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dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2018-11-15T16:12:09Z
dc.date.available2018-11-15T16:12:09Z
dc.date.created1923-05-01en_US
dc.identifier.urihttp://hdl.handle.net/11200/49346
dc.descriptionThis document describes the Loening PW-2-B, Type I, airplane and gives the results of flight performance tests, including observations made by the test pilots related to taxiing, take-off, landing, stability, maneuverability, visibility, maintenance, and adaptability. Also included are drawings showing the plane 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. 5, no. 433en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 2024en_US
dc.subjectAirplanes--Testingen_US
dc.subjectAirplanes--Flight testingen_US
dc.subjectAirplanes--Handling characteristicsen_US
dc.subjectAirplanes, Militaryen_US
dc.titlePerformance test of Loening PW-2-B type I, equipped with Packard 1237 high-compression engine (performance test report no. 87)en_US
dc.typeTexten_US


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