Airbus A350-900ULR vs. Mil Mi-26

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Airbus A350-900ULR versus Mil Mi-26
66.80 m 219 ft 2 in length 40.03 m 131.3 ft
17.05 m 55 ft 11 in height 8.15 m 26.7 ft
64.75 m 212 ft 5 in wingspan
2 Rolls-Royce Trent XWB engines 2 x Lotarev D-136 turboshaft engines
84,000 lbs thrust per engine 8,380 kW
168,000 lbs total thrust 16,760 kW
280,000 kg 617,300 lb MTOW 56,000 kg 123,459 lb
17,964 km 9,700 nm range 800 km 432 nm
552 mph 888 km/h cruise speed 255 km/h 158 mph
300-350 passengers in three classes 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.