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Deicing/Anti-Icing Fluid, Aircraft SAE Type I
- Aerospace Material Specification
Published January 18, 2006 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This specification covers a deicing/anti-icing material in the form of a fluid.
This revision of the document reflects two changes agreed to at the last G12 Fluids meeting in May of 2005. Section 3.4.5 has been reworded to allow the use of a chemically inert cup to prevent galvanic reactions in the hydrogen embrittlement test. Section 1.3.7 has been added to the document and suggests that the user may require the fluid manufacturer to demonstrate that the fluid as supplied has acceptable foaming behavior under actual application conditions.
|Aerospace Material Specification||Deicing/Anti-Icing Fluid, Aircraft SAE Type I Glycol (Conventional and Non-Conventional) Based|
|Aerospace Material Specification||Deicing/Anti-Icing Fluid, Aircraft SAE Type I Non-Glycol Based|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|TABLE 1||Total Immersion Corrosion|
The SAE G-12 Aircraft Ground Deicing committee addresses all facets of aircraft ground deicing equipment¿design, maintenance, operation, and in-service experience. It provides a focal point for the related activities of the various specialty groups and committees dealing with aircraft ground deicing. The group is comprised of eight subcommittees dedicated to creating, preparing, and maintaining all relevant specifications, standards, and requirements for aircraft ground deicing systems. These subcommittees include:G-12DF Deicing Facilities G-12HOT Hold-over Testing G-12M Methods G-12F Fluids G-12E Equipment G-12ID Ice Detection G-12T Training G-12FG Future Deicing Participants in the SAE G-12 committee include OEMs, suppliers, aircraft ground deicing equipment companies, consulting firms, government and others across the aerospace and defense industries.
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