A system includes an input/output interface, 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, display on the input/output interface a first component of an aircraft that is associated with the fault code, upon selection by a user of a first hyperlink associated with the first component, display a physical layout of the aircraft in which the first component is indicated, and upon selection by the user of a second hyperlink associated with the first component, display a first wiring diagram of the aircraft in which the first component is indicated.
Fault isolation
2021-12-28
Patent
Electronic Resource
English
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 |
Redundancy and fault isolation
AIAA | 1965
|British Library Conference Proceedings | 1994
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