| 摘要 |
Information allowing a pilot to safer and faster determine the status of an airplane, especially at take-off and landing. The information graphically illustrates to the pilot a relation between the length of a runway and a distance required for the airplane to accelerate to a predetermined velocity and decelerate to zero velocity. The information also comprises a graphical relation between a lowest, a highest weight of the airplane and the actual weight of the airplane and an illustration of the surroundings of the runway with an indication of the most relevant obstacle. During landing the display will show the highest weight for landing using wheel brake only. Different autobrake settings will also be depicted on the runway selected for landing. If values for idle and maximum reverse thurst exist these values will also be show adjacent to the non reverser value. Calculated values will depict the actual conditions loaded into the computer by the operator/pilot. As well as approach speeds and missed approach climb restrictions will apply. |
