An indicator assembly (300) for an aircraft landing gear for providing indication of a hard landing. The indicator assembly including an actuator member (314) pivotably movable when the pressure on a shock strut of the aircraft landing gear exceeds a desired load and stroke threshold indicative of a hard landing. A shear pin (306) is coupled to the actuator member which is configured to shear when a desired level of force is applied to at least a portion of the shear pin. A visibly recognizable indicator (308) is moved from a non-indicating position to an indicating position upon shearing of the shear pin.


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    Title :

    System for indicating an airplane hard landing


    Additional title:

    System zur Anzeige einer harten Flugzeuglandung
    Système pour indiquer un atterrissage brutal d'avion


    Contributors:

    Publication date :

    2015-10-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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