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The final production PW-9D (the 16th) was retained by
Boeing for the experimental installation of a 600hp
water-cooled Curtiss Conqueror V-1570 engine and, as
the XP-7 (Model 93), was eventually delivered to the
USAAC on 4 September 1928. Distinguished from the
PW-9D by a shorter, deeper nose with a larger radiator,
the XP-7 enjoyed some success during trials, proving
the suitability of the Conqueror for fighter installation,
but proposals to build four service evaluation P-7s were
As the XP-7, the last production PW-9 was used
to test the Conqueror engine for fighter use.
abandoned when it was concluded that the basic PW-9
airframe had reached the limit of its development. The
XP-7, the last Boeing fighter biplane to employ a liquid-cooled
engine, was reconverted to PW-9D standards.
| WEIGHTS |
| Take-off weight | 1479 kg | 3261 lb |
| Empty weight | 1 053 kg | 2 lb |
| DIMENSIONS |
| Wingspan | 9.75 m | 31 ft 12 in |
| Length | 7.31 m | 23 ft 12 in |
| Height | 2.74 m | 8 ft 12 in |
| Wing area | 22.39 m2 | 241.00 sq ft |
| PERFORMANCE |
| Max. speed | 269 km/h | 167 mph |
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