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Primer, Anodic Electrodeposition for Aircraft Applications
- Aerospace Material Specification
- AMS3144A
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
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
Revision A constitutes the Five-Year Review and update of this standard. The table below details the technical changes to the specification.
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Topic
Data Sets - Support Documents
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| Table 1 | Properties | |
| Table 2 | Acceptance tests | |
| Table 3 | Recertification properties | |
| Table 4 | Standard tolerances | |
| Table 5 | Aluminum test panels |
Issuing Committee
AMS G8 Aerospace Organic Coatings Committee
The AMS Committee G-8, Aerospace Organic Coatings, provides a forum to address common concerns such as application, corrosion, environmental compliance, material compatibility, OSHA requirements, performance requirements, specifications, surface preparation, and test methods. The three primary areas of activity are: 1. Writing and Maintaining Specifications 2. Cooperative Testing 3. Information Sharing and Networking
Reference
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