VC-25A Air Force One [+]Compare [E]dit [H]istory

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Object «VC-25A Air Force One» has attributes

Attribute Value
General
Manufacturer Boeing
Model VC-25A Air Force One
Country United States
Manufactured from 1986 year
Manufactured to 1990 year
Type Heavy Business Jets
Icao VC25
Performance
Engine 4x General Electric CF6-80C2B1
Power, hp Add
Power, lbf 56,700 lbf
Avionics Add
Max cruise speed 1,015 km/h
Approach speed 278 km/h
Travel range 12,686 km
Fuel economy 0.064 km/l
Service ceiling 13,746 m
Rate of climb 7.62 m/sec
Take off distance 3,190 m
Landing distance 2,438 m
Weights
Max take off weight 377,842 kg
Max landing weight 285,763 kg
Max payload 68,180 kg
Fuel tank capacity 202,939 l
Baggage volume 28.3 m³
Dimensions
Seats 12
Seats - business class Add
Seats - first class Add
Cabin height 2.54 m
Cabin width 6.13 m
Cabin length 57 m
Exterior length 70.6 m
Tail height 19.33 m
Fuselage diameter 6.49 m
Wing span 59.6 m
Wing tips Raked Wingtips

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There was one edit, no edits waiting approval. Last edited by qjast(1747), Oct 25, 2021 (46 fields were changed)
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