Brewster F2A Buffalo vs. Grumman OV-1 Mohawk

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Brewster F2A Buffalo versus Grumman OV-1 Mohawk
8.03 m 26 ft 4 in length 12.52 m 41 ft 1 in
3.66 m 12 ft height 3.89 m 12 ft 9 in
10.67 m 35 ft wingspan 14.63 m 48 ft
1 x Wright R-1820-40 Cyclone 9 9-cyl air-cooled radial piston engine engines 2 x Lycoming T53 turboprop engines
950 horsepower thrust per engine Approximately 1,100 hp each
950 horsepower total thrust Approximately 2,200 hp total
3,247 kg 7,159 lb MTOW 14,950 lb 6,781 kg
1,664 km 900 mi range 1,690 km 913 nm
259 km/h 161 mph cruise speed 230 mph 370 km/h
capacity Pilot and observer
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.