1993 BOEING 747 400


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    Aircraft Summary


    General

    Year
    1993
    Manufacturer
    BOEING
    Model
    747-400
    Condition
    Used
    Description
    1 x 1993 BEOING 747-400 PAX * Total Hours: 73629:33 Total Cycles: 15864 * ENGINES: PW-4056 * VERY GOOD CONDITION! THIS B747-400 PAX AIRCRAFT IS: "IN SERVICE" * IN EXECELLENT CONDITION * EMAIL FOR "OFFER DETAILS"! NEXT C-CHECK APRIL 2016 * NEXT D-CHECK APRIL 2018 * Max. Taxi Weight: 853,000 Pounds Max. Take Off Weight: 850,000 Pounds Max. Landing Weight: 630,000 Pounds Max. Zero Fuel Weight: 565,000 Pounds Fuel Capacity (US-G): 53864 LANDING GEAR * Auto Flight – 22 * Flight Control Computer 3 COLLINS Thrust Management Computer Communications - 23 HF Transceiver 2 COLLINS VHF

    Airframe

    Total Time
    73629.0
    Airframe Notes
    Total Hours: 73629:33 Total Cycles: 15864 Max. Taxi Weight: 853,000 Pounds Max. Take Off Weight: 850,000 Pounds Max. Landing Weight: 630,000 Pounds Max. Zero Fuel Weight: 565,000 Pounds Fuel Capacity (US-G): 53864 LANDING GEAR TC /s O TC@LO Available/Program Est. Overhal 12307/3720 8587 1080DAYS/10YRS 2017.03.16 12307/3720 8587 1080DAYS/10YRS 2017.03.16 12307/3720 8587 1080DAYS/10YRS 2017.03.16 12307/3720 8587 1080DAYS/10YRS 2017.03.16 12307/3720 8587 1080DAYS/10YRS 2017.03.16

    Engine Program

    Engine Program Notes
    PW-4056 TSN------CSN-----TSO-----CSO----Cycle Limit 51765--/-11200-/--5928--/-1404-/--7700 40937-/--7087-/- 20307-/--2849-/--8614 44729-/--9909-/-14912-/--2118-/-10010 57918-/-11063-/-4406-/--1011-/---5816 APU: PW-901A TSN------CSN----TSO--CSO--Cycle Limit 28655-/-15784-/-324-/-244-/-11722

    Avionics

    Avionics/Radios
    Auto Flight – 22 Flight Control Computer 3 COLLINS Thrust Management Computer Communications - 23 HF Transceiver 2 COLLINS VHF COM Transceiver 3 COLLINS Cockpit Voice Recorder 1 FAIRCHILD CMU 1 HONEYWELL AMP (Passenger Address) 1 HUGHES MULTIPLEXER 1 HUGHES SELCAL Decoder 1 MOTOROLA Indicating and Recording - 31 Digital Flight Data Recorder 1 HONEYWELL EICAS computer EFIS SYS GEN Flight Data Acquistn Mgmt Unit 1 BAE SYSTEMS CONTROL Maint control display panel Navigation - 34 Air Data Computer 3 HONEYWELL Enhance Grnd Prox Warning PC 1 SUNDSTRAND Inertial Reference Unit 3 HONEYWELL ILS Receiver 3 COLLINS DME Interrogator 2 ROCKWELL Marker Receiver Radio Altimeter Transceiver 3 COLLINS Weather Radar Transceiver 1 COLLINS TCAS Computer 1 BENDIX ATC Transponder 3 BENDIX ADF Receiver 2 COLLINS Flight Management Computer 1 HONEYWELL

    Interior

    Number of Seats
    344


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