Boeing 787-8 vs. Airbus H225 Super Puma

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Boeing 787-8 versus Airbus H225 Super Puma
57.0 m 187 ft 0 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
265.1 kN (59600 lbf) for Trent 1000-E, 321.6 kN (72300 lbf) for GEnx-1B70 thrust per engine 2,778 hp
2 * 265.1 kN (59600 lbf) for Trent 1000-E, 2 * 321.6 kN (72300 lbf) for GEnx-1B70 total thrust 5,556 hp
227,930 kg 502,500 lb MTOW 11,000 kg 24,251 lb
13,530 km 7,305 nmi range 857 km 463 nm
652 mph 1,050 kph cruise speed 242 km/h 150 mph
248 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.