|National origin||United States|
|Manufacturer||Douglas Aircraft Company|
|Designer||James H. Kindelberger, Arthur Emmons Raymond|
|First flight||January 1933|
The XFD was designed to the Bureau of Aeronautics Specification No. 311, requesting a carrier-based two-seat biplane fighter. On June 30, 1932, the Navy ordered the XFD, Vought XF3U, and Curtiss XF12C for testing. The XFD was all metal except for its fabric covering. The crew sat in tandem in a single bay, enclosed by a long canopy. It was fixed gear with a tailwheel. Powered by a Pratt & Whitney Wasp, it first flew in January 1933, and was evaluated by the Navy between June 18, 1933 and August 14, 1934. The XFD performed well, but the Navy had stopped using two-seat fighters; therefore, no orders were received.
Data from Angelucci, 1987. pp. 182-183
- Crew: 2
- Length: 25 ft 4 in (7.72 m)
- Wingspan: 31 ft 6 in (9.60 m)
- Height: 11 ft 1 in (3.37 m)
- Wing area: 295 ft2 (27.40 m2)
- Empty weight: 3,227 lb (1,464 kg)
- Gross weight: 4,672 lb (2,119 kg)
- Powerplant: 1 × Pratt & Whitney R-1535-64 14-cylinder air-cooled radial engine, 700 hp ( kW) each
- Maximum speed: 208 mph (335 km/h)
- Cruise speed: 170 mph (274 km/h)
- Range: 576 miles (927 km)
- Service ceiling: 23,700 ft (7,224 m)
- Rate of climb: 1,670 ft/min (8.48 m/s)
- Angelucci, 1987. pp. 182-183.
- Angelucci, Enzo (1987). The American Fighter from 1917 to the present. New York: Orion Books.
|Wikimedia Commons has media related to Douglas XFD.|
|This page uses Creative Commons Licensed content from Wikipedia (view authors).|