McDonnell-Douglas MD-11 vs. Airbus H225 Super Puma

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McDonnell-Douglas MD-11 versus Airbus H225 Super Puma
61.20 m 200 ft 10 in length 14.06 m 46 ft 2 in
17.6 m 57 ft 9 in height 4.38 m 14 ft 4 in
51.6 m 169 ft 4 in wingspan
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 2 x Turbomeca Makila 2A turboshaft engines
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 2,778 hp
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 5,556 hp
285,990 kg 630,400 lb MTOW 11,000 kg 24,251 lb
13,231 km 7,147 nm range 857 km 463 nm
961 km/h 597 mph cruise speed 242 km/h 150 mph
Max 410 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.