Boeing 747-8F vs. Airbus H225 Super Puma

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Boeing 747-8F versus Airbus H225 Super Puma
76.25 m 250 ft 2 in length 14.06 m 46 ft 2 in
19.33 m 63 ft 5 in height 4.38 m 14 ft 4 in
68.4 m 224 ft 6 in wingspan
4 x General Electric GEnx-2B67 turbofan engines engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 66,500 lbf thrust per engine 2,778 hp
Approximately 266,000 lbf total thrust 5,556 hp
442,253 kg 975,000 lb MTOW 11,000 kg 24,251 lb
8,130 km 4,390 nm range 857 km 463 nm
919 km/h 571 mph cruise speed 242 km/h 150 mph
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.