SAE AS7458A

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

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Standard:
  • AS7458
  • Revision: A
Revised:
  • 2009-07-20
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.

AS 7458 135 000 psi ultimate tensile strength at room temperature

AS 7458-1 135 000 psi ultimate tensile strength at room temperature, nickel-cadium plated.>Primarily for aerospace propulsion system applications where good strength 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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