SAE AS7458A
SAE AS7458A 2009-JUL-01 R Studs Steel Low Alloy Heat Resstant Normalzed and Tempered Roll Threaded 135 000 ps Tensle Strength
SAE AS7458A 2009-JUL-01 R Studs Steel Low Alloy Heat Resstant Normalzed and Tempered Roll Threaded 135 000 ps Tensle Strength
Type
This procurement specification covers aircraft quality studs made from a low alloy, heat resistant steel of the type identified under the Unified Numbering System as UNS K14675.
AS7458 135 000 psi ultimate tensile strength at room temperture.
AS7458-1 135 000 psi ultimate tensile strength at room temperture, nickel-cadmium plated.
Application
Primarily for aerospace propulsion system applications where good strength at temperatures up to approximately 900° F 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.