Brewster F2A Buffalo vs. de Havilland Canada DHC-2 Beaver

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Brewster F2A Buffalo versus de Havilland Canada DHC-2 Beaver
8.03 m 26 ft 4 in length 13.56 m 44 ft 6 in
3.66 m 12 ft height 5 m 16 ft 5 in
10.67 m 35 ft wingspan 16.56 m 54 ft 4 in
1 x Wright R-1820-40 Cyclone 9 9-cyl air-cooled radial piston engine engines 2 x Armstrong Siddeley Double Mamba turboprop engines
950 horsepower thrust per engine Approximately 3,100 hp (2,312 kW) each
950 horsepower total thrust Approximately 6,200 hp (4,624 kW) total
3,247 kg 7,159 lb MTOW 24,200 lb 10,977 kg
1,664 km 900 mi range 2,535 km 1,369 nm
259 km/h 161 mph cruise speed 228 mph 367 km/h
capacity Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.