| Manufacturer | Piper |
| Model | PA-24-260 Comanche |
| Modification | РА-24Т-260 |
| Country | USA |
| Years | 1956 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 10.97 m |
| Length | 7.62 m |
| Height | 2.29 m |
| Wing area | 16.50 m2 |
| Zero fuel weight | - |
| Empty weight | 860 kg |
| Maximum takeoff weight | 1450 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Lycoming IO540R1A5 |
| Power | 1 x 260 HP |
| Thrust | - |
| Maximum speed | 390 km/h |
| Cruising speed | 318 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | 7620 m |
| Hovering ceiling | - |
| Crew | 1 |
