SAE AMS 4338A-2007 Aluminum Alloy Extrusions 4 0Cu - 1 3Mg - 0 60Mn (2026-T3511) Solution Heat Treated and Stress Relieved by Stretching (UNS A92026)《4 0Cu 1 3Mg 0 60Mn (2026-T3511.pdf

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1、_SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report isentirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefr

2、om, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions.Copyright 2012 SAE InternationalAll rights reserved. No part of this publication may be

3、 reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE.TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada)Tel: +1 724-776-4970 (outside USA)Fax:

4、 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AMS4338AAEROSPACEMATERIALSPECIFICATIONAMS4338 REV. AIssued 2001-09Revised 2007-08Reaffirmed 2012-09Superse

5、ding AMS4338Aluminum Alloy, Extrusions4.0Cu - 1.3Mg - 0.60Mn (2026-T3511)Solution Heat Treated and Stress Relieved by Stretching(Composition similar to UNS A92026)RATIONALEAMS4338A has been reaffirmed to comply with the SAE five-year review policy.SAE AMS4338A Page 2 of 5SAE AMS4338A Page 3 of 5SAE AMS4338A Page 4 of 5SAE AMS4338A Page 5 of 5

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