This SAE Aerospace Design Standard defines a coupling, which is installed in a high pressure (1850 to 2000 psig) oxygen system of a civil transport aircraft for the purpose of mating to ground oxygen replenishment facilities. Dimensions developed from AND10089, Detail Specification Sheet for Fitting End, Design Standard, For Cone Connection. AS1219A has been reaffirmed to comply with the SAE five-year review policy.
Aircraft Oxygen Replenishment Coupling for Civil Transport Aircraft (Design Standard)
2020-02-28
Conference paper
English
Aircraft Oxygen Replenishment Coupling for Civil Transport Aircraft (Design Standard)
SAE Technical Papers | 2003
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Civil transport aircraft design methodology
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