| Manufacturer | Consolidated |
| Model | B-24A Liberator |
| Modification | B-24A |
| Country | USA |
| Years | 1939 |
| Type | Bomber |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 33.53 m |
| Length | 19.45 m |
| Height | 5.69 m |
| Wing area | 97.36 m2 |
| Zero fuel weight | - |
| Empty weight | 13608 kg |
| Maximum takeoff weight | 24312 kg |
| Normal takeoff weight | 17849 kg |
| Flight duration | - |
| Engine | 4 Pratt Whitney R-1830-33 (S3C4-G) Twin Wasp |
| Power | 4 x 1200 HP |
| Thrust | - |
| Maximum speed | 471 km/h |
| Cruising speed | 367 km/h |
| Rate of climb | 544 m/min |
| Practical range | 3541 km |
| Service ceiling | 9300 m |
| Hovering ceiling | - |
| Crew | - |
