AMS6346D Steel Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Aircraft Quality Hardened and Tempered, 125 ksi (862 MPa) Tensile Strength
Revised
10/16/2023
- Features
- Issuing Committee
- Content
- This specification covers an aircraft-quality, low-alloy steel in the form of heat-treated bars 1.50 inches (38.1 mm) and less in diameter or least distance between parallel sides.
- Content
- AMS6346D is the result of a Five-Year review and update of the specification. The revision updates the Title to include product quality, adds composition reporting (3.1.2), incorporates requirements for alternative grain size evaluation method (3.1.1, 3.3.2, 4.2, 8.4), clarifies macrostructure (3.3.1), revises tensile test requirements including note on data source (3.3.3), revises decarburization testing requirements (3.3.4.4), incorporates requirements for periodic testing per AMS2301 (4.2, 4.4.5), clarifies testing requirements (4.2), adds note on bar stock quality (8.5) and updates the requirements for product exceptions (8.6)
- Pages
- 8
- Citation
- SAE International Material Specification, Steel Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Aircraft Quality Hardened and Tempered, 125 ksi (862 MPa) Tensile Strength, SAE Standard AMS6346D, Revised October 2023, Reaffirmed June 2009, Issued October 1998, https://doi.org/10.4271/AMS6346D.