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/AMS5661F AEROSPACE MATERIAL SPECIFICATION AMS5661 REV. F Issued 1964-01 Revised 2
5、005-08 Reaffirmed 2012-02 Superseding AMS5661E Nickel-Iron Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 42.5Ni - 12.5Cr - 5.8Mo - 2.9Ti - 0.015B - 35Fe Consumable Electrode or Vacuum Induction Melted Solution, Stabilization, and Precipitation Heat Treated (Composition similar to UNS N09901) RATIONALE AMS5661F has been reaffirmed to comply with the SAE five-year review policy. SAE AMS5661F Page 2 of 8 SAE AMS5661F Page 3 of 8 SAE AMS5661F Page 4 of 8 SAE AMS5661F Page 5 of 8 SAE AMS5661F Page 6 of 8 SAE AMS5661F Page 7 of 8 SAE AMS5661F Page 8 of 8
