| Manufacturer | Boeing |
| Model | F-9 |
| Modification | F-9A |
| Country | USA |
| Years | 1942 |
| Type | Reconnaissance plane |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 31.62 m |
| Length | 22.78 m |
| Height | 5.82 m |
| Wing area | 131.92 m2 |
| Zero fuel weight | - |
| Empty weight | 15100 kg |
| Maximum takeoff weight | 22600 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 4 Wright R-1820-97 Cyclone |
| Power | 4 x 1200 HP |
| Thrust | - |
| Maximum speed | 478 km/h |
| Cruising speed | 320 km/h |
| Rate of climb | - |
| Practical range | 2800 km |
| Service ceiling | 10800 m |
| Hovering ceiling | - |
| Crew | - |
