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NUT, HEXAGON, DRILLED, BOSS CONNECTION, ALUMINUM - UNS A92014
- Aerospace Standard
Published May 02, 2006 by SAE International in United States
Downloadable datasets availableAnnotation ability available
THIS DOCUMENT HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE 5-YEAR REVIEW POLICY.
THE INITIAL SAE PUBLICATION OF THIS DOCUMENT WAS TAKEN DIRECTLY FROM U.S. MILITARY STANDARD MS9200C, NOTICE 1. THIS SAE STANDARD RETAINS THE SAME PART NUMBERS ESTABLISHED BY THE ORIGINAL MILITARY DOCUMENT.
ANY REQUIREMENTS ASSOCIATED WITH QUALIFIED PRODUCTS LISTS (QPL) MAY CONTINUE TO BE MANDATORY FOR DOD CONTRACTS. REQUIREMENTS RELATING TO QPL’S HAVE NOT BEEN ADOPTED BY THE SAE FOR THIS STANDARD AND ARE NOT PART OF THIS SAE DOCUMENT.
|Magazine Issue||AEROSPACE ENGINEERING 2013-02|
|Technical Paper||Residual Strength of an Aluminum Panel with a Centric Hole and One Cracked Ligament|
Data Sets - Support Documents
|TABLE 1||PART NUMBERS AND DIMENSIONS|
|TABLE 1||PART NUMBERS AND DIMENSIONS - CONTINUED|
|AMS2470||PROTECTIVE TREATMENTS for ALUMINUM BASE ALLOYS|
|AS291||Surface Texture, Roughness, Waviness and Lay|
|MIL-S-8879||This document is not part of the subscrption.|
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