An airplane off ground advisory system employs at least one position sensor (218a, 218b) attached for detection of an extended condition and a compressed condition of a main landing gear (MLG, 12a, 12b). A control system (200) receives an input from the position sensor (218a, 218b). The control system (200) records a toggling of the input from an extended to a compressed to an extended condition and providing an output. At least one indicator (222a, 222b) is coupled to the control system (200) to be activated by the output.


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    Titel :

    Airplane off ground advisory system


    Weitere Titelangaben:

    Flugzeugabhebewarnsystem
    Système de conseil hors sol d'un avion


    Beteiligte:

    Erscheinungsdatum :

    06.09.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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