| Manufacturer | Lockheed |
| Model | A-28(29) Hudson |
| Modification | A-28A |
| Country | USA |
| Years | 1938 |
| Type | Attack plane |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 19.96 m |
| Length | 13.51 m |
| Height | 3.62 m |
| Wing area | 51.19 m2 |
| Zero fuel weight | - |
| Empty weight | 5443 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 8393 kg |
| Flight duration | - |
| Engine | 2 Wright GR-1820-G102A |
| Power | 2 x 1100 HP |
| Thrust | - |
| Maximum speed | 397 km/h |
| Cruising speed | 328 km/h |
| Rate of climb | - |
| Practical range | 3150 km |
| Service ceiling | 7468 m |
| Hovering ceiling | - |
| Crew | - |
