SAE AMS-S-7108A-2006
Steel, Alloy (Manganese-Silicon-Nickel), Bars and Forging Stock (Aircraft Quality)

Standard No.

SAE AMS-S-7108A-2006

Release Date

2006

Published By

Society of Automotive Engineers (SAE)

Status

Be replaced

Replace By

SAE AMS-S-7108A-2011

Latest

SAE AMS-S-7108A-2011

Scope

This specification covers manganese-silicon-nickel alloy steel bars and forging stock of aircraft quality and suitable for heat treatment to 220,000 psi minimum tensile strength.

SAE AMS-S-7108A-2006 Referenced Document

• ASTM E23-06 Standard Test Methods for Notched Bar Impact Testing of Metallic Materials*， 2024-04-20 Update

SAE AMS-S-7108A-2006 history

• 2011 SAE AMS-S-7108A-2011 Steel, Alloy (Manganese-Silicon-Nickel), Bars and Forging Stock (Aircraft Quality)
• 2006 SAE AMS-S-7108A-2006 Steel, Alloy (Manganese-Silicon-Nickel), Bars and Forging Stock (Aircraft Quality)