1967 MCDONNELL DOUGLAS DC 8 63F
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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