| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Grumman |
| Model | Grumman F7F Tigercat |
| Country | United States |
| Manufactured from | 1943 year |
| Manufactured to | 1946 year |
| Type | Military Propellor Planes |
| Icao | F7F |
| Performance | |
| Engine | 2x Pratt & Whitney R-2800-34W Double Wasp |
| Power, hp | 2,100 hp |
| Power, lbf | Add |
| Avionics | Add |
| Max cruise speed | 741 km/h |
| Approach speed | 144 km/h |
| Travel range | 1,935 km |
| Fuel economy | Add |
| Service ceiling | 12,314 m |
| Rate of climb | 23.01 m/sec |
| Take off distance | 240 m |
| Landing distance | 270 m |
| Weights | |
| Max take off weight | 11,670 kg |
| Max landing weight | Add |
| Max payload | 2,000 kg |
| Fuel tank capacity | 2,748 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 | 13.84 m |
| Tail height | 5.05 m |
| Fuselage diameter | 1 m |
| Wing span | 15.7 m |
| Wing tips | No Winglets |