Master Minimum Equipment List (MMEL)

21-4 Item 9: Modified item title. Modified number installed. Added proviso a) and b). Item 10: Added remark. Item 11: Added remark. Item 12: Added remark. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. IV AIRCRAFT: PC-12/47E HIGHLIGHTS OF CHANGE PAGE NO. EXPLANATION OF CHANGE ATA 22 Autoflight 22-1 Item 1: Added (M). Item 2: Modified proviso. Item 3: Deleted (O). Item 4: Deleted (O). Added (M). 22-2 Item 5: Added to replace CAS message relief for “AFCS FAULT”. Item 6: Added to replace CAS message relief for “FD FAIL” and “Flight Director Fail”. 22-3 Item 7: Added to replace CAS message relief for Flight Control Channels. 22-4 Item 7: Relief continued. 22-5 Item 7: Relief continued. Item 8: Added. ATA 23 Communications 23-1 Item 3: Deleted. Item 4: Added remark. 23-2 Item 6, A) thru F): Added remarks. 23-3 Item 8: Updated to align with PL-106 Rev 6. 23-4 Item 8: Continued. Item 9: Removed. Reordered item titles 9 thru 14. Item 9: Updated remarks. 23-5 Item 11 B): Modified proviso b). Item 11 D) and E): Added remark. 23-8 Item 15: Added. Item 16: Added. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. V AIRCRAFT: PC-12/47E HIGHLIGHTS OF CHANGE PAGE NO. EXPLANATION OF CHANGE ATA 24 Electrical Power 24-1 Item 2: Revised remarks. ATA 25 Equipment/Furnishings 25-1 Item 2: Updated to align with PL-79, Rev 9. Item 4: Updated to align with PL-79, Rev 9. 25-2 Item 5: Updated to align with PL-79, Rev 9. 25-4 Item 10: Updated to align with PL-132 Rev 0. 25-7 Item 13: Updated to align with PL-100, Rev 3. ATA 27 Flight Controls 27-1 Item 1: Deleted. Item 2: Deleted. Item 4: Revised proviso. 27-2 Item 5: Added. Item 6: Added. ATA 28 Fuel 28-1 Item 1: Revised provisos. Item 3: Added to replace CAS message relief for “Low LVL sense fault”. ATA 30 Ice and Rain Protection 30-1 Item 3: Deleted (M). Added (O). Revised proviso. Item 5: Deleted ATA 31 Indicating/Recording Systems 31-3 Item 7: Deleted. 31-4 Item 8 B): Added additional relief. Item 9 A): Added item. Item 9 B): Added item. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. VI AIRCRAFT: PC-12/47E HIGHLIGHTS OF CHANGE PAGE NO. EXPLANATION OF CHANGE ATA 31 Indicating/Recording Systems (Cont’d) 31-4 Item 10: Added. ATA 33 Lights 33-1 Item 3: Removed asterisks and added remarks. 33-2 Item 7: Removed proviso. Updated number installed. Item 10: Added remark. Item 11: Added remark. Item 12: Added remark. ATA 34 Navigation 34-1 Item 1: Reworded such that this item encompassed the entire ADAHRS - so AFCS is also affected, and not just the PFD. 34-5 thru 6 Item 3 B): Updated to align with PL-105 Rev 4. 34-7 Item 5 C): Updated to align with PL-03 Rev 1. 34-8 Item 6: Added (M). Updated provisos. Item 8: Updated to align with PL-39 Rev 5. 34-10 Item 11 B): Added to replace GFR CAS messages. 34-12 Item 13 G): Added remark. 34-16 Item 15: Added. Item 16: Added. ATA 35 Oxygen 35-1 thru 2 Reordered item numbers and titles. Item 1: Update Category, NO. Installed, NO. Required for Dispatch. Updated remarks. Item 2: Added. Item 3: Deleted Revision 6. Item 4: Added. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. VII AIRCRAFT: PC-12/47E HIGHLIGHTS OF CHANGE PAGE NO. EXPLANATION OF CHANGE ATA 45 Central Maintenance System 45-1 Item 1: Updated Item title. Added remark. Item 2: Updated Item title. Revised remark. Added second proviso. ATA 46 Information Systems 46-1 Item 1 A): Deleted (M). Updated proviso. Added Proviso for channel B. 46-2 Item 1 B): Updated category and proviso. Item 2: Deleted (M). Added (O). Revised remarks. Added proviso. 46-3 Item 3: Deleted (M). Added (O). Revised remarks. Item 4: Revised remarks. 46-4 Item 6: Deleted (O). Added (M). 46-6 Item 7: Updated Title. Added (O). Revised remarks. ATA 52 Doors 52-1 Item 1: Title updated and revised remarks. Item 2: Deleted (M). Revised remarks. Item 3: Deleted (M). Revised remarks. Item 4: Deleted (M). Revised remarks. 52-2 Item 6: Updated Title. Added (O). Revised remarks. ATA 56 Windows 56-1 Item 1: Deleted (M). Revised remarks. ATA 73 Engine Fuel & Control 73-1 Added section. ATA 76 Engine Control 76-1 Added section. ATA 77 Engine Indicating 77-1 Deleted. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. VIII AIRCRAFT: PC-12/47E HIGHLIGHTS OF CHANGE PAGE NO. EXPLANATION OF CHANGE Section Two Crew Alerting System (CAS) Message Relief 2-1 thru 10 Deleted CAS message relief. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. IX AIRCRAFT: PC-12/47E DEFINITIONS Refer to the current FAA MMEL Policy Letter (PL)-25, MMEL/MEL Definitions, found on the FAA Dynamic Regulatory System (DRS) website at http://drs.faa.gov. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. X AIRCRAFT: PC-12/47E 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. Policy Letters are found on the FAA Dynamic Regulatory System (DRS) website at https://drs.faa.gov. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. XI AIRCRAFT: PC-12/47E 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 (STC) 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) and (O) Procedures should be based on the Maintenance and Operational Procedures for the Minimum Equipment List (Pilatus Aircraft PC-12) (M) and (O) Procedures, published by the aircraft manufacturer. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 1-1 AIRCRAFT: PC-12/47E LRU COMPONENT RELIEF SECTION ONE Deleted, Revision 6 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 21-1 AIRCRAFT: PC-12/47E 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. Air Cycle System C 1 0 (O) May be inoperative provided: a) Flight is conducted unpressurized, b) Flight is conducted at or below 10,000 ft. MSL, c) ACS Emergency Shut Off LEVER is PULLED, and d) Ambient conditions allow comfortable Cockpit/Cabin temperatures. | A) Fresh Air Ventilation Outlets C - 1 Any in excess of one may be inoperative provided the supply of fresh air is acceptable to the flightcrew. 2. Cabin Pressurization Control System A) Cabin Pressurization Control Unit (CPCU) Channels (MSN 1001 – 1719, 2001 and up) B 2 0 (M)(O) May be inoperative provided: a) Flight is conducted unpressurized, b) Flight is conducted at or below 10,000 ft. MSL, and c) OFV is deactivated in fully OPEN position, and d) Both CPCU channels are deactivated. | | | | | (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 21-2 AIRCRAFT: PC-12/47E 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 2. Cabin Pressurization Control System (Cont’d) B) Electronic Control and Monitoring Unit (ECMU) Channels (MSN 1721 – 1942) B 2 0 (M)(O) May be inoperative provided: a) Flight is conducted unpressurized, b) Flight is conducted at or below 10,000 ft. MSL, c) OFV is deactivated in fully open position, and d) Both ECMU channels are deactivated. | | | | | | | | | C) Emergency Dump Function B 1 0 (M)(O) May be inoperative provided: a) Flight is conducted unpressurized, b) Flight is conducted at or below 10,000 ft. MSL, c) OFV is deactivated in fully OPEN position, and d) Both CPCU/ECMU channels are deactivated. | | | | | | D) Cabin Pressure Outflow Valve (OFV) B 1 0 (M)(O) May be inoperative provided: a) Flight is conducted unpressurized, b) Flight is conducted at or below 10,000 ft. MSL, c) OFV is deactivated in fully OPEN position, and d) Both CPCU/ECMU channels are deactivated. | | | | | E) Cabin Pressure Relief Valve (CPRV) C 1 0 (M)(O) May be inoperative provided: a) Flight is conducted unpressurized, b) Flight is conducted at or below 10,000 ft. MSL, and c) CPRV is removed. | | | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 21-3 AIRCRAFT: PC-12/47E 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 3. Cabin Altitude Warning System B 1 0 (M)(O) May be inoperative provided: a) Flight is conducted unpressurized, b) Flight is conducted at or below 10,000 ft. MSL, c) OFV is deactivated in fully OPEN position, and d) Both CPCU/ECMU channels are deactivated. | | | | | | | | | 4. Cabin Differential Pressure Indication (MFD) B 1 0 (M)(O) May be inoperative provided: a) Flight is conducted unpressurized, b) Flight is conducted at or below 10,000 ft. MSL, c) OFV is deactivated in fully OPEN position, and d) Both CPCU/ECMU channels are deactivated. | | | | | | | | | 5. Cabin Altitude Indication (MFD) B 1 0 (M)(O) May be inoperative provided: a) Flight is conducted unpressurized, b) Flight is conducted at or below 10,000 ft. MSL, c) OFV is deactivated in fully OPEN position, and d) Both CPCU/ECMU channels are deactivated. | | | | | | | | | 6. Temperature Control System (Ground ECS Mode) D 1 0 May be inoperative. | 7. Cabin Or Cockpit Temperature Indication (MFD) C 1 0 May be inoperative. | 8. *** Vapor Cycle Cooling System (VCCS) D 1 0 (M) May be inoperative provided the VCCS is deactivated. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 21-4 AIRCRAFT: PC-12/47E 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 9. Auxiliary Heating System (Cabin and Underfloor) C 2 0 (M)(O) Auxiliary Cabin and Underfloor Heating may be inoperative provided: a) Auxiliary Cabin and Underfloor Heating Systems are deactivated, and b) Flight is conducted at IOAT’s above -15 °C. | | | | | | | | C 2 1 (M) Auxiliary Cabin Heating may be inoperative provided: a) It is deactivated, and b) Underfloor Heating System is operative. | | | | | 10. *** Auxiliary Electric Battery Heater System C 1 0 May be inoperative. | 11. *** Auxiliary Electric Engine Heater System C 1 0 May be inoperative. | 12. *** Electric Foot Warmer System C 1 0 May be inoperative. | 13. ECS Ground Mode Function D 1 0 May be inoperative. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 22-1 AIRCRAFT: PC-12/47E 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. Autopilot System C 1 0 (M)(O) May be inoperative provided: a) Autopilot is deactivated, b) AFM limitations are observed, c) Operations do not depend on its use, and d) Flight is conducted under VFR for single pilot operations. NOTE: Yaw damper will be inoperative after autopilot deactivation. | 2. Autopilot Disconnect Functions (Quick Release Controls) C 2 1 One may be inoperative provided: a) Operative one is on the pilot flying side, and b) Approach minimums do not require the use of the Autopilot. B 2 0 May be inoperative provided Autopilot is considered inoperative (refer to item 22-1). | 3. Yaw Damper C 1 0 May be inoperative provided autopilot is not used. NOTE: (For MSN 545, 1001 - 1719, 1721 - 1942) above FL 200 the aircraft must be flown only in balanced flight (slip ball centered +/-1 ball). For MSN 1720, 2001 and up, above FL 155 the aircraft must be flown only in balanced flight (slip-skid indicator +/-1 trapezoid) and above 140 KIAS (if practical). Use of the Prop Low Speed function (if installed) with flaps retracted configuration is not permitted. | | 4. *** Auto-Throttle C 1 0 (M) May be inoperative provided the system is deactivated. | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 22-2 AIRCRAFT: PC-12/47E 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 5. Automatic flight control system (AFCS) (Includes Autopilot (AP), Yaw Damper (YD), Tactile Feedback (TF), and Auto-Throttle (AT)) C 1 0 (M)(O) May be inoperative provided: a) AFCS is deactivated, b) AFM limitations are observed, c) Operations do not depend upon its use, and d) Flight is conducted under VFR for single pilot operations. NOTE: For MSN 545, 1001 - 1719, 1721 - 1942) above FL 200 the aircraft must be flown only in balanced flight (slip ball centered +/-1 ball). For MSN 1720, 2001 and up, above FL 155 the aircraft must be flown only in balanced flight (slip-skid indicator +/-1 trapezoid) and above 140 KIAS (if practical). Use of the Prop Low Speed function (if installed) with flaps retracted configuration is not permitted. | | | | | | | | | | | | | | | | | | | | | | 6. Flight Director C 1 0 (M)(O) May be inoperative provided: a) Autopilot is deactivated, b) Flight is conducted under VFR for single pilot operations, c) AFM limitations are observed, d) Operations do not depend upon flight director or autopilot use. NOTE: Yaw damper will be inoperative after autopilot deactivation. | | | | | | | | | | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 22-3 AIRCRAFT: PC-12/47E 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 7. Flight Controller | A) Channels C 2 1 (M)(O) Channel A may be inoperative provided: a) It is deactivated, and b) Flight is conducted under VFR for single pilot operations. | | | | | C 2 1 (M)(O) Channel B may be inoperative provided it is deactivated. | | C 2 0 (M)(O) May be inoperative provided: a) Both channels are deactivated, b) Flight is conducted under VFR for single pilot operations, c) Alternate procedures are established and used for dual pilot operations, d) AFM limitations are observed, and e) Operations do not depend upon Flight Controller use. NOTE: For MSN 545, 1001 – 1719, 1721 – 1942: above FL 200 the aircraft must be flown only in balanced flight (slip ball centered +/- ball). For MSN 1720, 2001 and up: above FL 155 the aircraft must be flown only in balanced flight (slip skid indicator +/- trapezoid) and above 140 KIAS (if practical). Use of the Prop Low Speed function (if installed) with flaps retracted configurations is not permitted. | | | | | | | | | | | | | | | | | | | | | | | | | | | (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 22-4 AIRCRAFT: PC-12/47E 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 7. Flight Controller (Cont’d) B) AP Button C 1 0 May be in operative provided Autopilot is considered inoperative (refer to item 22-1). | | | C) YD Button C 1 0 May be inoperative provided autopilot is not used. NOTE: (For MSN 545, 1001 - 1719, 1721 - 1942) above FL 200 the aircraft must be flown only in balanced flight (slip ball centered +/-1 ball). For MSN 1720, 2001 and up, above FL 155 the aircraft must be flown only in balanced flight (slip-skid indicator +/-1 trapezoid) and above 140 KIAS (if practical). Use of the Prop Low Speed function (if installed) with flaps retracted configuration is not permitted. | | | | | | | | | | | | | | | | | D) FD Button C 1 0 (O) May be inoperative provided: a) Flight is conducted under VFR for single pilot operations, b) AFM limitations are observed, and c) Operations do not depend upon flight director or autopilot use. | | | | | | | | E) AT Button C 1 0 May be inoperative provided Auto- throttle is considered inoperative (refer to item 22-4). | | (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 22-5 AIRCRAFT: PC-12/47E 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 7. Flight Controller (Cont’d) F) L/R Button C 1 0 May be inoperative provided associated green arrow indication points to pilot flying side. | | | G) MINIMUMS Knob/ PUSH RA/BARO Button C 1 0 (O) May be inoperative provided: a) Flight is conducted under VFR for single pilot operations, and b) Alternate procedures are established and used for dual pilot operations. | | | | | | H) Indication Light C - 0 May be inoperative. | 8. Touch Control Steering (TCS) Switch C 2 1 May be inoperative in open (inactive) position on pilot not flying side. | | C 2 0 May be inoperative provided: a) Flight director and autopilot are not used, b) Flight is conducted under VFR for single pilot operations, c) AFM limitations are observed, d) Operations do not depend upon Flight Director or Autopilot use. | | | | | | | | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 23-1 AIRCRAFT: PC-12/47E 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 and UHF) D - - Any in excess of those required by 14 CFR may be inoperative provided it is not powered by any Emergency Power Source and not required for emergency procedures. | A) MMDR (Communication) C 2 - Any in excess of those required by 14 CFR may be inoperative. 2. Cockpit Speakers C 2 - May be inoperative provided: a) One headset is operative and used by each flight crewmember, and b) A spare operative headset is readily available in the flightcrew compartment. 3. Audio Amplifiers Deleted, Revision 6. | A) Normal System Deleted, Revision 6. | B) Emergency System Deleted, Revision 6. | 4. Voice Activated Interphone System C 1 0 May be inoperative. | 5. Control Yoke Press to Talk Switches C 2 0 May be inoperative provided Hand Mic on affected side is operative. | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 23-2 AIRCRAFT: PC-12/47E 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 6. Static Wicks C - 0 May be inoperative provided no communication equipment is required for the flight. Following applies if communications are required for the flight. A) Left Winglet C 2 1 One may be inoperative or missing. | B) Right Winglet C 2 1 One may be inoperative or missing. | C) Rudder C 3 1 One may be inoperative or missing. | D) Stinger Deleted Revision 6. | E) Left Elevator C 2 1 One may be inoperative or missing. | F) Right Elevator C 2 1 One may be inoperative or missing. | 7. Passenger Address System (PA) A) Passenger Configuration B 1 0 (O) May be inoperative provided alternate, normal, and emergency procedures, and/or operating restrictions are established and 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 operate normally may be used. (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 23-3 AIRCRAFT: PC-12/47E 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 7. Passenger Address System (PA) (Cont’d) B) Cargo Configuration C 1 0 (O) May be inoperative provided alternate, normal, and emergency procedures, and/or operating restrictions are established and used. D 1 0 May be inoperative provided procedures do not require its use. 8. High Frequency (HF) Communication System D - - Any in excess of those required by 14 CFR may be inoperative. C - 1 (O) Non ETOPS: May be inoperative while conducting operations that require two LRCS provided: a) SATVOICE or CPDLC system operates normally, b) SATVOICE services are available as a LRCS over the intended route of flight and to all required alternates, c) Enroute procedures do not require its use, and d) Alternate procedures are established and used. | | | | | | (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 23-4 AIRCRAFT: PC-12/47E 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 8. High Frequency (HF) Communication System (Cont’d) C - 0 (O) Non ETOPS: May be inoperative while conducting operations that require two LRCS provided: a) SATVOICE and/or SATCOM CPDLC system operates normally, b) SATVOICE or CPDLC services are available as a LRCS over the intended route of flight and to all required alternates, c) Enroute procedures do not require its use, d) Alternate procedures are established and used, and e) SATVOICE/SATCOM CPDLC uses two independent FAA- accepted service providers. | | | | | | | | | | | | | | | | | | 9. Oxygen Mask Microphones C 2 1 May be inoperative on right side for operations not requiring a second in command. | | | 10. *** Selective Call Systems (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. A) Channels 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. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 23-5 AIRCRAFT: PC-12/47E 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 11. Emergency Locator Transmitter (ELT) | A) *** Survival Type ELTs D - - Any in excess of those required by 14 CFR may be inoperative or missing. B) *** Fixed ELTs A - 0 (M) May be inoperative provided: a) System is deactivated, and b) Repairs are made within 90 consecutive calendar-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 consecutive calendar-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. C) *** Remote ELT Switch D - 0 (M) May be inoperative provided: a) Remote ELT switch is deactivated, and b) ELT switch is placed in the ARMED mode. D) *** ELT Indicator Light D - 0 May be inoperative. | E) *** ELT Aural Alarm D - 0 May be inoperative. | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 23-6 AIRCRAFT: PC-12/47E 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. Flight Deck Headsets Earphones/Headphones and Boom Microphones (HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE) | A) Headset Boom Microphones 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. B) Headset Earphones/ Headphones C - 1 May be inoperative provided associated flight deck speaker operates normally. D - - Any in excess of those required by regulation may be inoperative. C) Active Noise Canceling/Reduction Function D - 0 May be inoperative provided normal audio function of headset is operative. D) Flight Deck Hand Microphones C - 0 May be inoperative provided associated boom microphone operates normally. D - 0 Any in excess of those required by regulation may be inoperative. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 23-7 AIRCRAFT: PC-12/47E 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 Deck Headsets Earphones/Headphones and Boom Microphones (OPERATOR OTHER THAN A HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE) | Flight Deck Headsets/ Headphones D - - Any in excess of those required by regulation may be inoperative. A) Headset Boom Microphones 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. B) Headset Earphones/ Headphones C - 1 May be inoperative provided associated flight deck speaker operates normally. C) Active Noise Canceling/Reduction Function D - 0 May be inoperative provided normal audio function of headset is operative. D) Flight Deck Hand Microphones C - 0 May be inoperative provided associated boom microphone operates normally. D - 0 Any in excess of those required by regulation may be inoperative. 14. *** Datalink D 1 0 May be inoperative provided that procedures do not require its use. | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 23-8 AIRCRAFT: PC-12/47E 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 15. *** SATCOM System D 1 0 May be inoperative provided that procedures do not require its use. | | 16. Audio Control Panel D - - For single pilot operations, Co-Pilot Audio Control Panel may be inoperative. | | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 24-1 AIRCRAFT: PC-12/47E 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. Emergency Power System (EPS) C 1 0 May be inoperative except for 14 CFR part 135 IFR passenger carrying operations. 2. Generator C 2 1 Generator 1 may be inoperative provided: a) Flight is conducted VFR, b) Flight is not conducted in known or forecast icing conditions, c) Operations do not require its use, and d) Flight is conducted above -15 °C IOAT. | 3. External Power System D 1 0 May be inoperative. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 25-1 AIRCRAFT: PC-12/47E 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. Cockpit Shoulder Harness C - - Right side may be inoperative provided Seat is not occupied. 2. Passenger Seat(s) (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) Affected seat(s) is blocked and placarded “DO NOT OCCUPY”. NOTE 1: A seat with an inoperative seat belt or shoulder harness is considered inoperative. NOTE 2: Affected seat(s) may include the seat(s) behind and/or adjacent outboard seats. | | | | | | | | | | | | 3. Positioning controls 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 - - May be inoperative and seat occupied provided seat is immovable in the taxi, takeoff, and landing (TTL) position. 4. Under Seat Baggage Restraining System C - - (O) May be inoperative provided: a) Baggage is not stowed under seat with inoperative restraining system, b) Associated seat is placarded “DO NOT STOW BAGGAGE UNDER THIS SEAT”, and c) Procedures are established to alert Cabin Crew of inoperative restraining system. | | | | | | | U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 25-2 AIRCRAFT: PC-12/47E 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 5. Armrests A) With Seat Positioning Controls for Taxi, Takeoff, and Landing (TTL) and/or Other Controls 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. | | | | | | | | | B) Without Seat Positioning Controls for Taxi, Takeoff, and Landing (TTL) and/or Other Controls D - - May be inoperative or missing and seat occupied provided it does not restrict access to any emergency exit, egress route, or main aisle. 6. Seat Belt/Air Bag Restraint Systems A) Seat Belt/Air Bags Required by 14 CFR D - - May be inoperative provided affected seat is blocked and placarded “DO NOT OCCUPY”. B) Seat Belt/Air Bags Not Required by 14 CFR D - - (M) May be inoperative or disconnected provided seat belt operates normally. 7. *** Non-Essential Equipment & Furnishings (NEF) - - 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 operators (insert name) Manual. (M) and (O) procedures, if required, must be available to the flightcrew and included in the operator’s appropriate document. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 25-3 AIRCRAFT: PC-12/47E 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 8. Flotation Equipment D - - Any in excess of those required by 14 CFR may be inoperative or missing. 9. Emergency Medical Kit (EMK) and/or Associated Equipment A - 0 Any in excess of those required by 14 CFR may be incomplete, missing, or inoperative. NOTE: Medical equipment installed in the aircraft as part of an 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. | | | | A) *** Tamper Seals or Tags C - - (O) May be inoperative, damaged, or missing provided proper installation and operation is verified at each preflight. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 25-4 AIRCRAFT: PC-12/47E 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 10. First Aid Kit (FAK) and/or Associated Equipment D - - Any in excess of those required by 14 CFR may be incomplete or removed. NOTE: Medical equipment installed in the aircraft as part of an 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. | | | | A) Tamper Seals or Tags C - - (O) May be inoperative, damaged, or missing provided proper FAK servicing is verified at each preflight. 11. Pilot Seat(s) A) Vertical Adjustment C 2 0 May be inoperative provided Seat is secured in a position acceptable to the pilot before flight (no additional Cushions acceptable). B) Fore and Aft Adjustment C 2 0 May be inoperative provided Seat is secured in a position acceptable to the pilot before flight (no additional Cushions acceptable). NOTE: Rudder Pedal Adjustment must be operative. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 25-5 AIRCRAFT: PC-12/47E 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 12. Storage Bins/Cabin, Galley and Lavatory Storage Compartments/Closets C - - (M) May be inoperative provided: a) Procedures are established to secure the affected bin, compartment, or closet CLOSED, b) Affected Bin compartment or closet is prominently placarded “DO NOT USE”, c) Any Emergency Equipment located in affected Compartment is considered inoperative, and d) Affected bin, compartment, or closet is not used for storage of any item(s) except for those permanently affixed. NOTE: For overhead bins, if no Partitions are installed, the entire Overhead Storage Compartment is considered one bin and inoperative. (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 25-6 AIRCRAFT: PC-12/47E 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 12. Storage Bins/Cabin, Galley and Lavatory Storage Compartments/Closets (Cont’d) C - - (M)(O) May be inoperative provided: a) For non-retractable doors, affected door is removed, b) For retractable doors, affected door is removed or secured in the retracted (fully open) position, c) Affected Bin or Compartment is not used for storage of any items, except those permanently affixed, d) Associated Bin or Compartment is prominently placarded “DO NOT USE”, e) Procedures are established and used to alert crewmembers and passengers of inoperative Bins, and f) Passengers are briefed that associated Bin or Compartment is not used. NOTE 1: For overhead bins, if no partitions are installed, the entire overhead bin is considered inoperative. NOTE 2: Any emergency equipment located in the affected bin, compartment, or closet (permanently affixed) is available for use. A) *** Storage Compartment Key Locks D - - (M) May be inoperative in the unlocked position provided doors can be secured by other means. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 25-7 AIRCRAFT: PC-12/47E 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 13. *** Cargo Restraint Systems A - - (M) May be inoperative or missing provided: a) Approved cargo‑loading limits are observed. The only source documents are: • Type certificate (TC), • Supplemental Type Certificate (STC), • Airplane Flight Manual (AFM), • Airplane Flight Manual Supplement (AFMS), • Pilot’s Operating Handbook (POH), • TC/STC Weight and Balance Manual (WBM), and b) Repairs are made within 120 consecutive calendar‑days. A - - May be inoperative or missing provided: a) Cargo Compartment remains empty, and b) Repairs are made within 120 consecutive calendar‑days. A - - Individual cargo areas may be inoperative provided: a) Aircraft is operated in accordance with Original Equipment Manufacturer (OEM) W&B source document, and b) Repairs are made within 120 consecutive calendar-days. | | | | | | | 14. Cockpit Sun Visors C - - May be inoperative or missing provided there is no field of vision restriction for the flightcrew. 15. “Fasten Seat Belt While Seated” Sign or Placards C - - One or more Signs or Placards may be illegible or missing provided a legible Sign or Placard is visible from each occupied Passenger Seat. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 25-8 AIRCRAFT: PC-12/47E 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 16. Cockpit Smoke Vision System D - 0 May be inoperative or missing. 17. Portable Flashlights/Flashlight Holders C - - May be inoperative or removed provided: a) Crewmember assigned to the affected position has an equivalent operative flashlight readily available, b) Inoperative flashlight remains in a certified location or is removed from the aircraft, and c) Location placarding is removed or obscured. D Any in excess of those required for the intended flight may be inoperative or missing. A) *** Tamper Seals or Tags C (O) May be inoperative, damaged, or missing provided proper installation and operation is verified at each preflight. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 6 DATE: XX/XX/XXXX PAGE NO. 26-1 AIRCRAFT: PC-12/47E TABLE KEY 1. REPAIR CATEGORY 2. NO. INSTALLED 3. NO. REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 26. Fire Protection Sequence No. Item 1 2 3 4 Change Bar 1. Portable Fire Extinguisher D - - Any in excess of those required by 14 CFR may be inoperative or removed provided: a) Inoperative fire extinguisher remains in a certified location until removed from the aircraft at the next suitable maintenance facility, b) Location placarding is removed or obscured, and c) Required distribution is maintained. NOTE: Inoperative fire extinguishers, removed from a certified location or removed from the aircraft, are subject to 49 CFR dangerous goods regulations. A) *** Tamper Seals or Tags C - - (O) May be inoperative, damaged, or missing provided proper installation and operation is verified at each preflight. |