| Manufacturer | Chengdu |
| Model | J-7IIA |
| Modification | J-7IIA |
| Country | China |
| Years | 1984 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 7.154 m |
| Length | 14.89 m |
| Height | 4.11 m |
| Wing area | 23.00 m2 |
| Zero fuel weight | - |
| Empty weight | 5375 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 7531 kg |
| Flight duration | - |
| Engine | 1 ТРД Liming (LM) Wopen-7ВM |
| Power | - |
| Thrust | - |
| Maximum speed | 2175 (M=2.04) km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 1740 km |
| Service ceiling | 18200 m |
| Hovering ceiling | - |
| Crew | 1 |
