Vertical Modes - Garmin G1000:Beechcraft Baron 58/G58 User Manual

Garmin g1000: user guide
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7.3 VERTICAL MODES

Table 7-2 lists the vertical modes with their corresponding controls and annunciations. The mode reference is
displayed next to the active mode annunciation for Altitude Hold, Vertical Speed, and Flight Level Change modes.
The NOSE UP/DN Wheel can be used to change the vertical mode reference while operating under Pitch Hold,
Vertical Speed, or Flight Level Change Mode. Increments of change and acceptable ranges of values for each of
these references using the NOSE UP/DN Wheel are also listed in the table.
Vertical Mode
Pitch Hold
Selected Altitude Capture
Altitude Hold
Vertical Speed
Flight Level Change, IAS Hold
Flight Level Change, Mach Hold
Vertical Path Tracking
VNV Target Altitude Capture
Glidepath
Glideslope
Takeoff
Go Around
* ALTS armed automatically when PIT, VS, FLC, TO, or GA active, and under VPTH when Selected Altitude is to be captured
instead of VNV Target Altitude
** ALTV armed automatically under VPTH when VNV Target Altitude is to be captured instead of Selected Altitude
7-8
Description
Holds the current aircraft pitch
attitude; may be used to climb/
descend to the Selected Altitude
Captures the Selected Altitude
Holds the current Altitude Reference ALT Key ALT nnnnn
Maintains the current aircraft vertical
speed; may be used to climb/descend
to the Selected Altitude
Maintains the current aircraft
airspeed (in IAS or Mach) while the
aircraft is climbing/descending to the
Selected Altitude
Captures and tracks descent legs of
an active vertical profile
Captures the Vertical Navigation
(VNV) Target Altitude
Captures and tracks the WAAS
glidepath on approach
Captures and tracks the ILS glideslope
on approach
Disengages the autopilot and
commands a constant pitch angle
and wings level on the ground in
preparation for takeoff
Disengages the autopilot and
commands a constant pitch angle
and wings level in the air
Table 7-2 Flight Director Vertical Modes
Garmin G1000 Pilot's Guide for the Hawker Beechcraft C90A/GT
Reference
Control Annunciation
(default)
PIT
*
ALTS
FT
VS Key
VS nnnn
FPM
+4000 fpm
FLC
nnn
KT
FLC Key
M 0.25 to
FLC
M .nnn
VNV
VPTH
Key
**
ALTV
GP
APR
Key
GS
TO
GA
Switch
GA
Reference
Change
Range
Increment
-15° to
0.5°
+20°
-4000 to
100 fpm
100 to
1 kt
226 kt
M 0.01
0.46
8.6°
190-00663-00 Rev. A

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