Boeing 767-300ER vs. Airbus H225 Super Puma

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Boeing 767-300ER versus Airbus H225 Super Puma
54.9 m 180 ft 3 in length 14.06 m 46 ft 2 in
15.85 m 52 ft height 4.38 m 14 ft 4 in
47.57 m 156 ft 1 in wingspan
Two Pratt & Whitney PW4060 turbofan engines engines 2 x Turbomeca Makila 2A turboshaft engines
Up to 63,300 pounds of thrust each thrust per engine 2,778 hp
Up to 126,600 pounds of thrust total thrust 5,556 hp
186,880 kg 412,000 lb MTOW 11,000 kg 24,251 lb
11,070 km 5,980 nm range 857 km 463 nm
528 MPH 850 km/h cruise speed 242 km/h 150 mph
Typically 218 (3-class) 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.