Airbus A321LR vs. Consolidated B-24 Liberator
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| Airbus A321LR |
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 |
| CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines |
| Over 33,000 lbs (147 kN) |
thrust per engine |
1,200 hp, 1,200 hp each |
| 66,000 lbs (294 kN) |
total thrust |
4,800 hp (calculated from 4 engines each with 1,200 hp) |
| 97,000 kg |
213,800 lb |
MTOW |
26,580 kg |
58,600 lb |
| 7,400 km |
4,000 nm |
range |
2,850 mi |
2,481 nm |
| 832 km/h |
517 mph |
cruise speed |
175 mph |
282 km/h |
| 180-220 passengers |
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.
