1967 MCDONNELL DOUGLAS DC 8 63F


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    Aircraft Summary


    General

    Year
    1967
    Manufacturer
    MCDONNELL DOUGLAS
    Model
    DC-8-63F
    Condition
    Used
    Description
    ALL AIRCRAFT ARE CONSIDERED SOLD "AS-IS /WHERE-IS". Configuration on Delivery: All Freighter with fwd bulkhead, couier compartment, adjustable 88" x 108" (MAC) Ancra roller system, FAA 121

    Airframe

    Total Time
    65500.0
    Airframe Notes
    65,500 TTAF 26,600Cycles Heavy Inspection, RVSM due now. Max Taxi/Ramp Weight: 353,000 lbs. Max Takeoff Weight: 349,000 lbs. Max Landing Weight: 258,000 lbs. Max Zero Fuel Weight: 244,000 lbs. Operating Empty Weight: 145,000 lbs. Estimated Payload: 99,000 lbs.

    Engine Program

    Engine Program Notes
    JT3D-7 Pratt & Whitney Cycles to 1st Limiter: 1,392 C-1, 3,494 C-1, 5,339 C-2, 3,566 T-2

    Avionics

    Avionics/Radios
    Sperry SP-50 A/P Sperry FD (2) Sundstrand Flight Recorder VHF Com (3) ADF (3) DME (2) TXP (2) RDR-1E Wx Radar Collins HF (3) Sundstrand Mk VII GPWS Windshear- Honeywell Selcal

    Additional Equipment

    Additional Equipment
    Burbank Stage III Hush Kits

    Inspection Status

    Inspection Status
    Fuel Capacity: 172.234 lbs., 25,707 USG Fuel Tanks: 8 Tank System Configuration on Delivery: All Freighter with fwd bulkhead, couier compartment 18 Pallets, Monarch Cargo Door STC. SPECIFICATIONS AND/OR DESCRIPTIONS ARE PROVIDED AS INTRODUCTORY INFORMATION ONLY, AND DO NOT CONSTITUTE REPRESENTATIONS OR WARRANTIES OF OK AVIATION, INC. ACCORDINGLY, YOU SHOULD RELY UPON YOUR OWN INSPECTION OF THE AIRCRAFT.


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