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SYSTEM AND METHOD FOR IDENTIFYING FAULTS IN AN AIRCRAFT

  • US 20160144983A1
  • Filed: 11/21/2014
  • Published: 05/26/2016
  • Est. Priority Date: 11/21/2014
  • Status: Active Grant
First Claim
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1. A method of identifying a fault in an aircraft having at least one monitored system, the method comprising:

  • receiving operational data from a plurality of sensors for the at least one monitored system during at least a portion of a flight;

    receiving user input data from a user input corresponding to the operation of the at least one monitored system;

    identifying a possible fault condition based on comparing the received operational data to at least one corresponding threshold;

    analyzing the user input data corresponding to the identified possible fault condition to determine when the user input data is symptomatic of the identified possible fault condition;

    identifying an actual fault condition, by a controller, when the user input data is determined to be symptomatic of the identified possible fault condition; and

    providing an indication of the identified actual fault condition.

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