The Boeing Company
Aircraft maintenance condition detection

Abstract:

A device includes a transceiver, a processor, a network interface, and a display interface. The transceiver is configured to receive health data from an aircraft. The processor is configured to determine whether the health data indicates a maintenance condition. The network interface is configured to send a first query to a maintenance database and to receive a first response to the first query indicating a list of parts associated with the maintenance condition. The network interface is also configured to send a second query to a historical maintenance database based on the list of parts and to receive a second response to the second query indicating failure rates of the parts. The display interface is configured to provide a graphical user interface (GUI) to a display. The processor is configured to generate the GUI indicating the list of parts ordered based on the failure rates.