| Manufacturer | North American |
| Model | NA-40 |
| Modification | NA-40B |
| Country | USA |
| Years | 1939 |
| Type | Bomber |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 20.12 m |
| Length | 14.57 m |
| Height | 4.57 m |
| Wing area | 55.60 m2 |
| Zero fuel weight | - |
| Empty weight | 5601 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 9070 kg |
| Flight duration | - |
| Engine | 2 Wright R-2600-A71-3 Double Cyclone |
| Power | 2 x 1600 HP |
| Thrust | - |
| Maximum speed | 464 km/h |
| Cruising speed | 406 km/h |
| Rate of climb | - |
| Practical range | 1900 km |
| Service ceiling | 7620 m |
| Hovering ceiling | - |
| Crew | - |
