| In May 1922, the former Lewis and Vought Corporation
was reorganised as the Chance Vought Corporation
and the first product of the company under its new
appellation was the UO-1 catapult-launched two-seat
observation floatplane. In 1926, two promising catapult
fighter designs were being developed by Boeing
(XF3B-1) and Curtiss (XF7C-1), but, as production deliveries
of these were some distance in the future, in
June 1926, the US Naval Bureau of Aeronautics (BuAer)
ordered for interim use aboard the catapults of US Navy
capital vessels a single-seat fighter variant of the two-seater as the UO-3. In October 1926, the designation of
this interim fighter, of which 20 had been ordered, was
changed to FU-1, and by April 1927 all had been delivered.
The FU-1 was a fabric-covered two-bay biplane
of wood and steel-tube construction powered by a
Wright J-5 (R-790) Whirlwind radial with an integral
supercharger and rated at 220hp. By comparison with
the UO-1, structural strength was increased to permit
unlimited aerobatics and diving speeds of up to
322km/h, and standard fighter armament of
two 7.62mm cowl guns was fitted. Provision
was made for interchangeable wheel and float undercarriages.
From October 1927 to June 1928, 12 of the
FU-1s were embarked aboard the battleships of the
Battle Fleet. They were subsequently fitted with wheel
undercarriages and were shore-based for three months
until replaced by Boeing F3B-1s, all 20 having been converted
to two-seat deck-landing trainers by the end of
1928 under the designation FU-2.
 | A three-view drawing (1280 x 914) |
WEIGHTS |
Take-off weight | 1258 kg | 2773 lb |
Empty weight | 941 kg | 2075 lb |
DIMENSIONS |
Wingspan | 10.46 m | 34 ft 4 in |
Length | 8.65 m | 28 ft 5 in |
Height | 3.10 m | 10 ft 2 in |
Wing area | 26.94 m2 | 289.98 sq ft |
PERFORMANCE |
Max. speed | 232 km/h | 144 mph |
Range | 660 km | 410 miles |
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