Airbus A310-300 vs. Consolidated B-24 Liberator

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Airbus A310-300 versus Consolidated B-24 Liberator
46.66 m 153 ft 1 in length 20.42 m 67 ft 0 in
15.8 m 51 ft 10 in height 5.49 m 18 ft
43.9 m 144 ft wingspan 33.53 m 110 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines
52,000 lb thrust per engine 1,200 hp, 1,200 hp each
104,000 lb total thrust 4,800 hp (calculated from 4 engines each with 1,200 hp)
148,768 kg 328,000 lb MTOW 26,580 kg 58,600 lb
8,050 km 4,348 nm range 2,850 mi 2,481 nm
482 knots 279 mph cruise speed 175 mph 282 km/h
190-230 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.