N7474C - 1991 BOEING 747 400


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    Aircraft Summary


    General

    Year
    1991
    Manufacturer
    BOEING
    Model
    747-400
    Serial Number
    24730
    Registration #
    N7474C
    Condition
    Used
    Description
    The plane does not have engines.

    Airframe

    Total Time
    16470
    Total Landings
    13617
    Airframe Notes
    Exterior Height 63’ 5” Wing Span 195’ 8” Length 231’ 10”

    Engine Program

    Engine Maintenance Program
    None

    Engine 1

    Engine 1 Notes
    The plane does not have engines.

    Auxiliary Power Unit

    APU
    Yes
    APU Notes
    Manufacturer & Model Pratt & Whitney Canada 901A Serial Number PCE900229 Total Time Since New 13,402 (As of May 2019) Total Cycles Since New 7,280 Last Shop Visit February 2014

    Avionics

    Avionics/Radios
    ACARS COMMUNICATION MANAGEMENT UNIT SINGLE COLLINS AIRPLANE PERSONALITY UNIT SINGLE COLLINS ALTITUDE ALERT SYSTEM CREW ALERTING CARD SINGLE BECO AIRCRAFT CONDITION MONITORING DATA MANAGEMENT UNIT SINGLE TELEDYNE QUICK ACCESS RECORDER SINGLE TELEDYNE AIR DATA COMPUTING AIR DATA COMPUTER TRIPLE HONEYWELL AIR DATA STANDBY STANDBY AIRSPEED INDICATOR SINGLE KOLLSMAN STANDBY ALTIMTER INDICATOR SINGLE TKK AIR TRAFFIC CONTROL SYSTEM DUAL ATC CONTROL PANEL SINGLE COLLINS ATC TRANSPONDER DUAL COLLINS AUTOPILOT/FLIGHT DIRECTOR SYSTEM COMPUTER-FLIGHT CONTROL TRIPLE COLLINS PANEL-AFCS MODE CONTROL SINGLE COLLINS MODULE - STAB TRIM/RUDDER DUAL BOEING AUTOMATIC DIRECTION FINDER ADF RECEIVER SINGLE BOEING DISTANCE MEASURING EQUIPMENT DME INTERROGATOR DUAL COLLINS EMERGENCY LOCATOR TRANSMITTER ELT TRANSMITTER SINGLE ELTA ELT CONTROL PANEL SINGLE BAE SYSTEMS ENHANCED GROUND PROXIMITY WARNING SYSTEM EGPWS COMPUTER SINGLE HONEYWELL FLIGHT MANAGEMENT COMPUTER SYSTEM FLIGHT MANAGEMENT COMPUTER DUAL HONEYWELL FLIGHT MANAGEMENT CONTROL DISPLAY TRIPLE HONEYWELL GLOBAL POSITIONING SYSTEM MULTI-MODE RECEIVER TRIPLE COLLINS INTEGRATED DISPLAY SYSTEM INTEGRATED DISPLAY UNIT SIX COLLINS INTEGRATED INTERFACE UNIT TRIPLE COLLINS ILS NAVIGATION SYSTEM MULTI-MODE RECEIVER TRIPLE COLLINS RADIO ALTIMTER SYSTEM RADIO ALTIMETER TRANSMITTER/RECEIVER TRIPLE THALES SELCAL SYSTEM SELCAL DECODER DUAL MOTOROLA STANDBY ATTITUDE REFERENCE SYSTEM STANDBY ATTITUDE INDICATOR SINGLE SFENA STATIC INVERTER/ILS PROCESSOR SINGLE SFENA STANDBY MAGNETIC COMPASS STANDBY COMPASS SINGLE AMETEK TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM TCAS COMPUTER SINGLE COLLINS VHF COMMUNICATION SYSTEM TRANSCEIVER A DUAL COLLINS TRANSCIEVER B SINGLE COLLINS CONTROL PANEL DUAL GABLES VHF OMNIRANGE NAVIGATIONAL SYSTEM VOR/MKR RECIEVER SINGLE HONEYWELL VOICE RECORDER SYSTEM COCKPIT VOICE RECORDER SINGLE FAIRCHILD CVR CONTROL PANEL UNIT SINGLE FARICHILD UNDER WATER LOCATOR DEVICE SINGLE DUKANE WEATHER RADAR SYSTEM WEATHER RADAR CONTROL PANEL SINGLE COLLINS WEATHER RADAR RECEIVER/TRANSMITTER DUAL COLLINS

    Exterior

    Exterior Notes
    Base White/Beige Stripe Red

    Interior

    Interior Notes
    Configuration State Room | 4 Zones (B - E) | Galley | Upper Deck


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