| Manufacturer | Curtiss |
| Model | P-40 Tomahawk |
| Modification | P-40 |
| Country | USA |
| Years | 1938 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.35 m |
| Length | 9.67 m |
| Height | 3.22 m |
| Wing area | 21.92 m2 |
| Zero fuel weight | - |
| Empty weight | 2439 kg |
| Maximum takeoff weight | 3272 kg |
| Normal takeoff weight | 2849 kg |
| Flight duration | - |
| Engine | 1 Allison V-1710-33 |
| Power | 1 x 1040 HP |
| Thrust | - |
| Maximum speed | 575 km/h |
| Cruising speed | 446 km/h |
| Rate of climb | 862 m/min |
| Practical range | - |
| Service ceiling | 9450 m |
| Hovering ceiling | - |
| Crew | - |
