A loss of communications system for an aircraft includes a fault module configured to detect a fault condition of the aircraft, and an emergency communication module configured to connect to a network, and to transmit condition data of the aircraft over the network when the fault condition is detected. The fault condition can include at least one of a loss of communication between the aircraft and a remote user or a forced landing of the aircraft. The condition data can include at least one of current location data, aircraft system health data, landing site location data, or landing site characteristics data.


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    Title :

    AIRCRAFT RECOVERY SYSTEMS


    Contributors:
    KATZ GENE I (author)

    Publication date :

    2017-09-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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