FASTENER TEST METHODS - METHOD 7 VIBRATION

Available format(s)

Hardcopy

Language(s)

English

Published date

30-11-2012

Publisher

Aerospace Industries Association

Defines a standard procedure for conducting accelerated vibration tests on any fastener system capable of providing a clamp-up load.

Committee	FSC 53GP
DevelopmentNote	Supersedes MIL STD 1312/7 (A). (08/2004)
DocumentType	Test Method
Pages	5
PublisherName	Aerospace Industries Association
Status	Current

SAE AS 4393 : 2015	NUT, SELF-LOCKING, UNS S66286, 1200 DEGREES F, 160,000 PSI, UNJ THREAD
NASA MSFC STD 561 : 2004	THREADED FASTENERS, REQUIREMENTS FOR SECURING OF FLIGHT HARDWARE USED ON SHUTTLE PAYLOADS AND EXPERIMENTS

NASM25027:2012

NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F

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NASM1312-7:2012