SAE AMS3144 PDF
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Primer, Anodic Electrodeposition for Aircraft Applications
Description
This specification establishes the requirements for a waterborne, corrosion inhibiting, chemical and solvent resistant, anodic electrodeposition epoxy primer capable of curing at 200 to 210 °F (93 to 99 °C).
History
| AMS3144B | 2025-06-30 | Latest | Revised |
| AMS3144A | 2019-10-17 | Historical | Revised |
| AMS3144 | 2012-11-27 | Historical | Issued |
| ISSUING COMMITTEE | AMS G8 Aerospace Organic Coatings Committee |
|---|---|
| DATE | 2012-11-27 |
| DOI | |
| ISCURRENT | |
| PAGE | 17 |
| PUBLISHER | SAE International |
| REVISED | ISSUED |
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