Boeing XP-7 / Model 93
1928
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Boeing XP-7 / Model 93

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.


Specification 
 WEIGHTS
    Take-off weight1479 kg3261 lb
    Empty weight1 053 kg2 lb
 DIMENSIONS
    Wingspan9.75 m31 ft 12 in
    Length7.31 m23 ft 12 in
    Height2.74 m8 ft 12 in
    Wing area22.39 m2241.00 sq ft
 PERFORMANCE
    Max. speed269 km/h167 mph

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