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Consolidated B-24 Liberator Specifications
Consolidated B-24 Liberator
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| Data for Aircraft | Consolidated B-24 Liberator |
| Year Introduced | |
| Number Built | |
| Rotor Diameter | |
| Wingspan | 110 ft 0 in (33.5 m) |
| Aspect Ratio | |
| Disc Loading | |
| Height | 18 ft 0 in (5.5 m) |
| Wing Area | 1,048 ft² (97.4 m²) |
| Wing Loading | 52.5 lb/ft² (256 kg/m²) |
| Length | 67 ft 8 in (20.6 m) |
| Lift-to-Drag Ratio | |
| Engine Type | Pratt & Whitney R-1830, 1,200 hp (900 kW) |
| Country of Origin | |
| Empty Weight | 36,500 lb (16,590 kg) |
| Max Landing Weight | |
| Max Ramp Weight | 65,000 lb (29,500 kg) |
| Useful Load | |
| Seats | |
| Crew | 7-10 |
| Power Loading | 0.0873 hp/lb (144 W/kg) |
| Thrust to Weight | |
| Cockpit Length | |
| Cockpit Width | |
| Cockpit Height | |
| Load Limit Negative | |
| Load Limit Positive | |
| Fuel Capacity | |
| Oil Capacity |
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