. | 24. Dump Pushbutton C 1 0 May be inoperative provided outflow valve can be controlled by Manual Cabin Pressure operation. | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 22-1 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 22. Autoflight Sequence No. Item 1 2 3 4 Change Bar 1. Flight Director System C 2 0 May be inoperative provided enroute or approach minimums do not require its use. | 2. Autopilot System B 1 0 (M) May be inoperative except where enroute operations, RVSM operations, or approach minimums require its use and provided AFM Limitations are observed. NOTE: Airplane must be operated at or below FL 310 when both autopilot and yaw damper are inoperative. | | 3. Yaw Damper System C 1 0 May be inoperative provided: a) Autopilot and Yaw Damper are disengaged by placing YD/AP DISC bar in DOWN position, and b) Airplane is operated at or below FL 310. | 4. Mach Trim C 1 0 May be inoperative provided airplane is operated in accordance with AFM Limitations. NOTE: Airplane must be operated at or below 0.78 Mach if autopilot is disengaged with Mach Trim inoperative. | | | 5. Control Wheel Autopilot Disconnect Button C 2 1 One may be inoperative provided: a) Autopilot is not used below 1500 ft. AGL, and b) Approach minimums do not require use of autopilot. | | B 2 0 May be inoperative provided autopilot is not used. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 22-2 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 22. Autoflight Sequence No. Item 1 2 3 4 Change Bar 6. Takeoff/Go-Around (TOGA) Button C 2 1 May be inoperative provided airplane is piloted from side with operative button when autopilot is used for coupled approaches. | C 2 0 (O) May be inoperative provided: a) Both thrust levers are operated manually for takeoff and go-around, and b) Autopilot and flight director are not used below 500 ft. AGL or MDA, whichever is higher. NOTE: Automatic Flight Director Takeoff and Go-Around Guidance are not available with both TOGA buttons inoperative. | | | | | | | | | 7. Flight Control Computer (FCC) A 2 0 One or both may be inoperative provided: a) Operations do not require an operational Autopilot, b) Airplane is operated at or below FL 310, c) Airplane is operated at or below 0.78M, and d) Repairs are made within 1 flight-day. NOTE: Loss of a single FCC results in loss of mach trim compensation, automatic stabilizer trim, yaw damper, and autopilot. | | | | | | | | | | 8. Pitch Synchronization Pushbutton C 2 0 9. FMS V-Speed Calculation and Upload System C 1 0 May be inoperative provided V-speeds are manually input and crosschecked between each pilot station. 10. Autopilot Coupler Deleted, Revision 2. | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 22-3 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 22. Autoflight Sequence No. Item 1 2 3 4 Change Bar 11. Flight Control Panel, Vertical Guidance Modes 1) Vertical Navigation (VNAV) Mode Selector Switch C 1 0 May be inoperative provided vertical navigation mode is considered inoperative and not used during autopilot operations. 2) Vertical Speed (VS) Mode Selector Switch C 1 0 May be inoperative provided vertical speed mode is considered inoperative and not used during autopilot operations. 3) Flight Level Change (FLC) Mode Selector Switch C 1 0 May be inoperative provided flight level change mode is considered inoperative and not used during autopilot operations. 4) Pitch Mode (PIT) C 1 0 May be inoperative provided pitch mode is considered inoperative and not used during autopilot operations. 12. Flight Control Panel, Lateral Guidance Modes 1) ½ BANK Mode Selector Switch C 1 0 May be inoperative provided autopilot operations do not require ½ bank selection. 2) Navigation (NAV) Mode Selector Switch C 1 0 May be inoperative provided NAV mode autopilot operations are not required. 3) Back Course (BC) Mode Selector Switch C 1 0 May be inoperative provided Back Course operations are not required. 4) Approach (APPR) Mode Selector Switch C 1 0 May be inoperative provided Approach Mode Operations are not required. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 22-4 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 22. Autoflight Sequence No. Item 1 2 3 4 Change Bar 13. *** Auto Throttle System C - 0 1) Auto Throttle Engage/Disengage Switch (on back of Thrust Lever Knob) C 2 1 | | C 2 0 Both may be inoperative provided Auto Throttle is not utilized. 2) Auto Throttle Quick Disconnect Switch (on front of Thrust Lever Knob) C 2 1 | | C 2 0 (M) Both may be inoperative provided Auto Throttle is disabled by pulling and collaring associated circuit breakers. | | | | 3) Auto Throttle Status Display C 2 1 May be inoperative provided airplane is piloted from side with the operative display. | | | C 2 0 (M) Both may be inoperative provided Auto Throttle is disabled by pulling and collaring associated circuit breakers. | | | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 23-1 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 23. Communications Sequence No. Item 1 2 3 4 Change Bar 1. Communications System (VHF, UHF) D - - Any in excess of those required by 14 CFR may be inoperative provided it is not powered by the Battery Bus and not required for emergency procedures. NOTE: Comm 1 is powered by the Battery Bus. | | 2. Passenger Address (PA) System 1) Passenger Configuration B 1 0 (O) May be inoperative provided alternate, normal and emergency procedures, and/or operating restrictions are used. NOTE: Any station function(s) that operate normally may be used. | | C 1 0 (O) May be inoperative provided: a) PA not required by 14 CFR, and b) Alternate, normal, and emergency procedures and/or operating restrictions are established and used. NOTE: Any station function(s) that operates normally may be used. | | a) Lavatory Speaker C 1 0 (O) May be inoperative provided alternate procedures are established and used. (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 23-2 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 23. Communications Sequence No. Item 1 2 3 4 Change Bar 2. Passenger Address (PA) System (Cont’d) 2) Cargo Only Configuration (Courier/Supernumerary Address System) C 1 0 (O) May be inoperative provided alternate, normal, and emergency procedures are established and used. | | | D 1 0 May be inoperative provided procedures do not require its use. a) Lavatory Speaker C 1 0 (O) May be inoperative provided alternate procedures are established and used. | D 1 0 May be inoperative provided procedures do not require its use. 3. Cockpit Speaker C 2 0 May be inoperative provided affected crewmember(s) has an operative headset available. | 4. Hand Held Microphone C - 0 One or more may be inoperative provided affected cockpit crewmember: a) Uses a boom microphone, and b) Has an operative Radio Push-to-Talk Switch. NOTE: Additional Radio Push-to-Talk (PTT) buttons installed on each side console and each Display Control Grip may be used in lieu of each Control Wheel Push-to-Talk Switch. | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 23-3 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 23. Communications Sequence No. Item 1 2 3 4 Change Bar 5. Cockpit Voice Recorder (CVR) (With Flight Data Recorder (FDR) Installed) A 1 0 May be inoperative provided: a) Flight Data Recorder (FDR) is operative, and b) Repairs are made within 3 flight-days. | 1) *** Independent Power Source C 1 0 | | 6. Cockpit Voice Recorder (CVR) (Without Flight Data Recorder (FDR) Installed) A 1 0 May be inoperative provided repairs are made within 3 flight-days. | | 1) *** Independent Power Source C 1 0 | | 7. Cockpit Voice Recorder (CVR) Installed for an Operator Other Than a Holder of an Air Carrier or Commercial Operator Certificate A 1 0 May be inoperative provided repairs are made in accordance with 14 CFR. | 1) *** Independent Power Source C 1 0 | | 8. *** Selective Call System (SELCAL) C - 0 (O) May be inoperative provided alternate procedures are established and used. | D - 0 May be inoperative provided procedures do not require its use. 1) Channel C - 0 (O) May be inoperative provided alternate procedures are established and used. | D - 0 May be inoperative provided procedures do not require its use. 9. Static Discharge Wick Deleted, Revision 2. | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 23-4 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 23. Communications Sequence No. Item 1 2 3 4 Change Bar 10. *** Crewmember Interphone System C 2 1 | | 1) Passenger Configuration | a) Flight Deck to Cabin, Cabin to Flight Deck Function B - - (O) May be inoperative provided flight deck to cabin and cabin to flight deck interphone functions operate normally on at least fifty percent of cabin handsets. NOTE: Any station function(s) that operates normally may be used. | | | | | | | C 1 0 (O) May be inoperative provided: a) Crewmember interphone system not required by 14 CFR, and b) Alternate normal and emergency procedures, and/or operating restrictions are used and established. NOTE: Any station function(s) that operates normally may be used. | | | | | | | | | | | b) Flight Deck to Ground Function C - 0 (O) May be inoperative provided alternate procedures are established and used. | | | D - 0 May be inoperative provided procedures do not require its use. | | 11. *** Automatic Cabin Briefing System D 1 0 (O) May be inoperative provided alternate procedures are established and used. | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 23-5 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 23. Communications Sequence No. Item 1 2 3 4 Change Bar 12. *** Emergency Locator Transmitter | *** Survival Type ELT D - - Any in excess of those required by 14 CFR may be inoperative or missing. | Fixed ELT A - 0 (M) May be inoperative provided: a) System is deactivated, and b) Repairs are made within 90 days. | | | A - 0 (M) May be missing provided: a) Placard stating “ELT not installed” is placed in view of the pilot, and b) Repairs are made within 90 days. | | | | | | D - - (M) Any in excess of those required by 14 CFR may be inoperative provided system is deactivated. | | | D - - Any in excess of those required by 14 CFR may be missing. | Remote ELT Switch C 1 0 (M) May be inoperative provided: a) Remote ELT Switch is deactivated, and b) ELT Switch is placed in ARMED mode. | | | | | ELT Indicator Light D - - | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 23-6 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 23. Communications Sequence No. Item 1 2 3 4 Change Bar 13. *** Flight Phone System D - - | 14. Headset Jack C 2 0 May be inoperative provided cockpit speakers are operative. | 15. Flight Deck Hand Microphone HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE C - 0 May be inoperative provided associated boom microphone operates normally. | | | | | | | D - 0 Any in excess of those required by regulation may be inoperative. | | Flight Deck Hand Microphone OPERATOR OTHER THAN A HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE D - 0 Any in excess of those required by regulation may be inoperative. | | | | | | | | C - 0 May be inoperative provided associated boom microphone operates normally. | | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 23-7 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 23. Communications Sequence No. Item 1 2 3 4 Change Bar 16. Flight Deck Headsets Earphones/Headphones and Boom Microphones HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE | | | | | | | | 1) Headset Boom Microphone A - 0 May be inoperative provided: a) Associated hand microphone is installed and operates normally, and b) Repairs are made within 3 flight-days. | | | | | | D - - Any in excess of those required by regulation may be inoperative. | | 2) Headset Earphone/Headphone C - 1 May be inoperative provided associated flight deck speaker operates normally. | | | D - - Any in excess of those required by regulation may be inoperative. | | 3) Active Noise Canceling/Reduction Function D - 0 May be inoperative provided normal audio function of headset is operative. | | | (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 23-8 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 23. Communications Sequence No. Item 1 2 3 4 Change Bar 16. Flight Deck Headsets Earphones/Headphones and Boom Microphones (Cont’d) OPERATOR OTHER THAN A HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE | | | | | | 1) Headset Boom Microphone A - 0 May be inoperative provided: a) Associated hand microphone is installed and operates normally, and b) Repairs are made in accordance with applicable regulations. | | | | | | | D - - Any in excess of those required by regulation may be inoperative. | | 2) Headset Earphone/ Headphone C - 1 May be inoperative provided associated flight deck speaker operates normally. | | | 3) Active Noise Canceling/ Reduction Function D - 0 May be inoperative provided normal audio function of headset is operative. | | 17. High Frequency (HF) Communication System D - - Any in excess of those required by 14 CFR may be inoperative. | Deleted, Revision 2. | 18. Headset Relief combined with ATA 23-14, Flight Deck Headsets Earphones/Headphones and Boom Microphones, Revision 2. | | | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 23-9 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 23. Communications Sequence No. Item 1 2 3 4 Change Bar 19. Alerting System (Audio/Visual) | 1) Passenger Configuration a) Flight Deck Call Visual Alerting System B 1 0 May be inoperative provided flight deck audio alerting system is operative. NOTE: Flight deck audio alerting must always be operative. | 20. Radio Push-to-Talk (PTT) Switch C 6 0 Any or all may be inoperative provided an operative Hand Held Microphone is available to crewmember(s) on side of failed PTT switch(es). | | C 6 2 Up to two may be inoperative at each cockpit crew position. NOTE: Each cockpit crew position has three radio push to talk buttons; one on yolk, one on side console and one on Display Control Grip. 21. Belts/No Smoke Cabin Chime C - - May be inoperative provided: a) Belts/No Smoke signs are visible to all passengers, and b) A Crewmember advises passengers verbally to secure their seat belts and when smoking is permitted. | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 23-10 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 23. Communications Sequence No. Item 1 2 3 4 Change Bar 22. Radio Tuning Control In Cursor Control Panel C 2 1 May be inoperative provided direct tuning is operative on at least one FMS. | | C 2 0 May be inoperative provided direct tuning is operative on two FMSs. A 2 0 May be inoperative provided: a) Direct turning is operative on one FMS, and b) Repairs are made within 1 flight-day. | 23. *** Satellite Communication System (SATCOM) C - 0 (O) May be inoperative provided alternate procedures are established and used. | D - 0 May be inoperative provided procedures do not require its use. 24. Yoke Mounted Microphone Holder C 2 0 One or both may be damaged, torn, or missing provided affected microphone is secured or removed. NOTE: Reference 23-4 if microphone is removed or rendered inaccessible. | 25. *** Airborne Flight Information System (AFIS) (VHF datalink and/or Satellite XM) C 1 0 (O) May be inoperative provided alternate procedures are established and used. | D 1 0 May be inoperative provided procedures do not require its use. 26. Flight Deck Hot Microphone D 2 0 May be inoperative provided Flight Deck communications are acceptable to affected crewmembers. | | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 24-1 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 24. Electrical Power Sequence No. Item 1 2 3 4 Change Bar 1. Left Battery B 1 0 (M) May be inoperative provided: a) Both generators are operative, b) APU generator is operative, c) A ground power unit is used for APU and engine starts with battery master switch selected to ON, d) Associated circuit breaker is pulled to disconnect it from its associated bus, and e) L BATT OFF message is displayed. NOTE: Observe APU altitude and electrical load limitations. | 2. Left Battery Temperature Indicating System C 1 0 (M) May be inoperative provided: a) Both generators are operative, b) APU generator is operative, c) A ground power unit is used for APU and engine starts, and d) Associated circuit breaker is pulled and collared to disconnect it from its associated bus, and e) L BATT OFF message is displayed. NOTE 1: Observe APU altitude and electrical load limitations. NOTE 2: Temperature Indicating System is not applicable/ indication is not displayed for airplanes with Concord Valve Regulated Lead-Acid Main Batteries installed (STC ST03511AT-D). | 3. Generator DC Voltage Display C 2 1 May be inoperative provided GEN OFF message and AMPS display of associated generating system are operative. | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 24-2 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 24. Electrical Power Sequence No. Item 1 2 3 4 Change Bar 4. DC External Power System C 1 0 5. Engine Generator Warning System C 2 1 May be inoperative provided: a) Associated Generator Volts and AMPS displays are operative, and b) Generator(s) output and engine vibration is closely monitored when airplane is operated. | 6. Engine Generator A 2 1 (M) One may be inoperative provided: a) APU is kept operating with its generator selected ON throughout flight, b) Inoperative generator switch is left in OFF, c) Integrity of affected engine starter/generator is verified safe for starter operation, and d) Repairs are made within 1 flight-day. NOTE: Observe APU altitude and electrical load limitations. | | 7. Main Batteries Voltage Display C 2 1 One may be inoperative provided BATT OFF EICAS message of each battery is verified operative before each takeoff. | 8. 60Hz AC Electrical Power System D 1 0 (M)(O) May be inoperative provided associated circuit breaker is pulled and collared. | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 24-3 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 24. Electrical Power Sequence No. Item 1 2 3 4 Change Bar 9. APU Generator C 1 0 May be inoperative provided: a) Both Batteries are operative, b) Both Battery Temperature Indicating Systems are operative, and c) Both Engine Generators are operative. NOTE: Operating Battery Temperature Indicating System is not required (not applicable/ indication is not displayed) for airplanes with Concord Valve Regulated Lead-Acid Main Batteries installed (STC ST03511AT-D). 10. *** 50Hz AC Electrical Power System D 1 0 (M)(O) May be inoperative provided associated circuit breaker is pulled and collared. | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 25-1 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 25. Equipment/Furnishings Sequence No. Item 1 2 3 4 Change Bar 1. Passenger Seats | 1) Passenger Seat (Includes all Configurations and Locations) D - - May be inoperative provided: a) Seat does not restrict access to any emergency exit, egress route, or main aisle, and b) The affected seat(s) is blocked and placarded “DO NOT OCCUPY”. NOTE 1: A seat with an inoperative seat belt or shoulder harness is considered to be inoperative. NOTE 2: Affected seat(s) may include the seat(s) behind and/or adjacent outboard seats. | | | | | | | | | | | | | 2) Positioning Control for Taxi, Takeoff, and Landing (TTL) (Mechanical and/or Electrical) D - - (M) May be inoperative and seat occupied provided seat is secured in the taxi, takeoff, and landing (TTL) position. | | | | | D - - (M) May be inoperative and seat occupied provided seat back is immovable in the taxi, takeoff, and landing (TTL) position. | | | | 3) Armrest | a) With Seat Positioning Control for Taxi, takeoff, and Landing (TTL) and/or Other Control D - - (M) May be inoperative or missing and seat occupied provided: a) Armrest does not restrict access to any emergency exit, egress route, or main aisle, and b) If Armrest with seat control is missing or removed, seat is secured in taxi, takeoff, and landing (TTL) position. | | | | | | | | | | (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 25-2 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 25. Equipment/Furnishings Sequence No. Item 1 2 3 4 Change Bar 1. Passenger Seats (Cont’d) 3) Armrest (Cont’d) b) Without Seat Positioning Control for Taxi, takeoff, and Landing (TTL) and/or Other Control D - - May be inoperative or missing and seat occupied provided it does not restrict access to any emergency exit, egress route, or main aisle. | | | | 4) Seat Belt/Air Bag Restraint System | | a) Seat Belt/Air Bag Required by 14 CFR D - - May be inoperative and occupied provided affected seat is blocked and placarded “DO NOT OCCUPY”. | | | b) *** Seat Belt/Air Bag Not Required by 14 CFR D - - (M) May be inoperative or disconnected provided seat belt operates normally. | | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 25-3 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 25. Equipment/Furnishings Sequence No. Item 1 2 3 4 Change Bar 2. Emergency Medical Equipment 1) *** Automatic External Defibrillator (AED) and/or Associated Equipment A - 0 (O) May be incomplete, inoperative, or removed provided: a) AED is labeled or placarded in a manner that will identify it as a unit that cannot be mistaken for a fully serviceable unit, b) Location placarding is removed or obscured, and c) Repairs or replacements are made within one flight. NOTE: Medical equipment installed in the aircraft as part of an Emergency Medical Service (EMS) operation is not considered part of the normal complement of equipment. No MMEL relief applies to that equipment and 14 CFR maintenance and inspection requirements do not apply. | | | | | | | | | | | | | | | | | | | | D - - Any in excess of those required by 14 CFR may be incomplete, inoperative, or removed. | *** Tamper Seal or Tag C - - (O) May be inoperative, damaged, or missing provided proper servicing is verified at each preflight. | | | (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 25-4 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 25. Equipment/Furnishings Sequence No. Item 1 2 3 4 Change Bar 2. Emergency Medical Equipment (Cont’d) 2) *** Emergency Medical Kit (EMK) and/or Associated Equipment A - 0 (O) May be incomplete or removed provided: a) EMK is labeled or placarded in a manner that will identify it as a unit that cannot be mistaken for a fully serviceable unit, b) Location placarding is removed or obscured, and c) Repairs or replacements are made within one flight. NOTE: Medical equipment installed in the aircraft as part of an Emergency Medical Service (EMS) operation is not considered part of the normal complement of equipment. No MMEL relief applies to that equipment and 14 CFR maintenance and inspection requirements do not apply. | | | | | | | | | | | | | | | | | | | | | D - - Any in excess of those required by 14 CFR may be incomplete or removed. | | *** Tamper Seal or Tag C - - (O) May be inoperative, damaged, or missing provided proper EMK servicing is verified at each preflight. | | | (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 2 DATE: XX/XX/XXXX PAGE NO. 25-5 AIRCRAFT: G150 TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 25. Equipment/Furnishings Sequence No. Item 1 2 3 4 Change Bar 2. Emergency Medical Equipment (Cont’d) 3) *** First Aid Kit (FAK) and/or Associated Equipment A - 0 (O) If more than one is required by 14 CFR, only one of the required FAKs may be incomplete or removed provided: a) The FAK is labeled or placarded in a manner that will identify it as a unit that cannot be mistaken for a fully serviceable unit, b) Location placarding is removed or obscured, and c) Repairs or replacements are made within one flight. NOTE: Medical equipment installed in the aircraft as part of an Emergency Medical Service (EMS) operation is not considered part of the normal complement of equipment. No MMEL relief applies to that equipment and 14 CFR maintenance and inspection requirements do not apply. | | | | | | | | | | | | | | | | | | | | | | D - - Any in excess of those required by 14 CFR may be incomplete or removed. | | *** Tamper Seal or Tag C - - (O) May be inoperative, damaged, or missing provided proper FAK servicing is verified at each preflight. | | |