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SAE AS7460

Revision C, April 1, 2017

Complete Document

Bolts and Screws, Titanium Alloy 6.0Al - 4.0V Procurement Specification For



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Product Details:

  • Revision: Revision C, April 1, 2017
  • Published Date: April 2017
  • 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 bolts and screws made of 6.0Al - 4.0V titanium alloy and of 160 ksi tensile strength at room temperature.

Application

Primarily for aerospace propulsion system applications where high strength, light weight fasteners are required for use up to approximately 600 °F.

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