SAE AS7458

Studs, Steel, Low Alloy, Heat Resistant Normalized and Tempered, Roll Threaded 135 000 psi Tensile Strength.

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Standard:
  • AS7458
Reaffirmed:
  • 2006-05-08
Revised:
  • 1991-02-01
Revision:
  • Historical. Access the latest revision: AS7458A
Issuing:
  • E-25 General Standards For Aerospace And Propulsion Systems
Scope:

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, and of 135 000 psi tensile strength at room temperature. 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.

History:
StandardPublishedRevisionStatus
AS7458A2009-07-20LatestRevised
AS74581991-02-01HistoricalReaffirmed
AKA:
  • SAE AS 7458
Sector:
  • Aerospace
Topic:
  • Parts

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