Airbus A330-200 vs. Airbus H225 Super Puma

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Airbus A330-200 versus Airbus H225 Super Puma
58.82 m 193 ft 0 in length 14.06 m 46 ft 2 in
17.39 m 57 ft 1 in height 4.38 m 14 ft 4 in
64 m 210 ft wingspan
2 Turbofans engines 2 x Turbomeca Makila 2A turboshaft engines
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine 2,778 hp
Depends on the engine variant total thrust 5,556 hp
251,000 kg 553,400 lb MTOW 11,000 kg 24,251 lb
15,094 km 8,150 nm range 857 km 463 nm
531 mph 855 km/h cruise speed 242 km/h 150 mph
220-260 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.