Airbus A310-300 vs. Brewster F2A Buffalo

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Airbus A310-300 versus Brewster F2A Buffalo
46.66 m 153 ft 1 in length 8.03 m 26 ft 4 in
15.8 m 51 ft 10 in height 3.66 m 12 ft
43.9 m 144 ft wingspan 10.67 m 35 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Wright R-1820-40 Cyclone 9 9-cyl air-cooled radial piston engine
52,000 lb thrust per engine 950 horsepower
104,000 lb total thrust 950 horsepower
148,768 kg 328,000 lb MTOW 3,247 kg 7,159 lb
8,050 km 4,348 nm range 1,664 km 900 mi
482 knots 279 mph cruise speed 259 km/h 161 mph
190-230 passengers capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.