| Manufacturer | Vought |
| Model | A-7A(B) Corsair II |
| Modification | А-7В |
| Country | USA |
| Years | 1965 |
| Type | Attack aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.81 m |
| Length | 14.05 m |
| Height | 4.87 m |
| Wing area | 34.83 m2 |
| Zero fuel weight | - |
| Empty weight | 8165 kg |
| Maximum takeoff weight | 19050 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 ТРД Pratt Whitney TF30-P-8 |
| Power | - |
| Thrust | 1 x 54.80 kN |
| Maximum speed | 920 km/h |
| Cruising speed | 831 km/h |
| Rate of climb | - |
| Practical range | 4540 km |
| Service ceiling | 11900 m |
| Hovering ceiling | - |
| Crew | 1 |
