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Coating, Corrosion Preventative, for Aircraft Integral Fuel Tanks for Use to 250 °F (121 °C)
- Aerospace Material Specification
Published September 13, 2007 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This specification covers three types of corrosion preventative coatings for protection of aircraft integral fuel tanks.
AMS-C-27725B results from a five-year update, clarification of test requirements, and addition of a nonchromated classification for fuel tank coatings.
|Aerospace Material Specification||Coating, Corrosion Preventative, for Aircraft Integral Fuel Tanks for Use to 250 °F (121 °C)|
|Aerospace Material Specification||Sealing Compound, Polythioether Rubber Fast Curing for Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C)|
Data Sets - Support Documents
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|TABLE 1||APPLICATION PROPERTIES|
|TABLE 2||STANDARD TOLERANCES|
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|TABLE 3||PANEL SIZE REQUIREMENTS|
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
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