Airbus A321XLR vs. Brewster F2A Buffalo

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Airbus A321XLR 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 LEAP-1A and P&W PW1100G engines 1 x Wright R-1820-40 Cyclone 9 9-cyl air-cooled radial piston engine
33,000 lbs (147 kN) thrust per engine 950 horsepower
66,000 lbs (294 kN) total thrust 950 horsepower
101,000 kg 222,700 lb MTOW 3,247 kg 7,159 lb
4,700 nmi 8,704 km range 1,664 km 900 mi
963km/h 598mph cruise speed 259 km/h 161 mph
180-220 seats (typical 2-class seating) 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.