This Aerospace Standard covers two basic Stall Warning Systems, one measures air flow and pressure distribution on the airfoil and the other measures the angle of airflow with respect to an arbitrary reference line. Each type of system includes, as a minimum, a sensor and the means for activating a device which warns the pilot of an impending stall. This standard contains no changes from the previous version, other than the addition of a stabilization notice page. This document has been determined to contain stable technical information which is not dynamic in nature.


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    Title :

    Minimum Performance Standard Stall Warning Equipment


    Publication date :

    2020-12-22



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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