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dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2016-08-19T18:17:59Z
dc.date.available2016-08-19T18:17:59Z
dc.date.created1925-06-15en_US
dc.date.issued1925-06-15en_US
dc.identifier.urihttp://hdl.handle.net/11200/48651
dc.descriptionThis document describes the Engineering Division XCO-6 airplane and gives the results of flight performance tests, including observations made by the test pilots related to taxiing, take-off, landing, climb and glide, landing, balance, maneuverability, accessibility, and visibility. Also included are drawings showing the biplane from three different angles.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 6, no. 521en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 2502en_US
dc.subjectBiplanesen_US
dc.subjectAirplanes--Testingen_US
dc.subjectAirplanes--Flight testingen_US
dc.subjectAirplanes--Handling characteristicsen_US
dc.subjectAirplanes, Militaryen_US
dc.titleOfficial performance test of Engineering Division XCO-6 equipped with '12' cylinder inverted Liberty engine (flying section report)en_US
dc.typeTexten_US


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