AS5528: Lubricant Application, Solid Film, Heat Cured, Corrosion Inhibiting - Technical Standard

Features

Issuing Committee: E-25 General Standards for Aerospace and Propulsion Systems

Scope

Content: 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.

Meta Tags

Topics: Aircraft propulsion systems
Titanium alloys
Aluminum alloys
Ferrous metals
Magnesium alloys
Copper alloys
Lubricating greases
Test procedures
Humidity

Details

DOI: https://doi.org/10.4271/AS5528

Pages: 7

Citation: SAE International Technical Standard, Lubricant Application, Solid Film, Heat Cured, Corrosion Inhibiting, SAE Standard AS5528, Issued July 2005, https://doi.org/10.4271/AS5528.

Additional Details

Publisher: SAE International

Published: 7/18/2005

Product Code: AS5528

Content Type: Technical Standard

Status: Issued

Language: English

Historical