Boeing 777-200 vs. Airbus H225 Super Puma

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Boeing 777-200 versus Airbus H225 Super Puma
63.7 m 209 ft 1 in length 14.06 m 46 ft 2 in
18.6 m 61 ft height 4.38 m 14 ft 4 in
64.8 m 212 ft 7 in wingspan
General Electric GE90-77B or GE90-94B, Pratt & Whitney PW4077 & PW4090, Rolls-Royce Trent 877 & Trent 895 engines 2 x Turbomeca Makila 2A turboshaft engines
Up to 94,000 pounds thrust per engine 2,778 hp
Up to 188,000 pounds total thrust 5,556 hp
299,370 kg 660,000 lb MTOW 11,000 kg 24,251 lb
5,240 nm 9,711 km range 857 km 463 nm
560 mph 901 km/h cruise speed 242 km/h 150 mph
305 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.