Airbus A321-200 vs. Consolidated B-24 Liberator

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Airbus A321-200 versus Consolidated B-24 Liberator
44.51 m 146 ft 0 in length 20.42 m 67 ft 0 in
11.76 m 38 ft 7 in height 5.49 m 18 ft
35.8 m 117 ft 5 in wingspan 33.53 m 110 ft
2 GE CFM56-5B3 engines 4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines
31,600 lbs thrust per engine 1,200 hp, 1,200 hp each
63,200 lbs total thrust 4,800 hp (calculated from 4 engines each with 1,200 hp)
89,000 kg 196,200 lb MTOW 26,580 kg 58,600 lb
4,000 nmi 7,408 km range 2,850 mi 2,481 nm
871 km/h 541 mph cruise speed 175 mph 282 km/h
185 to 220 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.