AMS3144A Primer, Anodic Electrodeposition for Aircraft Applications

Revised

10/17/2019

Features
Issuing Committee
Scope
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).
Meta TagsDetails
DOI
https://doi.org/10.4271/AMS3144A
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.
Additional Details
Publisher
Published
Oct 17, 2019
Product Code
AMS3144A
Content Type
Material Specification
Status
Revised
Language
English

Revisions