AMS6472H Steel, Bars and Forgings and Forging Stock, Nitriding, 1.6Cr - 0.35Mo - 1.1Al (0.38 - 0.43C) (135 Mod), Aircraft Quality, Hardened and Tempered, 112 ksi (772 MPa) Tensile Strength

Revised

12/26/2023

Features
Issuing Committee
Scope
Content
This specification covers an aircraft-quality, low-alloy steel in the form of heat-treated bars and forgings, and of forging stock.
Rationale
Content
AMS6472H is the result of a Five-Year Review and update of the specification. The revision updates the title to include product form and quality consistent with the Scope and Quality, adds composition reporting information (see 3.1.1), clarifies the macrostructure requirements (see 3.4.1 and 8.7), revises decarburization testing methods (see 3.4.4.4), incorporates the requirements of AMS2301 (see 4.2.1, 4.4.1, 4.4.3, and 4.4.5), adds ordering operations for forging stock (see 4.4.3), adds information on ordering bar (see 8.5), and updates the prohibition on product exceptions (note removed from Table 2; see 8.6).
Meta TagsDetails
DOI
https://doi.org/10.4271/AMS6472H
Pages
8
Citation
SAE International Material Specification, Steel, Bars and Forgings and Forging Stock, Nitriding, 1.6Cr - 0.35Mo - 1.1Al (0.38 - 0.43C) (135 Mod), Aircraft Quality, Hardened and Tempered, 112 ksi (772 MPa) Tensile Strength, SAE Standard AMS6472H, Revised January 2024, Reaffirmed February 2006, Issued February 1965, https://doi.org/10.4271/AMS6472H.
Additional Details
Publisher
Published
Dec 26, 2023
Product Code
AMS6472H
Content Type
Material Specification
Status
Revised
Language
English