Airbus A321-200 vs. Mil Mi-26

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Airbus A321-200 versus Mil Mi-26
44.51 m 146 ft 0 in length 40.03 m 131.3 ft
11.76 m 38 ft 7 in height 8.15 m 26.7 ft
35.8 m 117 ft 5 in wingspan
2 GE CFM56-5B3 engines 2 x Lotarev D-136 turboshaft engines
31,600 lbs thrust per engine 8,380 kW
63,200 lbs total thrust 16,760 kW
89,000 kg 196,200 lb MTOW 56,000 kg 123,459 lb
4,000 nmi 7,408 km range 800 km 432 nm
871 km/h 541 mph cruise speed 255 km/h 158 mph
185 to 220 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.