Airbus A321XLR vs. Mil Mi-26

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Airbus A321XLR 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
CFM LEAP-1A and P&W PW1100G engines 2 x Lotarev D-136 turboshaft engines
33,000 lbs (147 kN) thrust per engine 8,380 kW
66,000 lbs (294 kN) total thrust 16,760 kW
101,000 kg 222,700 lb MTOW 56,000 kg 123,459 lb
4,700 nmi 8,704 km range 800 km 432 nm
963km/h 598mph cruise speed 255 km/h 158 mph
180-220 seats (typical 2-class seating) 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.