Airbus A320-200 vs. Mil Mi-26

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Airbus A320-200 versus Mil Mi-26
38.7 m 127 ft 0 in length 40.03 m 131.3 ft
17.4 m 57 ft 1 in height 8.15 m 26.7 ft
35.8 m 117 ft 5 in wingspan
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 2 x Lotarev D-136 turboshaft engines
Between 21,000 - 33,000 lbf thrust per engine 8,380 kW
Between 42,000 - 66,000 lbf total thrust 16,760 kW
77,000 kg 169,800 lb MTOW 56,000 kg 123,459 lb
5,700 km 3,078 nm range 800 km 432 nm
530 mph 853 km/h cruise speed 255 km/h 158 mph
Typically between 140-180 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.