| Manufacturer | Grumman |
| Model | F-11 Tiger |
| Modification | F-11F-1 Tiger |
| Country | USA |
| Years | 1954 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 9.64 m |
| Length | 13.69 m |
| Height | 4.04 m |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | 6036 kg |
| Maximum takeoff weight | 10641 kg |
| Normal takeoff weight | 9541 kg |
| Flight duration | - |
| Engine | 1 ТРДФ J65-W-18 |
| Power | - |
| Thrust | - |
| Maximum speed | - |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 1783 km |
| Service ceiling | 15400 m |
| Hovering ceiling | - |
| Crew | 1 |
