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| Manufacturer | Chengdu, GAIC |
| Model | J-7IIIA (J-7D) |
| Modification | J-7IIIA |
| Country | China |
| Years | 1993 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 7.154 m |
| Length | 14.70 m |
| Height | 4.11 m |
| Wing area | 23.00 m2 |
| Zero fuel weight | - |
| Empty weight | 5275 kg |
| Maximum takeoff weight | 9560 kg |
| Normal takeoff weight | 8150 kg |
| Flight duration | - |
| Engine | 1 ТРДФ LMC WP-13FI |
| Power | - |
| Thrust | - |
| Maximum speed | 2167 km/h |
| Cruising speed | 964 km/h |
| Rate of climb | - |
| Practical range | 960 km |
| Service ceiling | 18000 m |
| Hovering ceiling | - |
| Crew | 1 |
