Boeing 747-8I vs. Airbus H225 Super Puma

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Boeing 747-8I versus Airbus H225 Super Puma
76.25 m 250 ft 2 in length 14.06 m 46 ft 2 in
19.35 m 63 ft 6 in height 4.38 m 14 ft 4 in
68.45 m 224 ft 7 in wingspan
4x General Electric GEnx 2B67 Turbofan engines 2 x Turbomeca Makila 2A turboshaft engines
66,500 pounds thrust per engine 2,778 hp
266,000 pounds total thrust 5,556 hp
443,613 kg 977,500 lb MTOW 11,000 kg 24,251 lb
8,000 nm 14,816 km range 857 km 463 nm
Mach 0.86 1,062 km/h cruise speed 242 km/h 150 mph
467 passengers (three-class configuration) 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.