AMS3144A Primer, Anodic Electrodeposition for Aircraft Applications
Revised
10/17/2019
- Features
- Issuing Committee
- Content
- 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).
- Pages
- 17
- Citation
- SAE International Material Specification, Primer, Anodic Electrodeposition for Aircraft Applications, SAE Standard AMS3144A, Revised October 2019, Issued November 2012, https://doi.org/10.4271/AMS3144A.