This SAE Aerospace Standard (AS) establishes the surface pretreatment, temperature and baking time required to cure AS5272 lubricant when it is applied over the surfaces of manufactured parts of various metals.
Rationale:
Clarify testing requirements for performance characteristics when used on threaded parts. General editorial update and reorganization of Requirements and Quality Assurance sections.
Related Topics:
Aluminum alloys
Magnesium alloys
Titanium alloys
Copper alloys
Lubricating greases
Humidity
Test procedures
Also known as: SAE AS 5528
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