| Manufacturer | Curtiss |
| Model | P-60A |
| Modification | P-60A |
| Country | USA |
| Years | 1942 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 12.59 m |
| Length | 10.26 m |
| Height | 3.77 m |
| Wing area | 25.56 m2 |
| Zero fuel weight | - |
| Empty weight | 3544 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 4366 kg |
| Flight duration | - |
| Engine | 1 Allison V-1710-75 |
| Power | 1 x 1425 HP |
| Thrust | - |
| Maximum speed | 676 km/h |
| Cruising speed | 578 km/h |
| Rate of climb | - |
| Practical range | 1200 km |
| Service ceiling | 9906 m |
| Hovering ceiling | - |
| Crew | - |
