SAE AS7460C - Online Standart

SAE AS7460C

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

Historical
Standard by SAE International, 2017-04-26

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About This Item

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. Hydrogen test requirement added to lot acceptance Table 3, Figures 1 to 7 redrawn.

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Standard Details

  • Publication Date: 2017-04-26

  • Standard Status: historical

  • Publisher: SAE International

  • Document Type: Aerospace Standard

  • Subject: Cutting, Titanium alloys, Tensile strength, Heat treatment, Conductivity, Identification numbers, Hazardous materials, Test procedures, Alloys

  • Official SAE: Doi link

Document History

  • New Version Available: AS7460D (2023-02-14)
  • This Version: AS7460C (2017-04-26)
  • Previous Version: AS7460B (2015-08-21)
  • Previous Version: AS7460A (2009-12-09)
  • Previous Version: AS7460 (2004-07-27)

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