Airbus A321LR vs. Brewster F2A Buffalo

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Airbus A321LR versus Brewster F2A Buffalo
44.51 m 146 ft 0 in length 8.03 m 26 ft 4 in
11.76 m 38 ft 7 in height 3.66 m 12 ft
35.8 m 117 ft 5 in wingspan 10.67 m 35 ft
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 1 x Wright R-1820-40 Cyclone 9 9-cyl air-cooled radial piston engine
Over 33,000 lbs (147 kN) thrust per engine 950 horsepower
66,000 lbs (294 kN) total thrust 950 horsepower
97,000 kg 213,800 lb MTOW 3,247 kg 7,159 lb
7,400 km 4,000 nm range 1,664 km 900 mi
832 km/h 517 mph cruise speed 259 km/h 161 mph
180-220 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.