Airbus A220-100 vs. Airbus H225 Super Puma

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Airbus A220-100 versus Airbus H225 Super Puma
35.0 m 114 ft 10 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 Turbofans (wing mounted) 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
63,100 kg 139,100 lb MTOW 11,000 kg 24,251 lb
6,390 km 3,451 nm range 857 km 463 nm
871 km/h 541 mph cruise speed 242 km/h 150 mph
Typical seating 2-class 100-120 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.