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 |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.