Airbus A340-500 vs. Mil Mi-26

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Airbus A340-500 versus Mil Mi-26
67.93 m 222 ft 10 in length 40.03 m 131.3 ft
17.53 m 57 ft 6 in height 8.15 m 26.7 ft
63.45 m 208 ft 2 in wingspan
4 Rolls-Royce Trent 500 engines 2 x Lotarev D-136 turboshaft engines
54,000 lbf (240 kN) thrust per engine 8,380 kW
216,000 lbf (960 kN) total thrust 16,760 kW
380,000 kg 837,800 lb MTOW 56,000 kg 123,459 lb
16,670 km 9,000 nm range 800 km 432 nm
475 knots 880 km/h cruise speed 255 km/h 158 mph
Typical seating 3-class 270-310 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.