Type This procurement specification covers aircraft quality bolts and screws 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 to 185 000 psi. Application Primarily for aerospace propulsion system applications 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 AS7452B-2014 history
2021SAE AS7452D-2021 Bolts and Screws, Steel, Low Alloy Heat Treated, Roll Threaded
2021SAE AS7452C-2021 Bolts and Screws, Steel, Low Alloy Heat Treated, Roll Threaded
2014SAE AS7452B-2014 Bolts and Screws@ Steel@ Low Alloy Heat Treated@ Roll Threaded
2009SAE AS7452A-2009 Bolts and Screws@ Steel@ Low Alloy Heat Treated@ Roll Threaded
2004SAE AS7452-2004 BOLTS AND SCREWS, STEEL, LOW ALLOY Heat Treated, Roll Threaded
1991SAE AS7452-1991 Bolts and Screws, Steel, Low Alloy Heat Treated, Roll Threaded