SAE AMS 4202D-2005 Aluminum Alloy Plate 5 7Zn - 2 2Mg - 1 6Cu - 0 22Cr (7475-T7351) Solution Heat Treated Stress Relieved by Stretching and Precipitation Heat Treated (UNS A97475)《.pdf

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/AMS4202D AEROSPACE MATERIAL SPECIFICATION AMS4202 REV. D Issued 1978-07 Revised 2005-07 Reaff

5、irmed 2012-03 Superseding AMS4202C Aluminum Alloy Plate 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T7351) Solution Heat Treated, Stress Relieved by Stretching, and Precipitation Heat Treated (Composition similar to UNS A97475) RATIONALE AMS4202D has been reaffirmed to comply with the SAE five-year review policy. SAE AMS4202D Page 2 of 9 SAE AMS4202D Page 3 of 9 SAE AMS4202D Page 4 of 9 SAE AMS4202D Page 5 of 9 SAE AMS4202D Page 6 of 9 SAE AMS4202D Page 7 of 9 SAE AMS4202D Page 8 of 9 SAE AMS4202D Page 9 of 9