AMS3144A: Primer, Anodic Electrodeposition for Aircraft Applications - Material Specification

Features

Issuing Committee: AMS G8 Aerospace Organic Coatings 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).

Rationale

Content: Revision A constitutes the Five-Year Review and update of this standard. The table below details the technical changes to the specification.

Meta Tags

Topics: Adhesives and sealants
Chemicals
Corrosion
Volatile organic compounds
Manufacturing processes
Coatings, colorants and finishes
Commercial aircraft
Containers
Resins
Materials properties

Details

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: SAE International

Published: Oct 17, 2019

Product Code: AMS3144A

Content Type: Material Specification

Status: Revised

Language: English

Historical