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FASTENER, RECESS DRIVE, 180 KSI, GENERAL SPECIFICATION FOR

contributor authorAIA/NAS - Aerospace Industries Association of America Inc.
date accessioned2017-09-04T16:41:57Z
date available2017-09-04T16:41:57Z
date copyright07/31/2013
date issued2013
identifier otherVQPQFFAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;quein/handle/yse/105318
description abstractThis specification describes requirements for aerospace externally threaded fasteners (see 6.3) of ultimate tensile stress 180 KSI Ftu and 108 KSI Fsu. It is intended as a replacement for MIL-B-87114 for NAS part standards at the 180 KSI strength level that previously called out MIL-B-87114 as the procurement specification. It is highly recommended that this specification not be called out on any new part standards either at the Standards Development Organization level or at the user community (company standard) level.Intended Use: The fasteners are intended for the assembly, repair, and maintenance of the structure of weapon systems (including aircraft and missiles) and supporting equipment.
languageEnglish
titleAIA/NAS NAS9925num
titleFASTENER, RECESS DRIVE, 180 KSI, GENERAL SPECIFICATION FORen
typestandard
page19
statusActive
treeAIA/NAS - Aerospace Industries Association of America Inc.:;2013
contenttypefulltext


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