Airbus A330-300 vs. Airbus H225 Super Puma

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Airbus A330-300 versus Airbus H225 Super Puma
63.66 m 208 ft 9 in length 14.06 m 46 ft 2 in
16.79 m 55 ft 1 in height 4.38 m 14 ft 4 in
60.3 m 197 ft 9 in wingspan
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 engines 2 x Turbomeca Makila 2A turboshaft engines
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) thrust per engine 2,778 hp
Depends on the engine type total thrust 5,556 hp
242,000 kg 533,600 lb MTOW 11,000 kg 24,251 lb
11,750 km 6,346 nm range 857 km 463 nm
900 km/h 559 mph cruise speed 242 km/h 150 mph
250-290 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.