| Manufacturer | North American |
| Model | F-10 |
| Modification | F-10 |
| Country | USA |
| Years | 1943 |
| Type | Reconnaissance plane |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 20.60 m |
| Length | 16.13 m |
| Height | 4.98 m |
| Wing area | 56.67 m2 |
| Zero fuel weight | - |
| Empty weight | 8980 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 14640 kg |
| Flight duration | - |
| Engine | 2 Wright R-2600-13 Cyclone |
| Power | 2 x 1700 HP |
| Thrust | - |
| Maximum speed | 485 km/h |
| Cruising speed | 404 km/h |
| Rate of climb | - |
| Practical range | 4850 km |
| Service ceiling | 7620 m |
| Hovering ceiling | - |
| Crew | - |
