McDonnell-Douglas MD-11 vs. Mil Mi-26

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McDonnell-Douglas MD-11 versus Mil Mi-26
61.20 m 200 ft 10 in length 40.03 m 131.3 ft
17.6 m 57 ft 9 in height 8.15 m 26.7 ft
51.6 m 169 ft 4 in wingspan
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 2 x Lotarev D-136 turboshaft engines
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 8,380 kW
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 16,760 kW
285,990 kg 630,400 lb MTOW 56,000 kg 123,459 lb
13,231 km 7,147 nm range 800 km 432 nm
961 km/h 597 mph cruise speed 255 km/h 158 mph
Max 410 passengers capacity Up to 90 passengers
rotor diameter 32.00 m 105 ft 0 in
rate of climb 8 m/s 1,574 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.