Flight control systems, flight control methods, and aircraft are provided. An aircraft including a system and a method for receiving (510), via a fuel switch (260, 450), a first control signal indicative of an off position on a fuel switch (260, 450), determining (520) a throttle (270, 410) resolver angle of a throttle (270, 410) controller in response to the first control signal, comparing (530) the throttle (270, 410) resolver angle to a threshold throttle (270, 410) angle, and generating (540) a pilot warning in response to the first control signal and the throttle (270, 410) resolver angle exceeding the threshold throttle (270, 410) angle.


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    Title :

    SYSTEM AND METHOD TO PREVENT UNINTENDED AIRCRAFT ENGINE SHUTDOWN


    Additional title:

    SYSTEM UND VERFAHREN ZUR VERHINDERUNG UNBEABSICHTIGTER FLUGZEUGMOTORABSCHALTUNG
    SYSTÈME ET PROCÉDÉ POUR EMPÊCHER L'ARRÊT INVOLONTAIRE D'UN MOTEUR D'AÉRONEF


    Contributors:

    Publication date :

    2023-10-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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