Kawasaki C-1 [+]Compare [E]dit [H]istory
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| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Kawasaki |
| Model | Kawasaki C-1 |
| Country | Japan |
| Manufactured from | 1970 year |
| Manufactured to | 1981 year |
| Type | Military Transport Planes |
| Icao | C1 |
| Performance | |
| Engine | 2x Pratt & Whitney JT8D-M-9 |
| Power, hp | Add |
| Power, lbf | 14,500 lbf |
| Avionics | Add |
| Max cruise speed | 806 km/h |
| Approach speed | 250 km/h |
| Travel range | 1,300 km |
| Fuel economy | Add |
| Service ceiling | 11,579 m |
| Rate of climb | 17.75 m/sec |
| Take off distance | 2,190 m |
| Landing distance | 1,180 m |
| Weights | |
| Max take off weight | 38,700 kg |
| Max landing weight | 23,320 kg |
| Max payload | 11,900 kg |
| Fuel tank capacity | 52,996 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 | 29 m |
| Tail height | 9.99 m |
| Fuselage diameter | Add |
| Wing span | 30.6 m |
| Wing tips | No Winglets |
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There was one edit, no edits waiting approval. Last edited by qjast(1747), Oct 25, 2021 (40 fields were changed)
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