SAE AS7468 PDF
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BOLTS AND SCREWS, COBALT-CHROMIUM-NICKEL ALLOY, CORROSION RESISTANT Forged Head, Roll Threaded After Aging, Fatigue Rated
Description
This procurement specification covers aircraft quality bolts and screws made from a corrosion resistant, work-strengthened, cobalt-chromium-nickel alloy of the type identified under the Unified Numbering System as UNS R30035, and of 260 000 psi tensile strength at room temperature.
History
| AS7468C | 2020-04-11 | Latest | Revised |
| AS7468B | 2012-11-19 | Historical | Reaffirmed |
| AS7468A | 1997-12-01 | Historical | Revised |
| AS7468 | 1991-01-17 | Historical | Issued |
| ISSUING COMMITTEE | E-25 General Standards for Aerospace and Propulsion Systems |
|---|---|
| DATE | 1991-01-17 |
| DOI | |
| ISCURRENT | |
| PAGE | 25 |
| PUBLISHER | SAE International |
| REVISED | ISSUED |
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