| Manufacturer | PZL |
| Model | P-23 Karas |
| Modification | P-23A |
| Country | Poland |
| Years | 193 |
| Type | Bomber |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 13.95 m |
| Length | 9.68 m |
| Height | 3.30 m |
| Wing area | 26.80 m2 |
| Zero fuel weight | - |
| Empty weight | 1928 kg |
| Maximum takeoff weight | 3428 kg |
| Normal takeoff weight | 2813 kg |
| Flight duration | - |
| Engine | 1 Bristol Pegasus IIM2 |
| Power | 1 x 600 HP |
| Thrust | - |
| Maximum speed | - |
| Cruising speed | 240 km/h |
| Rate of climb | - |
| Practical range | 1300 km |
| Service ceiling | 5800 m |
| Hovering ceiling | - |
| Crew | - |
