Form: This specification covers an aircraft-quality@ low-alloy steel in the form of sheet@ strip@ and plate. Application: Primarily for heat treated parts requiring through-hardening to minimum tensile strength of 200@ 000 psi (1@379 MPa) in section thickness up to 0.375 in. (9.52 mm) and proportionately lower strength in heavier thicknesses.
AMS6358D-1973由SAE - SAE International 发布于 1973-12-01,并于 2012-12-26 实施。
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