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