Boeing 777-8 vs. Airbus H225 Super Puma

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Boeing 777-8 versus Airbus H225 Super Puma
69.8 m 229 ft 1 in length 14.06 m 46 ft 2 in
19.5 m 64 ft height 4.38 m 14 ft 4 in
71.8 m 235 ft 6 in wingspan
2 x GE9X-105B1A engines 2 x Turbomeca Makila 2A turboshaft engines
105,000 lb thrust per engine 2,778 hp
210,000 lb total thrust 5,556 hp
351,500 kg 775,000 lb MTOW 11,000 kg 24,251 lb
16,000 km 8,638 nm range 857 km 463 nm
900 km/h 559 mph cruise speed 242 km/h 150 mph
365 (2-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.