Table of Contents

RATIONALE
1SCOPE
2APPLICABLE DOCUMENTS
3TECHNICAL REQUIREMENTS
4QUALITY ASSURANCE PROVISIONS
5PREPARATION FOR DELIVERY
6ACKNOWLEDGMENT
7REJECTIONS
8NOTES

Scope

1.1 Form This specification covers an aircraft-quality, low-alloy steel in the form of bars. 1.2 Application These bars have been used typically for parts, 0.50 inch (12.7 mm) and under in section thickness or diameter at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 35 HRC when properly hardened and tempered and also parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.

General Product Information

Published
Document Type	Standard
Status	Current
Publisher	SAE International
Pages
ISBN
Committee	AMS E
Supersedes	SAE AMS 6348 : 2013