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During 1928, the 600hp Curtiss H-1640 Chieftain 12-
cylinder air-cooled radial appeared to show promise as
a fighter power plant, and Curtiss was assigned the
task of mating this engine to the P-6 airframe. A USAAC
contract was placed for three aircraft which were designated
P-11s. In the event, the Chieftain proved unsatisfactory
and the P-11 was abandoned (together
with the projected Curtiss XP-14 that had been designed
around this engine). Two of the airframes that
had been ordered in January 1929 were completed as
P-6Ds and the third, which was fitted with a 575hp
Wright R-1820-9 Cyclone, was assigned the designation
YP-20 on delivery in October 1930. It was later fitted
with the V-1570 engine of the XP-22, complete with
cowling, the cantilever main undercarriage members
and three-blade propeller of this aircraft to become the
XP-6E.
| WEIGHTS |
| Take-off weight | 1466 kg | 3232 lb |
| Empty weight | 1124 kg | 2478 lb |
| DIMENSIONS |
| Wingspan | 9.60 m | 31 ft 6 in |
| Length | 7.24 m | 23 ft 9 in |
| Height | 2.79 m | 9 ft 2 in |
| Wing area | 23.41 m2 | 251.98 sq ft |
| PERFORMANCE |
| Max. speed | 301 km/h | 187 mph |
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