Grumman F2F
1933
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Grumman F2F

Developed from the FF-1, the XF2F-1 prototype single-seat carrier-borne biplane fighter made its first flight just a few months after deliveries began of the earlier type. In terms of performance it was a great improvement over naval fighters then operational and so the US Navy ordered it into production. The F2F-1 production version was powered by the 484.4kW Pratt & Whitney R-1535-72 radial engine, had a neat cockpit canopy which was faired into the rear fuselage and retained the type of retractable landing gear used on the FF-1.

Soon after all F2F-1 had been delivered, Grumman produced a new prototype, the XF3F-1, which flew for the first time in March 1935. This version was slightly larger and production aircraft entered service in the following year. F3F-1 and later F3F-2 were powered by 484.4kW R-1535-84 and 559kW Wright Cyclone engines respectively, although in general construction they were identical to the F2F-1. Maximum level speed of the F3F-2 was 434.5km/h, a clear 48km/h faster than the F3F-1. Altogether a total of 216 F2F/F3F were produced, remaining operational until the latter part of 1939.

3-View 
Grumman F2FA three-view drawing (1278 x 984)


Specification 
 MODELF2F-1
 CREW1
 ENGINE1 x Pratt-Whitney R-1535-72 Twin Wasp, 485kW
 WEIGHTS
    Take-off weight1745 kg3847 lb
    Empty weight1221 kg2692 lb
 DIMENSIONS
    Wingspan8.69 m28 ft 6 in
    Length6.53 m21 ft 5 in
    Height2.77 m9 ft 1 in
    Wing area21.37 m2230.02 sq ft
 PERFORMANCE
    Max. speed383 km/h238 mph
    Cruise speed225 km/h140 mph
    Range1585 km985 miles
 ARMAMENT2 x 7.62mm machine-guns

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