Type 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. Application Primarily for aerospace propulsion system applications in light alloys where good strength is required and the part is protected against corrosion. Safety - Hazardous Materials While the materials@ methods@ applications@ and processes described or referenced in this specification may involve the use of hazardous materials@ this specification does not address the hazards which may be involved in such use. It is the sole responsibility of the user to ensure familiarity with the safe and proper use of any hazardous materials and to take necessary precautionary measures to ensure the health and safety of all personnel involved.
SAE AS7456A-2009 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