Boeing 767-200ER vs. Airbus H225 Super Puma

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Boeing 767-200ER versus Airbus H225 Super Puma
48.5 m 159 ft 2 in length 14.06 m 46 ft 2 in
16.1 m 52 ft 10 in height 4.38 m 14 ft 4 in
47.8 m 156 ft 9 in wingspan
2 x GE CF6-80C2B4F engines 2 x Turbomeca Makila 2A turboshaft engines
62,020 lbs thrust per engine 2,778 hp
124,040 lbs total thrust 5,556 hp
164,200 kg 362,000 lb MTOW 11,000 kg 24,251 lb
12,200 km 6,587 nmi range 857 km 463 nm
850 km/hour 528 mph cruise speed 242 km/h 150 mph
249 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.