Airbus A220-300 vs. Mil Mi-26

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Airbus A220-300 versus Mil Mi-26
38.7 m 127 ft 0 in length 40.03 m 131.3 ft
11.5 m 37 ft 9 in height 8.15 m 26.7 ft
35.1 m 115 ft 2 in wingspan
2 x Pratt & Whitney PurePower PW1500G engines 2 x Lotarev D-136 turboshaft engines
21,000–23,000 lb thrust per engine 8,380 kW
42,000–46,000 lb total thrust 16,760 kW
70,900 kg 156,300 lb MTOW 56,000 kg 123,459 lb
6,297 km 3,402 nm range 800 km 432 nm
Mach 0.82 101,3 km/h cruise speed 255 km/h 158 mph
Typical seating 2-class 120-150 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.