{
  "$type": "site.standard.document",
  "coverImage": {
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  "description": "The invention relates to a method for modifying the installation configuration of an aircraft (1) and an aircraft (1) comprising an engine (10) housed in an engine compartment (22) and an engine control device (15) adapted to control at least one parameter of the engine (10), in which the engine…",
  "path": "/patents/1419010",
  "publishedAt": "2024-08-07T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D31/00",
    "AIRBUS OPERATIONS SL [ES]"
  ],
  "textContent": "The invention relates to a method for modifying the installation configuration of an aircraft (1) and an aircraft (1) comprising an engine (10) housed in an engine compartment (22) and an engine control device (15) adapted to control at least one parameter of the engine (10), in which the engine control device (15) is installed in said engine compartment (22).",
  "title": "METHOD FOR MODIFYING THE INSTALLATION OF AN ENGINE CONTROL DEVICE IN AN AIRCRAFT"
}