Using an airframe essentially similar to that of the export models, with increased fuel-tankage, lengthened forward fuselage and a Wright R-1820-40 nine-cylinder air-cooled radial engine similar to that of the F2A-2, but set forward 9 in (22,86 cm) for center of gravity reasons, producing 1,200 hp for take off and 900 hp at 14,000 ft (4,267 m). The F2A-3 embodied some armor and retained the quartet of 0.50 in (12.7 mm) Colt guns.
The F2A-3s were delivered to the USN between July and December 1941, but the higher loaded weight by comparison with earlier USN models adversely affected the performance and the type saw relatively brief service with the USN and the USMC, production of the Brewster fighter terminating in March 1942.
The photo shows pilot Lieutenant-Commander Joseph C. Clifton, pictured during a training flight."
Span: 35 ft 0 in (10.67 m)
Length: 26 ft 4 in (8.02 m)
Height: 12 ft 1 in (3.68 m)
Wing area: 208.9 sq ft (19.41 sq.m)
Empty weight: 4,732 lb (2,146 kg)
Loaded weight: 6,321 lb (2,867 kg)
Max speed: 284 mph (457 km/h) at sea level
Max speed: 321 mph (516 km/h) at 16,500 ft (5,030 m)
Climb: 2,290 ft (698 m)/min
Range: 965 mls (1,553 km)
