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

Standard:
Revised:
  • 2009-12-09
 
  • HISTORICAL Access the latest revision: AS7460C
Publisher:
  • SAE International
Pages:
21
Scope:

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

Rationale:

Updated para 3.5 by adding “two to” three threads in agreement with NASM1312-8 test methodology. Added additional difinitions to para 2.2. General updating for SAE requirements for obsolete specifications and standards.

History:
Standard Published Revision Status
AS7460C 2017-04-26 Latest Revised
2015-08-21 Historical Revised
2009-12-09 Historical Revised
2004-07-27 Historical Reaffirmed
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