| Manufacturer | North American |
| Model | B-25A-B Mitchell |
| Modification | B-25А |
| Country | USA |
| Years | 1940 |
| Type | Bomber |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 20.60 m |
| Length | 16.49 m |
| Height | 4.80 m |
| Wing area | 56.67 m2 |
| Zero fuel weight | - |
| Empty weight | 8104 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 12290 kg |
| Flight duration | - |
| Engine | 2 Wright R-2600-9 Cyclone |
| Power | 2 x 1700 HP |
| Thrust | - |
| Maximum speed | 509 km/h |
| Cruising speed | 422 km/h |
| Rate of climb | - |
| Practical range | 2180 km |
| Service ceiling | 8230 m |
| Hovering ceiling | - |
| Crew | - |
