1. Communication Systems (VHF, UHF) D - - Any in excess of those required by 14 CFR may be inoperative provided it is not powered by the Emergency AC Bus, Emergency DC Bus, Battery Bus, Battery Direct Bus, or the DC Transfer Bus and not required for emergency procedures. VHF Comm Control Panels Frequency Transfer Light C - 0 Frequency Transfer Switch C - 0 Frequency Transfer Knob C - 2 Frequency Indication C - 2 2. Passenger Address System (PA) Passenger Configuration B 1 0 (O) May be inoperative provided: Alternate, normal, and emergency procedures and/or operating restrictions are established and used, and Flight attendant alerting system and visual) is operative. NOTE: Any station function(s) that is operative may be used. C 1 0 (O) May be inoperative provided: PA not required by 14 CFR, and Alternate, normal, and emergency procedures and/or operating restrictions are established and used. NOTE: Any station function(s) that is operative may be used. (Continued)
16. *** ACARS 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. 17. Radio Tuning Unit (RTU) C 2 1 (O) One may be inoperative provided: FMS is equipped to allow tuning of radios, and Radio tuning function of the FMS is operative. | 18. High Frequency (HF) Communication System D - - Any in excess of required by 14 CFR may be inoperative. | C - 1 (O) May be inoperative while conducting operations that require two LRCS provided: Aircraft SATVOICE system operates normally, SATVOICE services are available as a LRCS over the intended route of flight, The ICAO Flight Plan is updated (as required) to notify ATC of the communications equipment status of the aircraft, and Alternate procedures are established and used.
1. Cockpit/Flight Deck/Flight Compartment and Instrument Lighting System C - - Individual lights may be inoperative provided: Remaining Lighting System lights are sufficient to clearly illuminate all required instruments, controls, and other devices for which they are provided, Remaining Lighting System lights are positioned so that direct rays are shielded from flightcrew members’ eyes, and Lighting configuration and intensity is acceptable to the flightcrew. | | NOTE 1: Individual button/switch lights and/or annunciations/indications are excluded from this relief. NOTE 2: Unaided operation (without NVGs) may be permitted with inoperative NVG supplemental lights; cracked or missing filters. 2. Passenger Cabin Normal Lighting System C - - Individual lights may be inoperative or missing provided: Adjacent is operative, and Inoperative lights do not exceed 50% of the total installed. | 3. Passenger Lighted Information Sign C - - (O) May be inoperative provided alternate procedures are established and used to notify cabin occupants. | | | 4. Aft Compartment Lighting System C 1 0 5. Baggage Compartment Lighting System (Interior/Exterior) C 1 0
11. Exterior Emergency Lighting System C 1 0 May be inoperative for other than night operations. | 12. *** Logo Light System D 1 0 13. Strobe System C 1 0 May be inoperative provided Anti-Collision Lights are installed and operative. | | 14. *** Pulse Light System D 1 0
49. *** GPS (on Aircraft with STC ST02970NY, ST01408WI-D, ST01615WI-D, or ST02967NY) C 2 0 (O) May be inoperative provided operations do not require its use. | | | | | NOTE: ADS-B Out function will not be available when both GPS are inoperative on aircraft with STC ST02972NY or ST02973NY. | | | | 50. *** Cursor Control Display (CCD) (Only on Aircraft with STC ST03371NY) A 2 1 Copilot position may be inoperative provided: Reversion Switch Panels (RSP) are operative, and Repairs are made within 3 flight days. | | | | NOTE: If bezel buttons are used, displays will revert back to legacy mode on aircraft with ST03371NY. | | | 51. *** Incidence Meter (M0051) D 1 0 (M) May be inoperative provided associated circuit breakers are pulled and collared.
5. *** Electric Main Entrance Door System (Post M2716) (F900C Only) C 1 0 (M) May be inoperative provided Door is verified to manually open and close freely. 6. Baggage Compartment External Door Reducing Gear Motor (Except F900C) C 1 0 (M) May be inoperative provided: Baggage compartment external door is closed manually, Baggage compartment external door is verified latched and locked before each flight, and REAR DOORS caution light is extinguished. 7. Baggage Compartment External Door Reducing Gear Motor (F900C only) C 1 0 (M) May be inoperative provided: Baggage compartment external door is closed manually, Baggage compartment external door is verified latched and locked before each flight, and DOORS* warning light is extinguished.