McDonnell-Douglas DC-10-30 vs. Airbus H225 Super Puma

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McDonnell-Douglas DC-10-30 versus Airbus H225 Super Puma
55.35 m 181 ft 8 in length 14.06 m 46 ft 2 in
17.8 m 58 ft 5 in height 4.38 m 14 ft 4 in
50.39 m 165 ft 4 in wingspan
3x GE CF6-50C Turbofan engines 2 x Turbomeca Makila 2A turboshaft engines
54,000 lbf thrust per engine 2,778 hp
162,000 lbf total thrust 5,556 hp
251,744 kg 555,000 lb MTOW 11,000 kg 24,251 lb
9,630 km 5,200 nm range 857 km 463 nm
507 knots 939 km/h cruise speed 242 km/h 150 mph
Up to 380 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.