1973 MCDONNELL DOUGLAS DC 10 10
Aircraft Summary
General
Year
1973
Manufacturer
MCDONNELL DOUGLAS
Model
DC-10-10
Condition
Used
Description
AIRCRAFT ARE CONSIDERED SOLD "AS-IS /WHERE-IS".
Max Taxi Wt: 449,000 lbs.
Max Gross Take-Off Wt: 446,000 lbs.
Max Landing Wt: 375,000 lbs.
Max Zero Fuel Wt: 355,000 lbs.
Basic Empty Wt: 213,944 lbs.
Fuel Capacity (gal): 21,622 gal.
Fuel Capacity (lbs): 145,201 lbs. 30,735 Cycles, STC Freighter Conversion, Payload-141,056 lbs.
Airframe
Total Time
84545.0
Airframe Notes
84,545 TT, 30,735 Cycles
Engine Program
Engine Program Notes
CF6-6D
#1 (Needs Repair) # 2 #3
62,683.38 / 65,630.20 / 54,739.63 TT
12,021.73 / 8358.60 / 3682.48 TSEHM
LIMITERS:
4270 / 2845 / 1088 Cycles REMAIN
First Limit: Stage 10 disc / Rear shaft / Fwd shaft
APU: TSCP700-4B
28,610.18 TT, 13,713 Cycles, 696.68 TSEHM, 300 Cycles
696.68 TSHSI / 300 Cycles
Inspection Status
Inspection Status
Last A Check: 6/5/01 (84,240 hrs)
Last C Check: C12 on 12/8/00 (83,848 hrs)
NLG Due OH: June 2004, cycles remaining 4149
LH MLG Due OH: Sept 2004, cycles remaining 5845
RH MLG Due OH: Nov 2006, cycles remaining 6600
Since this is a used aircraft, we encourage all buyers to have an independent inspection at a neutral facility, prior to purchasing this aircraft or any other used aircraft from us or anyone else. ALL AIRCRAFT SOLD BY THIS COMPANY ARE THEREFORE SOLD: "AS-IS / WHERE-IS", WITH NO REPRESENTATIONS AS TO FITNESS OR ANY OTHER WARRANTIES WHATSOEVER!
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