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North American B-25 Mitchell Specifications
North American B-25 Mitchell
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| Data for Aircraft | North American B-25 Mitchell |
| Year Introduced | |
| Number Built | |
| Rotor Diameter | |
| Wingspan | 67 ft 6 in (20.6 m) |
| Aspect Ratio | |
| Disc Loading | |
| Height | 17 ft 7 in (4.8 m) |
| Wing Area | 610 sqft (57 m²) |
| Wing Loading | 55 lb/ft² (270 kg/m²) |
| Length | 52 ft 11 in (16.1 m) |
| Lift-to-Drag Ratio | |
| Engine Type | Wright R-2600 "Cyclone", 1,850 hp (1,380 kW) |
| Country of Origin | |
| Empty Weight | 21,120 lb (9,580 kg) |
| Max Landing Weight | |
| Max Ramp Weight | 41,800 lb (19,000 kg) |
| Useful Load | |
| Seats | |
| Crew | six (two pilots, navigator/bombardier, turret gunner/engineer, radio operator/waist gunner, tail gunner |
| Power Loading | 0.110 hp/lb (182 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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