Garmin G1000 User Manual

®

G1000

Cockpit Reference Guide for the Cessna Citation Mustang

Integrated Flight Deck

FLIGHT INSTRUMENTS

EICAS

NAV/COM/TRANSPONDER/AUDIO PANEL

AUTOMATIC FLIGHT CONTROL SYSTEM

GPS NAVIGATION

FLIGHT PLANNING

PROCEDURES

HAZARD AVOIDANCE

ADDITIONAL FEATURES

ABNORMAL OPERATION

ANNUNCIATIONS & ALERTS

APPENDIX

INDEX

Copyright © 2006-2008 Garmin Ltd. or its subsidiaries. All rights reserved.

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.

Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.
Tel: [phone] Fax: [phone]

Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: [phone] Fax [phone]

Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park,
Southampton, SO40 9RB, U.K.
Tel: [phone] Fax: [phone]

Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: [phone] Fax: [phone]

Web Site Address: www.garmin.com

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

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Record of Revisions

Part Number Change 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

190-00600-02 Added Synthetic Vision

Added other GDU 9.01 parameters

Revision Date of Revision Affected Pages Description

A April, 2008 All Production release

190-00600-02 Rev. A

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RR-1

Record of Revisions

Blank Page

RR-2

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Table of Contents

FLIGHT INSTRUMENTS ................................................................................................................ 1

Selecting the Altimeter Barometric Pressure Setting ...................................................... 1

Selecting Standard Barometric Pressure .............................................................................1

Change Altimeter Barometric Pressure Setting Units ...................................................... 1

Synchronizing the Altimeter Barometric Pressure Settings ........................................... 1

Synchronize CDI......................................................................................................................... 1

Change Navigation Sources ................................................................................................... 2

Enable/Disable OBS Mode While Navigating with GPS .................................................... 2

Generic Timer ............................................................................................................................. 2

Configure Vspeed Bugs Individually ..................................................................................... 2

Turn Vspeed Bugs On or Off by Category ............................................................................ 3

Set Barometric Minimum Descent Altitude ........................................................................ 3

Displaying Wind Data ..............................................................................................................3

ENGINE INDICATION & CREW ALERTING SYSTEM .......................................................5

Crew Alerting System (CAS) ................................................................................................... 6

CAS Messages and Prioritization .......................................................................................... 6

NAV/COM/TRANSPONDER/AUDIO PANEL ......................................................................... 7

Enter or Change Flight ID ....................................................................................................... 7

ADF Tuning (Optional) .............................................................................................................. 7

DME Tuning................................................................................................................................. 7

Enter a Transponder Code....................................................................................................... 8

Selecting a COM Radio ............................................................................................................ 8

Selecting a NAV Radio ............................................................................................................. 8

NAV/COM Tuning ....................................................................................................................... 8

Intercom System (ICS) Isolation ............................................................................................ 9

Digital Clearance Recorder and Player .............................................................................. 10

AUTOMATIC FLIGHT CONTROL SYSTEM .......................................................................... 11

Flight Director Activation ..................................................................................................... 11

Vertical Modes ......................................................................................................................... 12

Lateral Modes .......................................................................................................................... 13

GPS NAVIGATION ........................................................................................................................ 15

Direct-to Navigation .............................................................................................................. 15

Activate a Stored Flight Plan ............................................................................................... 16

Activate a Flight Plan Leg ..................................................................................................... 16

Stop Navigating a Flight Plan .............................................................................................. 17

Vertical Navigation (VNAV)................................................................................................... 17

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Table of Contents

FLIGHT PLANNING ...................................................................................................................... 19

Weight Planning ...................................................................................................................... 19

Trip Planning ............................................................................................................................ 19

Create a New User Waypoint ............................................................................................... 21

Delete a User Waypoint ......................................................................................................... 22

Create a New Flight Plan ...................................................................................................... 22

Insert a Waypoint in the Active Flight Plan ...................................................................... 24

Enter an Airway in a Flight Plan .......................................................................................... 24

Invert An Active Flight Plan .................................................................................................. 25

Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 25

Store a Flight Plan .................................................................................................................. 26

Edit a Stored Flight Plan ....................................................................................................... 26

Delete a Waypoint from the Flight Plan ............................................................................ 26

Invert and Activate a Stored Flight Plan ........................................................................... 27

Copy a Flight Plan ................................................................................................................... 27

Delete a Flight Plan ................................................................................................................ 27

Graphical Flight Plan Creation ............................................................................................. 28

PROCEDURES ................................................................................................................................. 29

Load and Activate a Departure Procedure ....................................................................... 29

Activate A Departure Leg ..................................................................................................... 29

Load An Arrival Procedure .................................................................................................... 29

Activate An Arrival Leg ......................................................................................................... 30

Load and/or Activate an Approach Procedure ................................................................. 30

Activate An Approach in the Active Flight Plan ............................................................... 31

Activate a Vector to Final Approach Fix ............................................................................ 31

Activate A Missed Approach in the Active Flight Plan ................................................... 32

HAZARD AVOIDANCE ................................................................................................................33

Customizing the Hazard Displays on the Navigation Map ............................................ 33

XM Weather (Optional) .......................................................................................................... 33

Traffic Systems ........................................................................................................................ 34

Terrain Awareness & Warning System (TAWS) Display ................................................... 37

Airborne Color Weather Radar ............................................................................................ 39

ADDITIONAL FEATURES ........................................................................................................... 43

Synthetic Vision ....................................................................................................................... 43

Terminal Procedure Charts ...................................................................................................44

XM® Radio Entertainment..................................................................................................... 46

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Table of Contents

ABNORMAL OPERATION..........................................................................................................49

Reversionary Mode ................................................................................................................ 49

Abnormal COM Operation .................................................................................................... 49

Hazard Displays with Loss of GPS Position ....................................................................... 49

Unusual Attitudes ................................................................................................................... 50

Dead Reckoning ...................................................................................................................... 51

ANNUNCIATIONS & ALERTS ................................................................................................... 53

CAS Messages .......................................................................................................................... 53

Comparator Annunciations ................................................................................................... 55

Reversionary Sensor Annunciations ................................................................................... 55

AFCS Alerts ............................................................................................................................... 56

TAWS Alerts .............................................................................................................................. 57

Message Advisory Alerts ....................................................................................................... 59

Aural Alerts .............................................................................................................................. 59

MFD & PFD Message Advisories .......................................................................................... 59

Database Message Advisories ............................................................................................. 61

GMA 1347D Message Advisories ......................................................................................... 64

GIA 63W Message Advisories ............................................................................................... 65

GEA 71 Message Advisories .................................................................................................. 68

GTX 33 Message Advisories .................................................................................................. 68

GRS 77 Message Advisories .................................................................................................. 69

GMU 44 Message Advisories ................................................................................................ 70

GDL 69A Message Advisories ............................................................................................... 71

GWX 68 Alert Messages ......................................................................................................... 71

GDC 74B Message Advisories ............................................................................................... 72

GCU 475 Message Advisories ............................................................................................... 72

GMC 710 Message Advisories .............................................................................................. 73

Miscellaneous Message Advisories ..................................................................................... 73

APPENDIX ....................................................................................................................................... 77

PFD Softkey Map .................................................................................................................... 77

MFD Softkey Map ................................................................................................................... 82

INDEX .........................................................................................................................................Index-1

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Table of Contents

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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

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

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/

Alerts Appendix Index

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.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

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/

Alerts Appendix Index

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

Instruments EICAS

Flight

1

2

5

6

1

XPDR/Audio AFCS GPS Nav

Nav/Com/

5

7

3

Planning Procedures

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/

Alerts Appendix Index

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

by the AFM.

• Warning (red) – Immediate crew awareness and action required; Master
Warning triggered

• 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

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

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

OFF OFF

ON OFF

OFF ON

ON ON

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

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

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

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Control Pressed

Modes Selected

Lateral Vertical
FD Key Roll Hold (default) ROL Pitch Hold (default) PIT
AP Key Roll Hold (default) ROL Pitch Hold (default) PIT

CWS Button Roll Hold (default) ROL Pitch Hold (default) PIT

GA Switch Go Around GA Go Around GA

A LT Key Roll Hold (default) ROL Altitude Hold A LT

VS Key Roll Hold (default) ROL Vertical Speed VS

VNV Key Roll Hold (default) ROL Vertical Path Tracking* VPTH

GPS

NAV Key Navigation**

VOR

Pitch Hold (default) PIT

LOC

BC Key Backcourse*** BC Pitch Hold (default) PIT

APR Key Approach**

GPS
VOR
LOC

Pitch Hold (default)

Glidepath

Glideslope

PIT
GP
GS

HDG Key Heading Select HDG Pitch 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.

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

11

AFCS

VERTICAL MODES

Flight

InstrumentsEICAS

Vertical Mode Description Control Annunciation

Holds the current aircraft pitch attitude;

Pitch Hold

Nav/Com/

XPDR/AudioAFCSGPS Nav

Selected Altitude
Armed

Altitude Hold Holds the current Altitude Reference A LT Key A LT nnnnn 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 Key VS nnnn f p m

FLC nnn k T

FLC Key

FLC M .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

Instruments EICAS

Flight

Lateral Mode Description Control Annunciation

Holds current aircraft roll attitude

Roll Hold

Low Bank Limits maximum commanded roll angle

Heading Select Captures 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/Audio AFCS GPS Nav

Nav/Com/

Navigation, VOR
Enroute Arm/
Capture/Track

Captures and tracks selected navigation
source (GPS, VOR, LOC)

NAV

Key

VOR

Planning Procedures

Flight

Navigation, LOC
Arm/Capture/Track

LOC

(No Glideslope)
Backcourse Arm/

Capture/Track
Approach, GPS

Arm/Capture/Track
Approach, VOR

Arm/Capture/Track
Approach, ILS Arm/

Capture/Track
(Glideslope Mode
automatically armed)

Go Around

* No annunciation appears in the AFCS Status Box. The acceptable bank angle range is indicated in

green along the Roll Scale of the Attitude Indicator.

Captures and tracks a localizer signal
for backcourse approaches

Captures and tracks selected navigation
source (GPS, VOR, LOC)

Disengages autopilot and commands a
constant pitch angle and wings level

BC Key BC

VAPP

APR Key

GA

Switch

GPS

LOC

GA

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

13

Flight

InstrumentsEICAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

AFCS

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

14

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

GPS NAVIGATION

DIRECT-TO NAVIGATION

Direct-to Navigation using the MFD

1)

Press the Direct-to

2)

Enter the waypoint identifier.

3)

Press the ENT Key to confirm the identifier. The ‘Activate?’ field is
highlighted.

4)

If no altitude constraint or course is desired, press the ENT Key to activate.
To enter an altitude constraint, proceed to step 5.

5)

Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.

6)

Enter the desired altitude.

7)

Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 9.

8)

Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.

9)

Press the ENT Key. The cursor is now flashing in the VNV offset distance
field.

10)

Enter the desired offset distance before (-) the waypoint.

11)

Press the ENT Key. The ‘Activate?’ field is highlighted.

12)

Press the ENT Key to activate.

( )

Key on the MFD Control Unit.

GPS Navigation

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Direct-to Navigation using the PFD

1)

Press the Direct-to Key

2)

Turn the large FMS Knob to place the cursor in the desired selection field.

3)

Turn the small FMS Knob to begin selecting the desired identifier, location,
etc.

4)

Press the ENT Key.

5)

The cursor is now flashing on ‘ACTIVATE?’. If no altitude constraint or
course is desired, press the ENT Key to activate. To enter an altitude
constraint, proceed to step 6.

6)

Turn the large FMS Knob to place the cursor over the ‘ALT’ altitude field.

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

( )

on the PFD or controller.

15

Operation

Abnormal

Annun/

Alerts Appendix Index

GPS Navigation

7)

Turn the small FMS Knob to enter the desired altitude.

8)

Flight

InstrumentsEICAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

ACTIVATE A STORED FLIGHT PLAN

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 10.

9)

Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.

10)

Press the ENT Key. The cursor is placed in the ‘OFFSET’ field.

11)

Turn the small FMS Knob to enter the desired target altitude offset from

the selected Direct-to.

12)

Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to

highlight the ‘CRS’ field.

13)

Turn the small FMS Knob to enter the desired course to the waypoint.

14)

Press the ENT Key to highlight ‘ACTIVATE?’.

15)

Press the ENT Key again to activate the Direct-to.

1)

Press the FPL Key and turn the small FMS Knob to display the Flight Plan
Catalog Page.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight the desired flight plan

4)

Select the ACTIVE Softkey. The confirmation window is now displayed.

5)

With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel
the flight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and
press the ENT Key.

ACTIVATE A FLIGHT PLAN LEG

Abnormal

Operation

1)

From the Active Flight Plan Page, press the FMS Knob to activate the cursor

AlertsAppendixIndex

Annun/

and turn the large FMS Knob to highlight the desired waypoint.

2)

Select the ACT LEG Softkey.

OR

Press the MENU Key, select the ‘Activate Leg’ option from the page menu
and press the ENT Key. This step must be used when activating a leg from

the PFD.

3)

With ‘Activate’ highlighted, press the ENT Key.

16

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

GPS Navigation

STOP NAVIGATING A FLIGHT PLAN

1)

Press the FPL Key to display the Active Flight Plan Page.

2)

Press the MENU Key to display the Page Menu Window.

3)

Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT
Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan.
This will not delete the stored flight plan, only the active flight plan.

VERTICAL NAVIGATION (VNAV)

The navigation database only contains altitudes for procedures that call for “Cross
at” altitudes. If the procedure states “Expect to cross at,” the altitude is not in the
database. In this case the altitude may be entered manually.

Large White

Text

Large Light

Blue Text

Small Light

Blue Text

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

190-00600-02 Rev. A

Small Light

Blue Subdued

Text

Small White Text

with Altitude

Restriction Bar

Cross AT or ABOVE 5,000 ft

Cross AT 2,300 ft

Cross AT or BELOW 3,000 ft

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

17

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

GPS Navigation

Altitudes associated with arrival and approach procedures are “auto-designated”.

This means the system will automatically use the altitudes loaded with the arrival

Flight

InstrumentsEICAS

or approach for giving vertical flight path guidance outside the FAF. Note that these
altitudes will be displayed as small light blue text.

Altitudes that have been designated for use in vertical navigation may also be
made “non-designated” by placing the cursor over the desired altitude and pressing
the CLR Key. The altitude is now displayed only as a reference. It will not be used
to give vertical flight path guidance. Other displayed altitudes may change due to

Nav/Com/

XPDR/AudioAFCSGPS Nav

re-calculations or rendered invalid as a result of manually changing an altitude to a
non-designated altitude.

White Text Light Blue Text Light Blue

Subdued Text

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

Large Text

Small Text

Altitude calculated by
the system estimating
the altitude of the
aircraft as it passes
over the navigation
point. This altitude
is provided as a
reference and is not
designated to be used
in determining vertical
flight path guidance.

Altitude is not
designated to be used
in determining vertical
flight path guidance.
Altitude has been
retrieved from the
navigation database
and is provided as a
reference.

Altitude has been
entered by the pilot.
Altitude is designated
for use in giving
vertical flight path
guidance. Altitude
does not match the
published altitude in
navigation database or
no published altitude
exists.

Altitude is designated
for use in giving vertical
flight path guidance.
Altitude has been
retrieved from the
navigation database
or has been entered by
the pilot and matches
a published altitude
in the navigation
database.

The system cannot
use this altitude in
determining vertical
flight path guidance.

The system cannot
use this altitude in
determining vertical
flight path guidance.

18

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

FLIGHT PLANNING

WEIGHT PLANNING

All procedures apply to the MFD unless otherwise stated.

Flight Planning

Instruments EICAS

Flight

Entering Weight Parameters

The Weight Planning Page is displayed after system power-up. If it is necessary to
return to this page, turn the large
small

FMS

Knob to select the first rectangular page icon.

1)

Select the EMPTY WT Softkey to place the cursor in the Basic Empty

FMS

Knob to select the ‘AUX’ page group. Turn the

Weight field.

2)

Enter the desired aircraft empty weight.

3)

Press the ENT Key. The cursor is now over the ‘PILOT & STORES’ field.

4)

Enter the desired weight of Pilot & Stores.

5)

Press the ENT Key.

6)

Continue repeating these steps until all desired weights have been entered.

Entering Fuel Parameters

1)

If necessary, press the FMS Knob to activate the cursor.

2)

Turn the large FMS Knob to place the cursor in the ‘FUEL ON BOARD’ field.

3)

Select the FOB SYNC Softkey to enter the fuel on board quantity as read
from the aircraft fuel quantity sensors.

Or:

Manually enter the desired fuel quantity.

4)

Press the ENT Key. The cursor is now in the ‘FUEL RESERVES’ field.

5)

Enter the desired reserve fuel quantity.

6)

Press the FMS Knob to remove the cursor.

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

TRIP PLANNING

1)

Turn the large FMS Knob to select the ‘AUX’ page group.

2)

Turn the small FMS Knob to select the second rectangular page icon.

3)

The current ‘PAGE MODE’ is displayed at the top of the page: ‘AUTOMATIC’
or ‘MANUAL’. To change the page mode, select the AUTO or MANUAL
Softkey.

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

19

Flight Planning

4)

For Direct-to planning:

Flight

InstrumentsEICAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

a)

b)

c)

d)

Or:

For point-to-point planning:

a)

b)

c)

d)

Or:

For flight plan leg planning:

a)

b)

c)

d)

Select the WPTS Softkey and verify that the starting waypoint field
indicates ‘P.POS’ (present position).

If necessary, press the MENU Key and select ‘Set WPT to Present
Position’ to display ‘P.POS’.

Press the ENT Key and the flashing cursor moves to the ending
waypoint field.

Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.

Enter the identifier of the starting waypoint.

Once the waypoint’s identifier is entered, press the ENT Key to accept
the waypoint. The flashing cursor moves to the ending waypoint.

Again, enter the identifier of the ending waypoint.

Press the ENT Key to accept the waypoint.

Select the FPL Softkey (at the bottom of the display).

Turn the small FMS Knob to select the desired flight plan (already
stored in memory), by number.

Turn the large FMS Knob to highlight the ‘LEG’ field.

Turn the small FMS Knob to select the desired leg of the flight plan, or
select ‘CUM’ to apply trip planning calculations to the entire flight plan.
Selecting ‘FPL 00’ displays the active flight plan. If an active flight plan
is selected, ‘REM’ will be an available option to display planning data
for the remainder of the flight plan.

NOTE: The page mode must be set to ‘MANUAL’ to perform the following
steps.

20

5)

Turn the large FMS Knob to highlight the departure time (DEP TIME) field.

NOTE: The departure time on the Trip Planning Page is used for preflight

planning. Refer to the Utility Page for the actual flight departure time.

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Flight Planning

6)

Enter the departure time. Press the ENT Key when finished. Departure time
may be entered in local or UTC time, depending upon system settings.

7)

Enter the fuel flow. Press the ENT Key when finished. Note that in ‘AUTOMATIC’
page mode, fuel flow is provided by the system.

8)

The flashing cursor moves to the fuel onboard field. Modify the fuel onboard.
Press the ENT Key when finished. In ‘AUTOMATIC’ mode, fuel onboard is
provided by the entry made on the Weight Planning Page.

9)

The flashing cursor moves to the calibrated airspeed field. Enter a calibrated
airspeed. Press the ENT Key when finished.

CREATE A NEW USER WAYPOINT

1)

Turn the large FMS Knob to select the ‘WPT’ page group.

2)

Turn the small FMS Knob to select the User WPT Information Page.

3)

Select the NEW Softkey. A waypoint is created at the current aircraft
position.

4)

Enter the desired waypoint name.

5)

Press the ENT Key.

6)

The cursor is now in the ‘REFERENCE WAYPOINTS’ field. If desired, the
waypoint can be defined by a reference waypoint. Use one of the following
methods to enter the reference waypoint:

a)

Turn the small FMS Knob to the left to display a list of flight plan
waypoints. This list is populated only when there is an active flight
plan.

b)

Turn the large FMS Knob to select the desired waypoint.

c)

Press the ENT Key.

Or:

a)

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.

b)

Turn the small FMS Knob to the right to display the ‘NRST’ waypoints
to the aircraft’s current position.

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

Or:

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

21

Flight Planning

a)

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list

Flight

InstrumentsEICAS

7)

Nav/Com/

XPDR/AudioAFCSGPS Nav

8)

9)

10)

11)

Flight

PlanningProcedures

DELETE A USER WAYPOINT

1)

2)

3)

Hazard

Avoidance

4)

5)

Features

Additional

6)

7)

Abnormal

Operation

is displayed.

b)

Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

After pressing the ENT Key, the cursor is displayed in the ‘RAD’ (radial)
field. Enter the desired radial from the reference waypoint.

Press the ENT Key.

The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.

Press the ENT Key. The cursor is now placed for entering another reference

waypoint, if desired.

Press the FMS Knob to remove the flashing cursor.

Turn the large FMS Knob to select the ‘WPT’ page group.

Turn the small FMS Knob to select the User WPT Information Page.

Press the FMS Knob to activate the cursor.

Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’
field.

Turn the small FMS Knob to highlight the desired waypoint.

Select the DELETE Softkey.

The message ‘Would you like to delete the user waypoint?’ is displayed. With
‘YES’ highlighted, press the ENT Key.

CREATE A NEW FLIGHT PLAN

AlertsAppendixIndex

Annun/

NOTE: When creating a new flight plan in the Active Flight Plan Window,

the first leg is activated automatically after it is created.

22

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Flight Planning

Using the MFD

1)

Press the FPL Key.

2)

Turn the small FMS Knob to display the Flight Plan Catalog Page.

3)

Select the NEW Softkey to display a blank flight plan for the first empty storage
location.

4)

Turn the small FMS Knob to display the Waypoint Information Window.

5)

Enter the identifier of the departure waypoint.

6)

Press the ENT Key.

7)

Repeat step number 4, 5, and 6 to enter the identifier for each additional
flight plan waypoint.

8)

When all waypoints have been entered, press the FMS Knob to return to the
Flight Plan Catalog Page. The new flight plan is now in the list.

Using the PFD

NOTE: If a flight plan is active, an additional flight plan cannot be entered

using the PFD.

1)

Press the FPL Key.

2)

Turn the small FMS Knob to display the Waypoint Information Page.

3)

Turn the small FMS Knob to enter the first letter of the destination waypoint
identifier.

4)

Turn the large FMS Knob to the right to move the cursor to the next character
position.

5)

Repeat step 3 and 4 to spell out the rest of the waypoint identifier.

6)

Press the ENT Key and the cursor is now ready for entering of the next flight
plan waypoint.

7)

Repeat steps 3 through 6 to enter the identifier for each additional flight plan
waypoint.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

8)

Once all waypoints have been entered, press the FMS Knob to remove the
cursor. The new flight plan is now active.

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

23

Flight Planning

INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN

Flight

InstrumentsEICAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

1)

Press the FPL Key to display the active flight plan.

2)

If necessary, press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight the desired flight plan waypoint. The
new waypoint is inserted before the highlighted waypoint.

4)

Turn the small FMS Knob. The Waypoint Information Window is now
displayed.

5)

Enter the new flight plan waypoint by one of the following:

a)

Enter the user waypoint identifier, facility, or city.

b)

Press the ENT Key.

Or:

a)

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.

b)

Turn the small FMS Knob to the right to display the ‘NRST’ airport
waypoints to the aircraft’s current position.

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

Or:

a)

Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.

b)

Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

e)

Press the ENT Key again to “accept” the waypoint.

ENTER AN AIRWAY IN A FLIGHT PLAN

AlertsAppendixIndex

Annun/

1)

Press the FPL Key.

2)

Press the FMS Knob to activate the cursor (not required on the PFD).

3)

Turn the large FMS Knob to highlight the waypoint after the desired airway
entry point. If this waypoint is not a valid airway entry point, a valid entry
point should be entered at this time.

24

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Flight Planning

4)

Turn the small FMS Knob one click clockwise and select the LD AIRWY
Softkey, or press the MENU Key and select “Load Airway”. The Select
Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway”
menu item is available only when an acceptable airway entry waypoint has
been chosen (the waypoint ahead of the cursor position).

5)

Turn the FMS Knob to select the desired airway from the list, and press the
ENT Key. Low altitude airways are shown first in the list, followed by “all”

altitude airways, and then high altitude airways.

6)

Turn the FMS Knob to select the desired airway exit point from the list, and
press the ENT Key. ‘LOAD?’ is highlighted.

7)

Press the ENT Key. The system returns to editing the flight plan with the
new airway inserted.

INVERT AN ACTIVE FLIGHT PLAN

1)

Press the FPL Key to display the active flight plan.

2)

Press the MENU Key to display the Page Menu.

3)

Turn the large FMS Knob to highlight ‘Invert Flight Plan’.

4)

Press the ENT Key. The original flight plan remains intact in its flight plan
catalog storage location.

5)

With ‘OK’ highlighted, press the ENT Key to invert the flight plan.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT

PLAN

1)

Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.

Or, for a stored flight plan:

a)

Press the MFD FPL Key and turn the small FMS Knob to select the
Flight Plan Catalog Page.

b)

Press the FMS Knob to activate the cursor.

c)

Turn the large FMS Knob to highlight the desired flight plan.

d)

Select the EDIT Softkey.

2)

Turn the large FMS Knob to highlight the title for the approach, departure,
arrival, or airway to be deleted. Titles appear in white directly above the
procedure’s waypoints.

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

25

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Flight Planning

3)

Press the CLR Key to display a confirmation window.

4)

Flight

InstrumentsEICAS

With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.

STORE A FLIGHT PLAN

1)

After creating a flight plan on either the PFD or MFD, it may be saved by
pressing the MENU Key.

Nav/Com/

XPDR/AudioAFCSGPS Nav

2)

Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key.

3)

With ‘OK’ highlighted, press the ENT Key to store the flight plan.

EDIT A STORED FLIGHT PLAN

1)

Press the FPL Key for the MFD and turn the small FMS Knob to display the
Flight Plan Catalog Page.

2)

Press the FMS Knob to activate the cursor.

Flight

PlanningProcedures

3)

Turn the large FMS Knob to highlight the desired flight plan.

4)

Select the EDIT Softkey.

5)

Turn the large FMS Knob to place the cursor in the desired location.

6)

Enter the changes, then press the ENT Key.

7)

Hazard

Avoidance

Press the FMS Knob to return to the Flight Plan Catalog Page.

DELETE A WAYPOINT FROM THE FLIGHT PLAN

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

26

1)

Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.

Or, for a stored flight plan:

a)

Press the FPL Key of the MFD and turn the small FMS Knob to select
the Flight Plan Catalog Page.

b)

Press the FMS Knob to activate the cursor.

c)

Turn the large FMS Knob to highlight the desired flight plan.

d)

Select the EDIT Softkey.

2)

Turn the large FMS Knob to highlight the waypoint to be deleted.

3)

Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation
window.

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Flight Planning

4)

With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel
the delete request, turn the large FMS Knob to highlight ‘CANCEL’ and press
the ENT Key.

5)

Once all changes have been made, press the FMS Knob to remove the
cursor.

INVERT AND ACTIVATE A STORED FLIGHT PLAN

1)

Press the FPL Key for the MFD.

2)

Turn the small FMS Knob to select the Flight Plan Catalog Page.

3)

Press the FMS Knob to activate the cursor.

4)

Turn the large FMS Knob to highlight the desired flight plan.

5)

Select the INVERT Softkey. ‘Invert and activate stored flight plan?’ is
displayed.

6)

With ‘OK’ highlighted, press the ENT Key. The selected flight plan is now
inverted and activated. The original flight plan remains intact in its flight plan
catalog storage location.

COPY A FLIGHT PLAN

1)

Press the FPL Key for the MFD.

2)

Turn the small FMS Knob to select the Flight Plan Catalog Page.

3)

Press the FMS Knob to activate the cursor.

4)

Turn the large FMS Knob to highlight the flight plan to be copied.

5)

Select the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is
displayed.

6)

With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

DELETE A FLIGHT PLAN

1)

Press the FPL Key for the MFD.

2)

Turn the small FMS Knob to select the Flight Plan Catalog Page.

3)

Press the FMS Knob to activate the cursor.

4)

Turn the large FMS Knob to highlight the flight plan to be deleted.

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

27

Flight Planning

5)

Select the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is

Flight

InstrumentsEICAS

displayed.

6)

With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.

GRAPHICAL FLIGHT PLAN CREATION

1)

Press the FPL Key to display the Active Flight Plan Page on the MFD.

Nav/Com/

XPDR/AudioAFCSGPS Nav

2)

Press the Joystick to activate the map pointer. Use the Joystick to move
the pointer to the desired point on the map to be inserted as a waypoint in
the flight plan.

3)

The default insertion point is at the end of the flight plan. If the selected
waypoint is to be placed anywhere other than the end of the flight plan,
press the FMS Knob to activate the cursor. Waypoints are inserted
the cursor. Turn the large FMS Knob to select the desired insertion point.

4)

Flight

PlanningProcedures

Select the LD WPT Softkey. The selected waypoint is inserted at the selected
point. The default user waypoint naming is USR000, USR001, USR002, and
so on.

5)

To change the user waypoint name, follow the procedure for modifying a user
waypoint.

ABOVE

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

28

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

PROCEDURES

LOAD AND ACTIVATE A DEPARTURE PROCEDURE

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.

3)

Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a
list of available departures.

4)

Turn the large FMS Knob to highlight the desired departure.

5)

Press the ENT Key. A list of runways may be displayed for the departure. If
so, turn either FMS Knob to select the desired runway.

6)

Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a
list of available transitions.

7)

Turn the large FMS Knob to highlight the desired transition.

8)

Press the ENT Key.

9)

With ‘LOAD?’ highlighted, press the ENT Key. The departure is active when
the flight plan is active.

Procedures

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

ACTIVATE A DEPARTURE LEG

1)

Press the FPL Key for the MFD to display the active flight plan.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight the desired waypoint within the
departure.

4)

Select the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.

5)

With ‘ACTIVATE’ highlighted, press the ENT Key.

LOAD AN ARRIVAL PROCEDURE

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’.

3)

Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list
of available arrivals.

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

29

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Procedures

4)

Turn the large FMS Knob to highlight the desired arrival.

5)

Flight

InstrumentsEICAS

Press the ENT Key. A list of transitions is displayed for the selected arrival.

6)

Turn either FMS Knob to select the desired transition.

7)

Press the ENT Key. A list of runways may be displayed for the selected
arrival.

8)

Turn the large FMS Knob to highlight the desired runway.

9)

Nav/Com/

XPDR/AudioAFCSGPS Nav

Press the ENT Key.

10)

With ‘LOAD?’ highlighted, press the ENT Key.

11)

The arrival becomes part of the active flight plan.

ACTIVATE AN ARRIVAL LEG

1)

Press the FPL Key to display the active flight plan.

2)

Press the FMS Knob to activate the cursor.

3)

Flight

PlanningProcedures

Turn the large FMS Knob to highlight the desired waypoint within the
arrival.

4)

Select the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.

5)

With ‘ACTIVATE’ highlighted, press the ENT Key.

Hazard

Avoidance

LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE

Features

Additional

NOTE: If certain GPS parameters (WAAS, RAIM, etc.) are not available, some

published approach procedures for the desired airport may not be displayed
in the list of available approaches.

Abnormal

Annun/

Operation

AlertsAppendixIndex

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘SELECT APPROACH’.

3)

Press the ENT Key. A list of available approaches for the destination airport
is displayed.

4)

Turn either FMS Knob to highlight the desired approach.

5)

Press the ENT Key. A list of available transitions for the selected approach
procedure is now displayed.

6)

Turn either FMS Knob to select the desired transition. The “Vectors”
option assumes vectors will be received to the final course segment of

30

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Procedures

the approach and will provide navigation guidance relative to the final
approach course.

7)

Press the ENT Key. The cursor moves to the MINIMUMS field.

8)

If desired, the DA/MDA for the selected approach procedure may be
entered and displayed on the PFD. Turn the small

FMS

Knob in the

direction of the green arrow to change the display from OFF to BARO.

9)

Press the

FMS

ENT

Key. The cursor moves to the altitude field. Turn the small

Knob to enter the published DA/MDA for the selected approach

procedure.

10)

Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’

highlighted.

11)

Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.

Selecting ‘LOAD?’ enters the selected approach procedure into the active
flight plan, but is not currently active. Selecting ‘ACTIVATE?’ enters the
selected approach procedure into the active flight plan and activates the
first leg of the approach.

12)

Press the ENT Key.

ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.

3)

Press the ENT Key.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

ACTIVATE A VECTOR TO FINAL APPROACH FIX

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’.

3)

Press the ENT Key.

4)

The final approach course becomes the active leg.

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

31

Operation

Abnormal

Annun/

Alerts Appendix Index

Procedures

ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN

Flight

InstrumentsEICAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’.

3)

Press the ENT Key. A confirmation window is displayed.

4)

With ‘ACTIVATE’ highlighted, press the ENT Key.

Or:

Press the go-around button.

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

32

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Hazard Avoidance

HAZARD AVOIDANCE

CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP

1)

With the Navigation Map Page displayed, press the MENU Key to display
the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’
option.

2)

Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS
Knob to select ‘Weather’ to customize the display of weather features.
Select ‘Traffic’ to customize the display of traffic.

3)

Press the small FMS Knob to return to the Navigation Map Page.

XM WEATHER (OPTIONAL)

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

WARNING: Use of XM weather for hazardous weather penetration is not

recommended. Weather information provided by XM Radio Service is
approved only for weather avoidance, not penetration.

Displaying XM Weather on the Navigation Map Page

1)

Select the MAP Softkey.

2)

Select the NEXRAD or XM LTNG Softkey to display the desired weather.
Select the applicable softkey again to remove weather data from the
Navigation Map Page.

Display METAR and TAF information on the Airport Information Page

1)

Turn the large FMS Knob to select the WPT Page Group.

2)

Turn the small FMS Knob to select the Airport Information Page.

3)

Select the WX Softkey to display METAR and TAF text (METAR and TAF
information is updated every 12 minutes).

Displaying Weather on the Weather Data Link Page

1)

Turn the large FMS Knob to select the Map Page Group.

2)

Turn the small FMS Knob to select the Weather Data Link Page.

3)

Select the available softkeys to select the desired XM weather product.

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

33

Hazard Avoidance

4)

Select the LEGEND Softkey to view the legends for the selected products.

Flight

InstrumentsEICAS

If necessary, turn either FMS Knob to scroll through the list. Press the small
FMS Knob or the ENT Key to return to the map.

Map Panning Information – Weather Data Link Page

1)

Push in the Joystick to display the panning arrow.

2)

Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs,

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

or SIGMETs.

3)

Press the ENT Key to display pertinent information for the selected product.

Note that pressing the ENT Key when panning over an AIRMET or a
SIGMET displays an information box that shows the text of the report.
Panning over an airport with METAR information does not display more
information but allows the user to press the ENT Key and select that
Airport’s Information Page to display the text of the report. Pressing the
ENT Key when panning over a TFR displays TFR specific information.

Weather Products and Symbols

Echo Top (Cloud Top and Echo Top Mutually Exclusive)

Hazard

Avoidance

NEXRAD

Features

Additional

TRAFFIC SYSTEMS

Abnormal

Operation

Cloud Top

WARNING: Traffic information shown on the G1000 Multi Function Display

AlertsAppendixIndex

Annun/

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.

• If Trafc information Service (TIS) is congured, a STANDBY, OPERATE, and
TNA MUTE Softkey is displayed.

• If a Trafc Advisory System (TAS) is congured, a STANDBY, NORMAL, TEST,
and ALT MODE Softkey is displayed.

34

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Cell Movement

XM Lightning

SIGMETs/AIRMETs

City Forecast

METARs

Freezing Levels

Surface Analysis

Cyclone Warnings

County Warnings

Winds Aloft

190-00600-02 Rev. A

Hazard Avoidance

Traffic Symbol Description

Non-Threat Traffic

(intruder is beyond 5 nm and greater than 1200’ vertical separation)

Proximity Advisory (PA) (TAS only)

(intruder is within 5 nm and less than 1200’ vertical separation)

Traffic Advisory (TA)

(closing rate, distance, and vertical separation meet TA criteria)

Traffic Advisory Off Scale

Traffic Symbol Description

Traffic Information Service (TIS)

NOTE: If the G1000 is configured to use an optional Traffic Advisory System
(TAS), TIS is not available for use.

NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Displaying Traffic on the Traffic Map Page

1)

Turn the large FMS Knob to select the Map Page Group.

2)

Turn the small FMS Knob to select the Traffic Map Page.

3)

Select the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.

4)

Select the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.

5)

Rotate the Joystick clockwise to display a larger area or rotate counter­clockwise to display a smaller area.

Displaying Traffic on the Navigation Map

1)

Ensure TIS is operating. With the Navigation Map displayed, select the
MAP Softkey.

2)

Select the TRAFFIC Softkey. Traffic is now displayed on the map.

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

35

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Hazard Avoidance

Traffic Advisory System (TAS) (Optional)

Flight

InstrumentsEICAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

System Self Test

1)

Set the range to 2/6 nm.

2)

Select the STANDBY Softkey.

3)

Select the TEST Softkey.

4)

Self test takes approximately eight seconds to complete. When completed
successfully, traffic symbols are displayed and a voice alert “TAS System Test
OK” is heard. If the self test fails, the system reverts to Standby Mode and
a voice alert “TAS System Test Fail” is heard.

Displaying Traffic on the Traffic Map Page

1)

Turn the large FMS Knob to select the Map Page Group.

2)

Turn the small FMS Knob to select the second rectangular page icon.

3)

Select the NORMAL Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.

4)

Select the ALT MODE Softkey to change the altitude volume. Select the
desired altitude volume by pressing the BELOW, NORMAL, ABOVE, or
UNREST (unrestricted) Softkey. The selection is displayed in the Altitude
Mode field.

5)

Select the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.

6)

Rotate the Joystick clockwise to display a larger area or rotate counter­clockwise to display a smaller area.

Displaying Traffic on the Navigation Map

Abnormal

Operation

AlertsAppendixIndex

Annun/

36

1)

Ensure TAS is operating.

2)

With the Navigation Map displayed, select the MAP Softkey.

3)

Select the TRAFFIC Softkey. Traffic is now displayed on the map.

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Hazard Avoidance

TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY

WARNING: The TAWS display shows supplemental information only. It should
not be used for navigation.

NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.

NOTE: TAWS operation is only available when the G1000 is configured for a
TAWS-B installation.

Manual System Test

1)

While the TAWS Page is displayed, press the MENU Key.

2)

Turn the small FMS Knob to select ‘Test TAWS’.

3)

Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center
of the TAWS Page.

When all is in working order, “TAWS System Test, OK” is heard.

Display Terrain on the TAWS Page

1)

Turn the large FMS Knob to select the Map Page Group.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

2)

Turn the small FMS Knob to select the TAWS Page.

3)

If desired, select the VIEW Softkey to access the ARC and 360 softkeys.
When the ARC Softkey is selected, a radar-like 120° view is displayed.
Select the 360 Softkey to return to the 360° default display.

4)

Rotate the Joystick clockwise to display a larger area or rotate counter­clockwise to display a smaller area.

190-00600-02 Rev. A

Color Terrain/Obstacle Location

Red

Yellow

Black

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Terrain/Obstacle above or within 100’
below current aircraft altitude.

Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.

Terrain/Obstacle is more than 1000’

below aircraft altitude.

37

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Hazard Avoidance

Enable/Disable Aviation Data

Flight

InstrumentsEICAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

1)

While the TAWS Page is displayed, press the MENU Key.

2)

Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.

3)

Press the ENT Key.

TAWS Inhibit

NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active
waypoint in a GPS WAAS approach, a LOW ALT annunciation may appear on
the PFD next to the altimeter if the current aircraft altitude is at least 164
feet below the prescribed altitude at the Final Approach Fix.

Inhibit TAWS

While the TAWS Page is displayed, select the INHIBIT Softkey.

Or

:

1)

Press the MENU Key.

2)

Turn the small FMS Knob to select ‘Inhibit TAWS’.

3)

Press the ENT Key.

Enable TAWS

While the TAWS Page is displayed, select the INHIBIT Softkey.

Or

:

1)

While the TAWS Page is displayed, press the MENU Key.

2)

Turn the small FMS Knob to select ‘Enable TAWS’.

3)

Press the ENT Key.

AlertsAppendixIndex

Annun/

38

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Hazard Avoidance

AIRBORNE COLOR WEATHER RADAR

WARNING: Begin transmitting only when it is safe to do so. If it is desired to
transmit while the aircraft is on the ground, no personnel or objects should
be within 11 feet of the antenna.

CAUTION: In Standby Mode, the antenna is parked at the center line. It
is always a good idea to put the radar in Standby Mode before taxiing the
aircraft to prevent the antenna from bouncing on the bottom stop and possibly
causing damage to the radar assembly.

Displaying Weather on the Weather Radar Page

1)

Turn the large FMS Knob to select the Map Page Group.

2)

Turn the small FMS Knob to select the Weather Radar Page.

3)

Select the MODE Softkey.

4)

If the aircraft is on the ground, select the STANDBY Softkey to initiate the
one minute warm-up period. After the warm-up is complete, the radar will
enter the Standby Mode. After the aircraft is airborne, select the WEATHER
Softkey.

Or

:

If the aircraft is already airborne, select the WEATHER or GROUND
Softkey. The one-minute warm-up period will be initiated, after which the
radar will begin transmitting. The horizontal scan is initially displayed.

5)

Turn the Joystick to select the desired range.

6)

If desired, select the VERTICAL Softkey for vertical scanning.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Adjusting Antenna Tilt

Move the

Joystick

up or down to adjust the tilt of the antenna up or down. Moni-

tor the displayed tilt value in the TILT field.

When scanning vertically, a Tilt Line may be displayed to aid in positioning the tilt

of the antenna. If the Tilt Line is not displayed, perform the following steps:

1)

Press the MENU Key

2)

Turn the large FMS Knob to select ‘Show Tilt Line’.

3)

Press the ENT Key.

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

39

Alerts Appendix Index

Annun/

Hazard Avoidance

Adjusting Antenna Bearing

Flight

Move the

InstrumentsEICAS

or left. Monitor the displayed bearing value in the BEARING field.

Joystick

right or left to adjust the azimuth position of the antenna right

When scanning horizontally, a Bearing Line may be displayed to aid in positioning
the antenna for the vertical scan. If the Bearing Line is not displayed, perform the
following steps:

1)

Press the MENU Key

Nav/Com/

XPDR/AudioAFCSGPS Nav

2)

Turn the large FMS Knob to select ‘Show Bearing Line’.

3)

Press the ENT Key.

Vertically Scan a Storm Cell

1) While in the Horizontal Scan view, move the Joystick to place the Bearing

Line on the desired storm cell, or other area, to be vertically scanned.

2)

Select the VERTICAL Softkey. A vertical ‘slice’ of the selected area will now

Flight

PlanningProcedures

be displayed.

3)

Move the Joystick right or left to move the scanned “slice” a few degrees
right or left.

4)

Turn the Joystick to adjust the range.

5)

To select a new area to be vertically scanned, select the HORIZON Softkey

Hazard

Avoidance

to return to the Horizontal Scan view and repeat the previous steps.

Adjusting Gain

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

40

WARNING: Changing the gain in Weather Mode will cause precipitation
intensity to be displayed as a color not representative of the true intensity.
Remember to return the gain setting to ‘Calibrated’ for viewing the actual
intensity of precipitation.

1)

Select the GAIN Softkey to activate the cursor in the ‘GAIN’ field.

2)

Turn the small FMS Knob to adjust the gain for the desirable level. The
gain setting is visible in the gain field as a movable horizontal bar in
a flashing box. The line pointer is a reference depicting the calibrated
position.

3)

Press the FMS Knob to remove the cursor.

4)

Select the GAIN Softkey again to recalibrate the gain. ‘CALIBRATED’ will be
displayed in the ‘GAIN’ field.

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Hazard Avoidance

Ground Mapping

1)

Select the MODE Softkey.

2)

Select the GROUND Softkey to place the radar in Ground Map Mode.

3)

Select the BACK Softkey.

Sector Scan

1)

While in the Horizontal Scan Mode, move the Joystick right or left to place
the Bearing Line in the desired position. The location of the Bearing Line
will become the center point of the Sector Scan.

2)

Press the FMS Knob to display the cursor.

3)

Turn the large FMS Knob to place the cursor in the SECTOR SCAN field.

4)

Turn the small FMS Knob to select FULL, 60˚, 40˚, or 20˚ scan.

5)

If desired, readjust the Bearing Line with the Joystick to change the center
of the Sector Scan.

6)

Press the FMS Knob to remove the cursor.

Antenna Stabilization

1)

To activate or deactivate the antenna stabilization, select the MODE
Softkey.

2)

Select the STAB ON Softkey to activate antenna stabilization or select
the STAB OFF Softkey to deactivate. The current stabilization condition is
shown in the upper right of the weather radar display.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Weather Attenuated Color Highlight (WATCH®)

To activate or deactivate the WATCH® feature, select the WATCH Softkey. This

feature is only available in the Horizontal Scan Mode.

Weather Alert

To activate or deactivate Weather Alert, select the WX ALRT Softkey. Activating

and deactivating will also enable or inhibit the alert on the PFD.

Automatic Standby

When the weather radar system is in the Weather or Ground Map Mode, upon

landing the system will automatically switch to Standby Mode.

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

41

Operation

Abnormal

Annun/

Alerts Appendix Index

Hazard Avoidance

Flight

InstrumentsEICAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

42

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Additional Features

ADDITIONAL FEATURES

SYNTHETIC VISION

Synthetic Vision System (SVS) functionality is offered as an optional enhancement

to the G1000 Integrated Flight Deck System.

SVS is primarily comprised of a computer-generated forward-looking, attitude
aligned view of the topography immediately in front of the aircraft from the pilot’s
perspective. SVS information is shown on the primary flight display (PFD).

SVS offers a three-dimensional view of terrain and obstacles. Terrain and
obstacles that pose a threat to the aircraft in flight are shaded yellow or red.

In addition to SVS enhancement to the PFD, the following feature enhancements
have been added to the PFD:

• Pathways

• Flight Path Marker

• Horizon Heading Marks

• Terrain and Obstacle Alerting

• Three-dimensional Traffic

• Airport Signs

• Runway Display

Displaying Synthetic Terrain

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

1)

Press the PFD Softkey.

2)

Press the SYN VIS Softkey.

3)

Press the SYN TERR Softkey.

4)

Press the BACK Softkey to return to the previous page.

Displaying Pathways

1)

Press the PFD Softkey.

2)

Press the SYN VIS Softkey.

3)

If not already enabled, press the SYN TERR Softkey.

4)

Press the PATHWAY Softkey.

5)

Press the BACK Softkey to return to the previous page.

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

43

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Additional Features

Displaying Heading on the Horizon

Flight

Nav/Com/

Flight

1)

InstrumentsEICAS

XPDR/AudioAFCSGPS Nav

TERMINAL PROCEDURE CHARTS

PlanningProcedures

Press the PFD Softkey.

2)

Press the SYN VIS Softkey.

3)

If not already enabled, press the SYN TERR Softkey.

4)

Press the HRZN HDG Softkey.

5)

Press the BACK Softkey to return to the previous page.

Displaying Airport Signs

1)

Press the PFD Softkey.

2)

Press the SYN VIS Softkey.

3)

If not already enabled, press the SYN TERR Softkey.

4)

Press the APTSIGNS Softkey.

5)

Press the BACK Softkey to return to the previous page.

NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts® in

electronic form, it is still advisable to carry another source of charts on-board
the aircraft.

Hazard

Avoidance

SafeTaxi

®

SafeTaxi® is an enhanced feature that gives greater map detail as the map range

is adjusted in on the airport. The airport display on the map reveals runways with

Features

Additional

numbers, taxiways identifiers, and airport landmarks including ramps, buildings,
control towers, and other prominent features. Resolution is greater at lower map
ranges. The aircraft symbol provides situational awareness while taxiing.

Abnormal

Operation

Pressing the DCLTR Softkey (declutter) once removes the taxiway markings and

airport identification labels. Pressing the DCLTR Softkey twice removes VOR station

AlertsAppendixIndex

Annun/

ID, the VOR symbol, and intersection names if within the airport plan view. Pressing
the DCLTR Softkey a third time removes the airport runway layout, unless the airport
in view is part of an active route structure. Pressing the DCLTR Softkey again cycles
back to the original map detail.

The SafeTaxi database contains detailed airport diagrams for selected airports.

These diagrams aid in following ground control instructions by accurately displaying

44

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Additional Features

the aircraft position on the map in relation to taxiways, ramps, runways, terminals, and
services. This database is updated on a 56-day cycle.

ChartView

ChartView resembles the paper version of Jeppesen terminal procedures charts.
The charts are displayed in full color with high-resolution. The MFD depiction shows
the aircraft position on the moving map in the plan view of most approach charts and
on airport diagrams.

The ChartView database is updated on a 14-day cycle. If the ChartView database
is not updated within 70 days of the expiration date, ChartView will no longer
function.

FliteCharts

®

FliteCharts® resemble the paper version of National Aeronautical Charting Office
(NACO) terminal procedures charts. The charts are displayed with high-resolution
and in color for applicable charts. Current aircraft position is not displayed on
FliteCharts.

The FliteCharts database contains procedure charts for the United States only.
This database is updated on a 28-day cycle. If not updated within 180 days of the
expiration date, FliteCharts will no longer function.

View Charts from the Navigation Map Page

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

1)

Select the SHW CHRT Softkey when displayed.

Or

:

Move the map pointer to point to a desired point on the map and select the
SHW CHRT Softkey.

2)

Select the DP, STAR, APR, WX, or NOTAM Softkey to access charts for
departures, arrivals, approaches, weather or NOTAMs.

3)

Select the GO BACK Softkey to return to the previous page.

View Charts from the Active Flight Plan Page

1)

While viewing the Active Flight Plan Page, press the FMS Knob to activate
the cursor.

2)

Turn the large FMS Knob to select the departure airport, destination
airport, departure, arrival, or approach.

3)

Select the SHW CHRT Softkey. The appropriate chart is displayed, if
available for the item selected.

190-00600-02 Rev. A

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45

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Additional Features

4)

Select the GO BACK Softkey to return to the previous page.

Flight

Change Day/Night View

InstrumentsEICAS

1)

While viewing a chart press the MENU Key to display the Page Menu
OPTIONS.

2)

Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and
press the ENT Key.

3)

Nav/Com/

XPDR/AudioAFCSGPS Nav

Turn the large FMS Knob to move between the ‘FULL SCREEN’ and ‘COLOR
SCHEME’ Options.

4)

Turn the small FMS Knob to choose between the ‘On’ and ‘Off’ Full Screen
Options.

5)

Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’
Options.

6)

In Auto Mode, turn the large FMS Knob to select the percentage field and
change percentage with the small FMS Knob. The percentage of change is

Flight

PlanningProcedures

the day/night crossover point based on backlighting intensity.

7)

Press the FMS Knob when finished to remove the Chart Setup Menu.

XM® RADIO ENTERTAINMENT

The XM® Radio Page provides information and control of the audio entertainment

features of the XM Satellite Radio.

Hazard

Avoidance

Selecting the XM Radio Page

Features

1)

Additional

Turn the large FMS Knob to select the Auxiliary Page Group.

2)

Turn the small FMS Knob to select the displayed AUX - XM Information
Page.

Abnormal

Operation

3)

Select the RADIO Softkey to show the XM Radio Page where audio
entertainment is controlled.

AlertsAppendixIndex

Annun/

Active Channel and Channel List

The Active Channel Box on the XM Radio Page displays the currently selected
channel. The Channels List Box of the XM Radio Page shows a list of the available
channels for the selected category.

46

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Additional Features

Selecting a Category

The Category Box of the XM Radio Page displays the currently selected category

of audio.

1)

Select the CATGRY Softkey on the XM Radio Page.

2)

Select the CAT + and CAT - softkeys to cycle through the categories.

Or

:

Turn the small FMS Knob to display the ‘Categories’ list. Highlight the
desired category with the small FMS Knob.

3)

Press the ENT Key.

Select an Available Channel within the Selected Category

1)

While on the XM Radio Page, select the CHNL Softkey.

2)

Select the CH + Softkey to go up through the list in the Channel Box, or
move down the list with the CH – Softkey.

Or

:

Press the FMS Knob to highlight the channel list and turn the large FMS
Knob to scroll through the channels.

3)

With the desired channel highlighted, press the ENT Key.

Entering a Channel Directly

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

1)

While on the XM Radio Page, select the CHNL Softkey.

2)

Select the DIR CH Softkey. The channel number in the Active Channel Box
is highlighted.

3)

Select the numbered softkeys located on the bottom of the display to
directly select the desired channel number.

4)

Press the ENT Key to activate the selected channel.

Assigning Channel Presets

Up to 15 channels from any category can be assigned a preset number.

1)

On the XM Radio Page, with the desired channel active, select the
PRESETS Softkey to access the first five preset channels (PS1 - PS5).

2)

Select the MORE Softkey to access the next five channels (PS6 – PS10),
and again to access the last five channels (PS11 – PS15). Pressing the
MORE Softkey repeatedly cycles through the preset channels.

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

47

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Additional Features

3)

Select any one of the (PS1 - PS15) softkeys to assign a number to the

Flight

InstrumentsEICAS

active channel.

4)

Select the SET Softkey on the desired channel number to save the channel
as a preset.

Adjusting Volume

Radio volume is controlled at each passenger station.

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

48

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Abnormal Operation

ABNORMAL OPERATION

REVERSIONARY MODE

If the system detects a failure in PFD1, reversionary mode is entered
automatically. Reversionary mode must be entered manually in the case of
PFD2 or MFD failure.

combined with engine instrumentation on the remaining display.

Manual activation of reversionary display mode is accomplished by pressing the

DISPLAY BACKUP Button on the appropriate audio panel.

• PFD1 – By pressing the DISPLAY BACKUP Button on the left audio panel.

• MFD – By pressing the DISPLAY BACKUP Button on the left or the right

audio panel.

• PFD2 – By pressing the DISPLAY BACKUP Button on the right audio

panel.

NOTE: The Cessna Citation Mustang Airplane Flight Manual (AFM) always
takes precedence over the information found in this section.

. In reversionary mode, critical flight instrumentation is

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

ABNORMAL COM OPERATION

When a COM tuning failure is detected by the system, the emergency frequency
(121.500 MHz) is automatically loaded into the active frequency field of the COM
radio for which the tuning failure was detected. In the event of a failure of both PFDs,
the emergency frequency (121.500 MHz) automatically becomes the active frequency
on both COM radios.

HAZARD DISPLAYS WITH LOSS OF GPS POSITION

If GPS position is lost, or becomes invalid, selected hazards being displayed on the
Navigation Map Page are removed until GPS position is again established.

Loss of Hazard Functions with Loss of GPS

Position

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

49

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Abnormal Operation

UNUSUAL ATTITUDES

Flight

The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary

InstrumentsEICAS

functions are displayed in these situations.

The following information is removed from the PFD (and corresponding softkeys

are disabled) when the aircraft experiences unusual attitudes:

• Trafc Annunciations

• AFCS Annunciations

Nav/Com/

XPDR/AudioAFCSGPS Nav

• Flight director Com­mand Bars

• Inset Map

• Temperatures

• DME Information

Window

• Wind Data

• Selected Heading Box

Flight

PlanningProcedures

• Selected Course Box

• Transponder Status

• System Time

• PFD Setup Menu

• Windows displayed in

the lower right corner

of the PFD:
– Timer/References
– Nearest Airports
– Flight Plan
– Messages
– Procedures

• Barometric Minimum

Descent Altitude Box

Box

Hazard

Avoidance

• Glideslope, Glidepath,

and Vertical Deviation
Indicators

• Altimeter Barometric
Setting

• Selected Altitude

• VNV Target Altitude

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

50

Extreme Pitch Indication

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Abnormal Operation

DEAD RECKONING

While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS
solution or is unable to calculate a GPS position, the system automatically reverts to
Dead Reckoning (DR) Mode. In DR Mode, the G1000 uses its last-known position
combined with continuously updated airspeed and heading data (when available) to
calculate and display the aircraft’s current estimated position.

NOTE: Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic
(OCN) phase of flight. In all other phases, an invalid GPS solution produces
a “NO GPS POSITION” annunciation on the map and the G1000 stops
navigating in GPS Mode.

DR Mode is indicated on the G1000 by the appearance of the letters ‘DR’
superimposed in yellow over the ‘own aircraft’ symbol as shown in the following
figure. In addition, ‘DR’ is prominently displayed, also in yellow, on the HSI slightly
above and to the right of the aircraft symbol on the CDI as shown in the following
figure. Also, the CDI deviation bar is removed from the display. Lastly, but at the same
time, a ‘GPS NAV LOST’ alert message appears on the PFD.

Normal navigation using GPS/WAAS source data resumes automatically once a
valid GPS solution is restored.

It is important to note that estimated navigation data supplied by the G1000 in
DR Mode may become increasingly unreliable and must not be used as a sole means
of navigation. If, while in DR Mode, airspeed and/or heading data is also lost or
not available, the DR function is not be capable of estimating your position and,
consequently, the system may display a path that is different than the actual movement
of the aircraft. Estimated position information displayed by the G1000 through
DR while there is no heading and/or airspeed data available should not be used for
navigation.

DR Mode is inherently less accurate than the standard GPS/WAAS Mode due to the
lack of satellite measurements needed to determine a position. Changes in wind speed
and/or wind direction compounds the relative inaccuracy of DR Mode. Because of this
degraded accuracy, the crew must maintain position awareness using other navigation
equipment until GPS-derived position data is restored.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

51

Abnormal Operation

Flight

InstrumentsEICAS

CDI ‘DR’ Indication on PFD

Symbolic Aircraft

(Map pages and Inset Map)

Nav/Com/

XPDR/AudioAFCSGPS Nav

Dead Reckoning Indications

As a result of operating in DR Mode, all GPS-derived data is computed based upon
an estimated position and is displayed as yellow text on the display to denote degraded
navigation source information. This data includes the following:

• Navigation Status Box elds except Active Leg, TAS, and DTK

• GPS Bearing Pointer

• Wind data and pointers in the Wind Data Box on the PFD

Flight

PlanningProcedures

• Track Bug

• All Bearing Pointer Distances

• Active Flight Plan distances, bearings, and ETE values

Also, while the G1000 is in DR Mode, the autopilot will not couple to GPS, and
both TAWS and Terrain Proximity are disabled. Additionally, the accuracy of all nearest

Hazard

information (airports, airspaces, and waypoints) is questionable. Finally, airspace

Avoidance

alerts continue to function, but with degraded accuracy.

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

52

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

CAS MESSAGES

Annunciations & Alerts

ANNUNCIATIONS & ALERTS

Instruments EICAS

Flight

Messages

Warning Caution Advisory

AFT DOOR

AFT JBOX CB L-R*

AFT JBOX LMT L-R*

ANTISKID FAIL

BATTERY O’TEMP BATTERY O’TEMP Overheated NiCad battery (optional)

BATT TEMP FAIL Battery temperature sensor failure X X

CABIN ALT CABIN ALT CABIN ALT Cabin altitude potentially unsafe X X X

CABIN DOOR Cabin door not fully secured X

CHECK DOORS

DUCT O’HEAT L-R*

ENG A/I COLD L-R* ENG A/I COLD L-R*

ENG CTRL SYS L-R*

ENGINE FAIL L-R* An engine has failed

F/W SHUTOFF L-R* Fuel firewall shutoff valve fully closed X

FLAPS FAIL A flap system failure has occurred. X

FUEL BOOST L-R* FUEL BOOST L-R*

FUEL FLTR BP L-R*

FUEL LO INOP L-R* Fuel low level function failure X X

FUEL LVL LO L-R* Fuel level in tank is too low X

FUEL PRES LO L-R* Fuel pressure too low X X

FUEL TRANSFER Fuel transfer valve open X

GEN OFF L-R GEN OFF L-R*

HYD PRESS LO Hydraulic system pressure too low X X

HYD PUMP ON Hydraulic pump running too long X X

Description

Tailcone baggage door not fully
secured
Start control circuit breaker (located
in aft j-box) tripped
Current limiter blown (located in
aft j-box)
Antiskid Control Unit cannot perform
anti-skid functions

A door monitor has not been
properly tested or has failed
Duct temperature too high or sensor
disconnected
Engine anti-ice system ON and inlet
temperature is cold
FADEC has a fault that requires
maintenance

Electric fuel boost pump ON. Caution
condition is displayed when the
boost pump is operating in abnormal
conditions.
Engine fuel filter impending bypass
switch closed

One or both electrical generators
offline

Inhibits

ESI

TOPI

AIR

LOPI

X X X X

X X

ESDI

X X

EMER

X

X

X

X

X

X

GND

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

53

Annunciations & Alerts

Messages

Flight

Nav/Com/

Flight

Hazard

Additional

Warning Caution Advisory

InstrumentsEICAS

MFD COLD MFD temperature is below -20° C

NOSE DOOR L-R*

NO TIRE SPINDOWN

OIL PRESS LO L-R* Oil pressure less than redline low limit X X X

XPDR/AudioAFCSGPS Nav

PlanningProcedures

TAIL CONE BLD LK

Avoidance

Features

OXYGEN OFF Oxygen supply off X X X

P/S HTR L-R*

PRESS CTRL PRESS CTRL Pressure controller loss of integrity X X X

PRESS OFF

SPD BRK EXTEND Speed brakes extended X

STALL WARN FAIL Failure detected in stall warning system X X X X

STALL WARN HI

STALL WARN HTR

SURFACE DE-ICE

T2 HTR FAIL L-R* T2 probe heater failure X X X

TAIL DE-ICE FAIL De-ice system not operating normally X

W/S A/I FAIL L-R* W/S A/I FAIL L-R* Loss of power to windshield heater X

W/S O’HEAT L-R* W/S O’HEAT L-R*

WING DE-ICE FAIL De-ice system operating abnormally X

WOW MISCOMPARE Gear on-ground inputs do not agree X X X

One or both nose baggage doors not
fully secured
Antiskid control spindown function
not working

No current detected to pitot static
heater

Air Source Selector switch in OFF or
fresh air position

Stall warning system on ice­contaminated schedule
No power delivered to stall warning
vane heater
De-ice boots inflating/deflating as
designed

Tailcone temp high, possible bleed
air leak.

Windshield anti-ice power ON;
temperature too high

Description

X X

X X

*Only affected side displayed (L, R, or L-R) in a CAS message; applicable CAS messages listed here
display L-R for example.

Abnormal

Operation

Inhibits

ESI

TOPI

AIR

LOPI

X X

X X

X X X

ESDI

X

X

X

X

EMER

GND

AlertsAppendixIndex

Annun/

54

Name Inhibit

EMER Emergency Bus Mode Inhibit

ESI Engine Start Inhibit

TOPI Takeoff Operation Phase Inhibit

AIR In-Air Inhibit
LOPI Landing Operation Phase Inhibit
ESDI Engine Shutdown Inhibit

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Annunciations & Alerts

COMPARATOR ANNUNCIATIONS

Comparator

Window Text

ALT MISCOMP

Difference in altitude sensors is > 200 ft.

If both airspeed sensors detect < 35 knots, this is inhibited.

IAS MISCOMP

If either airspeed sensor detects > 35 knots, and the difference in sensors is > 10
kts.

If either airspeed sensor detects > 80 knots, and the difference in sensors is > 7
kts.

HDG MISCOMP

PIT MISCOMP

ROL MISCOMP

ALT NO COMP
IAS NO COMP

HDG NO COMP

PIT NO COMP

ROL NO COMP

Difference in heading sensors is > 6 degrees.

Difference in pitch sensors is > 5 degrees.

Difference in roll sensors is > 6 degrees.

No data from one or both altitude sensors.

No data from one or both airspeed sensors.

No data from one or both heading sensors.

No data from one or both pitch sensors.

No data from one or both roll sensors..

REVERSIONARY SENSOR ANNUNCIATIONS

Condition

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Reversionary

Sensor Window

Text

BOTH ON ADC1
BOTH ON ADC2

BOTH ON AHRS1

BOTH ON AHRS2

BOTH ON GPS1
BOTH ON GPS2

USING ADC1
USING ADC2

USING AHRS1

190-00600-02 Rev. A

Condition

Both PFDs are displaying data from the number one Air Data Computer.

Both PFDs are displaying data from the number two Air Data Computer.

Both PFDs are displaying data from the number one Attitude & Heading Reference
System.

Both PFDs are displaying data from the number two Attitude & Heading Reference
System.

Both PFDs are displaying data from the number one GPS receiver.

Both PFDs are displaying data from the number two GPS receiver.

PFD2 is displaying data from the #1 Air Data Computer.

PFD1 is displaying data from the #2 Air Data Computer.

PFD2 is displaying data from the #1 AHRS.

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

55

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Annunciations & Alerts

Reversionary

Sensor Window

Flight

InstrumentsEICAS

USING AHRS2

USING GPS1
USING GPS2

Nav/Com/

XPDR/AudioAFCSGPS Nav

Text

PFD1 is displaying data from the #2 AHRS.

PFD2 is displaying data from the #1 GPS.

PFD1 is displaying data from the #2 GPS.

Condition

AFCS ALERTS

Condition Annunciation Description

Pitch Failure Pitch axis control failure. AP is inoperative.

Roll Failure Roll axis control failure. AP is inoperative.

MET Switch Stuck,
or Pitch Trim Axis

Flight

PlanningProcedures

Control Failure

System Failure AP and MET are unavailable. FD may still be available.

Emergency
Descent Mode

Elevator Mistrim

Hazard

Avoidance

Up

Elevator Mistrim
Down

Features

Additional

Aileron Mistrim
Left

Aileron Mistrim

Abnormal

Operation

Right

Rudder Mistrim

AlertsAppendixIndex

Annun/

Left

Rudder Mistrim
Right

Preflight Test Performing preflight system test. Upon completion of the

If annunciated when AP is engaged, a failure has occurred in
the pitch trim system. If annunciated when AP is not engaged,
a failed or stuck switch is causing the annunciation.

AP engaged when aircraft altitude above 30,000 ft and
cabin pressurization is lost. Selected Heading set 90° left
of current heading; Selected Altitude set to 15000 ft

A condition has developed causing the pitch servo to
provide a sustained force in the nose up direction.

A condition has developed causing the pitch servo to
provide a sustained force in the nose down direction.

A condition has developed causing the roll servo to provide
a sustained left force.

A condition has developed causing the roll servo to provide
a sustained right force.

A condition has developed causing the yaw servo to
provide a sustained force.

A condition has developed causing the yaw servo to provide a
sustained force.

test, the aural alert will be heard.

Preflight system test has failed.

56

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190-00600-02 Rev. A

Annunciations & Alerts

TAWS ALERTS

Alert Type

Excessive Descent
Rate Warning (EDR)

Reduced Required
Terrain Clearance
Warning (RTC)

Imminent Terrain
Impact Warning (ITI)

Reduced Required
Obstacle Clearance
Warning (ROC)

Imminent Obstacle
Impact Warning
(IOI)

Reduced Required
Terrain Clearance
Caution (RTC)

Imminent Terrain
Impact Caution (ITI)

PFD/MFD

TAWS Page

Annunciation

MFD

Pop-Up Alert

or

or

or

or

or

or

Aural Message

“Pull Up”

“Terrain, Terrain; Pull Up,

*

Pull Up”*

or

“Terrain Ahead, Pull Up;

Terrain Ahead, Pull Up”

Terrain Ahead, Pull Up;

Terrain Ahead, Pull Up”

*

“Terrain, Terrain; Pull Up,

“Obstacle, Obstacle; Pull

*

“Obstacle Ahead, Pull Up;

Obstacle Ahead, Pull Up”

“Obstacle Ahead, Pull Up;

Obstacle Ahead, Pull Up”

*

“Obstacle, Obstacle; Pull

“Caution, Terrain; Caution,

*

“Terrain Ahead; Terrain

“Terrain Ahead; Terrain

*

“Caution, Terrain; Caution,

or

Pull Up”*

Up, Pull Up”*

or

or

Up, Pull Up”*

Terrain”*

or

Ahead”

Ahead”

or

Terrain”*

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

57

Annunciations & Alerts

Flight

Alert Type

InstrumentsEICAS

Reduced Required
Obstacle Clearance
Caution (ROC)

Nav/Com/

XPDR/AudioAFCSGPS Nav

Imminent Obstacle
Impact Caution (IOI)

Premature Descent
Alert Caution (PDA)

Altitude Callout
“500”

Flight

PlanningProcedures

Excessive Descent
Rate Caution (EDR)

Negative Climb
Rate Caution (NCR)

Hazard

* Default configuration

Avoidance

PFD/MFD

TAWS Page

Annunciation

MFD

Pop-Up Alert

or

Aural Message

“Caution, Obstacle; Cau-

*

tion, Obstacle”*

“Obstacle Ahead; Obstacle

“Obstacle Ahead; Obstacle

or

*

“Caution, Obstacle; Cau-

tion, Obstacle”*

“Too Low, Terrain”

None None “Five-Hundred”

*

“Don’t Sink”*

or

“Too Low, Terrain”

or

Ahead”

Ahead”

or

“Sink Rate”

or

TAWS System Status Annunciations

Features

Additional

Alert Type

Abnormal

Operation

TAWS System Test Fail None “TAWS System Failure”

TAWS Alerting is disabled None None

AlertsAppendixIndex

Annun/

No GPS position or
excessively degraded GPS
signal

System Test in progress None None

System Test pass None None “TAWS System Test OK”

58

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

PFD/MFD

TAWS Page

Annunciation

MFD

Pop-Up Alert

Aural Message

None “TAWS Not Available”

190-00600-02 Rev. A

Annunciations & Alerts

MESSAGE ADVISORY ALERTS

Alerts Window Message Audio Alert

PFD1 FAN FAIL – The cooling fan for PFD1 is inoperative.
PFD2 FAN FAIL – The cooling fan for PFD2 is inoperative.

None

MFD FAN FAIL – The cooling fan for the MFD is inoperative.
AV FAN FAIL – The cooling fan for remote avionics has failed.

AURAL ALERTS

Aural Alert Description

“Minimums, minimums” The aircraft has descended below the preset minimum descent altitude or

decision altitude.

“Vertical track” The aircraft is one minute from Top of Descent. Issued only when vertical

navigation is enabled.

“Traffic” The Traffic Information Service (TIS) has issued a Traffic Advisory alert

“TIS not available” The aircraft is outside the Traffic Information Service (TIS) coverage area (not

available when a TAS system is installed).

MFD & PFD MESSAGE ADVISORIES

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Message Comments

DATA LOST

– Pilot stored data

was lost. Recheck settings.

XTALK ERROR

– A flight display

crosstalk error has occurred.

PFD1 SERVICE

– PFD1 needs

service. Return unit for repair.

PFD2 SERVICE

– PFD2 needs

service. Return unit for repair.

MFD1 SERVICE

– MFD1 needs

service. Return unit for repair.

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

The pilot profile data was lost. System reverts
to default pilot profile and settings. The pilot
may reconfigure the MFD & PFDs with preferred
settings, if desired.

The MFD and PFDs are not communicating
with each other. The G1000 system should be
serviced.

The PFD and/or MFD self-test has detected a
problem. The G1000 system should be serviced.

59

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Annunciations & Alerts

MFD & PFD MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEICAS

MANIFEST

Message Comments

– PFD1 software

mismatch, communication halted.

MANIFEST

– PFD2 software

mismatch, communication halted.

Nav/Com/

MANIFEST

XPDR/AudioAFCSGPS Nav

– MFD1 software

mismatch, communication halted.

PFD1 CONFIG

– PFD1 config error.

Config service req’d.

PFD2 CONFIG

– PFD2 config error.

Config service req’d.

MFD1 CONFIG

error. Config service req’d.

Flight

PlanningProcedures

SW MISMATCH

– MFD1 config

– GDU software

version mismatch. Xtalk is off.

CAS INOP

Hazard

Software correction required.

Avoidance

PFD1 COOLING

Features

Additional

cooling. Reducing power usage.

PFD2 COOLING

cooling. Reducing power usage.

Abnormal

Operation

MFD1 COOLING

– No Dispatch.

– PFD1 has poor

– PFD2 has poor

– MFD1 has poor

cooling. Reducing power usage.

AlertsAppendixIndex

Annun/

PFD1 KEYSTK

– PFD1 [key name]

Key is stuck.

PFD2 KEYSTK

– PFD2 [key name]

Key is stuck.

MFD1 KEYSTK

– MFD [key name]

Key is stuck.

The PFD and/or MFD has incorrect software
installed. The G1000 system should be serviced.

The PFD configuration settings do not match
backup configuration memory. The G1000
system should be serviced.

The MFD configuration settings do not match
backup configuration memory. The G1000
system should be serviced.

The MFD and PFDs have different software
versions installed. The G1000 system should be
serviced.

The MFD and/or PFDs have a software mismatch.
A red ‘X’ will appear in the CAS display. The
G1000 system should be serviced.

The PFD and/or MFD is overheating and is
reducing power consumption by dimming the
display. If problem persists, the G1000 system
should be serviced.

A key is stuck on the PFD and/or MFD bezel.
Attempt to free the stuck key by pressing it
several times. The G1000 system should be
serviced if the problem persists.

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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Annunciations & Alerts

MFD & PFD MESSAGE ADVISORIES (CONT.)

Message Comments

CNFG MODULE

configuration module is
inoperative.

PFD1 VOLTAGE

voltage. Reducing power usage

PFD2 VOLTAGE

voltage. Reducing power usage

MFD1 VOLTAGE

voltage. Reducing power usage

– PFD1

– PFD1 has low

– PFD2 has low

– MFD1 has low

The PFD1 configuration module backup memory
has failed. The G1000 system should be
serviced.

The PFD1 voltage is low. The G1000 system
should be serviced.

The PFD2 voltage is low. The G1000 system
should be serviced.

The MFD voltage is low. The G1000 system
should be serviced.

DATABASE MESSAGE ADVISORIES

Message Comments

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 aviation

– PFD1 aviation

– PFD2 aviation

The MFD and/or PFD detected a failure in
the aviation database. Attempt to reload the
aviation database. If problem persists, the
G1000 system should be serviced.

database error exists.

MFD1 DB ERR

– MFD1 basemap

database error exists.

PFD1 DB ERR

– PFD1 basemap

database error exists.

PFD2 DB ERR

– PFD2 basemap

The MFD and/or PFD detected a failure in the
basemap database.

database error exists.

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 terrain

– PFD1 terrain

– PFD2 terrain

The MFD and/or PFD detected a failure in the
terrain database. Ensure that the terrain card is
properly inserted in display. Replace terrain card.
If problem persists, The G1000 system should be
serviced.

database error exists.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

61

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEICAS

Message Comments

MFD1 DB ERR

database missing.

PFD1 DB ERR

– PFD1 terrain

database missing.

Nav/Com/

PFD2 DB ERR

XPDR/AudioAFCSGPS Nav

– PFD2 terrain

database missing.

MFD1 DB ERR

database error exists.

PFD1 DB ERR

– PFD1 obstacle

database error exists.

PFD2 DB ERR

database error exists.

Flight

PlanningProcedures

MFD1 DB ERR

– PFD2 obstacle

database missing.

PFD1 DB ERR

– PFD1 obstacle

database missing.

PFD2 DB ERR

Hazard

database missing.

Avoidance

– PFD2 obstacle

MFD1 DB ERR

terrain database error exists.

Features

Additional

PFD1 DB ERR

– PFD1 airport

terrain database error exists.

PFD2 DB ERR

Abnormal

Operation

– PFD2 airport

terrain database error exists.

MFD1 DB ERR

AlertsAppendixIndex

Annun/

terrain database missing.

PFD1 DB ERR

– PFD1 airport

terrain database missing.

PFD2 DB ERR

– PFD2 airport

terrain database missing.

– MFD1 terrain

The terrain database is present on another LRU,
but is missing on the specified LRU.

– MFD1 obstacle

The MFD and/or PFD detected a failure in the
obstacle database. Ensure that the data card is
properly inserted. Replace data card. If problem
persists, The G1000 system should be serviced.

– MFD1 obstacle

The obstacle database is present on another LRU,
but is missing on the specified LRU.

– MFD1 airport

The MFD and/or PFD detected a failure in the
airport terrain database. Ensure that the data
card is properly inserted. Replace data card. If
problem persists, The G1000 system should be
serviced.

– MFD1 airport

The airport terrain database is present on
another LRU, but is missing on the specified LRU.

62

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Message Comments

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 Safe Taxi

– PFD1 Safe Taxi

– PFD2 Safe Taxi

The MFD and/or PFD detected a failure in the
Safe Taxi database. Ensure that the data card is
properly inserted. Replace data card. If problem
persists, The G1000 system should be serviced.

database error exists.

MFD1 DB ERR

database error exists.

– MFD1 Chartview

The MFD and/or PFDs detected a failure in the
ChartView database (optional feature). Ensure
that the data card is properly inserted. Replace
data card. If problem persists, The G1000 system
should be serviced.

MFD1 DB ERR

database error exists.

– MFD1 FliteCharts

The MFD and/or PFDs detected a failure in the
FliteCharts database (optional feature). Ensure
that the data card is properly inserted. Replace
data card. If problem persists, The G1000 system
should be serviced.

DB MISMATCH

database version mismatch. Xtalk
is off.

– Aviation

The PFDs and MFD have different aviation
database versions installed. Crossfill is off.
Install correct aviation database version in all
displays.

DB MISMATCH

database type mismatch. Xtalk is
off.

– Aviation

The PFDs and MFD have different aviation
database types installed (Americas, European,
etc.). Crossfill is off. Install correct aviation
database type in all displays.

DB MISMATCH

version mismatch.

– Terrain database

The PFDs and MFD have different terrain
database versions installed. Install correct terrain
database version in all displays.

DB MISMATCH

type mismatch.

– Terrain database

The PFDs and MFD have different terrain
database types installed. Install correct terrain
database type in all displays.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

63

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEICAS

DB MISMATCH

Message Comments

– Obstacle

database version mismatch.

DB MISMATCH

database mismatch.

Nav/Com/

XPDR/AudioAFCSGPS Nav

CAS INOP

– Airport Terrain

– No Dispatch.

Database correction required.

GMA 1347D MESSAGE ADVISORIES

Flight

PlanningProcedures

GMA1 FAIL
GMA2 FAIL

GMA XTALK

Hazard

has occurred.

Avoidance

GMA1 CONFIG

Features

Additional

error. Config service req’d.

GMA2 CONFIG

error. Config service req’d.

Abnormal

Operation

Message Comments

– GMA1 is inoperative. The audio panel self-test has detected a failure.
– GMA2 is inoperative.

– GMA crosstalk error

– GMA1 config

– GMA2 config

MANIFEST – GMA1 software

mismatch, communication halted.

AlertsAppendixIndex

Annun/

MANIFEST – GMA2 software

mismatch, communication halted.

GMA1 SERVICE – GMA1 needs

service. Return unit for repair.

GMA2 SERVICE – GMA2 needs

service. Return unit for repair.

The PFDs and MFD have different obstacle
database versions installed. Install correct
obstacle database version in all displays.

The PFDs and MFD have different airport terrrain
databases installed. Install correct airport terrain
database in all displays.

The MFD and/or PFDs have an aviation database
mismatch. A red ‘X’ will appear in the CAS
display. Load the same aviation database
version in the MFD and both PFDs.

The audio panel is unavailable. The G1000
system should be serviced.

An error has occurred in transferring data
between the two GMAs. The G1000 system
should be serviced.

The audio panel configuration settings do not
match backup configuration memory. The
G1000 system should be serviced.

The audio panel has incorrect software installed. The
G1000 system should be serviced.

The audio panel self-test has detected a problem in
the unit. Certain audio functions may still be avail­able, and the audio panel may still be usable. The
G1000 system should be serviced when possible.

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES

Message Comments

GIA1 CONFIG

– GIA1 config error.

Config service req’d.

GIA2 CONFIG

– GIA2 config error.

Config service req’d.

GIA1 CONFIG

– GIA1 audio config

error. Config service req’d.

GIA2 CONFIG

– GIA2 audio config

error. Config service req’d.

GIA1 COOLING

– GIA1

temperature too low.

GIA2 COOLING

– GIA2

temperature too low.

GIA1 COOLING

– GIA1 over

temperature.

GIA2 COOLING

– GIA2 over

temperature.

GIA1 SERVICE

– GIA1 needs

service. Return the unit for repair.

GIA2 SERVICE

– GIA2 needs

service. Return the unit for repair.

HW MISMATCH

– GIA hardware
mismatch. GIA1 communication
halted.

HW MISMATCH

– GIA hardware
mismatch. GIA2 communication
halted.

MANIFEST

– GIA1 software

mismatch, communication halted.

MANIFEST

– GIA2 software

mismatch, communication halted.

The GIA1 and/or GIA2 configuration settings do
not match backup configuration memory. The
G1000 system should be serviced.

The GIA1 and/or GIA2 have an error in the audio
configuration. The G1000 system should be
serviced.

The GIA1 and/or GIA2 temperature is too low
to operate correctly. Allow units to warm up to
operating temperature.

The GIA1 and/or GIA2 temperature is too high.
If problem persists, the G1000 system should be
serviced.

The GIA1 and/or GIA2 self-test has detected a
problem in the unit. The G1000 system should
be serviced.

A GIA mismatch has been detected, where only
one is WAAS capable.

The GIA1 and/or GIA 2 has incorrect software
installed. The G1000 system should be serviced.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

65

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEICAS

COM1 TEMP

Message Comments

– COM1 over temp.

Reducing transmitter power.

COM2 TEMP

– COM2 over temp.

Reducing transmitter power.

Nav/Com/

XPDR/AudioAFCSGPS Nav

COM1 SERVICE

– COM1 needs

service. Return unit for repair.

COM2 SERVICE

– COM2 needs

service. Return unit for repair.

COM1 PTT

– COM1 push-to-talk

key is stuck.

COM2 PTT

Flight

key is stuck.

PlanningProcedures

COM1 RMT XFR

– COM2 push-to-talk

– COM1 remote

transfer key is stuck.

COM2 RMT XFR

Hazard

Avoidance

transfer key is stuck.

LOI

– GPS integrity lost. Crosscheck

Features

Additional

with other NAVS.

GPS NAV LOST

navigation. Insufficient satellites.

Abnormal

Operation

GPS NAV LOST

navigation. Position error.

AlertsAppendixIndex

Annun/

GPS NAV LOST

– COM2 remote

– Loss of GPS

– Loss of GPS

– Loss of GPS

navigation. GPS fail.

ABORT APR

– Loss of GPS

navigation. Abort approach.

APR DWNGRADE

– Approach

downgraded.

The system has detected an over temperature
condition in COM1 and/or COM2. The
transmitter is operating at reduced power. If the
problem persists, the G1000 system should be
serviced.

The system has detected a failure in COM1
and/or COM2. COM1 and/or COM2 may still be
usable. The G1000 system should be serviced
when possible.

The COM1 and/or COM2 external push-to-talk
switch is stuck in the enable (or “pressed”)
position. Press the PTT switch again to cycle its
operation.
If the problem persists, the G1000 system should
be serviced.

The COM1 and/or COM2 transfer switch is stuck
in the enabled (or “pressed”) position. Press the
transfer switch again to cycle its operation. If
the problem persists, the G1000 system should
be serviced.

GPS integrity is insufficient for the current phase
of flight.

Loss of GPS navigation due to insufficient
satellites.

Loss of GPS navigation due to position error.

Loss of GPS navigation due to GPS failure.

Abort approach due to loss of GPS navigation.

Vertical guidance generated by WAAS is
unavailable, use LNAV only minimums.

66

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Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Message Comments

TRUE APR

Change HDG reference to TRUE.

– True north approach.

Displayed after passing the first waypoint of a
true north approach when the nav angle is set
to ‘AUTO’.

GPS1 SERVICE

service. Return unit for repair.

– GPS1 needs

A failure has been detected in the GPS1
and/or GPS2 receiver. The receiver may still be

GPS2 SERVICE

– GPS2 needs

available. The G1000 system should be serviced.

service. Return unit for repair.

NAV1 SERVICE

service. Return unit for repair.

– NAV1 needs

A failure has been detected in the NAV1
and/or NAV2 receiver. The receiver may still be

NAV2 SERVICE

– NAV2 needs

available. The G1000 system should be serviced.

service. Return unit for repair.

NAV1 RMT XFR

transfer key is stuck.

NAV2 RMT XFR

transfer key is stuck.

– NAV1 remote

– NAV2 remote

The remote NAV1 and/or NAV2 transfer switch
is stuck in the enabled (or “pressed”) state.
Press the transfer switch again to cycle its
operation. If the problem persists, the G1000
system should be serviced.

G/S1 FAIL

– G/S1 is inoperative.

A failure has been detected in glideslope
receiver 1 and/or receiver 2. The G1000 system

G/S2 FAIL

– G/S2 is inoperative.

should be serviced.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

G/S1 SERVICE

– G/S1 needs

service. Return unit for repair.

G/S2 SERVICE

– G/S2 needs

service. Return unit for repair.

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

A failure has been detected in glideslope
receiver 1 and/or receiver 2. The receiver may
still be available. The G1000 system should be
serviced when possible.

67

Operation

Abnormal

Annun/

Alerts Appendix Index

Annunciations & Alerts

GEA 71 MESSAGE ADVISORIES

Flight

InstrumentsEICAS

GEA1 CONFIG

Message Comments

– GEA1 config error.

Config service req’d.

GEA2 CONFIG

Nav/Com/

Config service req’d.

XPDR/AudioAFCSGPS Nav

MANIFEST

– GEA2 config error.

– GEA1 software

mismatch, communication halted.

MANIFEST

– GEA2 software

mismatch, communication halted.

GTX 33 MESSAGE ADVISORIES

Flight

PlanningProcedures

Message Comments

XPDR1 CONFIG

– XPDR1 config

error. Config service req’d.

XPDR2 CONFIG

Hazard

Avoidance

error. Config service req’d.

MANIFEST

Features

Additional

– XPDR2 config

– GTX1 software

mismatch, communication halted.

MANIFEST

Abnormal

Operation

mismatch, communication halted.

XPDR1 SRVC

service. Return unit for repair.

AlertsAppendixIndex

Annun/

XPDR2 SRVC

– GTX2 software

– XPDR1 needs

– XPDR2 needs

service. Return unit for repair.

XPDR1 FAIL

– XPDR1 is

inoperative.

XPDR2 FAIL

– XPDR2 is

inoperative.

The GEA1 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.

The GEA2 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.

The #1 GEA 71 has incorrect software installed.
The G1000 system should be serviced.

The #2 GEA 71 has incorrect software installed.
The G1000 system should be serviced.

The transponder configuration settings do not
match those of backup configuration memory.
The G1000 system should be serviced.

The transponder configuration settings do not
match those of backup configuration memory.
The G1000 system should be serviced.

The transponder has incorrect software installed.
The G1000 system should be serviced.

The transponder has incorrect software installed.
The G1000 system should be serviced.

The #1 transponder should be serviced when
possible.

The #2 transponder should be serviced when
possible.

There is no communication with the #1
transponder.

There is no communication with the #2
transponder.

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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Annunciations & Alerts

GRS 77 MESSAGE ADVISORIES

Message Comments

AHRS1 TAS

– AHRS1 not receiving

valid airspeed.

AHRS2 TAS

– AHRS2 not receiving

valid airspeed.

AHRS1 GPS

– AHRS1 using backup

GPS source.

AHRS2 GPS

– AHRS2 using backup

GPS source.

AHRS1 GPS

– AHRS1 not receiving

any GPS information.

AHRS2 GPS

– AHRS2 not receiving

any GPS information.

AHRS1 GPS

– AHRS1 not receiving

backup GPS information.

AHRS2 GPS

– AHRS2 not receiving

backup GPS information.

AHRS1 GPS

– AHRS1 operating

exclusively in no-GPS mode.

AHRS2 GPS

– AHRS2 operating

exclusively in no-GPS mode.

AHRS MAG DB

– AHRS magnetic

model database version mismatch.

The #1 AHRS is not receiving true airspeed from
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed.
The G1000 system should be serviced.

The #2 AHRS is not receiving true airspeed from
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed.
The G1000 system should be serviced.

The #1 AHRS is using the backup GPS path.
Primary GPS path has failed. The G1000 system
should be serviced when possible.

The #2 AHRS is using the backup GPS path.
Primary GPS path has failed. The G1000 system
should be serviced when possible.

The #1 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
G1000 system should be serviced.

The #2 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
G1000 system should be serviced.

The #1 AHRS is not receiving backup GPS
information. The G1000 system should be
serviced.

The #2 AHRS is not receiving backup GPS
information. The G1000 system should be
serviced.

The #1 AHRS is operating exclusively in no-GPS
mode. The G1000 system should be serviced.

The #2 AHRS is operating exclusively in no-GPS
mode. The G1000 system should be serviced.

The #1 AHRS and #2 AHRS magnetic model
database versions do not match.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

69

Annunciations & Alerts

GRS 77 MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEICAS

AHRS1 SRVC

Message Comments

– AHRS1 Magnetic-

field model needs update.

AHRS2 SRVC

field model needs update.

Nav/Com/

XPDR/AudioAFCSGPS Nav

GEO LIMITS

– AHRS2 Magnetic-

– AHRS1 too far

North/South, no magnetic compass.

GEO LIMITS

– AHRS2 too far

North/South, no magnetic compass.

MANIFEST

– GRS1 software

mismatch, communication halted.

Flight

PlanningProcedures

MANIFEST

– GRS2 software

mismatch, communication halted.

GMU 44 MESSAGE ADVISORIES

Message Comments

Hazard

Avoidance

HDG FAULT

– AHRS1

magnetometer fault has occurred.

Features

Additional

HDG FAULT

magnetometer fault has occurred.

Abnormal

Operation

AlertsAppendixIndex

Annun/

MANIFEST

– AHRS2

– GMU1 software

mismatch, communication halted.

MANIFEST

– GMU2 software

mismatch, communication halted.

The #1 AHRS earth magnetic field model is out
of date. Update magnetic field model when
practical.

The #2 AHRS earth magnetic field model is out
of date. Update magnetic field model when
practical.

The aircraft is outside geographical limits for
approved AHRS operation. Heading is flagged
as invalid.

The #1 AHRS has incorrect software installed.
The G1000 system should be serviced.

The #2 AHRS has incorrect software installed.
The G1000 system should be serviced.

A fault has occurred in the #1 GMU 44.
Heading is flagged as invalid. The AHRS uses
GPS for backup mode operation. The G1000
system should be serviced.

A fault has occurred in the #2 GMU 44.
Heading is flagged as invalid. The AHRS uses
GPS for backup mode operation. The G1000
system should be serviced.

The GMU 44 has incorrect software installed.
The G1000 system should be serviced.

70

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190-00600-02 Rev. A

Annunciations & Alerts

GDL 69A MESSAGE ADVISORIES

Message Comments

GDL69 CONFIG

– GDL 69 config

error. Config service req’d.

GDL69 FAIL

MANIFEST

– GDL 69 has failed. A failure has been detected in the GDL 69.

– GDL software

mismatch, communication halted.

GWX 68 ALERT MESSAGES

Message Comments

GWX CONFIG

– GWX config error.

Config service req’d.

GWX FAIL

GWX SERVICE

– GWX is inoperative. The GDU is not recieving status packet from the

– GWX needs

service. Return unit for repair.

MANIFEST

– GWX software

mismatch, communication halted.

WX ALERT

– Possible severe

weather ahead.

GDL 69 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.

The receiver is unavailable. The G1000 system
should be serviced

The GDL 69 has incorrect software installed.
The G1000 system should be serviced.

GWX 68 configuration settings do not match
those of the GDU configuration. The G1000
system should be serviced.

GWX 68 or the GWX 68 is reporting a fault.
The GWX 68 radar system should be serviced.

A failure has been detected in the GWX 68. The
GWX 68 may still be usable.

The GWX 68 has incorrect software installed.
The G1000 system should be serviced.

Possible severe weather detected within +/- 10
degrees of the aircraft heading at a range of 80
to 320 nm.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

71

Annunciations & Alerts

GDC 74B MESSAGE ADVISORIES

Flight

InstrumentsEICAS

ADC1 ALT EC

Message Comments

– ADC1 altitude error

correction is unavailable.

ADC2 ALT EC

– ADC2 altitude error

correction is unavailable.

Nav/Com/

ADC1 AS EC

XPDR/AudioAFCSGPS Nav

– ADC1 airspeed error

correction is unavailable.

ADC2 AS EC

– ADC2 airspeed error

correction is unavailable.

MANIFEST

– GDC1 software

mismatch, communication halted.

MANIFEST

mismatch, communication halted.

Flight

PlanningProcedures

– GDC2 software

GCU 475 MESSAGE ADVISORIES

Message Comments

GCU CNFG

Config service req’d.

Hazard

Avoidance

GCU FAIL

Features

Additional

MANIFEST

– GCU Config error.

– GCU is inoperative. A failure has been detected in the GCU 475.

– GCU software

mismatch, communication halted.

Abnormal

Operation

GCU KEYSTK

– GCU [key name]

Key is stuck.

AlertsAppendixIndex

Annun/

GDC1 or GDC2 is reporting that the altitude
error correction is unavailable.

GDC1 or GDC2 is reporting that the airspeed
error correction is unavailable.

The GDC 74B has incorrect software installed.
The G1000 system should be serviced.

GCU 475 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.

The GCU 475 is unavailable.
The GCU 475 has incorrect software installed.

The G1000 system should be serviced.
A key is stuck on the GCU 475 bezel. Attempt

to free the stuck key by pressing it several times.
The G1000 system should be serviced if the
problem persists.

72

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Annunciations & Alerts

GMC 710 MESSAGE ADVISORIES

Message Comments

GMC CONFIG

Config service req’d.

GMC FAIL

– GMC Config error.

Error in the configuration of the GMC 710.

– GMC is inoperative. A failure has been detected in the GMC 710.

The GMC 710 is unavailable.

MANIFEST

mismatch. Communication halted.

GMC KEYSTK

Key is stuck.

– GMC software

– GMC [key name]

The GMC 710 has incorrect software installed.
The G1000 system should be serviced.

A key is stuck on the GMC 710 bezel. Attempt
to free the stuck key by pressing it several
times. The G1000 system should be serviced if
the problem persists.

MISCELLANEOUS MESSAGE ADVISORIES

Message Comments

FPL WPT LOCK

waypoint is locked.

– Flight plan

Upon power-up, the G1000 system detects
that a stored flight plan waypoint is locked.
This occurs when an aviation database update
eliminates an obsolete waypoint. The flight
plan cannot find the specified waypoint and
flags this message. This can also occur with
user waypoints in a flight plan that is deleted.

Remove the waypoint from the flight plan if it
no longer exists in any database,
Or
update the waypoint name/identifier to reflect
the new information.

FPL WPT MOVE

waypoint moved.

– Flight plan

The system has detected that a waypoint
coordinate has changed due to a new aviation
database update. Verify that stored flight plans
contain correct waypoint locations.

TIMER EXPIRD

– Timer has expired. The system notifies the pilot that the timer has

expired.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

73

Annunciations & Alerts

MISCELLANEOUS MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEICAS

DB CHANGE

Message Comments

– Database changed.

Verify user modified procedures.

Nav/Com/

XPDR/AudioAFCSGPS Nav

DB CHANGE

– Database changed.

Verify stored airways.

FPL TRUNC

Flight

PlanningProcedures

truncated.

Hazard

LOCKED FPL

Avoidance

– Flight plan has been

– Cannot navigate

locked flight plan.

Features

Additional

WPT ARRIVAL

waypoint -[xxxx]

Abnormal

Operation

STEEP TURN

AlertsAppendixIndex

Annun/

INSIDE ARSPC
ARSPC AHEAD

– Arriving at

– Steep turn ahead. A steep turn is 15 seconds ahead. Prepare to

– Inside airspace. The aircraft is inside the airspace.

– Airspace ahead

less than 10 minutes.

ARSPC NEAR

– Airspace near and

ahead.

This occurs when a stored flight plan contains
procedures that have been manually edited.
This alert is issued only after an aviation
database update. Verify that the user-modified
procedures in stored flight plans are correct and
up to date.

This occurs when a stored flight plan contains
an airway that is no longer consistent with
the aviation database. This alert is issued only
after an aviation database update. Verify use
of airways in stored flight plans and reload
airways as needed.

This occurs when a newly installed aviation
database eliminates an obsolete approach
or arrival used by a stored flight plan. The
obsolete procedure is removed from the flight
plan. Update flight plan with current arrival or
approach.

This occurs when the pilot attempts to activate
a stored flight plan that contains locked
waypoint. Remove locked waypoint from flight
plan. Update flight plan with current waypoint.

Arriving at waypoint [xxxx], where [xxxx] is the
waypoint name.

turn.

Special use airspace is ahead of aircraft. The
aircraft will penetrate the airspace within 10
minutes.

Special use airspace is near and ahead of the
aircraft position.

74

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Annunciations & Alerts

MISCELLANEOUS MESSAGE ADVISORIES (CONT.)

Message Comments

ARSPC NEAR

than 2 nm.

APR INACTV

active.

– Airspace near – less

– Approach is not

Special use airspace is within 2 nm of the
aircraft position.

The system notifies the pilot that the loaded
approach is not active. Activate approach
when required.

SLCT FREQ

frequency for approach.

– Select appropriate

The system notifies the pilot to load the
approach frequency for the appropriate NAV
receiver. Select the correct frequency for the
approach.

SLCT NAV

approach.

– Select NAV on CDI for

The system notifies the pilot to set the CDI to
the correct NAV receiver. Set the CDI to the
correct NAV receiver.

PTK FAIL

bad geometry.

PTK FAIL

invalid leg type.

PTK FAIL

past IAF.

UNABLE V WPT

current vertical waypoint.

– Parallel track unavailable:

– Parallel track unavailable:

– Parallel track unavailable:

– Can’t reach

Bad parallel track geometry.

Invalid leg type for parallel offset.

IAF waypoint for parallel offset has been
passed.

The current vertical waypoint can not be
reached within the maximum flight path angle
and vertical speed constraints. The system
automatically transitions to the next vertical
waypoint.

VNV

– Unavailable. Unsupported

leg type in flight plan.

The lateral flight plan contains a procedure
turn, vector, or other unsupported leg type
prior to the active vertical waypoint. This
prevents vertical guidance to the active vertical
waypoint.

VNV

– Unavailable. Excessive track

angle error.

VNV

– Unavailable. Excessive

crosstrack error.

The current track angle error exceeds the limit,
causing the vertical deviation to go invalid.

The current crosstrack exceeds the limit,
causing vertical deviation to go invalid.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

75

Annunciations & Alerts

MISCELLANEOUS MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEICAS

VNV

– Unavailable. Parallel course

Message Comments

selected.

NO WGS84 WPT

– Non WGS 84

waypoint for navigation -[xxxx]

Nav/Com/

XPDR/AudioAFCSGPS Nav

TRAFFIC FAIL

– Traffic device has

failed.

FAILED PATH

– A data path has

failed.

MAG VAR WARN

– Large magnetic

variance. Verify all course angles.

Flight

PlanningProcedures

SVS

– SVS DISABLED: Out of

available terrain region.

Hazard

Avoidance

SVS

– SVS DISABLED: Terrain DB

resolution too low.

Features

Additional

SCHEDULER [#]

– <message>. Message criteria entered by the user.

A parallel course has been selected, causing
the vertical deviation to go invalid.

The selected waypoint [xxxx] does not use the
WGS 84 datum. Cross-check position with
alternate navigation sources.

The G1000 is no longer receiving data from
the traffic system. The traffic device should be
serviced.

A data path connected to the GDU or the GIA
63/W has failed.

The GDU’s internal model cannot determine
the exact magnetic variance for geographic
locations near the magnetic poles. Displayed
magnetic course angles may differ from the
actual magnetic heading by more than 2°.

Synthetic Vision is disabled because the aircraft
is not within the boundaries of the installed
terrain database.

Synthetic Vision is disabled because a terrain
database of sufficient resolution (9 arc-second
or better) is not currently installed.

Abnormal

Operation

AlertsAppendixIndex

Annun/

76

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

PFD SOFTKEY MAP

Select the BACK or OFF Softkey
to return to the top-level softkeys.

TRFC-1

TRFC-2

APPENDIX

Top Level PFD Softkeys

Appendix

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

INSET

OFF

DCLTR (3)

190-00600-02 Rev. A

Inset Map Softkeys

Displays Inset Map in PFD lower left corner

Removes Inset Map

Selects desired amount of map detail; cycles
through declutter levels:

DCLTR (No Declutter): All map features

visible
DCLTR-1: Declutters land data
DCLTR-2: Declutters land and SUA data
DCLTR-3: Removes everything except the

active flight plan

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

77

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Appendix

Select the BACK Softkey to
return to the top level softkeys.

BACK

MSG

ADC2

ADC1

AHRS1

AHRS2

Flight

InstrumentsEICAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

TRAFFIC

TOPO

TERRAIN

NEXRAD

XM LTNG

Cycles through traffic display options:

TRFC-1: Traffic displayed on inset map
TRFC-2: Traffic Map Page is displayed in

the inset map window

Displays topographical data (e.g., coast­lines, terrain, rivers, lakes) and elevation
scale on Inset Map

Displays terrain information on Inset Map

Displays NEXRAD weather and coverage
information on Inset Map (optional feature)

Displays XM lightning information on Inset
Map (optional feature)

Sensor Softkeys

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

SENSOR

78

Displays softkeys for selecting the #1 and
#2 AHRS and Air Data Computers

ADC1

ADC2

AHRS1

AHRS2

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Selects the #1 Air Data Computer

Selects the #2 Air Data Computer

Selects the #1 AHRS

Selects the #2 AHRS

190-00600-02 Rev. A

PFD Configuration Softkeys

Select the STD BARO or
BACK Softkey to return to

the top-level softkeys

ALT UNI T

METERS IN HPA

SYN VIS

SYN TERR

HRZN HDG

PATHWAY

APTSIGNS

Appendix

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

PFD

190-00600-02 Rev. A

SYN VIS

DFLTS

Displays second-level softkeys for

additional PFD configurations

Displays the softkeys for enabling or

disabling Synthetic Vision features

PATHWAY

Displays rectangular boxes representing

the horizontal and vertical flight path of

the active flight plan

SYN TERR

HRZN HDG

Enables synthetic terrain depiction

Displays compass heading along the

Zero-Pitch line

APTSIGNS

Displays position markers for airports

within approximately 15 nm of the

current aircraft position. Airport

identifiers are displayed when the

airport is within approximately 9 nm.

Resets PFD to default settings, including

changing units to standard

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

79

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Appendix

Flight

InstrumentsEICAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

WIND

DME

BRG1

BRG2

ALT UNIT

OPTN 1

OPTN 2

OPTN 3

OFF

METERS

IN

Displays softkeys to select wind data
parameters

Wind direction arrows with headwind
and crosswind components

Wind direction arrow and speed

Wind direction arrow with direction
and speed

Information not displayed

Select to display the DME information
window

Cycles the Bearing 1 Information
Window through NAV1 or GPS/
waypoint identifier and GPS-derived

distance information.

Cycles the Bearing 2 Information
Window through NAV2 or GPS/
waypoint identifier and GPS-derived

distance information.

Displays softkeys for setting the
altimeter and BARO settings to metric
units

When enabled, displays altimeter in
meters

Select to display the BARO setting as
inches of mercury

Abnormal

Operation

AlertsAppendixIndex

Annun/

80

HPA

Select to display the BARO setting as
hectopacals

STD BARO

Sets altimeter setting to standard
barometric pressure

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-02 Rev. A

Transponder Softkeys

Select the BACK Softkey to return
to the top-level softkeys.

Select the BACK Softkey to return
to the top-level softkeys.

MSG

MSG

Appendix

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

ADF/DME

XPDR

STBY

ON

ALT

GND

VFR

CODE

0 — 7

BKSP

Displays the ADF/DME Tuning Window

Displays transponder mode selection
softkeys

Selects Standby Mode (transponder does
not reply to any interrogations)

Selects Mode A (transponder replies to
interrogations)

Selects Mode C – Altitude Reporting Mode
(transponder replies to identification and
altitude interrogations)

Manually selects Ground Mode, the
transponder does not allow Mode A
and Mode C replies, but it does permit
acquisition squitter and replies to discretely
addressed Mode S interrogations.

Automatically enters the VFR code (1200 in
the U.S.A. only)

Displays transponder code selection
softkeys 0-7

Use numbers to enter code

Removes numbers entered, one at a time

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

81

Appendix

MAP

DCLTR

TRAFFIC

TOPO

BACK

TERRAIN

DCLTR-2

DCLTR-3

DCLTR-1

Select the BACK Softkey on this level to
return to the top softkey level.

NEXRAD

XM LTNG

(optional)(optional)

CAS ↓

CAS ↑

SHW CHRT

CHKLIST

(optional)(optional)

AIRWAYS

AIRWY LO

AIRWAY HI

AIRWY ON

IDENT

Flight

InstrumentsEICAS

TMR/REF

NRST

MSG

Nav/Com/

XPDR/AudioAFCSGPS Nav

MFD SOFTKEY MAP

Flight

PlanningProcedures

Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen

Displays Timer/References Window

Displays Nearest Airports Window

Displays Message Window

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

CAS ↑

CAS ↓

MAP

82

MFD Softkeys

Scroll up (Displayed only when a sufficient
number of items are displayed in the Crew
Alerting System Display to warrant scrolling)

Scroll down (Displayed only when a sufficient
number of items are displayed in the Crew Alert­ing System Display to warrant scrolling)

Enables second-level Navigation Map softkeys

TRAFFIC

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Displays traffic information on Navigation Map

190-00600-02 Rev. A

Appendix

DCLTR (3)

SHW CHRT

CHKLIST

TOPO

TERRAIN

AIRWAYS

NEXRAD

XM LTNG

BACK

Displays topographical data (e.g., coastlines,
terrain, rivers, lakes) and elevation scale on
Navigation Map

Displays terrain information on Navigation Map

Displays airways on the map; cycles through the
following:
AIRWAYS: No airways are displayed
AIRWY ON: All airways are displayed
AIRWY LO: Only low altitude airways are
displayed
AIRWY HI: Only high altitude airways are
displayed

Displays NEXRAD weather and coverage
information on Navigation Map (optional feature)

Displays XM lightning information on Navigation
Map (optional feature)

Returns to top-level softkeys

Selects desired amount of map detail; cycles
through declutter levels:

DCLTR (No Declutter): All map features visible
DCLTR-1: Declutters land data
DCLTR-2: Declutters land and SUA data
DCLTR-3: Removes everything except the active

flight plan

When available, displays optional airport and
terminal procedure charts

When available, displays optional checklists

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

190-00600-02 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

83

Alerts Appendix Index

Annun/

Appendix

Flight

InstrumentsEICAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

84

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190-00600-02 Rev. A