The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide guide lines for allowable leakage for in-service aircraft hydraulic components at a nominal 100 °F (38 °C) temperature and to outline the procedure for measuring such leakage. The limits to be applied to any specific aircraft should be adjusted before inclusion in a maintenance manual.This document is cancelled and superseded by ARP6175A, as documented in ARP6175A.
External Hydraulic Leakage for In-Service Components
2022-12-16
Conference paper
English
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