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
$74.00 USD
In Stock
Print  :
$82.00 USD
In Stock
AIA/NAS Aerospace Standards
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.