SAE AMS 4402-2006 Aluminum Alloy Extruded Profiles (2024-T432) 4 4Cu - 1 5Mg - 0 6Mn Annealed Stretch Formed Solution Heat Treated and Stress Relieved by Stretching (UNS A92027)《(2.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/AMS4402 AEROSPACE MATERIAL SPECIFICATION AMS4402 Issued 2006-09 Reaffirmed 2017-11 Aluminum All

5、oy, Extruded Profiles (2024-T432) 4.4Cu - 1.5Mg - 0.6Mn Annealed, Stretch Formed, Solution Heat Treated and Stress Relieved by Stretching (Composition similar to UNS A92027) RATIONALE AMS4402 has been reaffirmed to comply with the SAE Five-Year Review policy. SAE INTERNATIONAL AMS4402 Page 2 of 4_ SAE INTERNATIONAL AMS4402 Page 3 of 4_ SAE INTERNATIONAL AMS4402 Page 4 of 4_

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