Airbus A321LR vs. Mil Mi-26

versus
... or view the full comparison list here.
Airbus A321LR 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 International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 2 x Lotarev D-136 turboshaft engines
Over 33,000 lbs (147 kN) thrust per engine 8,380 kW
66,000 lbs (294 kN) total thrust 16,760 kW
97,000 kg 213,800 lb MTOW 56,000 kg 123,459 lb
7,400 km 4,000 nm range 800 km 432 nm
832 km/h 517 mph cruise speed 255 km/h 158 mph
180-220 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.