Airbus A300-600 vs. Consolidated B-24 Liberator

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Airbus A300-600 versus Consolidated B-24 Liberator
54.10 m 177 ft 6 in length 20.42 m 67 ft 0 in
16.5 m 54 ft 2 in height 5.49 m 18 ft
44.84 m 147 ft 1 in wingspan 33.53 m 110 ft
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines
56,000lb to 61,500lb thrust per engine 1,200 hp, 1,200 hp each
112,000–123,000 lb total thrust 4,800 hp (calculated from 4 engines each with 1,200 hp)
171,700 kg 378,600 lb MTOW 26,580 kg 58,600 lb
7,500 km 4,052 nm range 2,850 mi 2,481 nm
897 km/h 557 mph cruise speed 175 mph 282 km/h
210-250 passengers capacity 8,000 pounds
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.