N500WN - 1969 FOKKER F 28


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    Aircraft Summary


    General

    Year
    1969
    Manufacturer
    FOKKER
    Model
    F-28
    Serial Number
    11016
    Registration #
    N500WN
    Condition
    Used
    Description
    9193 Cycles

    Airframe

    Total Time
    9973.0

    Engine Program

    Engine Program Notes
    RB183-555-15 Engines 8000 Hours TBO Left: Serial Number 9032 9232 Hours TT 8626 Cycles SNEW 3594 Hours SMOH 844 Hours SML Right: Serial Number 9031 9289 Hours TT 8639 Cycles SNEW 3392 Hours SMOH Garrett GTCP-36-4A APU

    Avionics

    Avionics/Radios
    Collins Proline II Avionics: Smiths Autopilot Dual Collins VIR-32A Dual Collins ALT-55B Radal Dual King MST-67A Mode S Transponder Dual King KHF 953 w/SELCAL Dual IDC Encoding Altimeter Dual Sperry EDZ-800 Flight Director Dual Collins DME-42 Dual Universal UNS 1C FMS Bendix TCAS II CAS 67A Fairchild A100 CVR Dual Sperry Compass Dual Collins VHF-22A Dual Collins ADF-60 Dual Air Data Computer Sperry 5 Tube EFIS Wulfsberg VI EFONE Provisions for EGPWS

    Additional Equipment

    Additional Equipment
    5-Tube EFIS 35000 Foot Cabin LR Tanks (4344 Gal) Dual Sperry Electric Altimeters MACH Airspeed and Vehicle Speed Indicator Sperry UN-801 8.33 Spacing 3 Inch Standby Instruments Triple Baker Audio Single Point Refueling 1800 NM Range Motorola MA-135 SELCAL Gross Weight Increase Mod (66,500 lb) Sperry Comparator Warning

    Exterior

    Exterior Notes
    The exterior of the Fokker F28 is completed in overall Matterhorn white with platinum stripes. The paint was completed in September 2002.

    Interior

    Interior Notes
    24 Passenger interior completed in earth tone leather, fabric and ultra suede. Forward four place club seating and four place couch, eight place aft seating with two tables, mid cabin eight place seating with stand-up bar. Twilight taupe carpet with beige highlights, aft storage, two VHS tape decks, two TV monitors, CD player. Interior was completed in December 2001.

    Inspection Status

    Inspection Status
    Landing Gear O/H c/w January 1998 Low Utilization Certified "D" Check and SIP1/SIP2 & CCP c/w January 1998


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