Fokker XA-7
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| XA-7 | |
|---|---|
|
Atlantic-Fokker XA-7 |
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| Type | Attack |
| Manufacturer | Fokker-America |
| Maiden flight | April 1931 |
| Status | Prototype |
| Primary user | U.S. Army Air Corps |
| Number built | 1 |
The General Aviation / Fokker XA-7 was a prototype attack aircraft ordered in December 1929, and first flown in January 1931 by Fokker and then General Aviation Corporation after it bought Fokker-America in 1930, and entered in a competition held by the United States Army. However, the Curtiss A-8 won the competition, and A-7 development was not continued.
The XA-7 was a two-seat low-wing all-metal monoplane design. It featured a thick cantilever wing, tunnel radiator and two closely spaced open cockpits.
[edit] Specifications (Fokker XA-7)
General characteristics
- Crew: Two
- Length: 31 ft (9.45 m)
- Wingspan: 46 ft 9 in (14.25 m)
- Height: 9 ft 5 in (2.87 m)
- Wing area: 333 ft² (30.94 m²)
- Empty weight: 3866 lb (1754 kg)
- Max takeoff weight: 5650 lb (2563 kg)
- Powerplant: 1× Curtis Conqueror V-12 liquid cooled, 600 hp (448 kW)
Performance
- Maximum speed: 184 mph (296 km/hr)
- Stall speed: 61 mph (98 km/hr)
Armament
- 5 × .30 caliber machine guns and 488 lbs of bombs
[edit] External links
[edit] See also
Comparable aircraft
Related lists
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