-20-01 Cabin Overhead Air Outlet C - 0 | -20-02 Cockpit Overhead Air Outlet (Units -0001 thru -0500) C 2 0 | | -20-02 Cockpit Overhead Air Outlet (Units -0501 and on) C 4 0 | | -21-02 Baggage Compartment Warm Air Fan C 1 0 | | -21-03 Cabin Recirculation Fan (WEMAC Boost) (Units -0001 thru -0500) C 1 0 | | | -21-06 Glareshield Fan C 2 1 | -21-08 Nose Avionics Cooling Fan (Ref Des (Units -0001 thru -0500) C 1 0 | | | -30-01 Cabin Dump Function (Unpressurized) C 1 0 (M) May be inoperative provided: One outflow valve is removed, and Cabin pressurization system is considered inoperative (Refer to item 21-30-02). | | | | | | -30-02 Cabin Pressurization System | |
-00A (Unpressurized with cabin occupants) (Units -0001 thru -0500) C 1 0 (O) May be inoperative provided: Baggage compartment remains empty (excluding ballast and/or fly away kits), PRESSURIZATION NORM/MANUAL switch is selected to MANUAL, CABIN DUMP is selected ON, ISO VLV CLOSE is selected ON, Aircraft is operated at 13,500 feet cabin altitude or below, and Flight crew oxygen system is used as required by 14 CFR. NOTE 1: CABIN ALTITUDE amber message may appear at 8,500 feet cabin altitude. CABIN ALTITUDE red message may appear at 10,000 feet cabin altitude. NOTE 2: Operator's MEL should define which items are approved for inclusion in fly away kits and which materials can be used as ballast. | | | | | | | | | | | | | | | | | | | | | | | (Continued) -30-02 Cabin Pressurization System (Continued)
-00A (Unpressurized with cabin occupants) (Units -0501 and on) C 1 0 (O) May be inoperative provided: Baggage compartment remains empty (excluding ballast and/or fly away kits), PRESSURIZATION AUTO/MAN switch is selected to MANUAL, DUMP is selected to DUMP, BAG ISOL is selected to CLOSED, Aircraft is operated at 13,500 feet cabin altitude or below, and Flight crew oxygen system is used as required by 14 CFR. NOTE 1: ALTITUDE amber or red message may appear at 8,000 feet cabin altitude and CABIN ALTITUDE aural warning may sound. NOTE 2: Operator's MEL should define which items are approved for inclusion in fly away kits and which materials can be used as ballast. | | | | | | | | | | | | | | | | | | | | | | | | (Continued) -30-02 Cabin Pressurization System (Continued)
-00B (Unpressurized without cabin occupants) (Units -0001 thru -0500) C 1 0 (O) May be inoperative provided: Baggage compartment remains (excluding ballast and/or fly away kits), PRESSURIZATION NORM/MANUAL switch is selected to MANUAL, CABIN DUMP is selected ON, ISO VLV is selected ON, PASS OXY is selected OFF, No cabin occupants are carried, Aircraft is operated at or below, and Flight crew oxygen system is used as required by 14 CFR. NOTE 1: CABIN ALTITUDE amber message may appear at 8,500 feet cabin altitude. CABIN ALTITUDE red message may appear at 10,000 feet cabin altitude. NOTE 2: Operator's MEL should define which items are approved for inclusion in fly away kits and which materials can be used as ballast. | | | | | | | | | | | | | | | | | | | | | | | | | (Continued) -30-02 Cabin Pressurization System (Continued)
-30-04 Baggage Compartment Pressurization System (Excludes aft baggage door seal) (Units -0501 and on) C 1 0 May be missing or inoperative provided: BAG ISOL is selected to CLOSED, Aircraft is operated in accordance with AFM baggage pressurization system limitations, and Aircraft is operated at or below. NOTE: BAGGAGE ALTITUDE amber message may appear if baggage altitude exceeds 13,000 feet. | | | | | | | | | | | | -31-01 Cabin Pressurization Control Panel | | -01 Manual Altitude Lever ALT) C 1 0 May be inoperative provided cabin pressurization system is considered inoperative (Refer to item 21-30-02). | | | -02 Manual Rate Selector (RATE) C 1 0 May be inoperative or knob missing provided cabin pressurization system is considered inoperative (Refer to item | | | | (Continued) -31-01 Cabin Pressurization Control Panel (Continued) -03 Altitude Selector ("A" Knob) (Units -0001 thru -0500) C 1 0 May be inoperative or knob missing provided cabin pressurization system altitude select mode is considered inoperative (Refer to item 21-31-02-02). | | | |
-04 Cabin Pressurization Mode Switch (NORM/ALT SEL) -0001 thru -0500) C 1 0 May be inoperative provided non-selected mode is considered inoperative (Refer to item 21-31-02). | | | | -05 Cabin/Aircraft Altitude Selector Gauge -0001 thru -0500) C 1 0 May be inoperative or knob missing provided pressurization system altitude select mode is considered inoperative (Refer to item 21-31-02-02). | | | | -06 Cabin/Aircraft Altitude Selector Gauge Lighting (Units -0001 thru -0500) C 1 0 May be inoperative provided flight crew determines adequate natural or artificial lighting exists to read gauge. | | | -31-02 Cabin Pressurization System Mode | | -01 Automatic Schedule Mode (NORM) (Units -0001 thru -0500) C 1 0 May be inoperative provided: Altitude select mode is operative, PRESSURIZATION NORM / ALT SEL switch is selected to ALT SEL, Cabin differential pressure gauge/indication is operative, altitude gauge/indication is operative, Cabin vertical speed gauge/indication is operative, and Aircraft is operated at FL410 or below. | | | | | | | | | | | | |
-01 Automatic Schedule Mode -0501 and on) PRESSURIZATION FAULT message) C 1 0 May be inoperative provided: Altitude select mode is operative, MODE is selected to ALTITUDE SELECT on GTC Cabin Pressure Page, Cabin differential pressure gauge/indication is operative, Cabin altitude gauge/indication is operative, Cabin vertical speed gauge/indication is operative, and Aircraft is operated at FL410 or below. | | | | | | | | | | | | | (Continued) -31-02 Cabin Pressurization System Mode (Continued) -02 Altitude Select Mode (ALT SEL) (Units -0001 thru -0500) C 1 0 May be inoperative provided: Automatic schedule mode is operative, PRESSURIZATION NORM / ALT SEL switch is selected to NORM, Cabin differential pressure gauge/indication is operative, Cabin altitude gauge/indication is operative, Cabin vertical speed gauge/indication is operative, and Aircraft is operated at or below. | | | | | | | | | | | | |
-02 Altitude Select Mode (Units -0501 and on) C 1 0 May be inoperative provided: Automatic schedule mode is operative, MODE is selected to NORMAL on GTC Cabin Pressure Page, Cabin differential pressure gauge/indication is operative, Cabin altitude gauge/indication is operative, vertical speed gauge/indication is operative, and Aircraft is operated at or below. | | | | | | | | | | | | | -04 Any Mode (Excluding manual) (Units -0001 thru -0500) C 2 0 May be inoperative provided: Autopilot system is operative, PRESSURIZATION NORM/MANUAL switch is selected to MANUAL, and Aircraft is operated using manual pressurization. | | | | | | | (Continued) -31-02 Cabin Pressurization System Mode (Continued) -04 Any Mode (Excluding manual) -0501 and on) C 2 0 May be inoperative provided: Autopilot system is operative, PRESSURIZATION AUTO/MAN is selected to MANUAL, and Aircraft is operated manual pressurization. | | | | | | Manual Mode Deleted, revision 06. | -32-01 Altitude Gauge/Indication | |
-00A (Pressurized) C 1 0 (O) May be inoperative provided: Cabin pressurization system automatic schedule mode is operative and used, differential pressure gauge/indication is operative, and A chart is provided to convert differential pressure and aircraft altitude to cabin altitude. | | | | | | | | | -00B (Unpressurized) C 1 0 May be inoperative provided cabin pressurization system is considered inoperative (Refer to item 21-30-02). | | | -01 Gauge Lighting (Units -0001 thru -0500) C 1 0 May be inoperative provided flight crew determines adequate natural or artificial lighting exists to read gauge. | | | -32-02 Differential Pressure Gauge/Indication | | -00A (Pressurized) C 1 0 (O) May be inoperative provided: Cabin pressurization system automatic schedule mode is operative and used, Cabin altitude gauge/indication is operative, and A chart is provided to convert cabin and aircraft altitude to differential pressure. | | | | | | | | | -00B (Unpressurized) C 1 0 May be inoperative provided pressurization system is considered inoperative (Refer to item 21-30-02). | | | -32-03 Cabin Vertical Speed Gauge/Indication | |
-00A (Pressurized) -0501 and on) C 2 1 One may be inoperative provided: Affected PAC is selected OFF, MAX COOL is selected OFF, and Aircraft is operated at FL410 or below. | | | | | -00B (Unpressurized) C 2 0 May be inoperative provided cabin pressurization system is considered inoperative (Refer to item 21-30-02). | | | (Continued) -50-04 Pressurization Air Conditioning (PAC) System (Continued) -01A Bi-Level Flow Control Valve C 2 1 (M) One may be inoperative provided: Affected valve is secured closed, and Aircraft is operated at FL410 or below. | | | | | -01B Bi-Level Flow Control Valve (Units -0001 thru -0500) C 2 1 One may be inoperative provided: Associated ENG BLD AIR is selected OFF, ISOL VALVE is selected to CLSD, Opposite PAC is not selected to HIGH, Aircraft is not operated in known, forecast, or AFM-defined icing conditions, and Aircraft is operated at FL410 or below. | | | | | | | | | | |
-02 Cockpit C 1 0 | (Continued) -62-01 Temperature Indication System (Continued) -03 Supply Duct C 2 1 One may be inoperative provided: Associated air temperature control system automatic mode is considered inoperative (Refer to item 21-60-01-01), and Associated DUCT O'TEMP amber message is monitored during temperature adjustment. | | | | | | | | -70-01 Water Separator C 2 1 May be inoperative provided affected PAC is considered inoperative (Refer to item 21-50-04). | | |
-10-01 Autopilot Disconnect Button (AP/TRIM/NWS DISC) (Failed deselected) | | | -00A Left Control Wheel C 1 0 (O) May be inoperative provided: Right control wheel button is operative, Alternate procedures for disconnecting nose wheel steering during ground operations are established and used, A pilot remains seated in right seat with seat belt fastened during all autopilot operations, Autopilot system is not used AFM cruise minimum use height, and Approach minimums do not require use of autopilot system. | | | | | | | | | | | | | | | -00B Right Control Wheel C 1 0 May be inoperative provided: Left control wheel button is operative, A pilot remains seated in left seat with seat belt fastened during all autopilot operations, Autopilot system is not used below AFM cruise minimum use height, and Approach minimums do not require use of autopilot system. | | | | | | | | | | | -10-02 Autopilot Interrupt/Flight Director Sync Button (TCS) (Units -0001 thru -0500) C 2 0 | | | |
-10-02 Autopilot Interrupt/Flight Director Sync Button (CWS) -0501 and on) C 2 0 | | | | -10-03 Autopilot System (Units -0001 thru -0500) | | -00A (Single channel failed) (Units -0001 thru -0500) C 2 1 One may be inoperative provided operative autopilot channel is selected. | | -00B (Both channels failed) (Units -0001 thru -0500) B 2 0 (M) May be inoperative provided: Autopilot system is deactivated, Enroute procedures and approach minimums do not require use of autopilot system, Cabin pressurization system is not operated in manual mode, and Aircraft is not operated RVSM. NOTE: A PRIMARY STAB TRIM FAIL may result if autopilot system is deactivated before flight guidance system self test is completed. | | | | | | | | | | | | | | -10-03 Autopilot System (Units -0501 and on) AP FAIL message) B 1 0 (M) May be inoperative provided: Autopilot system is deactivated, Yaw damper is considered inoperative (Refer to item Enroute procedures and approach minimums do not require use of autopilot system, Cabin pressurization system is not operated in manual mode, and Aircraft is not operated RVSM. | | | | | | | | | | | -10-04 Takeoff/Go-Around Button (GA) | |
-01 Altitude (ALT button) C 1 0 May be inoperative provided appropriate annunciation appears in PFD flight director mode box. | | | -03 Approach (APP button) (Units -0001 thru -0500) C 1 0 May be inoperative provided appropriate annunciation appears in PFD flight director mode box. | | | -03 Approach (APPR button) -0501 and on) C 1 0 May be inoperative provided appropriate annunciation appears in PFD flight director mode box. | | | -04 Autopilot (AP button - A or B annunciation) (Units -0001 thru -0500) C 2 0 May be inoperative provided AP annunciation appears in PFD flight director mode box. | | | | -04 Autopilot (AP button) (Units -0501 and on) C 1 0 May be inoperative provided: AP annunciation appears in PFD flight director mode box, and Associated AP FAIL white message does not appear. | | | | | -05 Back Course (BC button) (Units -0001 thru -0500) C 1 0 May be inoperative provided appropriate annunciation appears in PFD flight director mode box. | | | (Continued) -13-03 Flight Guidance Controller Annunciator (Continued) -05 Back Course (B/C button) (Units -0501 and on) C 1 0 May be inoperative provided appropriate annunciation appears in PFD flight director mode box. | | |
-14 Vertical Speed (VS button) C 1 0 May be inoperative provided appropriate annunciation appears in PFD flight director mode box. | | | -15 Yaw Damper (YD button - A or B annunciation) (Units -0001 thru -0500) B 2 0 May be inoperative provided yaw damper is considered inoperative to item 22-10-05). | | | | -15 Yaw Damper (YD button) (Units -0501 and on) C 1 0 May be inoperative provided YD annunciation appears in PFD flight director mode box. | | | -13-04 Flight Guidance Controller Function Control (GC-810) (Units -0001 thru -0500) | | | | -13-04 Flight Guidance Controller Function Control (GMC 7200) -0501 and on) | | | | -01 Altitude (ALT button) B 1 0 May be inoperative provided: Procedures do not require its use, and Aircraft is not operated RVSM. | | | | -02 Approach (APR button) (Units -0001 thru -0500) B 1 0 May be inoperative provided procedures do not require its use. | | | -02 Approach (APPR button) -0501 and on) B 1 0 May be inoperative provided procedures do not require its use. | | | -03 Autopilot (AP button) B 1 0 May be inoperative provided autopilot system is considered inoperative (Refer to item 22-10-03). | | |
-20-01 Mach Trim System (Units -0501 and on) MACH TRIM FAIL message) C 1 0 May be inoperative provided aircraft is operated in accordance with AFM MACH TRIM FAIL message procedure. | | | | -30-01 *** Autothrottle System (Units -0001 thru -0500) (STC ST01720WI) C 1 0 (M) May be inoperative provided: Autothrottle system is deactivated, and Procedures do not require its use. | | | | -30-01 Autothrottle System (Units -0501 and on) or White AT FAIL message) C 1 0 (M) May be inoperative provided: Autothrottle system is deactivated, and Procedures do not require its use. | | | | -01A Throttle Disengage Button (ATS DISC) (Units -0001 thru -0500) B 2 1 One may be inoperative. | | | -01A Throttle Disengage Button (A/T DISC) (Units -0501 and on) B 2 1 One may be inoperative. | | | -01B Throttle Disengage Button (ATS DISC) (Units -0001 thru -0500) B 2 0 (O) May be inoperative provided: Autothrottle Control Panel Display (CPD) disengage switch is verified operative, and Autothrottles are disengaged below 500 ft AGL. | | | | | | -01B Throttle Disengage Button (A/T DISC) (Units -0501 and on) B 2 0 May be inoperative provided: Both throttle engage buttons are operative, Autothrottles are disengaged using throttle engage button, and Autothrottles are disengaged below 500 ft AGL. | | | | | | |
-00-01 *** Flight Phone / SATCOM System D - 0 May be inoperative provided procedures do not require its use. | | -01 Cockpit Handset D - 0 May be inoperative provided procedures do not require its use. | | -02 Handset D - 0 | -10-01 *** High Frequency (HF) Communication System | | -00A (Dual LRCS not required) D - - Any in excess of those required by 14 CFR may be inoperative. | | -00B (Dual LRCS required) C - 1 (O) May be inoperative while conducting operations which require two Long-Range Communication Systems (LRCS) provided: SATCOM voice or data link operates normally, Alternate procedures are established and used, SATCOM coverage is available over intended of flight, and If SATCOM voice is to be used over intended route of flight, SATCOM voice short codes (INMARSAT) or direct dial commercial numbers (IRIDIUM) must be available. If not available, prior coordination with appropriate ATS (FIR) facility is required. NOTE: SATCOM is to be used only as a backup to normal HF communications. | | | | | | | | | | | | | | | | | | | | | |
-50-02 *** / Observer Intercom System D 1 0 May be inoperative provided procedures do not require its use. | | -01 Switch / Headphone Jack Panel D - 0 | | -50-03 Cockpit Overhead Communication Speaker C 2 1 One may be inoperative provided: Affected speaker is not required for procedures, and A headset is used for associated inoperative speaker. | | | | | -50-04 Cockpit Hand Microphone | -00A D 2 - Any in excess of those required by 14 CFR may be inoperative. | | -00B C 2 0 May be inoperative provided associated boom microphone is operative. | | -01 Jack C - 0 May be inoperative provided associated hand microphone is considered inoperative (Refer to item 23-50-04). | | | -02 Holder D - 0 (O) May be inoperative provided associated hand microphone is secured by alternate means. | | | -50-05 Cockpit Headset and Boom Microphone D - - Any in excess of those required by 14 CFR may be inoperative. | | -01A Boom Microphone (For a holder of an Air Carrier or Commercial Operator Certificate) A - 0 May be inoperative provided: Associated hand microphone is installed and operative, and Repairs are made within three flight days. | | | | |
-01B Boom Microphone (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 operative, and Repairs are made in accordance with 14 CFR. | | | | | -02 Headset Earphones / Headphones C - 1 May be inoperative provided associated cockpit overhead communication speaker is operative. | | | -03 *** Active Noise Reduction (ANR) Function D - 0 May be inoperative provided normal audio function of headset is operative. | | -04 *** Powered Headset System (Units -0001 thru -0500) D - 0 May be inoperative provided headset jack is operative or headset is not used. | | | -04 Powered Headset System (Units -0501 and on) D - 0 May be inoperative provided headset jack is operative or headset is not used. | | | -50-06 Cockpit Headset System C 2 0 May be inoperative provided: Both cockpit overhead communication speakers are used, and Headset audio system is not required by 14 CFR or procedures. | | | | | | | -50-07 Push-to-talk (PTT) Switch (Failed deselected) | | -01 Yoke Switch B 2 1 (O) One may be inoperative provided alternate procedures are established and used for transmitting. | | | -03 *** Remote Pedestal Switch (Units -0001 thru -0500) C - 0 | | powered
-04 *** Remote Side Console Switch -0001 thru -0500) C - 0 | | | -50-08 Radio Management Unit (RMU) (Units -0001 thru -0500) C 2 1 (O) One may be inoperative provided: Standby radio control unit is verified operative, and COM 1 is verified operative. | | | | -60-01 Static Wick NOTE: May include mounting base provided no damage exists to attaching structure. | | | -02 Wing Tip Assembly (Each side) (Units -0001 thru -0500) (Excluding winglet-equipped aircraft) C 3 1 Two may be damaged or missing provided outermost wick is installed and not damaged. NOTE: Wing tip assembly is entire removable section outboard of fuel closure rib. | | | | | | | -03 *** Winglet (Each side) (Units -0001 thru -0500) C 2 1 One may be damaged or missing provided outermost wick is installed and not damaged. | | | -03 Winglet (Each side) (Units -0501 and on) C 2 1 One may be damaged or missing provided outermost wick is installed and not damaged. | | | -04 Wing Trailing Edge (Each side) C 2 1 One may be damaged or missing provided outermost wick is installed and not damaged. NOTE: Wing trailing edge is area between aileron and wing tip assembly. | | | | | | -05 Elevator (Each side) C 3 1 Two may be damaged or missing provided outermost wick is installed and not damaged. | | |
-20-01 Engine AC Generating System C 2 1 One may be inoperative provided affected windshield electric anti-ice system is considered inoperative (Refer to item | | | | -30-01 APU DC Generating System (Units -0001 thru -0500) C 1 0 May be inoperative provided APU SYSTEM GENERATOR is selected OFF. NOTE: APU GEN OFF cyan message may appear. | | | | | -30-01 APU DC Generating System (Units -0501 and on) C 1 0 May be inoperative provided APU GEN is selected OFF. NOTE: DC GEN OFF APU amber message may appear. | | | | | -30-02 Engine DC Generating System -0001 thru -0500) (Excluding split-bus aircraft) A 2 1 One may be inoperative provided: Associated GEN switch is selected OFF, APU DC generating system is used throughout flight, Aircraft is operated at FL310 or below, and Repairs are made within three flight days. NOTE: GEN OFF L or R amber message may appear. | | | | | | | | | | | | -30-02 Engine DC Generating System (Split-bus aircraft) | | |
-00B Right (Units -0501 and on) B 2 1 One may be inoperative provided: R GEN switch is selected OFF, BUS TIE switch is selected CLOSED, Flight remains within one hour of a suitable airport at all points along route, APU DC generating system is used throughout flight, and Aircraft is operated at FL310 or below. NOTE: DC GEN OFF R amber message may appear. | | | | | | | | | | | | | | Main Ship Battery Deleted, Revision 06. | -37-01 APU DC Amperage Gauge/Indication -0001 thru -0500) C 1 0 May be inoperative provided APU SYSTEM GENERATOR is selected OFF. NOTE: APU GEN OFF cyan message may appear. | | | | | -37-01 APU DC Amperage Gauge/Indication (Units -0501 and on) C 1 0 May be inoperative provided APU GEN is selected OFF. NOTE: DC GEN OFF APU amber message may appear. | | | | | -37-02 APU DC Voltage C 1 0 | | -40-01 External System D 1 0 | -50-01 *** AC Cockpit Outlet D - 0 May be inoperative provided procedures do not require its use. | | -60-01 *** DC Cockpit Outlet D - 0 May be inoperative provided procedures do not require its use. | |
-00-01 Required Documents Holder (Airworthiness Certificate, Registration, etc) D 1 0 (O) May be inoperative or missing provided an alternate means of securing and displaying documents is used. | | | -10-01 Cockpit Assist Handle D 1 0 | -10-03 Cockpit Sunvisor System (Including attach mechanism) D - 0 May be missing, or inoperative provided crewmember's field of vision is not obstructed. | | | -10-05 Flight Crew Seat (Per seat) | | -01A Armrest C 2 0 May be inoperative provided affected armrest is stowed in retracted position. | | -01B Armrest C 2 0 (M) May be missing, or inoperative provided affected armrest is removed. | | -02 *** Lumbar Support D 1 0 | | -03 Recline/Tilt Function C 1 0 (M) (O) May be inoperative provided: Affected seat is secured or failed in a position that permits normal visibility, Full flight control movement is available, and Crewmember can reach all necessary controls and equipment while restrained. | | | | | | | | | -04 *** Restraint Buckle Protective Padding D 1 0 May be damaged or missing. | | -05 Support D 1 0 May be inoperative provided full flight control movement is available. | | (Continued)
-10-05 Flight Crew Seat (Per seat) (Continued) -06 Vertical Adjustment C 1 0 (M) (O) May be inoperative provided: Affected seat is secured or failed in a position that permits normal visibility, Full flight control movement is available, and Crewmember can reach all necessary controls and equipment while restrained. | | | | | | | | | -10-07 *** Headset Hook D - 0 | | -10-08 Eye Reference Ball C 3 0 (O) May be inoperative or missing provided alternate procedures are established and used for eye position reference. | | | | -10-09 *** Yoke-mounted Holder D - 0 | | -01 *** D - 0 | | -20-03 *** Cabin Curtain D - 0 (M) May be missing, or inoperative provided curtain is secured open. | | -20-04 Electric Cabin Window Shade (Individual shades or entire system) D - 0 May be inoperative provided affected window shades are failed open or in a position that does not interfere with emergency procedures. | | | |
-20-05 Non-essential Equipment and Furnishings (NEF) - - 0 May be inoperative, damaged or missing provided that item(s) is deferred in accordance with operator’s NEF deferral program. NEF program procedures and processes are outlined in operator’s (insert name) Manual. (M) and (O) procedures, if required, must be available to flight crew and included in operator’s appropriate document. NOTE: Exterior lavatory door ashtray is not considered an NEF item. | | | | | | | | | | | | -20-06 Passenger Seat (Including side-facing seats, folding seats and couches) (Per seat) D - 0 May be inoperative provided: Seat does not block an emergency exit, Seat does not restrict any occupant access to aisle, and Affected seat(s) are blocked and placarded “DO NOT OCCUPY”. NOTE: Affected seat(s) may include seats near inoperative seat(s). | | | | | | | | | | -01 Armrest D - 0 May be missing, or inoperative with seat occupied provided: Armrest does not block an emergency exit, and Armrest does not restrict any cabin occupant from access to aisle. | | | | | | | -02A Seat Controls (Includes recline, headrest, footrest, floor tracking, pedestal tracking, swivel, and other positioning controls) D - 0 (M) May be inoperative with seat occupied provided seat is secured in taxi, takeoff and landing position. | | | | | |
-00A C - 0 (M) May be inoperative provided: Compartment does not contain any aircraft system protection devices, Any emergency equipment located in affected compartment is considered inoperative, Affected compartment is not used for storage of any item except for those permanently affixed, Procedures are established and used to secure compartment closed, and Affected compartment is prominently placarded "DO NOT USE". | | | | | | | | | | | | | | | | -00B C - 0 (M) May be inoperative provided: Affected door is removed, Affected compartment is not used for storage of any item, including those permanently affixed, occupants are briefed that affected compartment may not be used, and Affected compartment is prominently placarded "DO NOT USE". | | | | | | | | | | | (Continued) -50-02 Cabin Storage Compartment (Continued)
-01 Shelving D - 0 (O) May be inoperative provided: Any permanently affixed emergency equipment located on affected shelf is relocated and available for use, and Cabin occupants are briefed on location of relocated equipment. | | | | | | | -02 *** Key Lock D - 0 May be inoperative in unlocked position. | | -60-01 *** Cockpit Smoke Vision System (CSVS) D - 0 May be inoperative or missing. | | -60-02 *** Crash Axe / Survival Tool D - - Any in excess of those required by 14 CFR may be damaged or missing. | | -60-03 Emergency Medical Equipment | | -01 *** Automatic External Defibrillator (AED) (Includes associated equipment) D - 0 | | | | -02 *** Emergency Medical Kit (EMK) (Includes associated equipment) D - 0 | | | | -03 *** First Aid Kit (FAK) (Includes associated equipment) D - - Any in excess of those required by 14 CFR may be incomplete, missing, or inoperative. | | | -61-01 *** Life Preserver (Crew and passenger) D - - Any in excess of those required by 14 CFR may be missing, or inoperative provided affected preserver is placarded "INOPERATIVE" or removed. | | | |
-62-01 Emergency Locator Transmitter (ELT) | | -01 *** Survival Type D - - Any in excess of required by 14 CFR may be inoperative or missing. | | -02A Fixed, Automatic A - 0 (M) May be inoperative provided: System is deactivated or removed, and Repairs are made within 90 calendar days. | | | | | -02B Automatic D - - (M) Any in excess of those required by 14 CFR may be inoperative provided system is deactivated or removed. | | | -03 *** Buzzer (Tail-mounted) C 1 0 | | -64-01 *** Life Raft D - - Any in excess of those required by 14 CFR may be missing, or inoperative provided affected raft is placarded "INOPERATIVE" or removed. | | | |
-11-01 Baggage Compartment Smoke Detection System (Units -0001 thru -0500) C 1 0 May be inoperative provided: Baggage compartment remains empty (excluding ballast and/or fly away kits), ISO VLV CLOSE is selected ON, and Aircraft is operated at FL410 or below. NOTE 1: BAGGAGE ALTITUDE amber message may appear if baggage altitude exceeds 13,000 feet. NOTE 2: Operator's MEL should define which items are approved for inclusion in fly away kits and which materials can be used as ballast. | | | | | | | | | | | | | | | | | -11-01 Baggage Compartment Smoke Detection System -0501 and on) C 1 0 May be inoperative provided: Baggage compartment remains empty (excluding ballast and/or fly away kits), BAG ISOL is selected to CLOSED, and Aircraft is operated at FL410 or below. NOTE 1: BAGGAGE ALTITUDE amber message may appear if baggage altitude exceeds 13,000 feet. NOTE 2: Operator's MEL should define which items are approved for inclusion in fly away kits and which materials can be used as ballast. | | | | | | | | | | | | | | | | | -12-01 APU Fire Detection System (Amber APU FIRE DETECT FAIL or FIRE DETECT FAIL A message) C 1 0 May be inoperative provided APU is considered inoperative (Refer to item | | | |
-01 Wing Tank A 2 1 (O) One indication may be inoperative provided: Both fuel low level indicating systems and both fuel flow indicating systems are operative, Fuel required for to be flown is increased by 10%, Flight is restricted to a maximum of three hours, remaining within one hour of a suitable airport at all points along route, Both fuel tanks are fueled to a known, balanced quantity, APU use is limited to thirty cumulative minutes if LH indicator is inoperative, Fuel use is tracked, If autopilot is used, it is disconnected every twenty minutes to detect possible lateral fuel imbalance, monitor trim required and RETRIM L-R WING DOWN amber message, and Repairs are made within three flight cycles. | | | | | | | | | | | | | | | | | | | | | | | | | | (Continued) -41-02 Fuel Quantity Indicating System (Continued)
-30-01 Hydraulic Reservoir Quantity Indication B 2 1 (M) One may be inoperative provided: Quantity in associated reservoir is verified adequate on reservoir sight gauge prior to every flight, and Associated hydraulic pressure indication is monitored. | | | | | | |
-10-01 Air Anti-Ice Resistive Temperature Device (RTD) (All except TH001, TH002, TH003, TH004, TL017, TL019, TL021, TR018, TR020, TR022, TT017, TT018, TT019, TT020, and TT021) -0001 thru -0500) C - - May be inoperative provided: All ANTI-ICE ENGINE, STABILIZER, and SLAT switches are selected OFF, and Aircraft is not operated in forecast, or AFM-defined icing conditions. | | | | | | | | | -10-01 Bleed Air Anti-Ice Resistive Temperature Device (RTD) (All except TH001, TH002, TH003, TH004, TL017, TL019, TL021, TR018, TR020, TR022, TT017, TT018, TT019, TT020, and TT021) (Units -0501 and on) C - - May be inoperative provided: All ANTI-ICE ENGINE/STAB, and SLAT switches are selected OFF, and Aircraft is not operated in known, forecast, or AFM-defined icing conditions. | | | | | | | | | -10-02 Horizontal Stabilizer Bleed Air Anti-Ice System (Failed open) (Units -0001 thru -0500) C 2 1 (M) One may be inoperative provided: Affected valve is secured for no flow, Affected ANTI-ICE STABILIZER switch is selected OFF, and Aircraft is not operated in known, forecast, or AFM-defined icing conditions. | | | | | | | | -10-02 Horizontal Stabilizer Bleed Air Anti-Ice System (Failed open) (Units -0501 and on) C 2 1 (M) One may be inoperative provided: Affected is secured for no flow, Affected ANTI-ICE ENGINE/STAB switch is selected OFF, and Aircraft is not operated in known, forecast, or AFM-defined icing conditions. | | | | | | | |
-10-03 Leading Edge Slat Bleed Air Anti-Ice System (Units -0001 thru -0500) C 2 0 (M) May be inoperative provided: Both slat valves are secured for no flow, ANTI-ICE SLAT switch is selected OFF, and, Aircraft is not operated in forecast, or AFM-defined icing conditions. | | | | | | | | -10-03 Leading Edge Slat Air Anti-Ice System -0501 and on) C 2 0 (M) May be inoperative provided: Both slat valves are secured for no flow, Both ANTI-ICE SLATS switches are selected OFF, and, Aircraft is not operated in known, forecast, or AFM-defined icing conditions. | | | | | | | | -10-04 Wing Bleed Air Anti-Ice System (Inboard Leading Edge) (Units -0001 thru -0500) A 2 0 (M) May be inoperative provided: Both wing valves are secured for no flow, Both ANTI-ICE ENGINE switches are selected OFF, Aircraft is not operated in known, forecast, or AFM-defined icing conditions, and Repairs are made within three flight days. | | | | | | | | | | -10-04 Wing Bleed Air Anti-Ice System (Inboard Leading Edge) (Units -0501 and on) A 2 0 (M) May be inoperative provided: Both wing valves are secured for no flow, Both ANTI-ICE ENGINE/STAB switches are selected OFF, Aircraft is not operated in known, forecast, or AFM-defined icing conditions, and Repairs are made within three flight days. | | | | | | | | | |
-10-05 Wing Root Cuff Electric System A 2 0 (M) May be inoperative provided: Affected wing cuff is deactivated, Aircraft is not operated in forecast, or AFM-defined icing conditions, and Repairs are made within three flight days. | | | | | | | -20-01 Engine Anti-Ice System (Units -0001 thru -0500) A 2 1 (M) One may be inoperative provided: Affected valve is secured for no flow, Affected ANTI-ICE ENGINE switch is selected OFF, Aircraft is not operated in known, forecast, or AFM-defined icing conditions, and Repairs are made within three flight days. | | | | | | | | | | -20-01 Engine Anti-Ice System (Units -0501 and on) A 2 1 (M) One may be inoperative provided: Affected valve is secured for no flow, Affected ANTI-ICE ENGINE/STAB switch is selected OFF, Aircraft is not operated in known, forecast, or AFM-defined icing conditions, and Repairs are made within flight days. | | | | | | | | | | -30-03 Tube Heater (Excluding Standby) PITOT HTR FAIL L or R message) B 2 1 One may be inoperative provided: Aircraft is not operated at night, Aircraft is not operated in Instrument Meteorological Conditions (IMC), Pitot heater is not required by 14 CFR, and Aircraft is not operated in known, forecast, or AFM-defined icing conditions. | | | | | | | | | |
-40-02 Windshield Electric Anti-Ice System (Units -0501 and on) (Amber or White WSHLD HEAT INOP L or R message) C 2 1 (M) One may be inoperative provided: Affected windshield anti-ice system is deactivated, A to clear windshield of moisture is readily available, and Aircraft is not operated in known, forecast, or AFM-defined icing conditions. | | | | | | | | -40-04 Windshield Rain Repellant C 1 0 May be missing provided aircraft is not operated in precipitation within five nautical miles of airport used for takeoff, intended landing or any alternates required by 14 CFR. | | | | | -40-05 Frost Pane Defog System C 2 0 | -70-01 Drain Heater (Refreshment center and aft vanity basin) C - 0 (M) May be inoperative provided: Drain heaters are deactivated, and Refreshment center and aft vanity basin overboard drains are considered inoperative (Refer to item 38-30-04). | | | | | | |
-10-02 Switch Lights (Failed to illuminate) -0501 and on) (Continued) -15 Avionics Power (L / R AVN - ON / OFF) C 4 0 | | -23 Display Reversion (DISPLAY REV - NORM / REV) C 2 0 (O) May be inoperative provided switch functionality is verified operative. | | | -27 Engine / Stabilizer Anti-Ice (ENGINE/STAB - ON / OFF) C 4 0 (O) May be inoperative provided switch functionality is verified operative. NOTE: Use ANTI-ICE ON ENG/STAB white message to verify switch position. | | | | | -31 External Power (EXT PWR - ON / AVAIL) C 2 0 May be inoperative provided external power system is not used. | | -32 Fuel (BOOST PUMP - NORM / ON) C 4 0 (O) May be inoperative provided switch functionality is verified operative. NOTE: Use FUEL BST PUMP ON L-R and amber messages to verify switch position. | | | | | | -35 Interior Power (INTERIOR - ON) C 1 0 (O) May be inoperative provided switch functionality is verified operative. | | -36 Landing Light (LDG - ON) (Cyan light) C 2 0 May be inoperative provided landing lights are visually monitored. | | | (Continued)
-30-01 Aft Baggage Compartment C 3 0 | | -30-03 Single-point Refueling Panel Light C 1 0 | | -30-04 Tailcone Maintenance Light C 2 0 | -01 Door Proximity Switch (Failed to extinguish C 1 0 May be inoperative provided TAILCONE LIGHT switch is selected OFF prior to tailcone access door closure. | | | -40-01 Anti-Collision Light System (Wing strobe) | | -00A C 1 0 May be inoperative provided system is not required by 14 CFR. | | -00B A 1 0 May be inoperative provided: Position / navigation light system is operative, Ground recognition light is operative, and Repairs are made within three flight days. | | | | | | | -01 *** LED Wing Light (Per light) (LED element) (Units -0001 thru -0500 excluding winglet-equipped aircraft) C 36 32 Up to two elements may be inoperative on either Printed Circuit Board (PCB). NOTE: Anti-collision system is still considered operative. | | | | | | -40-02 Ground Recognition Light (Beacon) C 2 0 NOTE: Position / navigation or lights may be used on ground to alert nearby aircraft or personnel when engines are running or prior to start. | | | | -40-03 Landing Light |
-00A (Single failed) C 2 1 One may be inoperative provided a taxi light is operative. | | -00C (Both lights failed, day) C 2 0 May be inoperative provided aircraft is not operated at night. | | -01 Recognition Light Mode C 1 0 (O) May be inoperative provided at one landing light is verified operative for night operations. | | | -02 Pulse Light Mode D 1 0 (O) May be inoperative provided at least one landing light is verified operative for night operations. | | | -40-05 Position / Navigation System C 1 0 May be inoperative provided aircraft is not operated at night. | | -01 *** LED Wing Light (Per side) -0001 thru -0500 excluding winglet-equipped aircraft) C 2 1 One light assembly may be inoperative. NOTE: Position / navigation light system is still considered operative. | | | | | -01 LED Wing Light (Per side) -0001 thru -0500 Winglet-equipped aircraft and Units -0501 and on) C 2 1 One light assembly may be inoperative. NOTE: Position / navigation light system is still considered operative. | | | | | -02 *** LED Tail Light (LED element) (Units -0222, -0226 thru and Units -0001 thru -0223 thru -0225 incorporating SB750-33-20 Rev 0 only) C 72 66 Up to six elements may be inoperative. NOTE: Position / navigation light system is still considered operative. | | | | | | | -40-06 *** Pylon Work Light D 2 0 | |
-16-01 Altitude Alerting System A - 0 (O) May be inoperative provided: Autopilot with altitude hold and capture operates normally, Aircraft does not depart from an airport where repair or replacement can be made, Aircraft is not operated RVSM, and Repairs are made within three flight days. | | | | | | | | | | -01 Alert C - 0 May be inoperative provided: Visual alert operates normally, and Autopilot with altitude hold and capture operates normally. | | | | | -02 Visual Alert C - 0 May be inoperative provided: Aural alert operates normally, and Autopilot with altitude hold and capture operates normally. | | | | -18-01 Angle of Attack (AOA) System (Amber AOA PROBE FAIL L or R or STALL WARN L or R message) B 2 1 One may be inoperative on pilot not flying side provided affected stick shaker is considered inoperative (Refer to item | | | | | -01 *** Indexer C - 0 | | -02 Indicator (Units -0001 thru -0500) C - 0 May be inoperative provided both stick shakers are verified operative. | | -03 Stick Shaker (Amber AOA PROBE FAIL L or R or STALL WARN L or R message) B 2 1 One may be inoperative provider stick shaker on pilot flying side is operative. | | | |
-18-02 Angle of Attack (AOA) Heater | | -01 Probe (Units -0001 thru -0500) (Amber AOA HEAT FAIL L or R message) C 2 1 One may be inoperative provided aircraft is not operated in known, forecast, or AFM-defined icing conditions. | | | | -01 Vane (Units -0501 and on) (Amber AOA HEAT FAIL L or R message) C 2 1 One may be inoperative provided aircraft is not operated in known, forecast, or AFM-defined icing conditions. | | | | -02 Case C 2 1 One may be inoperative provided aircraft is not operated in known, forecast, or AFM-defined icing conditions. | | | -22-02 Standby Horizontal Situation Indicator (Heading information only) (Units -0001 thru -0500) B 1 0 May be inoperative provided: Dual heading information sources are operative, and Magnetic compass is operative. | | | | -23-01 Non-stabilized Magnetic Compass (Units -0001 thru -0500) | | | -00A (Day, VMC) B 1 0 May be inoperative provided: Any combination of two gyro, AHRS or INS-stabilized compass systems are operative, and Aircraft is not operated at night or in Instrument Meteorological Conditions (IMC). | | | | | | | (Continued)
-23-01 Non-stabilized Magnetic Compass (Units -0001 thru -0500) (Continued) -00B B 1 0 May be inoperative provided: Any combination of two gyro, AHRS or INS-stabilized compass systems are operative, Aircraft is operated with dual independent navigation capability, and Aircraft is operated under positive radar control by ATC on enroute portion of flight. | | | | | | | | | | -00C B 1 0 May be inoperative provided any combination of three gyro, AHRS or compass systems are operative. | | | | -01 Internal Lighting C 1 0 May be inoperative provided flight crew determines adequate natural or artificial lighting exists to read compass. | | | -24-01 Mechanical Slip / Skid Indicator (PFD bezel) (Units -0001 thru -0500) B 2 1 May be inoperative on pilot not flying side. | | | | -25-02 Display Unit (Center - DU3) (Units -0001 thru -0500) (Amber CHECK DU 3 message) C 1 0 May be inoperative provided: Affected display unit is installed in center position, and EICAS DSPLY is selected L or R, as desired. | | | | | -25-03 Flight Director System (Units -0001 thru -0500) (Cyan FGC A or B FAIL or Amber FD FAIL message) C 2 1 One may be inoperative provided flight director reverts or is selected to operative channel. | | | |
-06 HSI Mode Selector (PFD HSI) (Per side) -0001 thru -0500) C 1 0 May be inoperative provided current horizontal situation indicator display on PFD is acceptable to flight crew. | | | | -07 Weather / Terrain Selector (PFD WX) (Per side) (Units -0001 thru -0500) C 1 0 May be inoperative provided procedures do not require its use. | | | | | -09 Barometer Standard (PUSH STD) (Per side) -0501 and on) C 1 0 | | | | -11 Range / Pan Control (Knob) (Per side) -0501 and on) C 1 0 May be inoperative provided touchscreen controller for associated display is operative. | | | | -12 Clear (CLR) (Per side) (Units -0501 and on) C 1 0 | | | | -13 Enter (ENT) (Per side) (Units -0501 and on) C 1 0 | | | | -14 Cursor / Select (PFD / PUSH ENT) (Per side) (Units -0501 and on) C 3 0 | | | | (Continued)
-25-08 MFD Controller (Included on DC-840) (Units -0001 thru -0500) (Continued) -03 Map Mode Control (MFD MAP) (Per side) C 1 0 | | | -05 Weather / Terrain Selector (MFD WX) (Per side) C 1 0 May be inoperative provided weather radar is displayed on PFD when required. | | | -07 Joystick (Per side) C 1 0 | | -09 Traffic Control (TCAS) (Per side) C 1 0 May be inoperative provided button on opposite controller is operative. | | | -10 Aircraft Systems Control (ACFT SYS) (Per side) C 1 0 | | | -25-10 *** Synthetic Vision -0501 and on) C 1 0 May be inoperative provided procedures do not require its use. | | -25-11 Course / Heading Panel Function Control (RI-871) (Units -0001 thru -0500) | | | | -01 Course B 2 1 One may be inoperative provided procedures do not require its use. | | -02 Course Direct (CRS PUSH DIR) C 2 0 | |
-03 Heading Sync (HDG PUSH SYNC) C 2 0 | | -25-12 *** Electric Standby Instrument System (GH-3000) (Heading information only) (Units -0001 thru -0500) B 1 0 May be inoperative provided: Dual heading information sources are operative, and Magnetic compass is operative. | | | | | -25-13 Source Controller (SC-840) (Units -0001 thru -0500) | | | -01 Bearing Selector (BRG) (Per side) C 2 1 One may be inoperative provided procedures do not require its use. | | | -02 Navigation Source Selector (NAV-PREV-FMS) (Per side) C 3 0 May be inoperative provided: Button is operative on pilot flying side, and Flight director/autopilot is coupled to pilot flying side. | | | | | -25-14 Display Unit Bezel Controller (BL-870 or BL-871) (Units -0001 thru -0500) | | | | -01 Barometer Standard (STD) (Per side) C 1 0 | | | -02 MFD Range Control (Knob) (Per side) C 1 0 May be inoperative provided current map range is acceptable to the flight crew. | | | -03 Minimums Selector (MINIMUMS) (Per side) C 1 0 May be inoperative or knob may be missing provided procedures do not require its use. | | |
(Continued) -25-14 Display Unit Bezel Controller (BL-870 or BL-871) (Units -0001 thru -0500) (Continued) -04 Minimums Mode Selector (RA/BARO) (Per side) C 1 0 May be inoperative provided procedures do not require its use. | | | -30-01 *** Enhanced Vision System (EVS) D 1 0 | | -31-01 Localizer System C - - May be inoperative provided: Affected system is not on an emergency bus, Associated glideslope is considered inoperative (Refer to item 34-32-01), Procedures do not require its use, and System is not required by 14 CFR. | | | | | | | | | -32-01 Glideslope System C - - May be inoperative provided: Procedures do not require its use, and System is not required by 14 CFR. | | | | -34-01 Marker Beacon Receiver System C - 0 May be inoperative provided: Procedures do not require its use, and System is not required by 14 CFR. | | | |
-36-01 *** Reactive Windshear System (Includes TAWS windshear mode) (Amber WINDSHEAR FAIL message) C 1 0 (O) May be inoperative provided alternate procedures are established and used. | | | | | -41-01 Inertial Reference System (IRS) (Units -0016, -0067 and On and Units -0001 thru -0015, -0017 thru -0066 incorporating SB750-34-57) C 2 0 (O) May be inoperative provided: navigation systems as required by 14 CFR are operative, Affected IRS mode is selected to ATT, IRS 1 and 2 are verified capable of providing correct bank, and magnetic heading indications to associated PFD, and Aircraft is operated using applicable AFM limitations. | | | | | | | | | | | -42-01 Weather Radar System C 1 0 May be inoperative provided system is not required by 14 CFR. | | -01 *** Radar Control Panel (Units -0001 thru -0500) (Aircraft with two control panels) C 2 1 | | | | -44-01 Radio Altimeter System |
-00B (TAWS or TCAS II required) (Units -0001 thru -0500) A 1 0 (M) May be inoperative provided: Radio altimeter is deactivated, Approach minimums or operating procedures do not require its use, Basic TAWS modes are considered inoperative (Refer to item 34-44-03), TCAS II is considered inoperative (Refer to item 34-45-01), Autothrottle system, if installed, is considered inoperative, and Repairs are made within two flight days. NOTE 1: Landing gear warning system will function differently without radio altimeter input. Landing gear warning may occur at higher altitudes above ground with flaps extended. NOTE 2: Landing Operations Inhibit (LOPI) operation will be affected. LOPI may not activate during approach or | | | | | | | | | | | | | | | | | | | | | | | | (Continued) -44-01 Radio Altimeter System (Continued)
-00B (TAWS or TCAS II required) (Units -0501 and on) A 1 0 (M) May be inoperative provided: Radio altimeter is deactivated, Approach minimums or operating procedures do not require its use, TAWS modes are considered inoperative(Refer to item TCAS II is considered inoperative (Refer to item 34-45-01), and Repairs are made within two flight days. NOTE 1: Landing gear warning system will function differently without altimeter input. Landing gear warning may occur at higher altitudes above ground with flaps extended. NOTE 2: Landing Operations Phase Inhibit (LOPI) operation will be affected. LOPI may not activate during approach or go-around. | | | | | | | | | | | | | | | | | | | | | | -44-02 *** Surface Awareness System (Runway Awareness and Advisory System RAAS) (Units -0001 thru -0500) C 1 0 | | | | -44-02 *** Surface Awareness System (Smart Runway / Smart Landing) (Units -0001 thru -0500) C 1 0 | | | | -44-02 *** Surface Awareness System (SurfaceWatch) (Units -0501 and on) (White SURFACEWATCH FAIL message) C 1 0 | | | | |
-44-03 Terrain Awareness and Warning System (TAWS) (Including test mode) (Class A or B TAWS required) (Amber TERRAIN FAIL, TERR FAIL, GROUND PROX FAIL, or GPWS FAIL message) A 1 0 (O) May be inoperative provided: Alternate procedures are established and used, RNP AR procedures are not conducted, and Repairs are made within two flight days. | | | | | | | | | -01 Forward Looking Terrain Avoidance Function and Premature Descent Alert Function (Amber TERRAIN FAIL or TERR FAIL message) B 2 0 (O) May be inoperative provided alternate procedures are established and used. | | | | | | -02 Excessive Rate of Descent (Mode 1) and Altitude Loss After Takeoff or Missed Approach (Mode 3) (Amber GROUND PROX FAIL or GPWS FAIL message) A 2 0 (O) May be inoperative provided: Alternate procedures are established and used, and Repairs are made within two flight days. | | | | | | | -03A Voice Callouts (Mode 6) ("Five-Hundred") (Amber GROUND PROX FAIL or GPWS FAIL message) B 1 0 (O) May be inoperative provided alternate procedures are established and used. | | | | | -03B Callouts (Mode 6) (Other) (Amber GROUND PROX FAIL or GPWS FAIL message) C - 0 (O) May be inoperative provided alternate procedures are established and used. | | | | | (Continued)
-44-03 Terrain Awareness and Warning System (TAWS) (Including test mode) (Class A or B TAWS required) (Continued) -05A Excessive Downward Glideslope/Glidepath Deviation (Mode 5) (Class A TAWS required) (Amber GROUND PROX FAIL or GPWS FAIL message) B - 0 | | | | | | | -05B Excessive Downward Glideslope/Glidepath Deviation (Mode 5) (Class A TAWS required) (Amber GROUND PROX FAIL or GPWS FAIL message) C - 1 May be inoperative provided affected glideslope or glidepath is not used. | | | | | | | -06 Terrain Display (Class B TAWS required) C - 0 | | -06A Terrain Display (Individual display failed) (Class A TAWS required) C - 1 | | | -06B Terrain Display (All displays failed) A TAWS required) B - 0 | | | -07 Switch (Any excluding TAWS Test) (Units -0001 thru -0500) (Class B TAWS required) C - 0 | | | |
(Continued) -44-03 Terrain Awareness and Warning System (TAWS) (Including test mode) A or B TAWS required) (Continued) -07A Switch (Flap Override, Terrain Inhibit, Terrain Display Inhibit) (Units -0001 thru -0500) A TAWS required) B - 0 | | | | | | -07B Switch excluding TAWS Test) (Units -0001 thru -0500) (Class A TAWS required) C - 0 | | | | | -08 Annunciator / Indication (Class B TAWS required) C - 0 | | -08A Annunciator / Indication (Terrain Inhibited) (Class A TAWS required) B - 0 | | | -08B Annunciator / Indication (Other) (Class A TAWS required) C - 0 | | | -45-01 *** Traffic Alert and Collision Avoidance System (TCAS I or TCAS II) (Amber TCAS FAIL message) | | | | |
-00A (TCAS not required) C 1 0 (M) May be inoperative provided: System is deactivated, System is not required by 14 CFR, and Enroute or approach procedures do not require its use. | | | | | | -00B (TCAS required) B 1 0 (M) May be inoperative provided: System is deactivated, and Enroute or approach procedures do not require its use. | | | | -01 Traffic Advisory (TA) Display (TCAS II only) C - 0 (O) May be inoperative provided: Resolution Advisory (RA) display and audio function are operative, and Enroute or approach procedures do not require use of TCAS. | | | | | | -02A Resolution Advisory (RA) Display (TCAS II only) C 2 1 One may be inoperative on pilot not flying side. | | | -02B Resolution Advisory (RA) Display (TCAS II only) C 2 0 (O) May be inoperative provided: Traffic Advisory (TA) display and audio funciton are operative, TA-only mode is selected on TCAS controller or menu, and Enroute or approach procedures do not require use of TCAS. | | | | | | | (Continued) -45-01 *** Traffic Alert and Collision Avoidance System (TCAS I or TCAS II) (Continued)
-03A Traffic Advisory (TA) and Resolution Advisory (RA) Displays Failed (TCAS II only) C 2 1 One side may be inoperative provided: Traffic Advisory (TA) and Resolution Advisory (RA) displays are operative on pilot flying side, and Audio function is operative. | | | | | | -04 Audio Function B 1 0 May be inoperative provided enroute or approach procedures do not require use of TCAS. | | | -05 *** Airspace Selection Function (Above / below) C - 0 | | -45-02 *** Traffic Collision Avoidance Device (TCAD) D 1 0 | | -46-01 *** Lightning Detection System D 1 0 May be inoperative provided system is not required by 14 CFR. | | -51-01 Distance Measuring Equipment (DME) D - - Any in excess of required by 14 CFR may be inoperative. | | -52-01 ATC Transponder and Automatic Altitude Reporting System | | | -00A (Individual transponder failed) (White TRANSPONDER FAIL 1 or 2 message) D - 1 Any in excess of those required by 14 CFR may be inoperative. | | | |
-57-01 Global Navigation Satellite System (GNSS) (Including SBAS) C - 0 May be inoperative provided: System is not required by 14 CFR, and Operations do not require its use. NOTE 1: Enhanced function of TAWS may not be available. NOTE 2: ADS-B output may not be available. | | | | | | | | | | -01 *** Antenna/Jack (For portable device) D - 0 | | -60-01 Data Loader C - 0 | -60-02 Flight Management System (FMS) C - 0 May be inoperative provided: System is not required by 14 CFR, and Operations do not require its use. NOTE: Enhanced function of TAWS may not be available. | | | | | | | -01 Fuel Planning Function C - 0 | -61-01 Navigation Database C - - (O) May be out of currency provided: Current aeronautical charts are used to verify navigation fixes prior to each flight, Procedures are established and used to verify status and suitability of navigation facilities used to define route of flight, and Approach navigation radios are manually and identified. | | | | | | | | | |
-20-02 *** Therapeutic Oxygen System D 1 0 | | -30-01 *** Portable Oxygen System D - - Any in excess of those required by 14 CFR may be inoperative provided: Inoperative oxygen bottle is placarded "INOPERATIVE", removed from installed location, and placed out of sight so it cannot be mistaken for a functional unit, and Bottles not properly serviced are replaced, serviced, or removed at next available maintenance facility. | | | | | | | | | | | | -30-02 *** Protective Breathing Equipment (PBE) D - - Any in excess of required by 14 CFR may be inoperative or missing provided location placarding is removed or obscured. | | | |
-10-01 *** Potable System C - 0 (M) May be inoperative provided: System is drained, and Procedures are established and used to ensure system is not serviced. | | | | | -01 Individual Components C - 0 (M) Individual components may be inoperative provided: Associated components are deactivated or isolated, and Associated system components are verified not to have leaks. NOTE: Any portion of system operating normally may be used. | | | | | | | | | -30-01 *** Relief Tube (Cockpit) C - 0 (M) May be damaged or inoperative provided: All liquid is removed from relief tube, and Relief tube is placarded “DO NOT USE”. | | | | | | -30-02 Lavatory External Service System C 1 0 (M) Individual components may be inoperative provided: Associated components are deactivated or isolated, and Associated system components are verified not to have leaks. | | | | | | -01A Dump Cable C 1 0 May be inoperative provided lavatory is not serviced or used. | | -01B Dump Cable C 1 0 (M) May be inoperative provided lavatory is serviced by alternate | | (Continued)
-02 Refreshment Center C 1 0 (O) May be damaged or obstructed provided: All liquid is removed from refreshment center hot liquid storage and drip pan, Refreshment center hot liquid storage and drip pan are placarded “DO NOT USE”, and Ice drawer drain valve remains closed. | | | | | | | | | |
-00-01 *** Electronic Flight Bag (EFB) System | | -00A Class 3 EFB D - 0 May be inoperative provided procedures do not require its use. | | -00B Class 3 EFB C - 0 (O) May be inoperative provided alternate procedures are established and used. NOTE: Any function, program, or document which operates normally may be used. | | | | | | -01A Data Connectivity (Class 2) D - 0 May be inoperative provided procedures do not require its use. | | -01B Data Connectivity (Class 2) C - 0 (O) May be inoperative provided alternate procedures are established and used. | | -02A Power Connection (Class 1 & 2) D - 0 May be inoperative provided procedures do not require its use. | | -02B Power Connection (Class 1 & 2) C - 0 (O) May be inoperative provided alternate procedures are established and used. | | -03A Mounting Device (Class 2) D - 0 (M) May be inoperative provided: Associated EFB and hardware is secured by alternate means or removed from aircraft, and Procedures do not require its use. | | | | | -03B Mounting Device (Class 2) C - 0 (M) (O) May be inoperative provided: Associated EFB and hardware is secured by alternate means or removed from aircraft, and Alternate procedures are established and used. | | | | | |
-20-01 Auxiliary Power Unit (APU) (Amber APU SYS FAIL or APU FAIL message) C 1 0 (M) May be inoperative provided: APU is deactivated, and Procedures do not require its use. | | | -30-01 APU Fuel Shutoff Valve C 1 0 (M) May be inoperative provided: APU fuel shutoff is verified closed, and APU is considered inoperative (Refer to item 49-20-01). | | | | | -50-02 APU Bleed Air System -0001 thru -0500) C 1 0 (O) May be inoperative provided: APU SYSTEM BLEED AIR is selected OFF, and APU bleed air valve is verified closed. | | | | | -50-02 APU Bleed Air System (Units -0501 and on) C 1 0 (O) May be inoperative provided: APU BLEED AIR is selected OFF, and APU air valve is verified closed. | | | | | -01 Max Cool Function (Units -0001 thru -0500) C 1 0 (O) May be inoperative provided: APU SYSTEM BLEED AIR is not selected to MAX COOL, and Max cool valve is verified closed. | | | | -01 Max Cool Function (Units -0501 and on) C 1 0 (O) May be inoperative provided: MAX COOL is selected OFF, and Max cool valve is verified closed. | | |
-40-01 Nose Access Door (Per side) | | -01 Key Lock (Failed unlocked) D 1 0 May be inoperative provided door is verified closed and latched prior to each flight. | | | -02 Gas Spring D 1 0 May be inoperative or removed. NOTE: Precautions should be when opening door(s). | | | | -42-01 *** Battery Access Door Key Lock (Failed unlocked) D 2 0 May be inoperative provided door is verified closed and latched prior to each flight. | | | -46-01 *** Refueling (SPR) Access Door Key Lock | | | -00A (Failed unlocked) D 1 0 May be inoperative provided door is verified closed and latched to each flight. | | | -00B (Failed locked) C 1 0 NOTE: If over-wing refueling cap locks are also failed in locked position, refueling will not be possible. | | | -48-01 Tail Cone Access Door Key Lock (Failed unlocked) D 1 0 May be inoperative provided door is verified closed and latched to each flight. | | | -50-01 *** Cockpit Divider Door C 2 0 (M) May be inoperative provided door is secured open. | | -50-02 Lavatory Door C - 0 (M) May be inoperative provided door is secured open. | | -70-01 Door Warning System |
-70-01 Door Warning System (Continued) -08 Single-point Refueling (SPR) (Amber FUEL DOOR OPEN message) C 1 0 May be inoperative provided door is verified closed and latched to each flight. | | | | -09 Toilet External Service (Amber TOILET DOOR OPEN message) C 1 0 May be inoperative provided door is verified closed and latched prior to each flight. | | |
-10-01 Engine Fuel Filter (Impending bypass indication only) (Amber FUEL FLTR BYPASS L or R message) A 2 1 (M) Aircraft may be dispatched with one impending bypass indication provided: Fuel filter full bypass pin is visually verified not extended prior to each flight, and Repairs are made within ten flight hours. | | | | | | | -33-01 Fuel Flow Indicating System A 2 1 One may be inoperative provided: All fuel quantity indicating systems are operative, and Repairs are made within three flight days. | | | | |
-14-01 Engine RPM Gauge / Indication (Units -0001 thru -0500) | | | -01 Standby N1 A 2 1 One may be inoperative provided: Standby N2 and standby ITT indicators are operative, and Repairs are made within three flight cycles. | | | | | -02 Standby N2 C 2 1 One may be inoperative provided standby N1 and standby ITT indicators are operative. | | | -22-01 Engine ITT Gauge / Indication (Standby ITT) (Units -0001 thru -0500) C 2 1 One may be inoperative provided standby N1 and standby N2 indicators are operative. | | | | -32-01 Engine Vibration Monitor System (N1 or N2) C 4 2 One system may be inoperative on each engine provided no abnormal vibration exists. | | |
-30-01 Thrust Reverser C 2 0 (M) May be inoperative provided affected thrust reverser is deactivated and secured in forward thrust position. NOTE: Flight crew should review AFM THRUST REVERSERS limitations. | | | | | |
-20-01 Engine Oil Filter (Impending bypass indication only) -0001 thru -0500) (Cyan OIL FILTER BYPASS L or R message) A 2 1 Aircraft may be dispatched with one impending bypass indication provided aircraft is operated in accordance with AFM OIL FILTER BYPASS L or R cyan message procedure. | | | | | | -20-01 Engine Oil Filter (Impending bypass indication only) (Units -0501 and on) (White OIL FLTR BYPASS L or R message) A 2 1 Aircraft may be dispatched with one impending bypass indication provided aircraft is operated in accordance with AFM OIL FLTR BYPASS L or R white message procedure. | | | | | | -30-01 Engine Chip Detector C 2 1 (M) One may be inoperative provided a visual of affected chip detector before each flight reveals no anomalies. | | | -32-02 Oil Level Sensor C 2 1 One may be inoperative provided oil level is checked visually prior to each flight. | |