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 |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.