Airbus A318 vs. Mil Mi-26

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Airbus A318 versus Mil Mi-26
31.44 m 103 ft 2 in length 40.03 m 131.3 ft
12.56 m 41 ft 3 in height 8.15 m 26.7 ft
34.1 m 111 ft 11 in wingspan
2x CFM56-5B or 2x PW6000 engines 2 x Lotarev D-136 turboshaft engines
23,300 lb thrust per engine 8,380 kW
46,600 lb total thrust 16,760 kW
59,000 kg 130,000 lb MTOW 56,000 kg 123,459 lb
5,750 km 3,106 nm range 800 km 432 nm
963km/h 598mph cruise speed 255 km/h 158 mph
107 to 132 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.