Consolidated B-24 Liberator vs. Airbus H225 Super Puma

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Consolidated B-24 Liberator versus Airbus H225 Super Puma
20.42 m 67 ft 0 in length 14.06 m 46 ft 2 in
5.49 m 18 ft height 4.38 m 14 ft 4 in
33.53 m 110 ft wingspan
4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines engines 2 x Turbomeca Makila 2A turboshaft engines
1,200 hp, 1,200 hp each thrust per engine 2,778 hp
4,800 hp (calculated from 4 engines each with 1,200 hp) total thrust 5,556 hp
26,580 kg 58,600 lb MTOW 11,000 kg 24,251 lb
2,850 mi 2,481 nm range 857 km 463 nm
175 mph 282 km/h cruise speed 242 km/h 150 mph
8,000 pounds capacity 24-28
rotor diameter 16.2 m 53 ft 2 in
rate of climb 10.7 m/s 2,106 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.