| Manufacturer | Lancair |
| Model | Lancair IV |
| Modification | Lancair IV-P |
| Country | USA |
| Years | 1990 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 10.82 m |
| Length | 7.62 m |
| Height | - |
| Wing area | 9.10 m2 |
| Zero fuel weight | 998 kg |
| Empty weight | - |
| Maximum takeoff weight | 1610 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Continental TSIO-550 |
| Power | 1 x 350 HP |
| Thrust | - |
| Maximum speed | 531 km/h |
| Cruising speed | 455 km/h |
| Rate of climb | 456 m/min |
| Practical range | 2494 km |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 1 |
