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). Revision A constitutes the Five-Year Review and update of this standard. The table below details the technical changes to the specification.
Primer, Anodic Electrodeposition for Aircraft Applications
17.10.2019
Aufsatz (Konferenz)
Englisch
Primer, Anodic Electrodeposition for Aircraft Applications
SAE Technical Papers | 2012
EPOXY PRIMER PLATING Electrodeposition
SAE Technical Papers | 1995
Epoxy Primer Plating Electrodeposition
SAE Technical Papers | 1991
A Primer of Aircraft Multiplexing
SAE Technical Papers | 1991
Zinc-Chromate Primer Alternatives for Aircraft Engine Inserts & Fasteners
British Library Conference Proceedings | 1999
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