Airbus A320neo vs. Mil Mi-26

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Airbus A320neo versus Mil Mi-26
37.57 m 123 ft 3 in length 40.03 m 131.3 ft
11.76 m 38 ft 7 in height 8.15 m 26.7 ft
35.8 m 117 ft 5 in wingspan
2 x PW 1100G or 2 x CFM LEAP-1A engines 2 x Lotarev D-136 turboshaft engines
120kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine 8,380 kW
240kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust 16,760 kW
79,000 kg 174,200 lb MTOW 56,000 kg 123,459 lb
6,300 km 3,403 nm range 800 km 432 nm
M0.82 101,3 km/h cruise speed 255 km/h 158 mph
150-180 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.