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Based on the design of the XFT, the Model 3A was developed
as a contender in the US Army's Materiel Division
competition for a successor to the P-26 in service
with the USAAC. A low-wing all-metal semi-monocoque
monoplane with fully-retractable main undercarriage
members and an enclosed cockpit, the Model 3A
was powered by a Pratt & Whitney SR-1535-6 Twin
Wasp Junior 14-cylinder radial engine rated at 700hp for take-off. It had provision for one 7.62mm
and one 12.7mm gun in the fuselage. Completed
in July 1935, it was briefly tested at Wright Field
where it was found to be somewhat unstable and prone
to spinning. Returned to the manufacturer for modification,
the Model 3A was under test over the Pacific on 30
July, but failed to return, no trace of the aircraft nor its
pilot ever being found. The design of the Model 3A was
subsequently sold to Chance Vought Aircraft which
further developed it as the V-141.
 | A three-view drawing (1276 x 816) |
| MODEL | 3A (estimated data) |
| WEIGHTS |
| Take-off weight | 1769 kg | 3900 lb |
| DIMENSIONS |
| Wingspan | 10.21 m | 33 ft 6 in |
| Length | 6.78 m | 22 ft 3 in |
| Height | 2.77 m | 9 ft 1 in |
| Wing area | 17.37 m2 | 186.97 sq ft |
| PERFORMANCE |
| Max. speed | 434 km/h | 270 mph |
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