{
  "$type": "site.standard.document",
  "description": "A device includes circuitry configured to, during a first operation mode, generate a static pressure indication independently of a static pressure measurement limit. The circuitry is also configured to, during a second operation mode, generate the static pressure indication based on the static…",
  "path": "/patents/1370271",
  "publishedAt": "2024-10-17T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "G01C5/005",
    "THE BOEING COMPANY"
  ],
  "textContent": "A device includes circuitry configured to, during a first operation mode, generate a static pressure indication independently of a static pressure measurement limit. The circuitry is also configured to, during a second operation mode, generate the static pressure indication based on the static pressure measurement limit. The circuitry is further configured to generate a standby altitude indication based on the static pressure indication.",
  "title": "SYSTEMS AND METHODS OF GENERATING A SELECTIVELY LIMITED AIRCRAFT STATIC PRESSURE INDICATION"
}