SAE AS666D

SAE AS666D – Cavity Design and O-Ring Selection for Static Seal Use in Aircraft Tubeless Tire Wheels

This document has been declared “CANCELLED” as of January 2011. By this action this document will remain listed in the Numercial Section of the Aerospace Standards Index.

This document has not been maintained. The document??s primary purpose was to provide instructions for designing a static seal gland and o-ring for the wheel halves. Modern wheel static seal gland & o-ring design must take into account the wheel size use environment and type (for example demountable flange). The designs depend on these factors such that the designs will vary for different applications as opposed to having one design for all applications as AS 666 specifies.

Product Details

Published:

01/06/2011

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1 file 530 KB

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