McDonnell-Douglas DC-9-30 vs. Airbus H225 Super Puma

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McDonnell-Douglas DC-9-30 versus Airbus H225 Super Puma
36.36 m 119 ft 3 in length 14.06 m 46 ft 2 in
8.5 m 27 ft 11 in height 4.38 m 14 ft 4 in
28.44 m 93 ft 4 in wingspan
2x Pratt & Whitney JT8D engines 2 x Turbomeca Makila 2A turboshaft engines
15,000 pound-force thrust per engine 2,778 hp
30,000 pound-force (2 engines) total thrust 5,556 hp
54,885 kg 121,000 lb MTOW 11,000 kg 24,251 lb
2,632 km 1,422 nm range 857 km 463 nm
898 km/h 558 mph cruise speed 242 km/h 150 mph
Up to 139 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.