Airbus A380-800F vs. Mil Mi-26

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Airbus A380-800F versus Mil Mi-26
72.73 m 238 ft 7 in length 40.03 m 131.3 ft
24.09 m 79 ft height 8.15 m 26.7 ft
79.75 m 261 ft 8 in wingspan
4 x Engine Alliance GP7200 turbofan engines engines 2 x Lotarev D-136 turboshaft engines
70,000 to 80,000 pounds of thrust (311 to 356 kilonewtons) thrust per engine 8,380 kW
280,000 to 320,000 pounds total thrust 16,760 kW
590,000 kg 1,300,733 lb MTOW 56,000 kg 123,459 lb
14,800 km 7,992 nm range 800 km 432 nm
903 km/h 561 mph cruise speed 255 km/h 158 mph
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.