| Manufacturer | PZL |
| Model | PZL P-7 |
| Modification | Р-7а |
| Country | Poland |
| Years | 1930 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 10.30 m |
| Length | 7.15 m |
| Height | 2.75 m |
| Wing area | 17.20 m2 |
| Zero fuel weight | - |
| Empty weight | 1010 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 1410 kg |
| Flight duration | - |
| Engine | 1 Bristol Jupiter VII |
| Power | 1 x 485 HP |
| Thrust | - |
| Maximum speed | 320 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 560 km |
| Service ceiling | 8275 m |
| Hovering ceiling | - |
| Crew | - |
