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Standard
Historical
SAE AMS 3144A:2019-10-17
Primer, Anodic Electrodeposition for Aircraft Applications
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Summary
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).
Technical characteristics
| Publisher | SAE International |
| Publication Date | 10/17/2019 |
| Cancellation Date | 10/17/2019 |
| Page Count | 17 |
| EAN | --- |
| ISBN | --- |
| Weight (in grams) | --- |
Replaces
27/11/2012
Superseded
Historical
Previous versions
17/10/2019
Superseded
Historical
30/06/2025
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27/11/2012
Superseded
Historical
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