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Lubricant Application, Solid Film, Heat Cured, Corrosion Inhibiting
- Aerospace Standard
Published January 17, 2023 by SAE International in United States
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.
Address 3.2.1 heading. Allow flexibility for pretreatments provided performance requirements are met.
Data Sets - Support Documents
No Datasets Available
E-25 General Standards for Aerospace and Propulsion Systems
The SAE E-25 General Standards for Aerospace & Propulsion Systems committee addresses aerospace propulsion systems and components. These systems and components include bolts, screws, nuts, washers, studs, rivets, pins, covers, O-rings, brackets, plugs and associated procurement requirements, as well as solid film lubricants and design specifications for screw threads and fastener assembly requirements.
|AMS2488||Anodic Treatment - Titanium and Titanium Alloys Solution pH 13 or Higher|
|AMSQQP416||Plating, Cadmium (Electrodeposited)|
|AS5272||Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting Procurement Specification|
|AS8879||SCREW THREADS - UNJ PROFILE, INCH|
|ASTM D 1732||This document is not part of the subscrption.|
|ASTM D 3725||This document is not part of the subscrption.|
|ASTM F 22||This document is not part of the subscrption.|
|ASTMD1125||This document is not part of the subscrption.|
|ASTMD2510||This document is not part of the subscrption.|
|MIL-A-8625||This document is not part of the subscrption.|
|MIL-C-81302||This document is not part of the subscrption.|
|MIL-DTL-16232||This document is not part of the subscrption.|
|MIL-T-81533||This document is not part of the subscrption.|
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