In one example, a computing system to monitor aircraft operational parameters during turnaround of an aircraft is disclosed. The computing system may include at least one processor, and memory coupled to the at least one processor. The memory may include an analytics module to obtain at least one aircraft operational parameter during turnaround of an aircraft from an aircraft on-board system, analyze the at least one aircraft operational parameter related to the turnaround with respect to a threshold value or a range of threshold values, and generate an alert based on the analysis of the at least one obtained aircraft operational parameter.


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    Title :

    MONITORING AIRCRAFT OPERATIONAL PARAMETERS DURING TURNAROUND OF AN AIRCRAFT


    Contributors:

    Publication date :

    2018-08-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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