Airbus A220-100 vs. Consolidated B-24 Liberator

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Airbus A220-100 versus Consolidated B-24 Liberator
35.0 m 114 ft 10 in length 20.42 m 67 ft 0 in
11.5 m 37 ft 9 in height 5.49 m 18 ft
35.1 m 115 ft 2 in wingspan 33.53 m 110 ft
2 Turbofans (wing mounted) engines 4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines
21,000–23,000 lb thrust per engine 1,200 hp, 1,200 hp each
42,000–46,000 lb total thrust 4,800 hp (calculated from 4 engines each with 1,200 hp)
63,100 kg 139,100 lb MTOW 26,580 kg 58,600 lb
6,390 km 3,451 nm range 2,850 mi 2,481 nm
871 km/h 541 mph cruise speed 175 mph 282 km/h
Typical seating 2-class 100-120 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.