| Manufacturer | North American |
| Model | Mustang II |
| Modification | Mustang Mk.II |
| Country | USA |
| Years | 1942 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.28 m |
| Length | 9.82 m |
| Height | 2.64 m |
| Wing area | 21.65 m2 |
| Zero fuel weight | - |
| Empty weight | 2920 kg |
| Maximum takeoff weight | 4812 kg |
| Normal takeoff weight | 3904 kg |
| Flight duration | - |
| Engine | 1 Allison V-1710F20R (V-1710-81) |
| Power | - |
| Thrust | - |
| Maximum speed | 658 km/h |
| Cruising speed | 480 km/h |
| Rate of climb | 693 m/min |
| Practical range | - |
| Service ceiling | 9555 m |
| Hovering ceiling | - |
| Crew | - |
