Grumman OV-1 Mohawk [+]Compare [E]dit [H]istory
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| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Grumman |
| Model | Grumman OV-1 Mohawk |
| Country | United States |
| Manufactured from | 1959 year |
| Manufactured to | 1970 year |
| Type | Military Propellor Planes |
| Icao | OV1 |
| Performance | |
| Engine | 2x Lycoming T53-L-701 |
| Power, hp | 1,400 hp |
| Power, lbf | Add |
| Avionics | Add |
| Max cruise speed | 491 km/h |
| Approach speed | 135 km/h |
| Travel range | 1,519 km |
| Fuel economy | Add |
| Service ceiling | 7,620 m |
| Rate of climb | 17.78 m/sec |
| Take off distance | 358 m |
| Landing distance | 320 m |
| Weights | |
| Max take off weight | 8,215 kg |
| Max landing weight | 7,051 kg |
| Max payload | 1,050 kg |
| Fuel tank capacity | 1,045 l |
| Baggage volume | Add |
| Dimensions | |
| Seats | 2 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | Add |
| Cabin width | Add |
| Cabin length | Add |
| Exterior length | 12.5 m |
| Tail height | 3.86 m |
| Fuselage diameter | 1.7 m |
| Wing span | 14.63 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 (41 fields were changed)
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