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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 Reaffirmation Notice , April 2013


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Product Details:

  • Revision: Revision A, September 1, 2003
  • Published Date: April 2013
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 14
  • ANSI Approved: No
  • DoD Adopted: Yes

Description / Abstract:

The material covered by this specification is intended for general use in the manufacture of parts and componets hardened dy heat treatment to tensile a strengh of 180,000 psi or less.it is weldable dy fusion methods. The hardenability and weldability of this material are considered equivalent to that of mil-s-6050. 

AIA/NAS Aerospace Standards