1969 MCDONNELL DOUGLAS DC 8 63F
Aircraft Summary
General
Year
1969
Manufacturer
MCDONNELL DOUGLAS
Model
DC-8-63F
Condition
Used
Description
ALL AIRCRAFT ARE CONSIDERED SOLD "AS-IS /WHERE-IS". Configuration on Delivery: All Freighter Rosenbalm Cargo Door 18 Pallets, Brownline Cargo System. BAC Stage III Hushkit, FAA 121
Airframe
Airframe Notes
73,950 TTAF
24,600 Cycles
"C" Check Due
"D" Check Due August, 2005
Max Taxi/Ramp Weight: 356,000 lbs.
Max Takeoff Weight: 353,000 lbs.
Max Landing Weight: 265,000 lbs.
Max Zero Fuel Weight: 245,300 lbs.
Operating Empty Weight: 148,000 lbs.
Estimated Payload: 97,300 lbs.
Engine Program
Engine Program Notes
JT3D-7 Pratt & Whitney Cycles remaining to first limiter:
4,408 C-1
3,193 C-3
3,274 C-1
535 C-1
Avionics
Avionics/Radios
Sperry SP-30AL A/P
Sperry Z-14 FD (2)
Flight Recorder
ADF (2)
DME (2)
Collins TXP
Bendidx RDR-1E
Collins HF (2)
Sundstrand Mark VII
VHF Nav (2)
Inspection Status
Inspection Status
Fuel Capacity: 162,529 lbs., 24,258 USG
Fuel Tanks: 8 Tank System
Configuration on Delivery: All Freighter Rosenbalm Cargo Door 18 Pallets, Brownline Cargo System. BAC Stage III Hushkit.
SPECIFICATIONS AND/OR DESCRIPTIONS ARE PROVIDED AS INTRODUCTORY INFORMATION ONLY, AND DO NOT CONSTITUTE REPRESENTATIONS OR WARRANTIES OF OK CONSULTANTS, INC. ACCORDINGLY, YOU SHOULD RELY UPON YOUR OWN INSPECTION OF THE AIRCRAFT.
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