Airbus A220-300 vs. Airbus H225 Super Puma

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Airbus A220-300 versus Airbus H225 Super Puma
38.7 m 127 ft 0 in length 14.06 m 46 ft 2 in
11.5 m 37 ft 9 in height 4.38 m 14 ft 4 in
35.1 m 115 ft 2 in wingspan
2 x Pratt & Whitney PurePower PW1500G engines 2 x Turbomeca Makila 2A turboshaft engines
21,000–23,000 lb thrust per engine 2,778 hp
42,000–46,000 lb total thrust 5,556 hp
70,900 kg 156,300 lb MTOW 11,000 kg 24,251 lb
6,297 km 3,402 nm range 857 km 463 nm
Mach 0.82 101,3 km/h cruise speed 242 km/h 150 mph
Typical seating 2-class 120-150 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.