Browse Standards AMS6532B
Historical REVISED 2001-10-01

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 AMS6532B

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).

AMS6532H
2018-09-02
Latest
Revised
AMS6532G
2018-06-11
Historical
Revised
AMS6532F
2014-02-06
Historical
Revised
AMS6532E
2011-06-23
Historical
Revised
AMS6532D
2006-02-28
Historical
Revised
AMS6532C
2005-09-22
Historical
Revised
AMS6532B
2001-10-01
Historical
Revised
AMS6532A
1995-06-01
Historical
Revised

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