Steel, Bars and Forgings 3.1cr 11.5ni 13.5co 1.2mo (0.21 - 0.25c) Vacuum Melted, Annealed Heat Treatable to 280 Ksi (1931 Mpa) Tensile Strength

Standard:
Revised:
  • 2001-10-01
 
  • HISTORICAL Access the latest revision: AMS6532F
Publisher:
  • SAE International
Pages:
9
Scope:

This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock.

These products have been used typically for heat treated parts requiring a combination of high strength, high toughness, and weldability, but usage is not limited to such applications. Product after heat treatment should attain a minimum tensile strength of 280 ksi (1931 MPa) and yield strength of 235 ksi (1620 MPa).

History:
Standard Published Revision Status
AMS6532F 2014-02-06 Latest Revised
2011-06-23 Historical Revised
2006-02-28 Historical Revised
2005-09-22 Historical Revised
2001-10-01 Historical Revised
1995-06-01 Historical Revised
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