UNLIMITED FREE ACCESS TO THE WORLD'S BEST IDEAS

close

SAE - AMS3144A

(R) Primer, Anodic Electrodeposition for Aircraft Applications

active, Most Current
Organization: SAE
Publication Date: 1 October 2019
Status: active
Page Count: 17
scope:

Form

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).

Application

The primers covered by this specification are typically applied as base primers on military, general aviation, and commercial aircraft aluminum surfaces to protect against corrosion. They are suitable for use in a service temperature range from -65 to 250 °F (-54 to 121 °C).

Classification

The primers covered by this specification shall be classified as follows:

Type 1 - Standard pigments

Type 2 - Low IR (Infrared) pigments

Class C - Chromated - contains chromium-based corrosion inhibitors

Class N - Chrome-Free - contains no chromium-based corrosion inhibitors

Grade 1 - For use with hexavalent chrome conversion coating

Grade 2 - For use with non-hexavalent chromate conversion coating

Grade 3 - For use with cleaned and deoxidized only

Safety - Hazardous Materials

While the materials, methods, applications, and processes described or referenced in this specification may involve the use of hazardous materials, this specification does not address the hazards which may be involved in such use. It is the sole responsibility of the user to ensure familiarity with the safe and proper use of any hazardous materials and to take necessary precautionary measures to ensure the health and safety of all personnel involved.

Document History

AMS3144A
October 1, 2019
(R) Primer, Anodic Electrodeposition for Aircraft Applications
Form 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...
November 1, 2012
Primer, Anodic Electrodeposition for Aircraft Applications
Form 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...

References

Advertisement