North American B-25 Mitchell [+]Compare [E]dit [H]istory
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| Attribute | Value |
|---|---|
| General | |
| Manufacturer | North American Aviation NAA |
| Model | North American B-25 Mitchell |
| Country | United States |
| Manufactured from | 1940 year |
| Manufactured to | 1945 year |
| Type | Military Propellor Planes |
| Icao | B25 |
| Performance | |
| Engine | 2x Wright R-2600-92 Twin Cyclone |
| Power, hp | 1,700 hp |
| Power, lbf | Add |
| Avionics | Add |
| Max cruise speed | 437 km/h |
| Approach speed | 148 km/h |
| Travel range | 2,167 km |
| Fuel economy | Add |
| Service ceiling | 7,376 m |
| Rate of climb | 5.08 m/sec |
| Take off distance | Add |
| Landing distance | Add |
| Weights | |
| Max take off weight | 15,876 kg |
| Max landing weight | Add |
| Max payload | 3,060 kg |
| Fuel tank capacity | 3,687 l |
| Baggage volume | Add |
| Dimensions | |
| Seats | 5 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | Add |
| Cabin width | Add |
| Cabin length | Add |
| Exterior length | 16.13 m |
| Tail height | 4.98 m |
| Fuselage diameter | 1.4 m |
| Wing span | 20.6 m |
| Wing tips | No Winglets |
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Everyone can something to edit or add.
There was one edit, no edits waiting approval. Last edited by qjast(1747), Oct 26, 2021 (38 fields were changed)
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