SAE AMS 4342E-2007 Aluminum Alloy Extrusions 6 2Zn - 2 3Cu - 2 2Mg - 0 12Zr (7050-T74511) Solution Heat Treated Stress Relieved Straightened and Overaged (UNS A97050)《6 2Zn 2 3Cu 2.pdf

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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/AMS4342E AEROSPACE MATERIAL SPECIFICATION AMS4342 REV. E Issued 1978-04 Revised 2007-08 Reaffir

5、med 2017-11 Superseding AMS4342D Aluminum Alloy, Extrusions 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T74511) Solution Heat Treated, Stress Relieved, Straightened, and Overaged (Composition similar to UNS A97050) RATIONALE AMS4342E has been reaffirmed to comply with the SAE Five-Year Review policy. SAE INTERNATIONAL AMS4342E Page 2 of 5_ SAE INTERNATIONAL AMS4342E Page 3 of 5_ SAE INTERNATIONAL AMS4342E Page 4 of 5_ SAE INTERNATIONAL AMS4342E Page 5 of 5_