Boeing XP-4


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Boeing XP-4

The last aircraft built by Boeing against an order for 30 PW-9 single-seat fighters was retained by the company at the request of the USAAC for trials with a turbo-supercharged version of the 510hp Packard 1A-1500 water-cooled engine (utilised by the FB-2). The USAAC also requested an increase in wing area, because of the higher weights involved, and while the standard PW-9 upper wing was retained, an enlarged lower wing was introduced, resulting in an equi-span biplane with vertical N-type interplane struts. The standard PW-9 armament of two 7.62mm synchronised machine guns was augmented by a pair of similar-calibre weapons mounted beneath the lower wing outside the propeller arc. With these changes the aircraft was designated XP-4 (Model 58), and delivered on 27 July 1926, but the 6.32m2 increase in gross wing area by comparison with the PW-9 failed to compensate for the 370kg increase in loaded weight. The XP-4 proved to possess extremely unsatisfactory handling characteristics and after a few hours flying the test programme was abandoned.

  Take-off weight1656 kg3651 lb
  Empty weight1262 kg2782 lb
  Wingspan9.75 m32 ft 0 in
  Length7.29 m24 ft 11 in
  Height2.69 m9 ft 10 in
  Wing area28.71 m2309.03 sq ft
  Max. speed259 km/h161 mph
  Range603 km375 miles

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