Bombardier CS100 vs. Airbus H225 Super Puma

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Bombardier CS100 versus Airbus H225 Super Puma
35.00 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 x Pratt & Whitney PurePower PW1500G engines 2 x Turbomeca Makila 2A turboshaft engines
84.1 kN thrust per engine 2,778 hp
168.2 kN total thrust 5,556 hp
54,931 kg 121,100 lb MTOW 11,000 kg 24,251 lb
4,074 km 2,200 nm range 857 km 463 nm
871 km/h 541 mph cruise speed 242 km/h 150 mph
110 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.