Airbus A350-1000 vs. Mil Mi-26

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Airbus A350-1000 versus Mil Mi-26
73.79 m 242 ft 1 in length 40.03 m 131.3 ft
17.08 m 56 ft height 8.15 m 26.7 ft
64.75 m 212 ft 5 in wingspan
2 Trent XWB-97 turbofan engines engines 2 x Lotarev D-136 turboshaft engines
97,000 lb thrust per engine 8,380 kW
194,000 lb total thrust 16,760 kW
319,000 kg 703,300 lb MTOW 56,000 kg 123,459 lb
16,100 km 8,695 nm range 800 km 432 nm
1,099 km/h 683 mph cruise speed 255 km/h 158 mph
350 to 410 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.