SAE AS7466 PDF
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BOLTS AND SCREWS, NICKEL ALLOY, CORROSION AND HEAT RESISTANT Forged Head, Roll Threaded, Fatigue Rated
Description
This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07718 and of 185 000 psi tensile strength at room temperature, with maximum test temperature of parts at 800°F.
History
| AS7466F | 2021-03-25 | Latest | Revised |
| AS7466E | 2014-08-20 | Historical | Revised |
| AS7466D | 2013-09-19 | Historical | Revised |
| AS7466C | 2012-08-30 | Historical | Revised |
| AS7466B | 2005-06-07 | Historical | Revised |
| AS7466A | 2001-10-01 | Historical | Reaffirmed |
| AS7466 | 1991-01-22 | Historical | Issued |
| ISSUING COMMITTEE | E-25 General Standards for Aerospace and Propulsion Systems |
|---|---|
| DATE | 1991-01-22 |
| DOI | |
| ISCURRENT | |
| PAGE | 26 |
| PUBLISHER | SAE International |
| REVISED | ISSUED |
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