A comprehensive software system and a method for performing a comprehensive reliability analysis of an aircraft are provided. For example, an aircraft systems database is analyzed to extract information corresponding to an aircraft. A plurality of goodness-of-fit tests may be performed based upon the information using a plurality of statistics and a plurality of significance levels to generate a plurality of results of the plurality of goodness-of-fit tests. The plurality of results may be analyzed to determine a distribution model associated with a fit establishing a criteria. The distribution model may be applied to the information to determine a set of reliability indexes. A reliability report may be generated for a part of the aircraft based upon the set of reliability indexes. Maintenance of the part of the aircraft may be facilitated based upon the reliability report and/or illustrations generated based upon the set of reliability indexes.


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    Titel :

    AIRCRAFT MAINTENANCE AND AIRCRAFT RELIABILITY ENGINEERING SOFTWARE SYSTEM


    Beteiligte:

    Erscheinungsdatum :

    25.07.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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 / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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