SAE AMS 4326-2004 Aluminum Alloy 2013 Extruded Bar Rod and Profiles 1 0 Mg - 0 80 Si - 1 8 Cu - 0 20 Cr (2013 -T6511) Solution Heat Treated Stress-Relieved by Stretching and Aged (.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 is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising there

2、from, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2017 SAE International All rights reserved. No part of this p

3、ublication may be 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: +1 724-776-497

4、0 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/standards.sae.org/AMS4326 AEROSPACE MATERIAL SPECIFICATION AMS4326 Issued 2004-11 Reaffirmed 2017-11 Aluminum All

5、oy, 2013, Extruded Bar, Rod, and Profiles 1.0 Mg - 0.80 Si - 1.8 Cu - 0.20 Cr (2013 -T6511) Solution Heat Treated, Stress-Relieved by Stretching, and Aged (Composition similar to UNS A92013) RATIONALE AMS4326 has been reaffirmed to comply with the SAE Five-Year Review policy. SAE INTERNATIONAL AMS4326 Page 2 of 6_ SAE INTERNATIONAL AMS4326 Page 3 of 6_ SAE INTERNATIONAL AMS4326 Page 4 of 6_ SAE INTERNATIONAL AMS4326 Page 5 of 6_ SAE INTERNATIONAL AMS4326 Page 6 of 6_

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