| Manufacturer | PZL |
| Model | PZL-101 Gawron |
| Modification | PZL-101 |
| Country | Poland |
| Years | 1958 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 12.68 m |
| Length | 9.00 m |
| Height | 3.12 m |
| Wing area | 23.65 m2 |
| Zero fuel weight | - |
| Empty weight | 1018 kg |
| Maximum takeoff weight | 1660 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 PZL AI-14R |
| Power | 1 x 260 HP |
| Thrust | - |
| Maximum speed | 170 km/h |
| Cruising speed | 148 km/h |
| Rate of climb | - |
| Practical range | 240 km |
| Service ceiling | 2400 m |
| Hovering ceiling | - |
| Crew | 1 |
