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Ams 5731

This document is the SAE AMS5731L material specification for steel that is corrosion and heat resistant. It specifies the chemical composition ranges and processing requirements for bars, wire, forgings, tubing, and rings made of a steel with 15% chromium, 25.5% nickel, 1.2% molybdenum, 2.1% titanium, and other alloying elements. The specification has been reaffirmed in 2012 to comply with SAE's five-year review policy.

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2K views7 pages

Ams 5731

This document is the SAE AMS5731L material specification for steel that is corrosion and heat resistant. It specifies the chemical composition ranges and processing requirements for bars, wire, forgings, tubing, and rings made of a steel with 15% chromium, 25.5% nickel, 1.2% molybdenum, 2.1% titanium, and other alloying elements. The specification has been reaffirmed in 2012 to comply with SAE's five-year review policy.

Uploaded by

Naveen Karthik
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AEROSPACE AMS5731 REV.

L
MATERIAL
Issued 1963-01
SPECIFICATION Revised 2006-06
Reaffirmed 2012-07

Superseding AMS5731K
Steel, Corrosion and Heat-Resistant, Bars, Wire, Forgings, Tubing, and Rings
15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V
Consumable Electrode Melted, 1800 °F (982 °C) Solution Heat Treated
(Composition similar to UNS S66286)

RATIONALE

AMS5731L has been reaffirmed to comply with the SAE five-year review policy.

__________________________________________________________________________________________________________________________________________
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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 may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying,
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