AIR6130 Cadmium Plate Cyclic Corrosion Test

Current

05/20/2011

Features
Issuing Committee
Scope
Content
14-day material test to determine the cyclic effects of runway deicing compounds on cadmium plated parts.
Rationale
Content
Some runway and taxiway deicing/anti-icing compounds have been found to cause severe corrosion on aircraft components with cadmium plating. There is a need for users to understand the effect of these compounds on aircraft components when they are exposed repeatedly in a normal winter operating environment. The existing test in the SAE AMS1431 and 1435 specifications for runway deicers is a one-time 24 hour immersion test for cadmium corrosion, which does not accurately reflect how airplanes and airport equipment are affected by runway deicers. This new AIR document with the 14-day cyclic test is intended to provide better information to the end user/purchaser of the deicing compound regarding the cyclic effects on cadmium plated airplane parts or airport equipment. The document is intended to be referred to by the AMS1431 and 1435 specifications, which will then provide more useful information to the end user in the test report.
Meta TagsDetails
DOI
https://doi.org/10.4271/AIR6130
Pages
3
Citation
SAE International Information Report, Cadmium Plate Cyclic Corrosion Test, SAE Standard AIR6130, Issued May 2011, https://doi.org/10.4271/AIR6130.
Additional Details
Publisher
Published
May 20, 2011
Product Code
AIR6130
Content Type
Information Report
Status
Current
Language
English

Revisions