SAE AS5528A PDF
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Lubricant Application, Solid Film, Heat Cured, Corrosion Inhibiting
Description
This SAE Aerospace Standard (AS) establishes the surface pretreatment, temperature, and baking time required to cure AS5272 lubricant when it is applied over the surfaces of manufactured parts of various metals. This requirement is not mandatory for threaded product applications unless otherwise specified.
History
| AS5528F | 2023-01-17 | Latest | Revised |
| AS5528E | 2020-08-03 | Historical | Revised |
| AS5528D | 2020-03-10 | Historical | Revised |
| AS5528C | 2016-06-22 | Historical | Revised |
| AS5528B | 2014-07-08 | Historical | Revised |
| AS5528A | 2009-07-01 | Historical | Revised |
| AS5528 | 2005-07-18 | Historical | Issued |
| ISSUING COMMITTEE | E-25 General Standards for Aerospace and Propulsion Systems |
|---|---|
| DATE | 2009-07-01 |
| DOI | |
| ISCURRENT | |
| PAGE | 5 |
| PUBLISHER | SAE International |
| REVISED | REVISED |
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