Boeing 767-400ER vs. Airbus H225 Super Puma

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Boeing 767-400ER versus Airbus H225 Super Puma
61.3 m 201 ft 3 in length 14.06 m 46 ft 2 in
16.9 m 55 ft 5 in height 4.38 m 14 ft 4 in
51.9 m 170 ft 3 in wingspan
2 Pratt & Whitney PW4060 turbofan engines engines 2 x Turbomeca Makila 2A turboshaft engines
Up to 63,300 pounds thrust per engine 2,778 hp
Up to 126,600 pounds total thrust 5,556 hp
204,120 kg 450,100 lb MTOW 11,000 kg 24,251 lb
9,688 km 5,232 nm range 857 km 463 nm
530 mph 853 km/h cruise speed 242 km/h 150 mph
Typical three class arrangement for 245 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.