Airbus A321-200 vs. Airbus H225 Super Puma

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Airbus A321-200 versus Airbus H225 Super Puma
44.51 m 146 ft 0 in length 14.06 m 46 ft 2 in
11.76 m 38 ft 7 in height 4.38 m 14 ft 4 in
35.8 m 117 ft 5 in wingspan
2 GE CFM56-5B3 engines 2 x Turbomeca Makila 2A turboshaft engines
31,600 lbs thrust per engine 2,778 hp
63,200 lbs total thrust 5,556 hp
89,000 kg 196,200 lb MTOW 11,000 kg 24,251 lb
4,000 nmi 7,408 km range 857 km 463 nm
871 km/h 541 mph cruise speed 242 km/h 150 mph
185 to 220 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.