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 |