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dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2016-07-19T15:19:57Z
dc.date.available2016-07-19T15:19:57Z
dc.date.created1925-03-01en_US
dc.date.issued1925-03-01en_US
dc.identifier.urihttp://hdl.handle.net/11200/48637
dc.descriptionThis document describes the Curtiss PW-8A airplane and gives the results of flight performance tests, including observations made by the test pilots related to taxiing, take-off, climb, landing, balance, maneuverability, accessibility, and visibility. Also included are photographs showing the biplane from two different angles.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 5, no. 496en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 2436en_US
dc.subjectBiplanesen_US
dc.subjectCurtiss aircraften_US
dc.subjectAirplanes--Testingen_US
dc.subjectAirplanes--Flight testingen_US
dc.subjectAirplanes--Handling characteristicsen_US
dc.subjectAirplanes, Militaryen_US
dc.titleOfficial performance test of Curtiss PW-8A equipped with 400 H.P. Curtiss D-12 low compression engine (flying section report)en_US
dc.typeTexten_US


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