Airbus A220-100 vs. Mil Mi-26

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Airbus A220-100 versus Mil Mi-26
35.0 m 114 ft 10 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 Turbofans (wing mounted) 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
63,100 kg 139,100 lb MTOW 56,000 kg 123,459 lb
6,390 km 3,451 nm range 800 km 432 nm
871 km/h 541 mph cruise speed 255 km/h 158 mph
Typical seating 2-class 100-120 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.