Consolidated B-24 Liberator vs. Canadair CL-415
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| Consolidated B-24 Liberator |
versus |
Canadair CL-415 |
| 20.42 m |
67 ft 0 in |
length |
19.82 m |
65 ft 0 in |
| 5.49 m |
18 ft |
height |
8.66 m |
28 ft 5 in |
| 33.53 m |
110 ft |
wingspan |
28.6 m |
93 ft 1 |
| 4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines |
engines |
2 x Pratt & Whitney Canada PW123AF turboprop engines |
| 1,200 hp, 1,200 hp each |
thrust per engine |
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) |
| 4,800 hp (calculated from 4 engines each with 1,200 hp) |
total thrust |
4,300 to 4,760 shaft horsepower |
| 26,580 kg |
58,600 lb |
MTOW |
19,733 kg |
43,525 lb |
| 2,850 mi |
2,481 nm |
range |
1,600 km |
864 nm |
| 175 mph |
282 km/h |
cruise speed |
290 km/h |
180 mph |
| 8,000 pounds |
capacity |
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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.
