Airbus A340-200 vs. Airbus H225 Super Puma

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Airbus A340-200 versus Airbus H225 Super Puma
59.4 m 194 ft 11 in length 14.06 m 46 ft 2 in
16.8 m 55 ft 1 in height 4.38 m 14 ft 4 in
60.3 m 197 ft 9 in wingspan
4 x CFM International CFM56-5C4 engines 2 x Turbomeca Makila 2A turboshaft engines
34,000 lbf thrust per engine 2,778 hp
136,000 lbf total thrust 5,556 hp
275,000 kg 606,300 lb MTOW 11,000 kg 24,251 lb
12,400 km 6,699 nm range 857 km 463 nm
880 km/h 547 mph cruise speed 242 km/h 150 mph
Typical seating 3-class 210-250 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.