Airbus A350-800 vs. Mil Mi-26

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Airbus A350-800 versus Mil Mi-26
60.54 m 198 ft 7 in length 40.03 m 131.3 ft
17.05 m 55 ft 11 in height 8.15 m 26.7 ft
64.7 m 212 ft 5 in wingspan
2 Turbofans (wing mounted) engines 2 x Lotarev D-136 turboshaft engines
75,760 lb thrust per engine 8,380 kW
151,520 lb total thrust 16,760 kW
283,000 kg 623,900 lb MTOW 56,000 kg 123,459 lb
11,708 km 6,319 nm range 800 km 432 nm
552 mph 888 km/h cruise speed 255 km/h 158 mph
Typically carries 300 to 350 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.