Airbus A321neo vs. Airbus H225 Super Puma

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Airbus A321neo 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
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 2 x Turbomeca Makila 2A turboshaft engines
35,000 lb thrust per engine 2,778 hp
70,000 lb total thrust 5,556 hp
97,000 kg 213,800 lb MTOW 11,000 kg 24,251 lb
7,400 km 4,000 nm range 857 km 463 nm
828 km/h 514 mph cruise speed 242 km/h 150 mph
180 to 220 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.