Sequence No. Item 1 2 3 4 Change Bar 50-01 *** Cockpit Voice Recorder (CVR) -01 With Flight Data Recorder Installed A 1 0 May be inoperative provided: Flight data recorder operates normally, and Repairs are made within 3 flight days. -02 Without Flight Data Recorder Installed A 1 0 May be inoperative provided repairs are made within 3 flight days. -03 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 applicable 14 CFR. -04 Independent Power Source C 1 0 -50-02 *** Flight Deck Headsets Earphone/Headphones and Boom Microphones D - - Any in excess of those required by 14 CFR may be inoperative. -01 Headset Boom Microphones (For the Holder of an Air Carrier or Commercial Operator Certificate) A - 0 May be inoperative provided: Associated hand microphone is installed and operates normally, and Repairs are made within 3 flight days. -10 Headset Boom Microphones (For an Operator other than a Holder of an Air Carrier or Commercial Operator Certificate) A - 0 May be inoperative provided: Associated hand microphone is installed and operates normally, and Repairs are made in accordance with applicable regulations. (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 11 DATE: 02/04/2014 PAGE NO. 23-4 AIRCRAFT: Cessna 208/208B KEY REPAIR CATEGORY NO. INSTALLED NO. REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS 23. Communications Sequence No. Item 1 2 3 4 Change Bar
-50-02 *** Flight Deck Headsets Earphone/Headphones and Boom Microphones (Cont’d) -20 Headset Earphones/Headphones C - 1 May be inoperative provided associated flight deck speaker operates normally. -02 Active Noise Canceling/Reduction Function D - 0 May be inoperative provided normal audio function of headset is operative. -50-03 *** Headset System C - 0 May be inoperative provided associated cockpit speaker is operative. -50-04 Hand Microphone C 1 0 May be inoperative provided an operative boom/headset microphone(s) is available. -01 Hand Microphone Jack C 1 0 May be inoperative provided an operative boom/headset microphone(s) is available. -02 Hand Microphone Holder C 1 0 (O) May be inoperative provided microphone is secured by alternate means. -50-05 Cockpit Speakers System (Including Audio Amp) C 2 1 One may be inoperative provided: System is not required by 14 CFR, Affected speaker is not required for procedures, and Headset is used for associated inoperative speaker, including during emergency procedures. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 11 DATE: 02/04/2014 PAGE NO. 23-5 AIRCRAFT: Cessna 208/208B TABLE KEY REPAIR CATEGORY NO. INSTALLED NO. REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS 23. Communications Sequence No. Item 1 2 3 4 Change Bar -50-07 Panel (KMA 24 or KMA 24H)
-05 *** Intercom Squelch Control (VOX) C 1 0 May be inoperative provided associated squelch is acceptable to flightcrew. -50-08 Audio Panel (GMA 340/347) -01 Audio Selector (COM 1, COM 2, COM 3, NAV 1, NAV 2, DME, ADF, ADF 1, ADF 2, TEL Button or Annunciator) C - 0 Individual selectors may be inoperative provided: Procedures do not require use of associated communications system, and Associated communications system is not required by 14 CFR. -02 Mic Selector (COM 1 MIC, COM 2 MIC, COM 3 MIC, PA Button or Annunciator) C 4 0 Individual selectors may be inoperative provided: Procedures do not require use of associated communications system, and Associated communications system is not required by 14 CFR. -03 Speaker Selector (SPKR Button or Annunciator) C 1 0 May be inoperative provided speakers are not required or used. -04 *** Split Comm Selector (COM 1/2 Button or Annunciator) C - 0 (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 11 DATE: 02/04/2014 PAGE NO. 23-7 AIRCRAFT: Cessna 208/208B KEY REPAIR CATEGORY NO. INSTALLED NO. REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS 23. Communications Sequence No. Item 1 2 3 4 Change Bar -50-08 Audio Panel (GMA 340/347) (Cont’d) -05 Intercom Selector (PILOT, CREW Button or Annunciator)
Associated communications system is not required by 14 CFR. -03 Mic Selector Annunciator (COM 1 MIC, COM 2 MIC, COM 3 MIC) C - 0 May be inoperative provided crew refers to PFD frequency boxes for active transmit frequency (shown in green). -04 Audio Selector (COM 1, COM 2, COM 3, TEL, MUSIC, DME, NAV 1, NAV 2, ADF, AUX Button or Annunciator) C - 0 Individual selectors may be inoperative provided: Procedures do not require use of associated communications system, and Associated communications system is not required by 14 CFR. -06 Speaker Selector (SPKR Button or Annunciator) C - 0 May be inoperative provided speakers are not required or used. (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 11 DATE: 02/04/2014 PAGE NO. 23-10 AIRCRAFT: Cessna 208/208B TABLE KEY REPAIR CATEGORY NO. INSTALLED NO. REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS 23. Communications Sequence No. Item 1 2 3 4 Change Bar -50-09 Audio Panel (GMA 1347) (Cont’d) -07 Manual Squelch Selector (MAN SQ Button or Annunciator) C - 0 May be inoperative provided associated squelch is acceptable to flightcrew. -08 Clearance Playback (PLAY Button) D - 0 -10 C - 0 (O) May be inoperative provided flightcrew verify no stations are isolated. -09 Intercom Selector (PILOT, COPLT Button or Annunciator)
REVISION NO. 11 DATE: 02/04/2014 PAGE NO. 24-2 AIRCRAFT: Cessna 208/208B TABLE KEY REPAIR CATEGORY NO. INSTALLED NO. REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS 24. Electrical Sequence No. Item 1 2 3 4 Change Bar -32-01 *** On Board Battery Charger System (STC SA2536SO) -01 C 1 0 May be inoperative provided: On board battery charger override control switch is placed to OFF, and Aircraft charging system operates normally. -02 Battery Minder (STC SA02291AK) C 1 0 May be inoperative provided the aircraft charging system operates normally. -32-02 *** Battery State of Charge Indicator (STC SA02291AK) C 1 0 May be inoperative provided not required for 14 CFR part 135 passenger carrying operations. -39-01 Cockpit 12-Volt Direct Current Power Outlet C 1 0 (M) May be inoperative provided system is deactivated. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 11 DATE: 02/04/2014 PAGE NO. 25-1 AIRCRAFT: Cessna 208/208B TABLE KEY REPAIR CATEGORY NO. INSTALLED NO. REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS 25. Equipment/Furnishings Sequence No. Item 1 2 3 4 Change Bar -10-01 Flightcrew Seat (per seat) -01 Seat Back Adjustment C 1 0 May to be inoperative provided: Affected seat is failed in a latched position that permits pilot normal visibility,
Aircraft is not operated in known, forecast, or POH/AFM defined icing conditions, and Autopilot is disengaged prior to operating standby flap system. (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 11 DATE: 02/04/2014 PAGE NO. 27-2 AIRCRAFT: Cessna 208/208B TABLE KEY REPAIR CATEGORY NO. INSTALLED NO. REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS 27. Flight Controls Sequence No. Item 1 2 3 4 Change Bar -50-02 Primary Flap System (Continued) -02 TKS Equipped Aircraft C 1 0 (M) May be inoperative provided: Standby flap system is operative, Flap position indicator is operative, Aircraft is not operated in known, forecast, or POH/AFM defined icing, and Autopilot is disengaged prior to operating standby flap system. -03 Non TKS/Non Pneumatic Booted Aircraft C 1 0 (M) May be inoperative provided: Standby flap system is operative, Flap position indicator is operative, and Autopilot is disengaged prior to operating standby flap system. -50-03 Standby Flap System C 1 0 May be inoperative provided the primary flap system is operative. -70-01 Rudder Gust Lock C 1 0 (M) May be inoperative provided gust lock is secured in the unlocked position.
Sequence No. Item 1 2 3 4 Change Bar -25-02 *** MultiFunction Display (GMX200, BendixKing, or Equivalent) (Cont’d) -20 *** C 1 0 May be inoperative in accordance with existing TCAS MMEL relief. -09 *** Weather Information Datalink (FIS) D 1 0 May be inoperative. -10 *** Chartview (CHART) D 1 0 May be inoperative or out of currency. NOTE: Comply with POH/AFM Limitations. -25-03 Copilot Side Primary Flight Display (PFD) or STC SA02153LA-D Only) B - 0 May be inoperative for operations not requiring second in command. -25-04 Radio Magnetic Indicator (RMI) C - 0 -25-05 Aviation Database for G600 (Aircraft modified by STC SA02017SE-D or SA02153LA-D Only) Deleted, Revision 11. -25-06 Obstacle Database for G600 (Aircraft modified by STC SA02017SE-D or SA02153LA-D Only) Deleted, Revision 11. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 11 DATE: 02/04/2014 PAGE NO. 34-10 AIRCRAFT: Cessna 208/208B TABLE KEY REPAIR CATEGORY NO. INSTALLED NO. REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS 34. Navigation Sequence No. Item 1 2 3 4 Change Bar -25-07 Safe Taxi Database Deleted, Revision 11. -01 G600 (Aircraft modified by Deleted, Revision 11.
-20 C 3 0 May be inoperative provided remote annunciator panel is installed and operative. -30 C 3 0 May be inoperative provided marker audio is operative and used. -03 Selector/Mute (MKR-MUTE Button or Annunciator) C 1 0 May be inoperative provided procedures do not require marker -04 Sensitivity Annunciator (HI - LO) C 2 0 -05 Sensitivity Selector (SENS Button) C 1 0 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 11 DATE: 02/04/2014 PAGE NO. 34-13 AIRCRAFT: Cessna 208/208B TABLE KEY REPAIR CATEGORY NO. INSTALLED NO. REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS 34. Navigation Sequence No. Item 1 2 3 4 Change Bar -34-03 Marker Beacon Receiver (GMA1347) -01 Marker Beacon Function C 1 0 May be inoperative provided: Procedures do not require its use, and System is not required by 14 CFR. -02 Selector/Mute (MKR-MUTE Button or Annunciator) C - 0 May be inoperative provided procedures do not require marker audio. -03 High Sensitivity Selector (HI SENS Button or Annunciator) C - 0 May be inoperative provided: Procedures do not require its use, and System is not required by 14 CFR. -42-01 Weather Detection Equipment C 1 0 May be inoperative provided system is not required by 14 CFR.
REVISION NO. 11 DATE: 02/04/2014 PAGE NO. 34-15 AIRCRAFT: Cessna 208/208B TABLE KEY REPAIR CATEGORY NO. INSTALLED NO. REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS 34. Navigation Sequence No. Item 1 2 3 4 Change Bar -44-01 Terrain Awareness Warning System (TAWS)/Ground Proximity Warning System Class B TAWS Equipment Required (Cont’d) -50 *** Windshear Mode (Reactive) C 1 0 (O) May be inoperative provided alternate procedures are established and used. -02 Terrain System Forward Looking Terrain Avoidance (FLTA) and Premature Descent Alert (PDA) Functions B 1 0 -03 *** Terrain Displays C - 0 -04 *** Runway Awareness and Advisory System (RAAS) C 1 0 -05 *** Class C TAWS/GPWS Equipment C 1 0 (O) May be inoperative provided alternate procedures are established and used. NOTE: Any mode that operates normally may be used. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 11 DATE: 02/04/2014 PAGE NO. 34-16 AIRCRAFT: Cessna 208/208B KEY REPAIR CATEGORY NO. INSTALLED NO. REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS 34. Navigation
Sequence No. Item 1 2 3 4 Change Bar -44-02 Radio Altimeter -01 A 1 0 (M) May be inoperative provided: Approach minimums or operating procedures do not require its use, System is deactivated and secured, and Repairs are made within 2 flight days. -02 C 1 0 May be inoperative provided approach procedures do not require its use. -45-01 *** Traffic Alert and Collision Avoidance System -01 Traffic and Collision Avoidance System (TCAS I) -10 B - 0 (M) May be inoperative provided: System is deactivated and secured, and Enroute or approach procedures do not require its use. -20 C - 0 (M) May be inoperative provided: Not required by 14 CFR, System is deactivated and secured, and Enroute or approach procedures do not require its use. (Continued) U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 11 DATE: 02/04/2014 PAGE NO. 34-17 AIRCRAFT: Cessna 208/208B TABLE KEY REPAIR CATEGORY NO. INSTALLED NO. REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS 34. Navigation Sequence No. Item 1 2 3 4 Change Bar
REVISION NO. 10 DATE: 08/20/2013 PAGE NO. 73-1 AIRCRAFT: Cessna 208/208B KEY REPAIR CATEGORY NO. INSTALLED NO. REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS 73. Engine Fuel and Control Sequence No. Item 1 2 3 4 Change Bar -20-01 Auto Start System (STC SA02291AK) C 1 0 May be inoperative provided manual ground start procedures and limits are observed. -20-02 Single Red Line Computer System (STC SA02291AK) C 1 0 May be inoperative provided inoperative SRL System procedures and limits are observed. -20-03 Torque Temperature Limiter System (STC SA02291AK) C 1 0 May be inoperative provided inoperative SRL System procedures and limits are observed. -20-04 Fuel Flow Indicator C 1 0 May be inoperative provided the left and fuel quantity indicators are operative. -20-05 *** Shadin ETM Fuel Flow function (STC SA02291AK) C 1 0 May be inoperative provided the left and right fuel quantity indicators are operative. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 8 DATE: 01/23/2013 PAGE NO. 76-1 AIRCRAFT: Cessna 208/208B TABLE KEY REPAIR CATEGORY NO. INSTALLED NO. REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS 76. Engine Control Sequence No. Item 1 2 3 4 Change Bar -00-01 *** Fuel Condition Lever LowIdle Lock Assembly (STC SA01296SE) C 1 0 (M) May be inoperative provided lock assembly is deactivated. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM EQUIPMENT LIST REVISION NO. 8 PAGE NO. 77-1
80. Starting Sequence No. Item 1 2 3 4 Change Bar -00-01 Starter/Generator Speed Sensor (Cont’d) -02 G1000 (867 SHP) A 1 0 (O) May be inoperative provided: Starter switch is turned off when Ng obtains a minimum of 55 percent Ng. STARTER ON amber annunciator is monitored in accordance with POH/AFM starting engine normal procedures, Alternate procedures are established and used for tracking engine starts, and Engine is not operated for more than 10 starts. | | | | | | | | | | | | | |