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Figure 7-4 Flight Director Selection IndicationsPilot-side Flight Director SelectedCopilot-side Flight Director Selected
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 369
Automatic utomatic utomatic Flight Control System ystem
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
Command BarsBars
Upon activation of the flight director, Command Bars are displayed in magenta on the PFDs as single cues or cross pointers. The Aircraft Symbol (in yellow) changes to accommodate the Command Bar format; the Command Bars do not override the Aircraft Symbol. The single-cue Command Bars (Figure 7-5) move together vertically to indicate pitch commands and bank left or right to indicate roll commands. Command Bars displayed as a cross pointer (Figure 7-6) move independently to indicate pitch (horizontal bar) and roll (vertical bar) commands. Both PFDs show the same Command Bar format. Noteote: The split-cue aircraft symbol and cross pointer command bars are not available when SVS is installed.
Aircraft
SymbolCommand BarsFigure 7-6 Cross-pointer Command BarsFigure 7-5 Single-cue Command BarsAircraft SymbolCommand Bars
Changing Command Bar format:
1) Use the FMS Knob to select the AUX - System Setup Page on the MFD.
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight ‘Format Active’ in the ‘Flight Director’ box.
4) Turn the small FMS Knob to highlight the desired format.
’SNGL CUE’ to display Command Bars as a single cue (Aircraft Symbol in figure 7-5).
Or:
’X-POINTER’ to display Command Bars as a cross pointer (Aircraft Symbol in Figure 7-6).
If the attitude information being sent to the flight director becomes invalid or unavailable, the Command Bars are removed from the display. The flight director Command Bars also disappear if the pitch exceeds +30˚/-20˚ or bank exceeds 65˚.
370 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Automatic utomatic utomatic Flight Control System ystem
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
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
Description
Control
Annunciation
Reference Range
Reference Change Increment
Pitch Hold
Holds the current aircraft pitch attitude; may be used to climb/descend to the Selected Altitude
(default)
PIT
-20° to +20°
0.5°
Selected Altitude Capture
Captures the Selected Altitude
*
ALTS
Altitude Hold
Holds the current Altitude Reference
ALT Key
ALT
nnnnn ft
Vertical Speed
Maintains the current aircraft vertical speed; may be used to climb/descend to the Selected Altitude
VS Key
VS
nnnn fpm
-5000 to +5000 fpm
100 fpm
Flight Level Change, IAS Hold
Maintains the current aircraft airspeed (in IAS or Mach) while the aircraft is climbing/descending to the Selected Altitude
FLC Key
FLC
nnn kt
80 to
250 kt
1 kt
Flight Level Change, Mach Hold
FLC
M .nnn
M 0.40 to 0.63
M 0.01
Vertical Path Tracking
Captures and tracks descent legs of an active vertical profile
VNV Key
VPTH
VNV Target Altitude Capture
Captures the Vertical Navigation (VNV) Target Altitude
**
ALTV
Glidepath
Captures and tracks the WAAS glidepath on approach
APR Key
GP
Glideslope
Captures and tracks the ILS glideslope on approach
GS
Takeoff
Commands a constant pitch angle and wings level on the ground in preparation for takeoff
GA Switch
TO
10°
Go Around
Disengages the autopilot and commands a constant pitch angle and wings level in the air
GA
8°
* 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
　
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