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SAE AS7458

Revision B, January 1, 2016

Complete Document

Studs, Steel, Low Alloy, Heat Resistant Normalized and Tempered, Roll Threaded 135000 psi Tensile Strength



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Product Details:

  • Revision: Revision B, January 1, 2016
  • Published Date: January 2016
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 19
  • ANSI Approved: No
  • DoD Adopted: Yes

Description / Abstract:

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 temperature.

AS7458-1 135 000 psi ultimate tensile strength at room temperature, 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.
AIA/NAS Aerospace Standards