| 摘要 |
A flight control computer 500 is configured to display information related to automatically controlled engine thrust levels during a reduced thrust flight period of an aircraft, the information corresponding to one or more parameters stored in the flight control computer. The information may be displayed in an alphanumeric or graphical format corresponding to first, second 506 and third 508 engine thrust levels which are used to achieve a quiet climb. Alphanumerically displayed information may be formatted in accordance with a sequential order of the automatically controlled engine thrust levels. Graphically displayed information may include a plan or vertical view of a planned flight path 502. |
