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static leak
just finished 73p annual. now going for static system chk. i am sure it had a leak. now starting to run it down. any suggestions. looking at the t connectors and diagrams it appears there is a connector in the wing root and another line terminating line in the mid cabin . could this be a misprint? we will start with the instruments last handled. ie. pressure differential, altitude alerter . absolute pressure tranducer. any guidance will be appreciated. J
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