This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars.
These bars have been used typically for parts with sections 1.50 inch (38.100 mm) and under in nominal thickness requiring a minimum tensile strength of 125 ksi (863 MPa), but usage is not limited to such application.
These bars have been used typically for parts with sections 1.50 inch (38.100 mm) and under in nominal thickness requiring a minimum tensile strength of 125 ksi (863 MPa), but usage is not limited to such application.
SAE AMS6346A History
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$35.00 $70.00
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