Airbus A340-200 vs. Mil Mi-26

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Airbus A340-200 versus Mil Mi-26
59.4 m 194 ft 11 in length 40.03 m 131.3 ft
16.8 m 55 ft 1 in height 8.15 m 26.7 ft
60.3 m 197 ft 9 in wingspan
4 x CFM International CFM56-5C4 engines 2 x Lotarev D-136 turboshaft engines
34,000 lbf thrust per engine 8,380 kW
136,000 lbf total thrust 16,760 kW
275,000 kg 606,300 lb MTOW 56,000 kg 123,459 lb
12,400 km 6,699 nm range 800 km 432 nm
880 km/h 547 mph cruise speed 255 km/h 158 mph
Typical seating 3-class 210-250 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.