A system includes an input/output interface (300), a processor, and a non-transitory computer-readable medium having instructions stored thereon. The instructions, when executed, cause the processor to receive a fault code (102), display on the input/output interface (300) a first component of an aircraft that is associated with the fault code (106), upon selection by a user of a first hyperlink (422) associated with the first component, display a physical layout (510) of the aircraft (200) in which the first component is indicated, and upon selection by the user of a second hyperlink (430) associated with the first component, display a first wiring diagram (610) of the aircraft (200) in which the first component is indicated.


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    Title :

    FAULT ISOLATION


    Additional title:

    FEHLERISOLIERUNG
    ISOLATION DE DÉFAUTS


    Contributors:

    Publication date :

    2022-04-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G06Q Datenverarbeitungssysteme oder -verfahren, besonders angepasst an verwaltungstechnische, geschäftliche, finanzielle oder betriebswirtschaftliche Zwecke, sowie an geschäftsbezogene Überwachungs- oder Voraussagezwecke , DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTING PURPOSES



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