Computer-controlled production and post-overhaul testing of servo-actuators is already a fact. Some challenges still exist for performing similar testing on components installed in the aircraft.An implementation of such a scheme is presented, using state-of-the-art technology. The objective of the described technique is to perform diagnostic testing on flight control hardware sufficient to determine whether the component may be left on the aircraft.


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    Title :

    Computer Aided Diagnostic Testing of Installed Flight Control Servo- Actuators


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Aerospace Technology Conference and Exposition ; 1993



    Publication date :

    1993-09-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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