TEFLON-IMPREGNATED OR CODEPOSITED HARD COATING TREATMENT OF ALUMINUM ALLOYS
- Aerospace Material Specification
|Aerospace Material Specification||Hard Anodic Coating Treatment of Aluminum Alloys|
|Aerospace Material Specification||Hard Anodic Coating on Aluminum and Aluminum Alloys|
|Aerospace Material Specification||Aluminum Alloy, Extruded Profiles (6056-T4511) 1.0Si - 0.90Mg - 0.80Cu - 0.60Mn - 0.40Zn Solution Heat Treated and Stress-Relieved by Stretching|
Data Sets - Support Documents
|Unnamed Dataset 1|
The committee of Finishes, Processes, and Fluids, AMS Committee B, shall prepare, coordinate, and revise documents related to processing technology, such as plating, brazing, coatings and compounds, through the participation of process suppliers, users, and interested government agencies. Committee activities shall provide a forum for the cooperative interchange of ideas and experience of the participants, resulting in the publication of specifications that embody sound, established aerospace industry practices and requirements to serve the suppliers and customers of aerospace processes.