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SAE AMS 3144:2012-11-27
Primer, Anodic Electrodeposition for Aircraft ApplicationsMore info
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).
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| ICS | 49.040 : Coatings and related processes used in aerospace industry |
| Number of pages | 17 |
| Set | AEROPAKS10U-10 |
| Year | 2012 |
| Document history | |
| Country | USA |
| Keyword | SAE 3144;SAE AMS3144;SAE AMS3144;SAE AMS 3144 |