Brewster F2A Buffalo vs. Mil Mi-26

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Brewster F2A Buffalo versus Mil Mi-26
8.03 m 26 ft 4 in length 40.03 m 131.3 ft
3.66 m 12 ft height 8.15 m 26.7 ft
10.67 m 35 ft wingspan
1 x Wright R-1820-40 Cyclone 9 9-cyl air-cooled radial piston engine engines 2 x Lotarev D-136 turboshaft engines
950 horsepower thrust per engine 8,380 kW
950 horsepower total thrust 16,760 kW
3,247 kg 7,159 lb MTOW 56,000 kg 123,459 lb
1,664 km 900 mi range 800 km 432 nm
259 km/h 161 mph cruise speed 255 km/h 158 mph
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.