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BOLT, SELF-RETAINING, IMPEDANCE TYPE - Rev.2

contributor authorAIA/NAS - Aerospace Industries Association of America Inc.
date accessioned2017-09-04T16:39:16Z
date available2017-09-04T16:39:16Z
date copyright06/28/2013
date issued2013
identifier otherVKPVEFAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;quein/handle/yse/102916
description abstractThis specification establishes the requirements for an impedance-type self-retaining bolt that is intended for critical applications.Intended Use: The self-retaining bolts covered by this specification are primarily intended for use in shear applications (see NASM33602) at dynamic points in flight control linkages, engine control mechanisms, field controls, bell crank systems, and other dynamic joint assemblies of aircraft where the failure or omission of cotter pin or locking wire would affect safety of flight or endanger personnel. For procurement purposes, this is a critical application item.
languageEnglish
titleAIA/NAS NASM83050num
titleBOLT, SELF-RETAINING, IMPEDANCE TYPE - Rev.2en
typestandard
page17
statusActive
treeAIA/NAS - Aerospace Industries Association of America Inc.:;2013
contenttypefulltext


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