{
  "$type": "site.standard.document",
  "coverImage": {
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  "description": "A system for detecting and correcting a thrust control malfunction in an aircraft engine. The system includes an electronic engine control (EEC) (18) unit that includes a first processing subsystem (A) and a second processing subsystem (B), and a thrust control malfunction accommodation (TCMA)…",
  "path": "/patents/1092743",
  "publishedAt": "2003-10-08T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D21/00",
    "BOEING CO [US]"
  ],
  "textContent": "A system for detecting and correcting a thrust control malfunction in an aircraft engine. The system includes an electronic engine control (EEC) (18) unit that includes a first processing subsystem (A) and a second processing subsystem (B), and a thrust control malfunction accommodation (TCMA) circuit (16) included in the first processing subsystem and the second processing subsystem. Additionally, the system includes a TCMA software package executed by the first processing subsystem (A) and the second processing subsystem (B), thereby providing redundant execution of the TCMA software package.",
  "title": "Thrust control malfunction accommodation system and method"
}