| Manufacturer | Grumman |
| Model | F7F-1 Tigercat |
| Modification | F7F-1 |
| Country | USA |
| Years | 1943 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 15.70 m |
| Length | 13.85 m |
| Height | 5.05 m |
| Wing area | 42.27 m2 |
| Zero fuel weight | - |
| Empty weight | 7238 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 10730 kg |
| Flight duration | - |
| Engine | 2 Pratt Whitney R-2800-22W Double Wasp |
| Power | 2 x 2100 HP |
| Thrust | - |
| Maximum speed | 687 km/h |
| Cruising speed | 350 km/h |
| Rate of climb | - |
| Practical range | 2880 km |
| Service ceiling | 11000 m |
| Hovering ceiling | - |
| Crew | - |
