This manual reflects the operation of System Software version 0435.11 or later for the Cessna
Citation Mustang. Some differences in operation may be observed when comparing the information
in this manual to earlier or later software versions.
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted,
disseminated, downloaded or stored in any storage medium, for any purpose without the express
written permission of Garmin. Garmin hereby grants permission to download a single copy of this
manual and of any revision to this manual onto a hard drive or other electronic storage medium to
be viewed for personal use, provided that such electronic or printed copy of this manual or revision
must contain the complete text of this copyright notice and provided further that any unauthorized
commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin® and G1000® are registered trademarks of Garmin Ltd. or its subsidiaries. WATCH®,
FliteCharts®, and SafeTaxi® are trademarks of Garmin Ltd. or its subsidiaries. These trademarks may
not be used without the express permission of Garmin.
NavData® is a registered trademark of Jeppesen, Inc.; XM® is a registered trademark of XM
Satellite Radio, Inc.
April, 2008 190-00600-02 Rev. A Printed in the U.S.A.
Warnings, Cautions & Notes
WARNING: The G1000 TAWS feature does not relieve the pilot from the
responsibility of being aware of surroundings during flight. The TAWS feature
is only to be used as an aid for terrain avoidance. Terrain data is obtained from
third party sources. Garmin is not able to independently verify the accuracy
of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory
in nature and should not be relied upon as the sole source of obstacle and
terrain avoidance information. Always refer to current aeronautical charts
for appropriate minimum clearance altitudes.
WARNING: The altitude calculated by G1000 GPS receivers is geometric
height above Mean Sea Level and could vary significantly from the altitude
displayed by pressure altimeters, such as the GDC 74B Air Data Computer,
or other altimeters in aircraft. GPS altitude should never be used for vertical
navigation. Always use pressure altitude displayed by the G1000 PFD or
other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in
the G1000 system must be updated regularly in order to ensure that the
information remains current. Pilots using any outdated database do so
entirely at their own risk.
WARNING: Do not use basemap (land and water data) information for
primary navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING: Traffic information shown on the G1000 Multi Function Display
is provided as an aid in visually acquiring traffic. Pilots must maneuver
the aircraft based only upon ATC guidance or positive visual acquisition of
conflicting traffic.
WARNING: XM Weather should not be used for hazardous weather
penetration. Weather information provided by the GDL 69A is approved only
for weather avoidance, not penetration.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-02 Rev. A
Warnings, Cautions & Notes
WARNING: NEXRAD weather data is to be used for long-range planning
purposes only. Due to inherent delays in data transmission and the relative
age of the data, NEXRAD weather data should not be used for short-range
weather avoidance.
WARNING: The Garmin G1000, as installed in the Cessna Citation Mustang
aircraft, has a very high degree of functional integrity. However, the pilot
must recognize that providing monitoring and/or self-test capability for all
conceivable system failures is not practical. Although unlikely, it may be
possible for erroneous operation to occur without a fault indication shown
by the G1000. It is thus the responsibility of the pilot to detect such an
occurrence by means of cross-checking with all redundant or correlated
information available in the cockpit.
WARNING: For safety reasons, G1000 operational procedures must be learned
on the ground.
WARNING: The United States government operates the Global Positioning
System and is solely responsible for its accuracy and maintenance. The GPS
system is subject to changes which could affect the accuracy and performance
of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a
precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs,
information presented by the G1000 can be misused or misinterpreted and,
therefore, become unsafe.
WARNING: To reduce the risk of unsafe operation, carefully review and
understand all aspects of the G1000 Pilot’s Guide documentation and the
Cessna Citation Mustang Airplane Flight Manual. Thoroughly practice basic
operation prior to actual use. During flight operations, carefully compare
indications from the G1000 to all available navigation sources, including
the information from other NAVAIDs, visual sightings, charts, etc. For safety
purposes, always resolve any discrepancies before continuing navigation.
WARNING: The illustrations in this guide are only examples. Never use
the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory
Circular, Subject: Thunderstorms, and the Aeronautical Information Manual
(AIM) recommend avoiding “by at least 20 miles any thunderstorm identified
as severe or giving an intense radar echo.”
190-00600-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Warnings, Cautions & Notes
WARNING: Lamp(s) inside this product may contain mercury (HG) and must
be recycled or disposed of according to local, state, or federal laws. For
more information, refer to our website at www.garmin.com/aboutGarmin/
environment/disposal.jsp.
WARNING: Because of anomalies in the earth’s magnetic field, operating
the G1000 within the following areas could result in loss of reliable attitude
and heading indications. North of 70° North latitude and south of 70° South
latitude. An area north of 65° North latitude between longitude 75º West
and 120º West. An area south of 55° South latitude between longitude 120º
East and 165º East.
CAUTION: The PFD and MFD displays use a lens coated with a special
anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive
cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTIREFLECTIVE COATING. It is very important to clean the lens using a clean,
lint-free cloth and an eyeglass lens cleaner that is specified as safe for antireflective coatings.
CAUTION: The Garmin G1000 does not contain any user-serviceable parts.
Repairs should only be made by an authorized Garmin service center.
Unauthorized repairs or modifications could void both the warranty and the
pilot’s authority to operate this device under FAA/FCC regulations.
NOTE: All visual depictions contained within this document, including screen
images of the G1000 panel and displays, are subject to change and may not
reflect the most current G1000 system and aviation databases. Depictions
of equipment may differ slightly from the actual equipment.
NOTE: This device complies with part 15 of the FCC Rules. Operation is
subject to the following two conditions: (1) this device may not cause harmful
interference, and (2) this device must accept any interference received,
including interference that may cause undesired operation.
NOTE: The data contained in the terrain and obstacle databases comes from
government agencies. Garmin accurately processes and cross-validates the
data, but cannot guarantee the accuracy and completeness of the data.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-02 Rev. A
Warnings, Cautions & Notes
NOTE: This product, its packaging, and its components contain chemicals
known to the State of California to cause cancer, birth defects, or reproductive
harm. This notice is being provided in accordance with California’s Proposition
65. If you have any questions or would like additional information, please
refer to our web site at www.garmin.com/prop65.
NOTE: Interference from GPS repeaters operating inside nearby hangars can
cause an intermittent loss of attitude and heading displays while the aircraft
is on the ground. Moving the aircraft more than 100 yards away from the
source of the interference should alleviate the condition.
NOTE: Use of polarized eyewear may cause the flight displays to appear dim
or blank.
190-00600-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Warnings, Cautions & Notes
Blank Page
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-02 Rev. A
Record of Revisions
Part NumberChange Summary
190-00600-00
Rev A
Initial release
Rev B
Added Additional Features section
190-00600-01
Rev A
Rev B
Rev C
Production release
Added CAS INOP system messages
Added COM 3 function for HF
Added TAS
Removed automatic Reversionary Mode operation
190-00600-02Added Synthetic Vision
Added other GDU 9.01 parameters
RevisionDate of RevisionAffected PagesDescription
AApril, 2008AllProduction release
190-00600-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
RR-1
Record of Revisions
Blank Page
RR-2
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
INDEX .........................................................................................................................................Index-1
190-00600-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
iii
Table of Contents
Blank Page
iv
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-02 Rev. A
Flight Instruments
FLIGHT INSTRUMENTS
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
Turn the BARO Knob to select the desired setting.
SELECTING STANDARD BAROMETRIC PRESSURE
Press the BARO Knob.
CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS
1)
Select the PFD Softkey to display the second-level softkeys.
2)
Select the ALT UNIT Softkey.
3)
Select the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Or
:
Select the HPA Softkey to display the barometric pressure setting in
hectopascals.
4)
Select the BACK Softkey to return to the top-level softkeys.
SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS
InstrumentsEICAS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
1)
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 BARO in the SYNCHRONIZATION
Window.
4)
Turn the
small
SYNCHRONIZE CDI
1)
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 CDI in SYNCHRONIZATION Window.
4)
Turn the
190-00600-02 Rev. A
small
FMS Knob clockwise to ON or counterclockwise to OFF.
FMS Knob clockwise to ON or counterclockwise to OFF.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Additional
Features
Operation
Abnormal
Annun/
AlertsAppendixIndex
1
Flight Instruments
CHANGE NAVIGATION SOURCES
Flight
InstrumentsEICAS
1)
Select the CDI Softkey to change from GPS to VOR1 or LOC1. This places
the light blue tuning box over the NAV1 standby frequency in the upper left
corner of the PFD.
2)
Select the CDI Softkey again to change from VOR1 or LOC1 to VOR2
or LOC2. This places the light blue tuning box over the NAV2 standby
Nav/Com/
XPDR/AudioAFCSGPS Nav
frequency.
3)
Select the CDI Softkey a third time to return to GPS.
ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS
1)
Select the OBS Softkey to select OBS Mode.
2)
Turn a CRS Knob to select the desired course to/from the waypoint. Press
the CRS Knob to synchronize the Selected Course with the bearing to the
next waypoint.
Flight
PlanningProcedures
3)
Select the OBS Softkey again to disable OBS Mode.
GENERIC TIMER
1)
Select the TMR/REF Softkey, then turn the large FMS Knob to select the
time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then
Hazard
Avoidance
Features
Additional
Abnormal
Operation
press the ENT Key. The UP/DOWN field is now highlighted.
2)
Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS
Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now
highlighted.
3)
Press the ENT Key to START, STOP, or RESET the timer (if the timer is
counting DOWN, it will start counting UP after reaching zero). Press the
CLR Key or the TMR/REF Softkey to remove the window.
CONFIGURE VSPEED BUGS INDIVIDUALLY
AlertsAppendixIndex
Annun/
1)
Select the TMR/REF Softkey.
2)
Turn the
3)
Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
large
FMS Knob to highlight the desired Vspeed.
speed has been changed from a default value, an asterisk appears next to
the speed).
2
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-02 Rev. A
Flight Instruments
4)
Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field
5)
Turn the
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
small
FMS Knob clockwise to ON or counterclockwise to OFF.
TURN VSPEED BUGS ON OR OFF BY CATEGORY
1)
Press the TMR/REF Softkey.
2)
Press the MENU Key.
3)
Turn the FMS Knob to highlight the desired option.
4)
Press the ENT Key. Press the TMR/REF Softkey to remove the window.
SET BAROMETRIC MINIMUM DESCENT ALTITUDE
1)
Select the TMR/REF Softkey.
2)
Turn the large FMS Knob to highlight the OFF/BARO field to the right of
‘MINIMUMS’.
3)
Turn the small FMS Knob clockwise to BARO.
4)
Press the ENT Key.
5)
Use the small FMS Knob to enter the desired altitude.
6)
Press the ENT Key.
7)
To remove the window, press the CLR Key or the TMR/REF Softkey.
InstrumentsEICAS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
DISPLAYING WIND DATA
1)
Select the PFD Softkey.
2)
Select the WIND Softkey to display wind data below the Selected Heading.
3)
Select one of the OPTN softkeys to change how wind data is displayed.
4)
To remove the Wind Data Window, select the OFF Softkey.
190-00600-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Operation
Abnormal
Annun/
AlertsAppendixIndex
3
Flight Instruments
Flight
InstrumentsEICAS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Blank Page
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
4
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-02 Rev. A
EICAS
ENGINE INDICATION & CREW ALERTING SYSTEM
InstrumentsEICAS
Flight
1
2
5
6
1
XPDR/AudioAFCSGPS Nav
Nav/Com/
5
7
3
PlanningProcedures
Flight
8
6
2
4
3
Avoidance
Hazard
Additional
Features
EICAS Display (Normal Mode)
1
Engine Fan Rotation
Speed
2
Oil Pressure & Speed
3
Fuel Display
4
CAS Display
190-00600-02 Rev. A
9
7
8
10
10
EIS Display (Reversionary Mode)
5
Interstage Turbine
Temperature
6
Engine High Pressure
8
Cabin Pressure Altitude
and Change Rate
9
Trim Indicator
Turbine Rotation
10
Speed
7
Electrical Display
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Flap Indicator
Operation
Abnormal
Annun/
AlertsAppendixIndex
5
EICAS
CREW ALERTING SYSTEM (CAS)
Flight
InstrumentsEICAS
NOTE: Refer to the Annunciations and Alerts section for specific CAS
messages.
NOTE: Refer to the Airplane Flight Manual (AFM) for emergency
procedures.
Nav/Com/
XPDR/AudioAFCSGPS Nav
NOTE: If there is a mismatch between databases or software on the PFDs,
CAS is inoperative.
When CAS messages are present while in reversionary mode, the CAS Window
appears on the display along with the flight instruments and EIS.
Flight
PlanningProcedures
CAS Display
CAS Window
Hazard
Avoidance
Features
Additional
CAS MESSAGES AND PRIORITIZATION
Abnormal
Operation
AlertsAppendixIndex
Annun/
NOTE: Information on CAS messages in this pilot’s guide is always superseded
• Caution (yellow) – Immediate crew awareness and possible future corrective
action required; Master Caution triggered
• Advisory (white) – Crew awareness required and subsequent action may be
required
6
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Reversionary ModeNormal Mode
CAS Messages
190-00600-02 Rev. A
NAV/COM/TRANSPONDER/AUDIO PANEL
ENTER OR CHANGE FLIGHT ID
1)
Press the TMR/REF Softkey, then turn the large FMS Knob to highlight the
Flight ID field.
2)
Turn the small FMS Knob to enter the first character.
3)
Turn the large FMS Knob to select the next field.
4)
Turn the small FMS Knob to enter the next desired character.
5)
Repeat steps 3 and 4 until the desired Flight ID is entered.
6)
Press the ENT Key. In the FLT ID field, ‘updating’ is momentarily displayed.
Do not perform any other G1000 functions until ‘updating’ is no longer
displayed.
ADF TUNING (OPTIONAL)
1)
Press the ADF/DME Softkey.
2)
Turn the small FMS Knob to enter the first digit of the desired ADF
frequency.
3)
Turn the large FMS Knob to select the next desired field.
4)
Turn the small FMS Knob to enter the desired number.
5)
Repeat steps 3 and 4 until the desired ADF frequency is entered.
6)
Press the ENT Key to accept the new frequency.
7)
Press the ENT Key again to transfer the frequency to the active field.
8)
Turn the large FMS Knob to select the MODE field.
9)
Turn the small FMS Knob to select ANT, ADF, ADF/BFO, or ANT/BFO.
10)
Press the ENT Key to complete the selection.
Nav/Com/XPDR/Audio Panel
InstrumentsEICAS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
AlertsAppendixIndex
DME TUNING
1)
Press the ADF/DME or DME Softkey.
2)
Turn the large FMS to select the DME source field.
3)
Turn the small FMS Knob to select the desired Nav radio.
4)
Press the ENT Key to complete the selection.
190-00600-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
7
Nav/Com/XPDR/Audio Panel
ENTER A TRANSPONDER CODE
Flight
InstrumentsEICAS
1)
Press the XPDR Softkey to display the transponder mode selection softkeys.
2)
Press the XPDR1 or XPDR2 Softkey to select the active transponder.
3)
Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
4)
Press the digit softkeys to enter the code in the code field. When entering
Nav/Com/
XPDR/AudioAFCSGPS Nav
the code, the next key in sequence must be pressed within 10 seconds, or
the entry is cancelled and restored to the previous code. Five seconds after
the fourth digit has been entered, the transponder code becomes active.
SELECTING A COM RADIO
Transmit/Receive
Press the COM1 MIC, COM2 MIC
Flight
PlanningProcedures
the audio panel.
Receive Only
Press the COM1, COM2
SELECTING A NAV RADIO
Hazard
Avoidance
1)
Press the CDI Softkey to select NAV1 (VOR1/LOC1) or NAV2 (VOR2/LOC2).
, or
COM3 MIC Key (HF, if installed) on
, or
COM3 Key (HF, if installed) on the audio panel.
2)
Pressing the NAV1, NAV2, DME, or ADF Key on the audio panel selects
Features
Additional
and deselects the navigation radio audio source. All radio keys can be
selected individually or together.
NAV/COM TUNING
Abnormal
Operation
1)
Press the small tuning knob to select the desired radio for tuning. A light
AlertsAppendixIndex
Annun/
blue box highlights the radio frequency to be tuned.
2)
Turn the respective tuning knobs to enter the desired frequency into the
standby frequency field. The large knob enters MHz and the small knob
enters kHz.
3)
Press the Frequency Transfer Key to place the frequency into the active
frequency field.
8
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-02 Rev. A
Nav/Com/XPDR/Audio Panel
INTERCOM SYSTEM (ICS) ISOLATION
Press the PILOT and/or COPLT Key on either audio panel to select those isolated
from hearing the Nav/Com radios and music.
Copilot
Side
Passenger
Hears
Selected
Radios,
Aural
Alerts, Pilot,
Copilot,
Passengers,
Music
Selected
Radios,
Aural Alerts,
Copilot,
Passengers,
Music
Passengers,
Pilot, Music
Passengers,
Music
PILOT Key
Annunciator
OFFOFF
ONOFF
OFFON
ONON
COPLT Key
Annunciator
Pilot Hears
Selected
Radios, Aural
Alerts, Pilot,
Copilot,
Passengers,
Music
Selected
Radios, Aural
Alerts, Pilot
Selected
Radios, Aural
Alerts, Pilot,
Passengers,
Music
Selected
Radios, Aural
Alerts, Pilot,
Copilot
Copilot
Hears
Selected
Radios,
Aural
Alerts, Pilot,
Copilot,
Passengers,
Music
Selected
Radios,
Aural Alerts,
Copilot,
Passengers,
Music
Selected
radios,
Aural Alerts,
Copilot
Selected
Radios,
Aural
Alerts, Pilot,
Copilot
Pilot Side
Passenger
Hears
Selected
Radios,
Aural
Alerts, Pilot,
Copilot,
Passengers,
Music
Copilot,
Passengers,
Music
Selected
Radios,
Aural
Alerts, Pilot,
Passengers,
Music
Passengers,
Music
InstrumentsEICAS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
AlertsAppendixIndex
190-00600-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
9
Nav/Com/XPDR/Audio Panel
DIGITAL CLEARANCE RECORDER AND PLAYER
Flight
InstrumentsEICAS
NOTE: Only the audio for the selected
not recorded for COM3 MIC.
Record
1)
Nav/Com/
XPDR/AudioAFCSGPS Nav
Press the REC Key to begin recording.
2)
Press the REC Key again to stop recording.
Play
1)
Press the PLAY Key once to play the latest recorded memory block.
2)
Press the PLAY Key once while playing to stop.
3)
Press the PLAY Key twice quickly while playing to begin playing the
Flight
previously recorded block.
PlanningProcedures
the previously recorded block.
Each subsequent two presses will skip back to
COM MIC
Key is recorded. Audio is
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
10
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-02 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
NOTE: If sensor information (other than attitude) required for a flight director
mode becomes invalid or unavailable, the flight director automatically reverts
to the default mode for that axis.
NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.
FLIGHT DIRECTOR ACTIVATION
An initial press of a key listed in the following table (when the flight director is not
active) activates the pilot-side flight director in the listed modes.
AFCS
InstrumentsEICAS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
Control Pressed
Modes Selected
LateralVertical
FD KeyRoll Hold (default)ROLPitch Hold (default)PIT
AP KeyRoll Hold (default)ROLPitch Hold (default)PIT
CWS ButtonRoll Hold (default)ROLPitch Hold (default)PIT
GA SwitchGo AroundGAGo AroundGA
A LT KeyRoll Hold (default)ROLAltitude HoldA LT
VS KeyRoll Hold (default)ROLVertical SpeedVS
VNV KeyRoll Hold (default)ROLVertical Path Tracking*VPTH
GPS
NAV KeyNavigation**
VOR
Pitch Hold (default)PIT
LOC
BC KeyBackcourse***BCPitch Hold (default)PIT
APR KeyApproach**
GPS
VOR
LOC
Pitch Hold (default)
Glidepath
Glideslope
PIT
GP
GS
HDG KeyHeading SelectHDGPitch Hold (default)PIT
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
**The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before
NAV
or
APR
Key press activates flight director.
***The selected navigation receiver must have a valid LOC signal before BC Key press activates flight
director.
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
AlertsAppendixIndex
190-00600-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
11
AFCS
VERTICAL MODES
Flight
InstrumentsEICAS
Vertical ModeDescriptionControlAnnunciation
Holds the current aircraft pitch attitude;
Pitch Hold
Nav/Com/
XPDR/AudioAFCSGPS Nav
Selected Altitude
Armed
Altitude HoldHolds the current Altitude ReferenceA LT KeyA LTnnnnn f T
Vertical Speed
Flight Level Change,
Flight
IAS Hold
PlanningProcedures
Flight Level Change,
Mach Hold
VNAV
Hazard
Avoidance
VNAV Target
Altitude Armed
Features
Additional
Glidepath
Glideslope
Abnormal
Operation
Go Around
AlertsAppendixIndex
Annun/
* ALTS armed automatically when PIT, VS, FLC, or GA active, and under VPTH when Selected Altitude
is to be captured instead of VNAV Target Altitude
** ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of
Selected Altitude
may be used to climb/descend to the
Selected Altitude
AFCS armed to capture the altitude
displayed in the Selected Altitude
window
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 the VNAV flight
path
AFCS armed to capture the altitude
displayed in the VNAV Target Altitude
window
Captures and tracks the WAAS
glidepath on approach
Captures and tracks the ILS glideslope
on approach
Disengages the autopilot and
commands a constant pitch attitude
and wings level
(default)PIT
*ALTS
VS KeyVSnnnn f p m
FLCnnn k T
FLC Key
FLCM .nnn
VNV
Key
**ALTV
APR Key
GA
Switch
VPTH
GP
GS
GA
12
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-02 Rev. A
AFCS
LATERAL MODES
InstrumentsEICAS
Flight
Lateral ModeDescriptionControlAnnunciation
Holds current aircraft roll attitude
Roll Hold
Low BankLimits maximum commanded roll angle
Heading SelectCaptures and tracks Selected Heading
Navigation, GPS
Arm/Capture/Track
or rolls wings level, depending on
commanded bank angle
(default)ROL
BANK
Key
HDG
Key
*
HDG
GPS
XPDR/AudioAFCSGPS Nav
Nav/Com/
Navigation, VOR
Enroute Arm/
Capture/Track
Captures and tracks selected navigation
source (GPS, VOR, LOC)