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to any specific aircraft should be adjusted before inclusion in a maintenance manual.This document is cancelled and superseded by ARP6175A, as documented in ARP6175A.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    External Hydraulic Leakage for In-Service Components


    Publication date :

    2022-12-16



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English