SAE AS5528F PDF
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Lubricant Application, Solid Film, Heat Cured, Corrosion Inhibiting
Category: AS
Tags: Aluminum alloys, Conductivity, Fasteners, Humidity, Magnesium alloys, Metal finishing, Test procedures, Titanium alloys
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.
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 | 2023-01-17 |
| DOI | |
| ISCURRENT | Current |
| PAGE | 5 |
| PUBLISHER | SAE International |
| REVISED | REVISED |
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