Boeing 787-9 vs. Airbus H225 Super Puma

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Boeing 787-9 versus Airbus H225 Super Puma
63.0 m 206 ft 9 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
GEnx-1B / Trent 1000 engines 2 x Turbomeca Makila 2A turboshaft engines
76,100 pounds thrust per engine 2,778 hp
152,200 pounds total thrust 5,556 hp
254,000 kg 560,000 lb MTOW 11,000 kg 24,251 lb
14,140 km 7,635 nmi range 857 km 463 nm
652 mph 1,050 kph cruise speed 242 km/h 150 mph
290 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.