AMS3144: 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).

Meta Tags

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

Details

DOI: https://doi.org/10.4271/AMS3144

Pages: 17

Citation: SAE International Material Specification, Primer, Anodic Electrodeposition for Aircraft Applications, SAE Standard AMS3144, Issued November 2012, https://doi.org/10.4271/AMS3144.

Additional Details

Publisher: SAE International

Published: Nov 27, 2012

Product Code: AMS3144

Content Type: Material Specification

Status: Issued

Language: English

Historical