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| Manufacturer | Curtiss |
| Model | P-40B(C) Tomahawk |
| Modification | P-40C |
| Country | USA |
| Years | 1940 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.38 m |
| Length | 9.68 m |
| Height | 3.23 m |
| Wing area | 21.92 m2 |
| Zero fuel weight | - |
| Empty weight | 2636 kg |
| Maximum takeoff weight | 3655 kg |
| Normal takeoff weight | 3424 kg |
| Flight duration | - |
| Engine | 1 Allison V-1710-33 |
| Power | 1 x 1150 HP |
| Thrust | - |
| Maximum speed | 555 km/h |
| Cruising speed | 435 km/h |
| Rate of climb | 808 m/min |
| Practical range | - |
| Service ceiling | 8992 m |
| Hovering ceiling | - |
| Crew | - |
