Hello. Sign In
Standards Store
SAE AMS-S-6758 Revision A, September 1, 2003
Complete Document
Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality)
Includes all amendments and changes through Non-Current , September 2003
Page Count:14
$72.00 USD
In Stock
Print :
$80.00 USD
In Stock
AIA/NAS Aerospace Standards
IHS Standards Expert
IHS Knowledge Collections
The material covered by this specification is intended for general use in the manufacture of parts and components hardened by heat treatment to tensile a strength of 180,000 psi or less. It is weldable by fusion methods. The hardenability and weldability of this material are considered equivalent to that of MIL-S-6050.