Boeing 787-10 vs. Airbus H225 Super Puma

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Boeing 787-10 versus Airbus H225 Super Puma
68.0 m 223 ft 2 in length 14.06 m 46 ft 2 in
17 m 55 ft 9 in height 4.38 m 14 ft 4 in
60 m 196 ft 1 wingspan
2x Rolls-Royce Trent 1000 or General Electric GEnx-1B engines 2 x Turbomeca Makila 2A turboshaft engines
76,000 N thrust per engine 2,778 hp
2 x 76,000 N total thrust 5,556 hp
254,000 kg 560,000 lb MTOW 11,000 kg 24,251 lb
11,910 km 6,430 nmi range 857 km 463 nm
652 mph 1,050 kph cruise speed 242 km/h 150 mph
330 passengers 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.