Comparisons / Comparison of VC-25A Air Force One and McDonnell Douglas DC-10-40

Comparison of VC-25A Air Force One and McDonnell Douglas DC-10-40 [S]ave

Attribute
VC-25A Air Force One
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McDonnell Douglas DC-10-40
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General
ManufacturerBoeingMcDonnell Douglas
ModelVC-25A Air Force OneMcDonnell Douglas DC-10-40
CountryUnited StatesUnited States
Manufactured from (year)19861973
Manufactured to (year)19901983
TypeHeavy Business JetsJumbo Passenger Jets
IcaoVC25DC10
Performance
Engine4x General Electric CF6-80C2B13x Pratt & Whitney JT9D-59A
Power, lbf (lbf)56,70053,000
Max cruise speed (km/h)1,015982
Approach speed (km/h)278276
Travel range (km)12,6869,445
Fuel economy (km/l)0.064-
Service ceiling (m)13,74612,802
Rate of climb (m/sec)7.6210.16
Take off distance (m)3,1903,000
Landing distance (m)2,4381,800
Weights
Max take off weight (kg)377,842251,744
Max landing weight (kg)285,763182,798
Max payload (kg)68,18044,356
Fuel tank capacity (l)202,939138,742
Baggage volume (m³)28.3130.7
Dimensions
Seats12399
Cabin height (m)2.542.41
Cabin width (m)6.135.7
Cabin length (m)5736.7
Exterior length (m)70.655.5
Tail height (m)19.3317.7
Fuselage diameter (m)6.496
Wing span (m)59.650.4
Wing tipsRaked WingtipsNo Winglets



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