| Manufacturer | Consolidated |
| Model | B-41 |
| Modification | ХВ-41 |
| Country | USA |
| Years | 1943 |
| Type | Bomber |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 33.53 m |
| Length | 20.47 m |
| Height | 5.49 m |
| Wing area | 97.46 m2 |
| Zero fuel weight | - |
| Empty weight | 16556 kg |
| Maximum takeoff weight | 28587 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 4 Pratt Whitney R-1830-43 Twin Wasp |
| Power | 4 x 1250 HP |
| Thrust | - |
| Maximum speed | 465 km/h |
| Cruising speed | 322 km/h |
| Rate of climb | - |
| Practical range | 5000 km |
| Service ceiling | 8690 m |
| Hovering ceiling | - |
| Crew | - |
