This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Coating, Corrosion Preventative, for Aircraft Integral Fuel Tanks for Use to 250 °F (121 °C)
- Aerospace Material Specification
Published March 09, 2016 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This specification establishes requirements for three types of corrosion preventative coatings for protection of aircraft integral fuel tanks.
This revision is a 5-year update which incorporates the G-8 committee standard specification format, clarifies certain test requirements, and adds a DiEGME resistant grade along with appropriate DiEGME resistance qualification test methods.
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|Unnamed Dataset 3|
|Unnamed Dataset 4|
|Unnamed Dataset 5|
|Unnamed Dataset 6|
|Unnamed Dataset 7|
|Table 2||Acceptance tests|
|Table 3||Standard tolerances|
|Table 4||Test panel plan|
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
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.