This SAE Aerospace Recommended Practice (ARP) defines procedures for testing aircraft engine fuel pumps for the purpose of determining their resistance to deterioration, during steady state endurance test, while receiving MIL-T-5624 Grade JP-4 fuel as a homogenous mixture of gas and liquid expressed as a ratio of vapor volume to liquid volume (V/L). If any of the above conditions do not apply, refer to Section 2. ARP492C has been reaffirmed to comply with the SAE five-year review policy.


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    Title :

    Aircraft Engine Fuel Pump Cavitation Endurance Test


    Publication date :

    2021-03-09



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English