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 2012 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:/www.sae.org/technical/standards/AMS5703D AEROSPACE MATERIAL SPECIFICATION AMS5703 REV. D Issued 1971-11 Revised 2
5、006-09 Reaffirmed 2012-02 Superseding AMS5703C Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 41.5Ni - 16Cr - 37Fe - 2.9Cb - 1.8Ti Consumable Electrode or Vacuum Induction Melted 1750 F (954 C) Solution, Stabilization, and Precipitation Heat Treated (Composition similar to UNS N09706) RATIONALE AMS5703D has been reaffirmed to comply with the SAE five-year review policy. SAE AMS5703D Page 2 of 7 SAE AMS5703D Page 3 of 7 SAE AMS5703D Page 4 of 7 SAE AMS5703D Page 5 of 7 SAE AMS5703D Page 6 of 7 SAE AMS5703D Page 7 of 7
