This procurement specification covers aircraft quality studs made from a low alloy steel of the type identified under the Unified Numbering System as UNS G87400, and of a series of room temperature tensile strengths ranging from 125 000 psi to 185 000 psi. Primarily for aerospace propulsion system applications in light alloys where good strength is required and the part is protected against corrosion.
SAE AS7456-1991 history
2021SAE AS7456C-2021 Studs, Steel, Low Alloy Heat Treated, Roll Threaded
2016SAE AS7456C-2016 Studs@ Steel@ Low Alloy Heat Treated@ Roll Threaded
2010SAE AS7456B-2010 Studs, Steel, Low Alloy Heat Treated, Roll Threaded
2009SAE AS7456A-2009 Studs@ Steel@ Low Alloy Heat Treated@ Roll Threaded
2006SAE AS7456-2006 Studs, Steel, Low Alloy Heat Treated, Roll Threaded
1991SAE AS7456-1991 Studs, Steel, Low Alloy Heat Treated, Roll Threaded