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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 documentÂ’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
- File Size:
- 1 file , 530 KB
