Bolts and Screws, Steel, Corrosion and Heat Resistant 1650 °F Solution Heat Treated Precipitation Heat Treated Before Roll Threaded
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Product Code: AS7479
Date Published: 1991-01-09 - A newer version of this standard is available.
Date Reaffirmed: May 1995
Issuing Committee:
E-25 General Standards For Aerospace And Propulsion Systems
Scope
This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286, and of 130 000 psi tensile strength at room temperature, with maximum test temperature of parts at 1200 °F.
Product Status: In Stock
File Size:
1199K
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| Current & Historical versions of this standard |
|---|
| Standard |
Date published |
?Status |
| AS7479B |
2008-08-21 |
Revised |
| AS7479A |
2001-05-01 |
Reaffirmed |
| AS7479 |
1991-01-09 |
Reaffirmed |
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- Nut, Self-Locking, Double Hexagon, Reduced Envelope, UNS S66286, Silver Plated Threads Only
- Bolt, Machine - Double Hexagon Extended Washer Head, Corrosion and Heat Resistant Steel, UNS S66286, UTS 130 ksi min, .3125-24 UNJF-3A
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