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SAE AMS-S-7108
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SAE AMS-S-7108 Revision B, March 1, 2016
Steel, Alloy (Manganese-Silicon-Nickel), Bars and Forging Stock (Aircraft
Quality)
Description / Abstract:
The materials covered by this specification are intended for use in the manufacture of aircraft parts and components which are to be heat-treated to a tensile strength of 220,000 to 240,000 psi. These steels combine high tensile strength and good ductility with relatively good impact strength at room and lower temperatures.
SAE AMS-S-7108 Revision B, March 1, 2016
Steel, Alloy (Manganese-Silicon-Nickel), Bars and Forging Stock (Aircraft
Quality)