{
  "$type": "site.standard.document",
  "description": "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)…",
  "path": "/patents/1417269",
  "publishedAt": "2023-10-04T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D27/40",
    "GULFSTREAM AEROSPACE CORP [US]"
  ],
  "textContent": "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.",
  "title": "SYSTEM AND METHOD TO PREVENT UNINTENDED AIRCRAFT ENGINE SHUTDOWN"
}