Airbus A310-300 vs. Airbus H225 Super Puma

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Airbus A310-300 versus Airbus H225 Super Puma
46.66 m 153 ft 1 in length 14.06 m 46 ft 2 in
15.8 m 51 ft 10 in height 4.38 m 14 ft 4 in
43.9 m 144 ft wingspan
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Turbomeca Makila 2A turboshaft engines
52,000 lb thrust per engine 2,778 hp
104,000 lb total thrust 5,556 hp
148,768 kg 328,000 lb MTOW 11,000 kg 24,251 lb
8,050 km 4,348 nm range 857 km 463 nm
482 knots 279 mph cruise speed 242 km/h 150 mph
190-230 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.