| Manufacturer | Curtiss |
| Model | Hawk 75 |
| Modification | Hawk 75A-4 |
| Country | USA |
| Years | 1935 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.39 m |
| Length | 8.77 m |
| Height | 3.72 m |
| Wing area | 21.92 m2 |
| Zero fuel weight | - |
| Empty weight | 2060 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 2610 kg |
| Flight duration | - |
| Engine | 1 Wright R-1820-G205A |
| Power | 1 x 1200 HP |
| Thrust | - |
| Maximum speed | 520 km/h |
| Cruising speed | 464 km/h |
| Rate of climb | - |
| Practical range | 1465 km |
| Service ceiling | 10000 m |
| Hovering ceiling | - |
| Crew | - |
