Coating, Corrosion Preventive, Polyurethane For Aircraft Integral Fuel Tanks for Use to 250 °F (121 °C)
- Aerospace Material Specification
This specification covers two types of polyurethane coatings.
The coating materials covered by this specification have been used typically for the protection of aircraft integral fuel tanks against corrosion from fuel contaminants but usage is not limited to such applications. They are suitable for use in a service temperature range from -65 to +250 °F (-54 to +121 °C).
|Aerospace Material Specification||Sealing Compound, Fuel Resistant, Integral Fuel Tanks and Fuel Cell Cavities|
|Aerospace Material Specification||Sealing Compound, Polysulfide (T) Synthetic Rubber for Integral Fuel Tank and Fuel Cell Cavities Low Density for Intermittent Use to 360 °F (182 °C)|
|Aerospace Material Specification||Sealing Compound, Topcoat, Fuel Tank Buna-N Type|
Data Sets - Support Documents
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