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AIA/NAS - NAS1069

TENSION FATIGUE TEST PROCEDURE FOR AERONAUTICAL FASTENERS

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Organization: AIA/NAS
Publication Date: 30 November 2012
Status: inactive
Page Count: 25
scope:

This procedures applies to such items as blots, screws, nuts, rivets, blind fasteners, and proprletary items used to perform similar functions.

Purpose

The purpose of this procedure is to provide a standardized method of tension fatigue testing of aeronautical fasteners  using tension-tension cycles.

 

 

Document History

NAS1069
November 30, 2012
TENSION FATIGUE TEST PROCEDURE FOR AERONAUTICAL FASTENERS
This procedures applies to such items as blots, screws, nuts, rivets, blind fasteners, and proprletary items used to perform similar functions. Purpose The purpose of this procedure is to provide a...
January 1, 1959
Tension Fatigue Test Procedure for Aeronautical Fasteners
This procedure applies to such items as bolts, screws, nuts, rivets, blind fasteners, and proprietary items used to perform similar functions.

References

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