{
  "$type": "site.standard.document",
  "description": "A method for operating an aircraft (22) having a first propulsion unit (28A) and a second propulsion unit (28B). During this method a propulsion unit-inoperative event is identified where the first propulsion unit (28A) is inoperative and the second propulsion unit (28B) is operative. A trimmed…",
  "path": "/patents/1396122",
  "publishedAt": "2026-02-04T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D27/10",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A method for operating an aircraft (22) having a first propulsion unit (28A) and a second propulsion unit (28B). During this method a propulsion unit-inoperative event is identified where the first propulsion unit (28A) is inoperative and the second propulsion unit (28B) is operative. A trimmed parameter for the second propulsion unit (28B) is converted to an actual parameter for the second propulsion unit (28B). The actual parameter is monitored over a period of time the second propulsion unit (28B) operates during the propulsion unit-inoperative event. An action is performed in response to determining that the second propulsion unit (28B) has operated for at least a time threshold with the actual parameter being equal to or greater than a parameter threshold.",
  "title": "OPERATING AIRCRAFT PROPULSION SYSTEM DURING ENGINE-INOPERATIVE EVENT"
}