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.
SYSTEM AND METHOD TO PREVENT UNINTENDED AIRCRAFT ENGINE SHUTDOWN
SYSTEM UND VERFAHREN ZUR VERHINDERUNG UNBEABSICHTIGTER FLUGZEUGMOTORABSCHALTUNG
SYSTÈME ET PROCÉDÉ POUR EMPÊCHER L'ARRÊT INVOLONTAIRE D'UN MOTEUR D'AÉRONEF
04.10.2023
Patent
Elektronische Ressource
Englisch
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