Airbus A300-600 vs. Airbus H225 Super Puma

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Airbus A300-600 versus Airbus H225 Super Puma
54.10 m 177 ft 6 in length 14.06 m 46 ft 2 in
16.5 m 54 ft 2 in height 4.38 m 14 ft 4 in
44.84 m 147 ft 1 in wingspan
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 2 x Turbomeca Makila 2A turboshaft engines
56,000lb to 61,500lb thrust per engine 2,778 hp
112,000–123,000 lb total thrust 5,556 hp
171,700 kg 378,600 lb MTOW 11,000 kg 24,251 lb
7,500 km 4,052 nm range 857 km 463 nm
897 km/h 557 mph cruise speed 242 km/h 150 mph
210-250 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.