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The first radial-engined Hawk resulted from the mating
of a P-1A airframe with a 390hp Curtiss R-1454 engine
as the XP-3 in October 1926. The failure of the Curtiss
engine led to its substitution by a 410hp Pratt & Whitney
R-1340-9, with which it was tested in April 1928 as
the XP-3A. Five production examples had been ordered
in December 1927 as P-3As, deliveries commencing in
September 1928. The P-3A was powered by the
R-1340-3 version of the Wasp, also rated at 410hp, and
the first production example was flown with various experimental
cowlings as the second XP-3A. Both this
and the original XP-3A were eventually to become
XP-21s, the second XP-3A undergoing further conversion
(after testing as an XP-21) to P-1F standards. Armament
of the P-3A comprised two 7.62mm
machine guns and this type was fitted with a Townend
ring after service entry.
| WEIGHTS |
| Take-off weight | 1265 kg | 2789 lb |
| Empty weight | 887 kg | 1956 lb |
| DIMENSIONS |
| Wingspan | 9.63 m | 31 ft 7 in |
| Length | 6.83 m | 22 ft 5 in |
| Height | 2.67 m | 8 ft 9 in |
| Wing area | 23.41 m2 | 251.98 sq ft |
| PERFORMANCE |
| Max. speed | 246 km/h | 153 mph |
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