Airbus A320-200 vs. Consolidated B-24 Liberator

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Airbus A320-200 versus Consolidated B-24 Liberator
38.7 m 127 ft 0 in length 20.42 m 67 ft 0 in
17.4 m 57 ft 1 in height 5.49 m 18 ft
35.8 m 117 ft 5 in wingspan 33.53 m 110 ft
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines
Between 21,000 - 33,000 lbf thrust per engine 1,200 hp, 1,200 hp each
Between 42,000 - 66,000 lbf total thrust 4,800 hp (calculated from 4 engines each with 1,200 hp)
77,000 kg 169,800 lb MTOW 26,580 kg 58,600 lb
5,700 km 3,078 nm range 2,850 mi 2,481 nm
530 mph 853 km/h cruise speed 175 mph 282 km/h
Typically between 140-180 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.