| Manufacturer | North American |
| Model | P-51A Mustang |
| Modification | P-51A-10-NA |
| Country | USA |
| Years | 1943 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.28 m |
| Length | 9.75 m |
| Height | 2.64 m |
| Wing area | 21.65 m2 |
| Zero fuel weight | - |
| Empty weight | 2918 kg |
| Maximum takeoff weight | 4808 kg |
| Normal takeoff weight | 3901 kg |
| Flight duration | - |
| Engine | 1 Allison V-1710-81 |
| Power | 1 x 1200 HP |
| Thrust | - |
| Maximum speed | 628 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | 9555 m |
| Hovering ceiling | - |
| Crew | - |
