This procedure is intended to apply to any aircraft fuel pump which supplies liquid hydrocarbon fuel either directly to an aircraft engine or to another pump mounted on an aircraft engine, except that it is not intended to apply to a fuel pump mounted in a fuel tank.


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    Title :

    AIRCRAFT FUEL PUMP CAVITATION ENDURANCE TEST


    Publication date :

    1957-11-15



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English