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This standard establishes the recommended requirements for application of AMS3144 anodic electrodeposition primer to aerospace components. Adherence to these requirements will help facilitate satisfactory performance of the applied primer.

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).

This specification establishes the requirements for coating systems having high durability for use as aircraft exterior surface finishes. These coating systems normally are comprised of a surface treatment, a primer, and a topcoat and include a chemical stripper and a cleaning compound for topcoat washing.

This specification establishes requirements for a tape that is used to perform organic coatings adhesion testing.

This specification establishes requirements for thermoset protective coatings in powder form.

This specification covers two types of two-component, epoxy, chemical and solvent resistant primer coatings formulated primarily for spray application. These coatings are compatible with epoxy and polyurethane topcoats.

This specification provides the minimum requirements for the application of AMS3143 powder coatings to aerospace components.

This specification establishes requirements for thermoset protective coatings in powder form.

This specification establishes requirements for a high gloss paint system for use on commercial/business aircraft.

This specification establishes requirements for pressure-sensitive adhesive tape designed for masking and color separation during aircraft painting operations.

This specification establishes requirements for three types of corrosion preventative coatings for protection of aircraft integral fuel tanks.

This standard establishes the minimum requirements for training, examination, and certification of aerospace coatings application personnel applying liquid organic coatings to interior structural or exterior substrates. It establishes criteria for the certification of personnel requiring appropriate knowledge of the technical principles underlying aircraft surface preparation and coatings application for both protective and decorative purposes. Persons who successfully complete the requirements of this certification standard are considered to be able to successfully and consistently perform a broad spectrum of aerospace coatings application tasks to achieve the desired engineering purposes. This certification is not intended to determine or replace any aerospace coating operation’s proprietary engineering for the depainting, preparation, or subsequent application of organic coatings materials to aircraft surfaces.

This specification establishes requirements for a temporary protective coating (TPC) intended to protect aluminum surfaces from damage and corrosion. This specification also establishes requirements for an alkaline remover used to strip the specified TPCs.

Amendment 1 of AMSSTD595A.

This SAE Standard defines the general requirements and provides a system for the control of quality for conformal coatings suitable for application to printed circuit assemblies.

This specification covers interior aircraft cabin coatings, which when tested under specified conditions exhibit low heat release and smoke release properties.

Performance based requirements to enhance corrosion protection on the airframe.

This test method covers procedures to qualitatively determine the visual and physical condition of a liquid organic coating component (pigmented base, base without pigment, curing solution, or thinner) in a container. Also covered is evaluation of the component container to determine any degradation.