Airbus A321XLR vs. Airbus H225 Super Puma

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Airbus A321XLR 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 LEAP-1A and P&W PW1100G engines 2 x Turbomeca Makila 2A turboshaft engines
33,000 lbs (147 kN) thrust per engine 2,778 hp
66,000 lbs (294 kN) total thrust 5,556 hp
101,000 kg 222,700 lb MTOW 11,000 kg 24,251 lb
4,700 nmi 8,704 km range 857 km 463 nm
963km/h 598mph cruise speed 242 km/h 150 mph
180-220 seats (typical 2-class seating) 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.