| Manufacturer | Grumman |
| Model | P-50 |
| Modification | XP-50 |
| Country | USA |
| Years | 1941 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 12.80 m |
| Length | 9.72 m |
| Height | 3.66 m |
| Wing area | 28.24 m2 |
| Zero fuel weight | - |
| Empty weight | 3678 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 4789 kg |
| Flight duration | - |
| Engine | 2 Wright XR-1820-67/69 Cyclone |
| Power | 2 x 1200 HP |
| Thrust | - |
| Maximum speed | 682 km/h |
| Cruising speed | 337 km/h |
| Rate of climb | 1220 m/min |
| Practical range | 2011 km |
| Service ceiling | 12190 m |
| Hovering ceiling | - |
| Crew | - |
