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Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
SECTION 6 – AUTOMATIC
FLIGHT CONTROL
6-6
Vertical Speed Mode (VS)
1. Press the
VS
key. The flight director is now
activated (if not already active) and VS’ is
displayed in green in the Active Mode field and
the Vertical Speed Bug will appear on the Verti-
cal Speed Indicator. Pitch and roll commands
are given to manually maintain vertical speed.
Press the
AP
key to engage the autopilot for
maintaining the current vertical speed.
Altitude Hold mode is automatically armed with
ALT’ displayed white in the Armed Mode field
to the right of the ‘VS’ annunciation.
2. If the autopilot is engaged, the Vertical Speed
Bug can be adjusted in 100 fpm increments
by pressing the
NOSE UP/NOSE DN
keys to set
the desired vertical speed. The vertical speed
setting will be displayed in the Selected Vertical
Speed box above the VSI and in the Vertical
Speed Reference field in the AFCS Status Bar.
Figure 6-14 Vertical Speed Hold Mode
Vertical Speed
Reference Bug
Selected Vertical
Speed
Selected Altitude
Altitude Hold is Armed
Flight Director
command bars
indicating a climb
at the prescribed
vertical speed,
to the Selected
Altitude
Vertical Speed Reference
Vertical Speed mode is active
3. Vertical speed may also be changed by pressing
and holding the
CWS
button to manually estab-
lish the desired vertical speed using the control
wheel. When the
CWS
button is released, the
current vertical speed will be maintained. This
method must be used when using only the
flight director.
4. A desired altitude may be entered in the
Selected Altitude Box by turning the
ALT
knob. With Altitude Hold mode armed, as the
selected altitude is reached ‘ALT’ will flash in
green for 10 seconds in the Acitve Mode field,
after which the annunciation stops flashing.
This signals the altitude capture is complete
and the selected altitude will be maintained.
If only the flight director is engaged, pitch and
roll commands are given to manually maintain
the selected altitude.
If no altitude has been selected, Altitude Hold
will not become active and the current vertical
speed will be maintained.
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