|Wright XF3W Apache|
|National origin||United States|
|First flight||5 May 1926|
Development and design
After the U.S. Navy declared its preference for radial engines, Wright developed the P-1 Simoon. To demonstrate the engine, the F3W was designed to carry it. The F3W was a single-seat biplane, with a steel tubing fuselage and wood wings, covered by fabric. Designed to be a carrier-based fighter and powered by the Simoon engine, its performance was poor. After the Navy took delivery of the aircraft, they installed a rival company's engine, the Pratt & Whitney R-1340 radial. The aircraft was redesignated XF3W, and flew with the new engine for the first time on 5 May 1926.
The Navy used the XF3W as a test bed for the Pratt & Whitney engine until 1930, during which time the aircraft set a number of records. On 6 September 1926, the XF3W set the world altitude record for seaplanes of 38,500 ft (11,700 m). On 6 April 1930, it set the landplane altitude record of 43,166 ft (13,157 m). The XF3W was also fitted with a single centreline float to evaluate the concept of basing floatplanes on battleships.
Data from Angelucci, 1987. p. 462.
- Crew: 1
- Length: 22 ft 1 in (6.73 m)
- Wingspan: 27 ft 4 in (8.33 m)
- Height: 8 ft 6 in (2.59 m)
- Wing area: 215 ft2 (19.97 m2)
- Empty weight: 1,414 lb (641 kg)
- Gross weight: 2,128 lb (965 kg)
- Powerplant: 1 × Pratt & Whitney R-1340-B, 450 hp (336 kW) each
- Maximum speed: 162 mph (261 km/h)
- Service ceiling: 38,560 ft (11,753 m)
- Angelucci, 1987. p. 462.
- Johnson, E.R (2011). United States Naval Aviation, 1919-1941: Aircraft, Airships and Ships Between the Wars. United States: McFarland Publishing. pp. 353. ISBN 9780786445509.
- Angelucci, Enzo (1987). The American Fighter from 1917 to the present. New York: Orion Books. ISBN 0-517-56588-9.
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