Disclosed is a landing gear controller for an aircraft. The controller is configured to: detect an extension time for a landing gear, and if the detected extension time meets a predetermined criterion, provide a warning signal to indicate potential failure of a landing gear uplock hook. Also disclosed is a landing gear system, a method to detect failure of a landing gear uplock hook, and an aircraft.


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    Title :

    LANDING GEAR CONTROLLER


    Additional title:

    FAHRWERKSREGLER
    ORGANE DE COMMANDE DE TRAIN D'ATTERRISSAGE


    Contributors:

    Publication date :

    2024-02-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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