Studs, Steel, Low Alloy, Heat Resistant, Normalized and Tempered, Roll Threaded, 135 000 psi Tensile Strength
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Product Code: AS7458
Revision Number: A
Date Published: 2009-07-20
Issuing Committee:
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.
AS7458 135 000 psi ultimate tensile strength at room temperture.
AS7458-1 135 000 psi ultimate tensile strength at room temperture, nickel-cadmium plated.
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.
Product Status: In Stock
File Size:
128K
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| Current & Historical versions of this standard |
|---|
| Standard |
Date published |
?Status |
| AS7458A |
2009-07-20 |
Revised |
| AS7458 |
1991-02-01 |
Reaffirmed |
|
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