Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT
190-00663-00 Rev. A
5-132
FLIGHT MANAGEMENT
13)
Note the altitude constraints associated with each of the approach waypoints as seen in Figure 5-124. These
altitudes are loaded from the database and are displayed as light blue text, indicating these values are
“designated” for use in computing vertical deviation guidance.
Note: To no longer use the displayed altitude for calculating vertical deviation guidance, perform the
following:
a
) Press the
FMS
Knob to activate the cursor.
b
) Turn the small
FMS
Knob to highlight the desired altitude.
c
) Press the
CLR
Key.
d
) Press the
FMS
Knob to deactivate the cursor.
After making the altitude “non-designated”, it is displayed as white text.
Altitude constraint values associated with the Final Approach Fix (FAF) and waypoints beyond the FAF cannot be
designated for vertical guidance. These altitude values are always displayed as white text, as in Figure 5-124.
Vertical guidance to the FAF and on to the Missed Approach Point (MAP) is given using the WAAS GPS altitude
source, therefore, the displayed altitude values are for reference only.
Figure 5-124 Vertical Guidance is Active to the FAF
Summary of Contents for G1000:Beechcraft Baron 58/G58
Page 1: ...Hawker Beechcraft C90A GT...
