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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STANDARD

Steel, Bars and Forgings, 3.1Cr - 11.5Ni - 13.5Co - 1.2Mo (0.21 - 0.25C), Vacuum Melted, Annealed, Heat Treatable to 290 ksi (1999 MPa) Tensile Strength

AMS6478B

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STANDARD

Steel, Corrosion-Resistant, Plate 13Cr - 8.0Ni - 2.2Mo - 1.1Al Vacuum Induction Plus Consumable Electrode Melted Solution Heat Treated, Precipitation Hardenable

AMS5864D

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STANDARD

Steel, Corrosion-Resistant, Bars, Wire, and Forgings 12Cr - 11Ni - 1.7Ti - 1Mo Vacuum Induction Plus Vacuum Consumable Electrode Remelted Solution Heat Treated, Precipitation Hardenable

AMS5936D

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