Airbus A320-200 vs. Airbus H225 Super Puma

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Airbus A320-200 versus Airbus H225 Super Puma
38.7 m 127 ft 0 in length 14.06 m 46 ft 2 in
17.4 m 57 ft 1 in height 4.38 m 14 ft 4 in
35.8 m 117 ft 5 in wingspan
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 2 x Turbomeca Makila 2A turboshaft engines
Between 21,000 - 33,000 lbf thrust per engine 2,778 hp
Between 42,000 - 66,000 lbf total thrust 5,556 hp
77,000 kg 169,800 lb MTOW 11,000 kg 24,251 lb
5,700 km 3,078 nm range 857 km 463 nm
530 mph 853 km/h cruise speed 242 km/h 150 mph
Typically between 140-180 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.