| Manufacturer | Grumman |
| Model | F-14A Tomcat |
| Modification | F-14A |
| Country | USA |
| Years | 1974 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | - |
| Length | 19.10 m |
| Height | 4.88 m |
| Wing area | 52.49 m2 |
| Zero fuel weight | - |
| Empty weight | 18100 kg |
| Maximum takeoff weight | 33720 kg |
| Normal takeoff weight | 27100 kg |
| Flight duration | - |
| Engine | 2 Ф Pratt Whitney TF30-P-414A, |
| Power | - |
| Thrust | - |
| Maximum speed | - |
| Cruising speed | 740-1000 km/h |
| Rate of climb | - |
| Practical range | 2965-3200 km |
| Service ceiling | 16150- 17000 m |
| Hovering ceiling | - |
| Crew | - |
