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dc.creatorUnited States. Army. Air Service. Engineering Division.
dc.date.accessioned2018-07-13T18:30:38Z
dc.date.available2018-07-13T18:30:38Z
dc.date.created1921-10-01
dc.identifier.urihttp://hdl.handle.net/11200/49148
dc.descriptionThis document describes the Spad 13 airplane and gives the results of flight performance tests, including observations made by the test pilots related to taxiing, take-off, landing, balance, maneuverability, accessibility, and adaptability. Also included are images 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. 3, no. 286en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 1667en_US
dc.subjectBiplanesen_US
dc.subjectAirplanes, Militaryen_US
dc.subjectSPAD airplanesen_US
dc.subjectAirplanes--Testingen_US
dc.subjectAirplanes--Flight testingen_US
dc.subjectAirplanes--Handling characteristicsen_US
dc.titlePerformance test of Spad 13 equipped with 220 H.P. Wright engine (flight test branch performance test report no. 60)en_US
dc.typeTexten_US
dc.relation.referencesen_US


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