SAE AMS 3144:2012-11-27
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SAE AMS 3144:2012-11-27

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 11/27/2012
Page Count 17
Themes Aerospace
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