Airbus A319neo vs. Mil Mi-26

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Airbus A319neo versus Mil Mi-26
33.84 m 111 ft 0 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
110kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine 8,380 kW
220kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust 16,760 kW
75,500 kg 166,400 lb MTOW 56,000 kg 123,459 lb
6,850 km 3,702 nm range 800 km 432 nm
530 mph 853 km/h cruise speed 255 km/h 158 mph
120-150 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.