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SAE AMS6532B

Superseded

Superseded

View Superseded by

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

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

10-01-2001

Superseded date

09-22-2005

Superseded by

SAE AMS6532C

US$112.10
Excluding Tax where applicable

DocumentType
Standard
Pages
9
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

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

US$112.10
Excluding Tax where applicable