| Manufacturer | Samolot |
| Model | SP-1 |
| Modification | SP-1 |
| Country | Poland |
| Years | 1926 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 8.92 m |
| Length | 6.10 m |
| Height | 2.30 m |
| Wing area | 15.00 m2 |
| Zero fuel weight | - |
| Empty weight | 530 kg |
| Maximum takeoff weight | 715 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Salmson AC9 |
| Power | 1 x 120 HP |
| Thrust | - |
| Maximum speed | 190 km/h |
| Cruising speed | 158 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 1 |
