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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2012 SAE International All rights reserved. No part of this publication m
3、ay 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: +1 724-776-4970 (outside U
4、SA) 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:/www.sae.org/technical/standards/AMS4252B AEROSPACE MATERIAL SPECIFICATION AMS4252 REV. B Issued 1989-10 Revised 2005-03 Reaff
5、irmed 2012-04 Superseding AMS4252A Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated, Stress Relieved, and Overaged (Composition Similar to UNS A97150) RATIONALE AMS4252B has been reaffirmed to comply with the SAE five-year review policy. SAE AMS4252B Page 2 of 7 SAE AMS4252B Page 3 of 7 SAE AMS4252B Page 4 of 7 SAE AMS4252B Page 5 of 7 SAE AMS4252B Page 6 of 7 SAE AMS4252B Page 7 of 7
