
Steel, Bars, and Forgings, Aircraft Quality, 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength
NORM herausgegeben am 1.12.2024
Bezeichnung normen: SAE AMS6325M
Ausgabedatum normen: 1.12.2024
Land: Amerikanische technische Norm
Kategorie: Technische Normen SAE
This specification covers an aircraft-quality, low-alloy steel in the form of heat-treated bars and forgings.
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Material Specification