Garmin Cessna Citation Mustang Reference Guide

®

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 © 2006-2010 Garmin Ltd. or its subsidiaries. All rights reserved.

This manual reflects the operation of System Software version 0435.20 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]

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Southampton, SO40 9RB, U.K.
Tel: [phone] Fax: [phone]

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

For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount
and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836.

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® is a registered trademark 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.; and XM® is a registered trademark of
XM Satellite Radio, Inc.; Honeywell® and Bendix/King® are registered trademarks of Honeywell
International, Inc.; CO Guardian is a trademark of CO Guardian, Inc.

June, 2010 190-00600-03 Rev. A Printed in the U.S.A.

Warnings, Cautions & Notes

WARNING: Navigation and terrain separation must NOT be predicated upon
the use of the terrain avoidance feature. The terrain avoidance feature is NOT
intended to be used as a primary reference for terrain avoidance and does
not relieve the pilot from the responsibility of being aware of surroundings
during flight. The terrain avoidance 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 the 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 the aircraft. GPS altitude should never be used for vertical
navigation. Always use pressure altitude displayed by the PFD or other
pressure altimeters in aircraft.

WARNING: Do not use outdated database information. Databases used in
the 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 system displays is provided as an
aid in visually acquiring traffic. Pilots must maneuver the aircraft based upon
TCAS II Resolution Advisories (if installed), 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

190-00600-03 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 G1000 Integrated Flight Deck, 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 self­test 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 system. 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, system 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 system utilize GPS as a
precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs,
information presented by the system 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 system 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 system 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.”

190-00600-03 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 variation in the earth’s magnetic field, operating the
system within the following areas could result in loss of reliable attitude and
heading indications. North of 72° North latitude at all longitudes. South of
70° South latitude at all longitudes. North of 65° North latitude between
longitude 75° W and 120° W. (Northern Canada). North of 70° North latitude
between longitude 70° W and 128° W. (Northern Canada). North of 70° North
latitude between longitude 85° E and 114° E. (Northern Russia). South of
55° South latitude between longitude 120° E and 165° E. (Region south of
Australia and New Zealand).

WARNING: Do not use GPS to navigate to any active waypoint identified as
a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are
derived from an unknown map reference datum that may be incompatible
with the map reference datum used by GPS (known as WGS84) and may be
positioned in error as displayed.

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 system 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 panel and displays, are subject to change and may not reflect
the most current system and databases. Depictions of equipment may differ
slightly from the actual equipment.

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Warnings, Cautions & Notes

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.

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.

NOTE: The purpose of this Cockpit Reference Guide is to provide the pilot
a resource with which to find operating instructions on the major features
of the G1000 system more easily. It is not intended to be a comprehensive
operating guide. Complete operating procedures for the system are found
in the G1000 Integrated Flight Deck Pilot’s Guide.

190-00600-03 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Warnings, Cautions & Notes

Blank Page

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 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

Rev A Added Synthetic Vision

Added other GDU 9.01 parameters

190-00600-03 Added GDU 10.01 parameters

Added GSD 41
Added GMA -20
Added new page navigation
TCAS II
Radar Altimeter
Added AOPA Airport Directory
Added dual navigation database capability
Added database synchronization

Revision Date of Revision Affected Pages Description

A June, 2010 All Production release

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Record of Revisions

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190-00600-03 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/Radar Altimeter (RA Optional) 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

Select Transponder Mode ....................................................................................................... 8

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

Selecting a NAV Radio ............................................................................................................. 9

NAV/COM Tuning ....................................................................................................................... 9

Intercom System (ICS) Isolation .......................................................................................... 10

Passenger Address (PA) System ........................................................................................... 10

Clearance Recorder and Player ...........................................................................................11

AUTOMATIC FLIGHT CONTROL SYSTEM .......................................................................... 13

Flight Director Activation ..................................................................................................... 13

Vertical Modes ......................................................................................................................... 14

Lateral Modes .......................................................................................................................... 15

GPS NAVIGATION ........................................................................................................................ 17

Direct-to Navigation .............................................................................................................. 17

Activate a Stored Flight Plan ............................................................................................... 18

Activate a Flight Plan Leg ..................................................................................................... 18

Stop Navigating a Flight Plan .............................................................................................. 19

Vertical Navigation (VNAV)................................................................................................... 19

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Table of Contents

FLIGHT PLANNING ...................................................................................................................... 21

Weight Planning ...................................................................................................................... 21

Trip Planning ............................................................................................................................ 21

Create a New User Waypoint Defined by Latitude & Longitude ................................. 23

Create a New User Waypoint Defined by Radials from Other Waypoints ................. 24

Create a New User Waypoint Defined by a Radial & Distance from Another

Waypoint ............................................................................................................................. 26

Delete a User Waypoint ......................................................................................................... 27

Create a New Flight Plan ...................................................................................................... 28

Import a Flight Plan from an SD Card ................................................................................ 29

Insert a Waypoint in the Active Flight Plan ...................................................................... 29

Enter an Airway in a Flight Plan .......................................................................................... 30

Invert An Active Flight Plan .................................................................................................. 31

Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 31

Store a Flight Plan .................................................................................................................. 32

Edit a Stored Flight Plan ....................................................................................................... 32

Delete a Waypoint from the Flight Plan ............................................................................ 32

Invert and Activate a Stored Flight Plan ........................................................................... 33

Copy a Flight Plan ................................................................................................................... 33

Delete a Flight Plan ................................................................................................................ 33

Graphical Flight Plan Creation ............................................................................................. 34

Export a Flight Plan to an SD Card ..................................................................................... 34

PROCEDURES ................................................................................................................................. 35

Load and Activate a Departure Procedure ....................................................................... 35

Activate A Departure Leg ..................................................................................................... 35

Load An Arrival Procedure .................................................................................................... 35

Activate An Arrival Leg ......................................................................................................... 36

Load and/or Activate an Approach Procedure ................................................................. 36

Activate An Approach in the Active Flight Plan ............................................................... 37

Activate a Vector to Final Approach Fix ............................................................................ 37

Activate A Missed Approach in the Active Flight Plan ................................................... 38

HAZARD AVOIDANCE ................................................................................................................39

Customizing the Hazard Displays on the Navigation Map ............................................ 39

XM Weather (Subscription Optional) ................................................................................. 39

Traffic Systems ........................................................................................................................ 41

Terrain Awareness & Warning System (TAWS-B).............................................................. 45

Airborne Color Weather Radar ............................................................................................ 47

ADDITIONAL FEATURES ........................................................................................................... 51

Synthetic Vision (Optional) ................................................................................................... 51

Terminal Procedure Charts ...................................................................................................53

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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Table of Contents

AOPA Airport Directory ......................................................................................................... 55

XM® Radio Entertainment (Subscription Optional) ........................................................ 55

ABNORMAL OPERATION..........................................................................................................59

Reversionary Mode ................................................................................................................ 59

Abnormal COM Operation .................................................................................................... 59

Audio Panel Fail-safe Operation.......................................................................................... 59

Hazard Displays with Loss of GPS Position ....................................................................... 60

Unusual Attitudes ................................................................................................................... 60

Dead Reckoning ...................................................................................................................... 61

ANNUNCIATIONS & ALERTS ................................................................................................... 63

CAS Messages .......................................................................................................................... 63

Comparator Annunciations ................................................................................................... 65

Reversionary Sensor Annunciations ................................................................................... 66

TAWS-B Alerts .......................................................................................................................... 67

TCAS II Alerts and Annunciations ........................................................................................ 68

Aural Alerts .............................................................................................................................. 70

Flight Plan Import/Export Messages .................................................................................. 70

MFD & PFD Message Advisories .......................................................................................... 72

Database Message Advisories ............................................................................................. 73

GMA 1347D/1347D-20 Message Advisories ....................................................................... 76

GIA 63W Message Advisories ............................................................................................... 77

GSD 41 Message Advisories.................................................................................................. 79

GEA 71 Message Advisories .................................................................................................. 80

GTX 33/33D Message Advisories .......................................................................................... 80

GRS 77 Message Advisories .................................................................................................. 81

GMU 44 Message Advisories ................................................................................................ 82

GDL 69A Message Advisories ............................................................................................... 83

GWX 68 Alert Messages ......................................................................................................... 83

GDC 74B Message Advisories ............................................................................................... 84

GCU 475 Message Advisories ............................................................................................... 84

GMC 710 Message Advisories .............................................................................................. 85

Miscellaneous Message Advisories ..................................................................................... 85

APPENDIX ....................................................................................................................................... 91

PFD Softkey Map .................................................................................................................... 91

MFD Softkey Map ................................................................................................................... 99

Database Updates ................................................................................................................ 101

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

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Table of Contents

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 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)

Press the PFD Softkey to display the second-level softkeys.

2)

Press the ALT UNIT Softkey.

3)

Press the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).

Or

:

Press the HPA Softkey to display the barometric pressure setting in
hectopascals.

4)

Press 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

FMS Knob clockwise to ON or counterclockwise to OFF.

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

190-00600-03 Rev. A 1

small

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

Flight Instruments

CHANGE NAVIGATION SOURCES

Flight

InstrumentsEICAS

1)

Press 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)

Press 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)

Press the CDI Softkey a third time to return to GPS.

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

1)

Press the OBS Softkey to select OBS Mode.

2)

Turn the CRS Knob to select the desired course to/from the waypoint. Press
the CRS Knob to slew the CDI Course Pointer to a course bearing directly
to the waypoint.

Flight

PlanningProcedures

3)

Press the OBS Softkey again to disable OBS Mode.

GENERIC TIMER

1)

Press 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)

Press 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

190-00600-03 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/RADAR ALTIMETER (RA OPTIONAL) MINIMUM DESCENT

ALTITUDE

1)

Press the TMR/REF Softkey.

2)

Turn the large FMS Knob to highlight the OFF/BARO/RAD ALT field to the
right of ‘MINIMUMS’.

3)

Turn the small FMS Knob clockwise to select BARO or RAD ALT.

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)

Press the PFD Softkey.

2)

Press the WIND Softkey to display wind data below the Selected Heading.

3)

Press one of the OPTN softkeys to change how wind data is displayed.

4)

To remove the Wind Data Window, press the OFF Softkey.

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Operation

Abnormal

Annun/

Alerts Appendix Index

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

190-00600-03 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

Avoidance

4

9

3

7

Hazard

Additional

Features

10

8

10

EICAS Display (Normal Mode)

1

Engine Fan Rotation
Speed

2

Oil Pressure & Speed

5

Interstage Turbine
Temperature

6

Engine High Pressure

EIS Display (Reversionary Mode)

8

Cabin Pressure Altitude
and Change Rate

9

Trim Indicator

Turbine Rotation

3

Fuel Display

4

CAS Display

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Speed

7

Electrical Display

10

Flap Indicator

Operation

Abnormal

Annun/

Alerts Appendix Index

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 ap-

pears on the display along with the flight instruments and EIS.

Flight

PlanningProcedures

CAS Display

Hazard

Avoidance

Features

Additional

CAS MESSAGES AND PRIORITIZATION

Abnormal

Operation

NOTE: Information on CAS messages in this pilot’s guide is always superseded

AlertsAppendixIndex

Annun/

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

CAS Window

Reversionary ModeNormal Mode

CAS Messages

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 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 to update the Flight ID.

ADF TUNING (OPTIONAL)

Nav/Com/XPDR/Audio Panel

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

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.

DME TUNING

1)

Press the ADF/DME Softkey.

2)

If two DMEs are installed, 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.

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Nav/Com/XPDR/Audio Panel

ENTER A TRANSPONDER CODE

Flight

InstrumentsEICAS

1)

Press the XPDR Softkey (XPDR/TFC if the TCAS II option is available).

2)

Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.

3)

Press the digit softkeys to enter the code in the code field. When entering
the code, the next key in sequence must be pressed within 10 seconds, or

Nav/Com/

XPDR/AudioAFCSGPS Nav

the entry is cancelled and restored to the previous code. Five seconds after
the fourth digit has been entered, the transponder code becomes active.

SELECT TRANSPONDER MODE

With TCAS II Option

1)

Press the XPDR/TFC Softkey.

2)

Press the MODE Softkey to display the transponder mode selection

Flight

PlanningProcedures

softkeys.

3)

Press the desired transponder mode softkey (STBY, ON, or ALT ).

Without TCAS II Option

1)

Press the XPDR Softkey.

2)

Hazard

Avoidance

If the aircraft is equipped with two transponders, press the XPDR1 or
XPDR2 Softkey to select the active transponder.

3)

Press the desired transponder mode softkey (STBY, ON, ALT, or GND).

Features

Additional

SELECTING A COM RADIO

Transmit/Receive

Abnormal

Operation

AlertsAppendixIndex

Annun/

Receive Only

8

Press the COM1 MIC, COM2 MIC

, or

COM3 MIC Key (HF, if installed) on

the audio panel.

Press the COM1, COM2

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

, or

COM3 Key (HF, if installed) on the audio panel.

190-00600-03 Rev. A

Nav/Com/XPDR/Audio Panel

SELECTING A NAV RADIO

1)

To begin navigating using a navigation radio, press the CDI Softkey on the
PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).

2)

Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or
deselect the navigation radio audio source. All radio keys can be selected
individually or together.

NAV/COM TUNING

1)

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.

2)

Press the appropriate Frequency Transfer Key to place the frequency into
the active frequency field.

Or

:

1)

Press the COM or NAV Key on the MFD/PFD Control Unit to select the
desired COM or NAV frequency box.

2)

Turn the FMS Knob to tune the desired frequency (large knob for MHz;
small knob for kHz).

3)

Press the

Frequency Transfer

Key to transfer the frequency to the active field.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

190-00600-03 Rev. A 9

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Nav/Com/XPDR/Audio Panel

INTERCOM SYSTEM (ICS) ISOLATION

Flight

Pressing the INTR COM Key on either Audio Panel selects and deselects the

InstrumentsEICAS

intercom on both Audio Panels. The annunciator is lit when the intercom is active.
The intercom connects the pilot and copilot together. Either the pilot or copilot may
select or deselect the intercom.

The MAN SQ Key allows either automatic or manual control of the intercom
squelch setting. Pressing the MAN SQ Key enables manual squelch control, indicated
by the MAN SQ annunciator.

Nav/Com/

XPDR/AudioAFCSGPS Nav

• WhentheMANSQAnnunciatorisextinguished(AutomaticSquelchison),

the ICS Knob controls only the volume (pressing the ICS Knob has no effect on the
VOL/SQ selection).

• Whenthe MANSQAnnunciatorisilluminated (Manual Squelch),theICS
Knob controls either volume or squelch (selected by pressing the ICS Knob and
indicated by the VOL or SQ annunciation).

Cabin Address (GMA 1347D-20 only)

Flight

PlanningProcedures

The CABIN Key initiates two way communication between the pilot or copilot and
the passengers in the cabin. The annunciator is lit when the cabin intercom is active
on either Audio Panel.

When the flight crew wants to communicate with the passengers, the pilot or
copilot presses the CABIN Key to signal that communication is desired. The cabin
signal must be acknowledged to begin intercom conversation.

Hazard

Avoidance

When the passengers want to communicate with the pilot/copilot, they press the
“COCKPIT CALL” switch at their seat in the cabin. The CABIN annunciator flashes on
both Audio Panels to signal the pilot and copilot that cabin communication is desired.

Features

Additional

The cockpit call signal must be acknowledged by pressing the CABIN Key to begin
intercom conversation.

Abnormal

Operation

PASSENGER ADDRESS (PA) SYSTEM

A passenger address system is provided by pressing the PA Key to deliver messages

AlertsAppendixIndex

Annun/

to the passengers. The message is heard by the other pilot on the cockpit speaker
(if selected on) or on the headset if the PA Key is enabled on both audio panels. PA
messages are one way from the flight deck to the passengers.

10

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Nav/Com/XPDR/Audio Panel

CLEARANCE RECORDER AND PLAYER

GMA 1347D

NOTE: Only the audio for the selected
not recorded for COM3 MIC.

Record

1)

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
previously recorded block.

Each subsequent two presses will skip back to

the previously recorded block.

GMA 1347D-20

COM MIC

Key is recorded. Audio is

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio

to the Pilot. Pressing the play key on the Copilot’s Audio Panel plays recorded
audio to the Copilot.

COM audio is recorded automatically. Recorded audio is stored in separate memory
blocks. Once 2.5 minutes of recording time have been reached, the recorder begins
recording over the stored memory blocks, starting from the oldest block.

The PLAY Key controls the play function. The PLAY annunciator is illuminated to

indicatewhenplayisinprogress.ThePLAYannunciatorextinguishesafterplayback

is finished.

Pressing the PLAY Key once plays the latest recorded memory block and then
returns to normal operation. Pressing the PLAY Key again during play of a memory
block stops play. If a COM input signal is detected during play of a recorded memory
block, play is halted.

190-00600-03 Rev. A 11

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Nav/Com/XPDR/Audio Panel

Pressing the PLAY Key twice within one-half second while audio is playing plays

the previous block of recorded audio. Each subsequent two presses of the PLAY Key

Flight

InstrumentsEICAS

within one-half second backtracks through the recorded memory blocks to reach and
play any recorded block.

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

12

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 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

Takeoff (on ground)

Go Around

TOGATakeoff (on ground)

Go Around

TO

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

190-00600-03 Rev. A 13

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

AFCS

VERTICAL MODES

Flight

InstrumentsEICAS

Vertical Mode Description Control Annunciation

Holds the current aircraft pitch attitude;

Pitch Hold

Nav/Com/

Selected Altitude

XPDR/AudioAFCSGPS Nav

Armed

Altitude Hold Holds the current Altitude Reference A LT Key A LT nnnnn f T

Vertical Speed

Flight Level Change,
IAS Hold

Flight

PlanningProcedures

Flight Level Change,
Mach Hold

VNAV

Hazard

VNAV Target

Avoidance

Altitude Armed

Features

Additional

Glidepath

Glideslope

Abnormal

Operation

Takeoff

AlertsAppendixIndex

Annun/

Go Around

* 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

Commands a constant pitch angle
and wings level on the ground in
preparation for takeoff

Disengages the autopilot and
commands a constant pitch angle and
wings level in the air

(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

TO

GA

14

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

AFCS

LATERAL MODES

Instruments EICAS

Flight

Lateral Mode Description Control Annunciation

Holds current aircraft roll attitude

Roll Hold

or rolls wings level, depending on

(default) ROL

commanded bank angle

XPDR/Audio AFCS GPS Nav

Low Bank Limits maximum commanded roll angle

Heading Select Captures and tracks Selected Heading

Navigation, GPS
Arm/Capture/Track

BANK

Key

HDG

Key

*

HDG

GPS

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

Captures and tracks a localizer signal
for backcourse approaches

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

BC Key BC

VAPP

APR Key

GPS

LOC

Avoidance

Hazard

Additional

Features

Operation

Abnormal

automatically armed)

Annun/

Alerts Appendix Index

Takeoff

Go Around

Commands a constant pitch angle
and wings level on the ground in
preparation for takeoff

Disengages the autopilot and
commands a constant pitch angle and

TO

GA

Switch

GA

wings level in the air

* 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.

190-00600-03 Rev. A 15

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Flight

InstrumentsEICAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

AFCS

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

16

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 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 counterclockwise 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 or MFD Controller.

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 counterclockwise to place the cursor over the
‘ALT’ altitude field.

190-00600-03 Rev. A 17

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

( )

on the PFD.

Operation

Abnormal

Annun/

Alerts Appendix Index

GPS Navigation

7)

Turn the small FMS Knob to enter the desired altitude constraint.

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 offset distance (-) 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 on the MFD, or MFD Controller, 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.

18

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 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

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

190-00600-03 Rev. A 19

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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 are designated for use in vertical navigation may also be made “non­designated” 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 re-calculations

Nav/Com/

XPDR/AudioAFCSGPS Nav

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.

20

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

FLIGHT PLANNING

WEIGHT PLANNING

All procedures apply to the MFD unless otherwise stated.

Flight Planning

Instruments EICAS

Flight

Entering Weight Parameters

Turn the large

FMS

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

Knob to select the Weight Planning Page.

1)

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

TRIP PLANNING

FMS

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

1)

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

2)

Turn the small FMS Knob to select the Trip Planning Page.

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.

190-00600-03 Rev. A 21

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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)

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

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.

22

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

190-00600-03 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)

The flashing cursor moves to the ground speed (GS) field. Enter the ground
speed. Press the

ENT

Key when finished. Note that in ‘automatic’ page

mode, ground speed is provided by the system.

8)

The flashing cursor moves to the fuel flow field. Enter the fuel flow. Press
the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel flow
is provided by the system.

9)

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.

10)

The flashing cursor moves to the calibrated airspeed (CALIBRATED AS) field.

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

11)

The flashing cursor moves to the altitude (IND ALTITUDE) field. Enter the

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

12)

The flashing cursor moves to the barometric setting (PRESSURE) field. Enter

the desired baro setting. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, the baro setting is provided by the setting entered
on the PFD.

13)

The flashing cursor moves to the air temperature (TOTAL AIR TEMP) field. Enter

the desired air temperature. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, air temperature is provided by the system outside
air temperature.

CREATE A NEW USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

1)

Turn the large FMS Knob on the Control Unit 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.

190-00600-03 Rev. A 23

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Alerts Appendix Index

Annun/

Flight Planning

6)

The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint

Flight

InstrumentsEICAS

can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.

a)

Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.

b)

Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.

Nav/Com/

XPDR/AudioAFCSGPS Nav

7)

With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.

8)

Turn the small FMS Knob to select LAT/LON (latitude and longitude).

9)

Press the ENT Key.

CREATE A NEW USER WAYPOINT DEFINED BY RADIALS FROM OTHER

WAYPOINTS

1)

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Turn the large FMS Knob on the Control Unit 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 ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.

a)

Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.

b)

Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.

7)

With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.

8)

Turn the small FMS Knob to select RAD/RAD (radial/radial).

9)

Press the ENT Key.

10)

The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first

waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:

24

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Flight Planning

a)

When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.

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’ airports 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.

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 ‘USER’ waypoints.

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

11)

Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter

the desired radial from the reference waypoint.

12)

Press the ENT Key.

13)

Repeat step 10 to enter the next waypoint name.

14)

Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field for the

second waypoint. Enter the desired radial from the reference waypoint.

15)

Press the ENT Key.

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Alerts Appendix Index

16)

Press the FMS Knob to remove the flashing cursor.

190-00600-03 Rev. A 25

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Flight Planning

CREATE A NEW USER WAYPOINT DEFINED BY A RADIAL & DISTANCE FROM

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ANOTHER WAYPOINT

1)

Turn the large FMS Knob on the MFD Control Unit 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 ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.

a)

Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.

b)

Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.

7)

With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.

8)

Turn the small FMS Knob to select RAD/DIS (radial/distance).

9)

Press the ENT Key.

10)

The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first

waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:

a)

When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.

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’ airports to
the aircraft’s current position.

26

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Flight Planning

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.

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 ‘USER’ waypoints.

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

11)

Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter

the desired radial from the reference waypoint.

12)

Press the ENT Key.

13)

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

distance from the reference waypoint.

14)

Press the ENT Key.

Instruments EICAS

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Nav/Com/

Planning Procedures

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Avoidance

Hazard

Additional

Features

15)

Press the FMS Knob to remove the flashing cursor.

DELETE A 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)

Press the FMS Knob to activate the cursor.

4)

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

5)

Turn the small FMS Knob to highlight the desired waypoint.

6)

Select the DELETE Softkey.

7)

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

190-00600-03 Rev. A 27

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Alerts Appendix Index

Flight Planning

CREATE A NEW FLIGHT PLAN

Flight

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

the first leg is activated automatically after it is created.

Creating an active flight plan:

1)

Press the FPL Key.

2)

Press the FMS Knob to activate the cursor (only on MFD).

3)

Turn the small FMS Knob to display the Waypoint Information Window.
(Turning it clockwise displays a blank Waypoint Information Window,
turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan,
nearest, recent, user, or airway waypoints).

4)

Enter the identifier, facility, or city name of the departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key. The
active flight plan is modified as each waypoint is entered.

5)

Repeat step numbers 3 and 4 to enter each additional flight plan waypoint.

6)

When all waypoints have been entered, press the FMS Knob to remove the
cursor.

Creating a stored flight plan:

1)

Press the FPL Key.

2)

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

3)

Select the NEW Softkey; or press the MENU Key, highlight ‘Create New
Flight Plan’, and press the ENT Key to display a blank flight plan for the
first empty storage location.

4)

Turn the small FMS Knob to display the Waypoint Information Window.
(Turning it clockwise displays a blank Waypoint Information Window,
turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan,
nearest, recent, user, or airway waypoints).

5)

Enter the identifier, facility, or city name of the departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key.

6)

Repeat step numbers 4 and 5 to enter each additional flight plan waypoint.

7)

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.

28

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Flight Planning

IMPORT A FLIGHT PLAN FROM AN SD CARD

1)

Insert the SD card containing the flight plan in the top card slot on the
MFD.

2)

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

3)

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

4)

Press the FMS Knob to activate the cursor.

5)

Turn either FMS Knob to highlight an empty or existing flight plan.

6)

Select the IMPORT Softkey.

If an empty flight plan is selected, a list of the available flight plans on the
SD card will be displayed.

Or:

If an existing flight plan is selected, an ‘Overwrite existing flight plan? OK
or CANCEL’ prompt is displayed. Press the ENT Key to choose to overwrite
the selected flight plan and see a list of the available flight plans on the SD
card. If overwriting the existing flight plan is not desired, select ‘CANCEL’
using the FMS Knob, press the ENT Key, select another existing or empty
flight plan, and again select the IMPORT Softkey.

7)

Turn the small FMS Knob to highlight the desired flight plan for importing.

8)

Press the ENT Key.

INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

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:

190-00600-03 Rev. A 29

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Alerts Appendix Index

Flight Planning

a)

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Avoidance

6)

b)

c)

d)

a)

b)

c)

d)

a)

b)

c)

d)

Press the

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

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Or:

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

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

Or:

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

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

Turn the large FMS Knob to select the desired user waypoint.

Press the ENT Key.

ENT

Key again to “accept” the waypoint.

ENTER AN AIRWAY IN A FLIGHT PLAN

Features

Additional

1)

Press the FPL Key.

2)

Abnormal

Operation

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30

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.

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).

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Flight Planning

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.

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.

3)

Press the CLR Key to display a confirmation window.

4)

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

Instruments EICAS

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Alerts Appendix Index

190-00600-03 Rev. A 31

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Flight Planning

STORE A FLIGHT PLAN

Flight

InstrumentsEICAS

1)

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

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

Nav/Com/

XPDR/AudioAFCSGPS Nav

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.

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.

Flight

6)

PlanningProcedures

Enter the changes, then press the ENT Key.

7)

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

DELETE A WAYPOINT FROM THE FLIGHT PLAN

1)

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

Hazard

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Abnormal

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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.

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.

32

5)

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

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Flight Planning

INVERT AND ACTIVATE A STORED FLIGHT PLAN

1)

Press the FPL Key on the MFD or MFD Control Unit.

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 on the MFD or MFD Control Unit.

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

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Avoidance

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Features

DELETE A FLIGHT PLAN

1)

Press the FPL Key on the MFD or MFD Control Unit.

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.

5)

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

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Alerts Appendix Index

Flight Planning

GRAPHICAL FLIGHT PLAN CREATION

Flight

InstrumentsEICAS

1)

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

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

Nav/Com/

XPDR/AudioAFCSGPS Nav

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)

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.

Flight

PlanningProcedures

EXPORT A FLIGHT PLAN TO AN SD CARD

1)

Insert the SD card into the top card slot on the MFD.

2)

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

3)

Hazard

Avoidance

Features

Additional

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

4)

Press the FMS Knob to activate the cursor.

5)

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

6)

Select the EXPORT Softkey.

7)

Press the ENT Key to confirm the export.

ABOVE

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34

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 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

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Planning Procedures

Flight

ACTIVATE A DEPARTURE LEG

1)

Press the FPL Key on the MFD or MFD Control Unit to display the active
flight plan.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight the TO waypoint of the desired leg
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.

190-00600-03 Rev. A 35

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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 TO waypoint of the desired leg
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

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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

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 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 or
optional RAD ALT.

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

Instruments EICAS

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Flight

Avoidance

Hazard

1)

Press the PROC Key.

2)

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

3)

Press the ENT Key.

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.

190-00600-03 Rev. A 37

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Additional

Features

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/

38

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 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 (SUBSCRIPTION 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

190-00600-03 Rev. A 39

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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

SIGMETs, PIREPs or AIREPs.

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)

Icing Potential

Hazard

Avoidance

Turbulence PIREPs

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

40

Cyclone Warnings

AIREPs

NEXRAD

Cloud Top

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Cell Movement

XM Lightning

SIGMETs/AIRMETs

City Forecast

METARs

Freezing Levels

Surface Analysis

Winds Aloft

County Warnings

190-00600-03 Rev. A

Hazard Avoidance

TRAFFIC SYSTEMS

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.

• 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.

• IfaTCASIIsystemiscongured,aREL, ABS, TRC STBY, TA ONLY, TA/RA,
TEST, and ALT RNG Softkey is displayed.

Traffic Symbol Description

Non-Threat Traffic

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

Proximity Advisory (PA) (TAS and TCAS II only)

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

Traffic Advisory (TA)

(Potential collision area is within 20 to 48 seconds)

Traffic Advisory Off Scale

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Resolution Advisory (RA) (TCAS II only)

(Potential collision area is within 15 to 35 seconds)

Resolution Advisory Off Scale (TCAS II only)

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.

190-00600-03 Rev. A 41

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Hazard Avoidance

Displaying Traffic on the Traffic Map Page

Flight

InstrumentsEICAS

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.

Nav/Com/

XPDR/AudioAFCSGPS Nav

‘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.

Flight

PlanningProcedures

Traffic Advisory System (TAS) (Optional)

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.

Hazard

Avoidance

3)

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

4)

Features

Additional

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.

Abnormal

Operation

5)

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

AlertsAppendixIndex

Annun/

6)

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

System Self Test

1)

With the Traffic Map Page displayed, set the range to 2/6 nm.

2)

Select the STANDBY Softkey.

3)

Select the TEST Softkey.

42

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Hazard Avoidance

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 Navigation Map

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.

Traffic Collision Avoidance System (TCAS II) (Optional)

NOTE: If the system is configured to use TIS, the optional TCAS II is not
available for use.

WARNING: The TCAS II system is intended for advisory use only. TCAS II is
intended to help the pilot locate transponder-equipped traffic visually and
to provide advisory vertical maneuver guidance to avoid traffic. It is the
responsibility of the pilot to see and maneuver to avoid traffic, terrain, and
obstacles.

System Test

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

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 TEST Softkey. The aural annunciation “TCAS Test” will be
heard. A test pattern of traffic symbols is displayed on the Traffic Page
and inset map on the PFD. The VSI will display a red no descent indication
and a green climb indication of 2000 feet per min. and red from 2000
to 4000+. The pitch display will also display the appropriate indications
appropriate with the VSI. The self test takes approximately eight seconds
to complete, after which a voice alert “TCAS Test Passed” is heard. In the
event the system test fails, a voice alert “TCAS Test Failed” is heard and a
visual annunciation ‘TCAS FAIL’ appears on the PFD. In addition, a visual
annunciation ‘FAIL’ appears in the Operating Mode box on the Traffic Map
Page.

190-00600-03 Rev. A 43

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Hazard Avoidance

Displaying Traffic on the Traffic Map Page

Flight

InstrumentsEICAS

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 TA ONLY or TA/RA Softkey to begin displaying traffic. ‘TA/RA’ or
‘TA ONLY’ respectively, is displayed in the TCAS Mode field.

4)

Select the STANDBY Softkey to place the system in the Standby Mode.

Nav/Com/

XPDR/AudioAFCSGPS Nav

‘TFC STBY’ will be displayed in the TCAS Mode field.

5)

Select the ABS (absolute) or REL (relative) Softkey to display intruder
altitude as an absolute altitude or an altitude relative to own aircraft
altitude.

6)

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

Changing the Altitude Range

Flight

Hazard

Additional

Abnormal

Annun/

1)

PlanningProcedures

On the Traffic Page, select the

2)

Select one of the following Softkeys:

AB

OVE: Displays non-threat and proximity traffic from 9900 feet above the

ALT RNG

aircraft to 2700 feet below the aircraft. Typically used during climb phase
of flight.

Avoidance

NO

RMAL: Displays non-threat and proximity traffic from 2700 feet above

the aircraft to 2700 feet below the aircraft. Typically used during enroute
phase of flight.

BE

Features

LOW: Displays non-threat and proximity traffic from 2700 feet above the

aircraft to 9900 feet below the aircraft. Typically used during descent phase
of flight.

Operation

UN

3)

AlertsAppendixIndex

Displaying Traffic on the Navigation Map

REST (unrestricted): All traffic is displayed.

To return to the Traffic Page, select the BACK Softkey.

Softkey.

44

1)

Ensure TCAS II system is operating. With the Navigation Map displayed,
select the MAP Softkey.

2)

Select the TRAFFIC Softkey. Traffic will now be displayed on the map.

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Hazard Avoidance

TERRAIN AWARENESS & WARNING SYSTEM (TAWS-B)

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 system is configured for
a TAWS-B installation.

Manual System Test

1)

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

2)

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

3)

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

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

Display Terrain and Obstacles on the TAWS-B Page

1)

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

2)

Turn the small FMS Knob to select the TAWS-B 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 increase the display range or rotate
counter-clockwise to decrease the display range.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Color Terrain/Obstacle Location

Red

Yellow

Black

190-00600-03 Rev. A 45

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.

Alerts Appendix Index

Annun/

Hazard Avoidance

Enable/Disable Aviation Data

Flight

InstrumentsEICAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

1)

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

Or

:

1)

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

2)

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

3)

Press the ENT Key.

Abnormal

Operation

AlertsAppendixIndex

Annun/

Displaying Terrain and Obstacles on the Navigation Map

1)

With the Navigation Map displayed, press the MAP Softkey.

2)

Select the TERRAIN Softkey. Terrain and obstacles will now be displayed
on the map.

46

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 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.

190-00600-03 Rev. A 47

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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

Flight

PlanningProcedures

now 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/

48

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

190-00600-03 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.

190-00600-03 Rev. A 49

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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/

50

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Additional Features

ADDITIONAL FEATURES

SYNTHETIC VISION (OPTIONAL)

WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. SVS is intended as an aid to situational
awareness only and may not provide either the accuracy or reliability upon
which to solely base decisions and/or plan maneuvers to avoid terrain,
obstacles, or traffic.

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

to the G1000 Integrated Flight Deck.

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:

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

• Pathways

• Flight Path Marker

• Horizon Heading Marks

• Terrain and Obstacle Alerting

• Three-dimensional Traffic

• Airport Signs

• Runway Display

Displaying Synthetic Terrain

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.

190-00600-03 Rev. A 51

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Additional Features

Displaying Pathways

Flight

InstrumentsEICAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

NOTE: When the optional TCAS II system issues a Resolution Advisory (RA)

Pathways are automatically removed from the display. Pathways may again
be displayed by the pilot manually selecting Pathways.

NOTE: Pathways are not available when the cross-pointer (X-Pointer) flight
director format is selected.

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.

Displaying Heading on the Horizon

1)

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

Features

Additional

Abnormal

Annun/

Operation

AlertsAppendixIndex

52

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.

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Additional Features

TERMINAL PROCEDURE CHARTS

NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may
be necessary to carry another source of charts on-board the aircraft.

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

numbers, taxiways identiers, 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.

Selecting the DCLTRSoftkey(declutter)onceremovesthetaxiwaymarkingsand
airport identification labels. Selecting the DCLTR Softkey twice removes VOR station
ID, the VOR symbol, and intersection names if within the airport plan view. Selecting
the DCLTR Softkey a third time removes the airport runway layout, unless the airport
in view is part of an active route structure. Selecting the DCLTR Softkey again cycles
back to the original map detail.

The SafeTaxi database contains detailed airport diagrams for selected airports.

These diagrams provide the pilot with situational awareness by displaying the aircraft

position in relation to taxiways, ramps, runways, terminals, and services. This

information should not be used by the pilot as the basis for maneuvering the aircraft
on the ground. This database is updated on a 56-day cycle.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

ChartView (Optional)

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® (Optional)

FliteCharts® resemble the paper version of AeroNav Services terminal procedures
charts. The charts are displayed with high-resolution and in color for applicable
charts. Current aircraft position is not displayed on FliteCharts.

190-00600-03 Rev. A 53

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Additional Features

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

Flight

InstrumentsEICAS

expirationdate,FliteChartswillnolongerfunction.

View Charts from the Navigation Map Page

1)

Select the SHW CHRT Softkey when displayed.

Or

:

Nav/Com/

XPDR/AudioAFCSGPS Nav

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, and NOTAM softkeys to access charts for
departures, arrivals, approaches, weather and NOTAMs Note that NOTAMS
are only available with ChartView.

3)

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

View Charts from the Active Flight Plan Page

Flight

PlanningProcedures

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 will be displayed, if

Hazard

Avoidance

available for the item selected.

4)

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

Change Day/Night View

Features

Additional

1)

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

Abnormal

Operation

2)

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

AlertsAppendixIndex

Annun/

3)

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.

54

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Additional Features

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
the day/night crossover point based on backlighting intensity.

7)

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

AOPA AIRPORT DIRECTORY

AOPA Airport Directory adds enhanced airport information when viewing airports
on the WPT-Airport Information Page.

This database is updated four times per year. Check fly.garmin.com for the current
database.

View Airport Directory Information

While viewing the WPT-Airport Information Page, if necessary, select the
INFO-1 Softkey to change the softkey label to display INFO-2. AOPA
airport information is displayed on the right half of the display.

XM® RADIO ENTERTAINMENT (SUBSCRIPTION OPTIONAL)

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

Selecting the XM Radio Page

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

1)

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.

3)

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

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.

190-00600-03 Rev. A 55

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Additional Features

Selecting a Category

Flight

Nav/Com/

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

InstrumentsEICAS

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

:

XPDR/AudioAFCSGPS Nav

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.

Flight

PlanningProcedures

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

Hazard

Avoidance

1)

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

2)

Features

Additional

Abnormal

Operation

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

AlertsAppendixIndex

Annun/

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). Selecting the
MORE Softkey repeatedly cycles through the preset channels.

56

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Additional Features

3)

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

4)

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

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

190-00600-03 Rev. A 57

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Additional Features

Flight

InstrumentsEICAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

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58

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Abnormal Operation

ABNORMAL OPERATION

REVERSIONARY MODE

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

AUDIO PANEL FAIL-SAFE OPERATION

If there is a failure of both Audio Panels, a fail-safe circuit connects the pilot’s headset
and microphone directly to the COM1 transceiver and the copilot’s headset directly to
the COM2 transceiver. Audio is not available on the speakers. If there is a failure of one
Audio Panel, that side only has access to their respective on-side fail-safe COM.

NOTE: Audio is not available on the speakers in case of an Audio Panel and
its cross-side GIA unit simultaneous failure.

If there is a failure of one Audio Panel, the remaining Audio Panel does not have

accessto theotherside’sCOM orNAV.For example,if thepilotside AudioPanel

190-00600-03 Rev. A 59

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Abnormal Operation

fails,thecopilotsideAudioPanelhas accessto all theradios exceptfor COM1 and

NAV1. In this case, the copilot can receive the audio from NAV2 and operate COM2

Flight

InstrumentsEICAS

for transmission/reception.

In addition, if there is a failure of one Audio Panel, the following functions are no
longer available on the failed side; NAV/ILS audio, speaker, cockpit/cockpit-passengers
intercom, aural warning alerts on headset, entertainment inputs, and digital recording
radio. Also, if a stereo headset is in use, and an Audio Panel fails, only the left channel
will be heard in the headphones.

Nav/Com/

XPDR/AudioAFCSGPS Nav

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.

Flight

PlanningProcedures

Loss of Hazard Functions with Loss of GPS

Position

UNUSUAL ATTITUDES

The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary
functions are displayed in these situations.

Hazard

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

Avoidance

aredisabled)whentheaircraftexperiencesunusualattitudes:

• TrafcAnnunciations

Features

Additional

• AFCSAnnunciations

• FlightDirector

Command Bars

Abnormal

Operation

• InsetMap

• Temperatures

• DMEInformation

AlertsAppendixIndex

Annun/

Window

• WindData

• SelectedHeadingBox

• SelectedCourseBox

• TransponderStatus
Box

• SystemTime

• PFDSetupMenu

• Windowsdisplayedin

the lower right corner

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

• BarometricMinimum

DescentAltitudeBox

• Glideslope,Glide-

path, and Vertical
Deviation Indicators

• AltimeterBarometric

Setting

• SelectedAltitude

• VNV Target Altitude

60

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Abnormal Operation

Extreme Pitch Indication

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. The CDI deviation bar is displayed in yellow, but will be removed from the
display after 20 minutes. 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 may 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.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-03 Rev. A 61

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Abnormal Operation

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

Flight

InstrumentsEICAS

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.

Nav/Com/

XPDR/AudioAFCSGPS Nav

CDI ‘DR’ Indication on PFD

Symbolic Aircraft

(Map pages and Inset Map)

Dead Reckoning Indications

Flight

As a result of operating in DR Mode, all GPS-derived data is computed based upon

PlanningProcedures

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

Hazard

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

Avoidance

• CurrentTrackIndicator

• AllBearingPointerDistances

• ActiveFlightPlandistances,bearings,andETEvalues

Features

Additional

Also, while the G1000 is in DR Mode, the autopilot will couple to GPS for up to 20

minutes. TAWS is also disabled. Additionally, the accuracy of all nearest information

Abnormal

Operation

(airports, airspaces, and waypoints) is questionable. Finally, airspace alerts continue
to function, but with degraded accuracy.

AlertsAppendixIndex

Annun/

62

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Annunciations & Alerts

ANNUNCIATIONS & ALERTS

CAS MESSAGES

Messages

Warning Caution Advisory

AFT DOOR Tailcone baggage door not fully secured

AFT JBOX CB L-R* Start control circuit breaker (located in aft j-box) tripped

AFT JBOX LMT L-R* Current limiter blown (located in aft j-box)

ANTISKID FAIL Antiskid Control Unit cannot perform anti-skid functions

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

BATT TEMP FAIL Battery temperature sensor failure

CABIN ALT CABIN ALT CABIN ALT Cabin altitude potentially unsafe

CABIN DOOR Cabin door not fully secured

CHECK DOORS A door monitor has not been properly tested or has failed

CVR FAIL Cockpit voice Recorder has failed

DUCT O’HEAT L-R* Duct temperature too high or sensor disconnected

ENG A/I COLD L-R* ENG A/I COLD L-R* Engine anti-ice system ON and inlet temperature is cold

ENG CTRL SYS L-R* FADEC has a fault that requires maintenance

ENGINE FAIL L-R* An engine has failed

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

FDR FAIL Flight Data Recorder is not recording data

FLAPS FAIL A flap system failure has occurred.

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

FUEL FLTR BP L-R* Engine fuel filter impending bypass switch closed

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

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

FUEL PRES LO L-R* Fuel pressure too low

FUEL TRANSFER Fuel transfer valve open

GEN OFF L-R GEN OFF L-R* One or both electrical generators offline

HYD PRESS LO Hydraulic system pressure too low

HYD PUMP ON Hydraulic pump running too long

MFD COLD MFD temperature is below -20° C

NOSE DOOR L-R* One or both nose baggage doors not fully secured

NO TIRE SPINDOWN Antiskid control spindown function not working

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

OXYGEN OFF Oxygen supply off

Electric fuel boost pump ON. Caution condition is displayed
when the boost pump is operating in abnormal conditions.

Description

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-03 Rev. A 63

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Annunciations & Alerts

Messages

Flight

Warning Caution Advisory

InstrumentsEICAS

P/S HTR L-R* P/S HTR L-R* No current detected to pitot static heater

PRESS CTRL PRESS CTRL Pressure controller loss of integrity

PRESS OFF Air Source Selector switch in OFF or fresh air position

SPD BRK EXTEND Speed brakes extended

Nav/Com/

XPDR/AudioAFCSGPS Nav

STALL WARN FAIL Failure detected in stall warning system

STALL WARN HI Stall warning system on ice-contaminated schedule

STALL WARN HTR No power delivered to stall warning vane heater

SURFACE DE-ICE De-ice boots inflating/deflating as designed

T2 HTR FAIL L-R* T2 probe heater failure

TAIL CONE BLD LK Tailcone temp high, possible bleed air leak.

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

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

W/S O’HEAT L-R* W/S O’HEAT L-R* Windshield anti-ice power ON; temperature too high

Flight

PlanningProcedures

WING DE-ICE FAIL De-ice system operating abnormally

WOW MISCOMPARE Gear on-ground inputs do not agree

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

Description

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

64

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Annunciations & Alerts

COMPARATOR ANNUNCIATIONS

Note that operating the system in the vicinity of metal buildings or other metal
structures can cause sensor differences that may result in nuisance miscompare

annunciationsduringstartup,shutdown,orwhiletaxiing.

Comparator

Window Text

ALT MISCOMP

IAS MISCOMP

HDG MISCOMP

PIT MISCOMP

ROL MISCOMP

ALT NO COMP

IAS NO COMP

HDG NO COMP

PIT NO COMP

ROL NO COMP

Difference in altitude sensors is > 200 ft.

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

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

If either airspeed sensor detects > 80 knots, and the difference in sensors is
> 10 kts.

Difference in heading sensors is > 10 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..

Condition

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

190-00600-03 Rev. A 65

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Operation

Abnormal

Annun/

Alerts Appendix Index

Annunciations & Alerts

REVERSIONARY SENSOR ANNUNCIATIONS

Flight

InstrumentsEICAS

Sensor Window

BOTH ON ADC1
BOTH ON ADC2

BOTH ON AHRS1

Nav/Com/

XPDR/AudioAFCSGPS Nav

BOTH ON AHRS2

BOTH ON GPS1
BOTH ON GPS2

Flight

PlanningProcedures

Hazard

Avoidance

Reversionary

Text

USING ADC1

USING ADC2

USING AHRS1
USING AHRS2

USING GPS1

USING GPS2

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.

PFD1 is displaying data from the #2 AHRS.

PFD2 is displaying data from the #1 GPS.

PFD1 is displaying data from the #2 GPS.

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

66

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Annunciations & Alerts

TAWS-B 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)

Reduced Required
Obstacle Clearance
Caution (ROC)

Imminent Obstacle
Impact Caution (IOI)

Premature Descent
Alert Caution (PDA)

Altitude Callout
“500”

Excessive Descent
Rate Caution (EDR)

Negative Climb
Rate Caution (NCR)

PFD/MFD
TAWS-B Page
Annunciation

MFD

Pop-Up Alert

Aural Message

“Terrain, Terrain; Pull Up,

“Terrain, Terrain; Pull Up,

“Obstacle, Obstacle; Pull

““Obstacle, Obstacle; Pull

“Caution, Terrain; Caution,

“Caution, Terrain; Caution,

“Caution, Obstacle;

Caution, Obstacle”

“Caution, Obstacle;

Caution, Obstacle”

“Too Low, Terrain”

None None “Five-Hundred”

“Don’t Sink”

“Pull Up”

Pull Up”

Pull Up”

Up, Pull Up”

Up, Pull Up”

Terrain”

Terrain”

“Sink Rate”

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-03 Rev. A 67

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Annunciations & Alerts

TAWS-B System Status Annunciations

Flight

InstrumentsEICAS

Alert Type

PFD/MFD

Alert

Annunciation

TAWS-B Page
Annunciation

System Test in Progress TAWS TEST None

System Test Pass None None

Nav/Com/

XPDR/AudioAFCSGPS Nav

TAWS Alerting is disabled

None None

MFD Terrain or Obstacle
database unavailable or invalid.
TAWS operating with PFD

None TERRAIN DATABASE FAILURE None

Terrain or Obstacle databases

TAWS-B System Test Fail TAWS FAIL

Terrain or Obstacle database

Flight

PlanningProcedures

unavailable or invalid, invalid
software configuration, system

TAWS FAIL

audio fault

No GPS position NO GPS POSITION

Excessively degraded GPS

Hazard

signal, Out of database

Avoidance

None

coverage area

Aural

Message

“TAWS System

Test OK”

“TAWS System

Failure”

“TAWS System

Failure”

“TAWS Not

Available”

“TAWS Not

Available”

Features

Additional

TCAS II ALERTS AND ANNUNCIATIONS

Abnormal

Operation

AlertsAppendixIndex

Annun/

TCAS II Self-test
Initiated (TEST)

Mode

PFD Mode

Annunciation

None

Traffic Advisory and
Resolution Advisory

None TA/RA

(TA/RA)

68

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

MFD Traffic Map Page

Mode Annunciation

TEST

(‘TEST MODE’ also shown in
white on top center of page)

Traffic

Display

Status Icon

(Other Maps)

190-00600-03 Rev. A

Annunciations & Alerts

Mode

PFD Mode

Annunciation

MFD Traffic Map Page

Mode Annunciation

Traffic Advisory Only
(TA ONLY)

TCAS II Standby
(TFC STBY)

on ground

in air

STANDBY or STANDBY*

(also shown in white in

center of page)

TCAS II Failed

* Annunciation appears yellow while in flight.

TCAS II Modes

Traffic Map Page

Annunciation

NO DATA Data is not being received from the TCAS II unit

DATA FAILED

FAILED Incorrect data format received from the TCAS II unit

Data is being received from the TCAS II unit, but the unit is self­reporting a failure

Description

TA ONLY

FAIL

Traffic

Display

Status Icon

(Other Maps)

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

TCAS II Failure Annunciations

Traffic Status Banner

Annunciation

A Resolution Advisory is outside the selected display range*.

RA OFF SCALE

TA OFF SCALE

RA X.X ± XX ↕

190-00600-03 Rev. A 69

Annunciation is removed when traffic comes within the selected
display range

A Traffic Advisory is outside the selected display range*.
Annunciation is removed when traffic comes within the selected
display range.

System cannot determine bearing of Resolution Advisory**.
Annunciation indicates distance in nm, altitude separation in hundreds
of feet, and altitude trend arrow (climbing/descending).

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Description

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Annunciations & Alerts

Traffic Status Banner

Flight

InstrumentsEICAS

Annunciation

TA X.X ± XX ↕

System cannot determine bearing of Traffic Advisory**.
Annunciation indicates distance in nm, altitude separation in hundreds

Description

of feet, and altitude trend arrow (climbing/descending).

TCAS II unit has failed (unit is self-reporting a failure or sending
incorrectly formatted data)

Nav/Com/

XPDR/AudioAFCSGPS Nav

TRFC FAIL

NO TCAS DATA Data is not being received from the TCAS II unit

*Shown as symbol on Traffic Map Page
**Shown in center of Traffic Map Page

TCAS II Traffic Status Annunciations

AURAL ALERTS

Aural Alert Description

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

Flight

Hazard

PlanningProcedures

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

“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

Avoidance

decision altitude.

navigation is enabled.

available when a TAS system is installed).

FLIGHT PLAN IMPORT/EXPORT MESSAGES

Features

Additional

Abnormal

Annun/

In some circumstances, some messages may appear in conjunction with others.

Flight Plan Import/Export

Operation

Results

‘Flight plan successfully imported.’ A flight plan file stored on the SD card was successfully

imported as a stored flight plan.

AlertsAppendixIndex

‘File contained user waypoints only.
User waypoints imported success­fully. No stored flight plan data was
modified.’

The file stored on the SD card did not contain a flight plan,
only user waypoints. These waypoints have been saved to the
system user waypoints. No flight plans stored in the system
have been modified.

‘No flight plan files found to import.’ The SD card contains no flight plan data.

‘Flight plan import failed.’ Flight plan data was not successfully imported from the SD card.

70

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Description

190-00600-03 Rev. A

Annunciations & Alerts

Flight Plan Import/Export

Description

Results

‘Flight plan partially imported.’ Some flight plan waypoints were successfully imported from

the SD card, however others had errors and were not imported.
A partial stored flight plan now exists in the system.

‘File contained user waypoints only.’ The file stored on the SD card did not contain a flight plan,

only user waypoints. One or more of these waypoints did not
import successfully.

‘Too many points. Flight plan trun­cated.’

The flight plan on the SD card contains more waypoints than
the system can support. The flight plan was imported with as
many waypoints as possible.

‘Some waypoints not loaded. Way­points locked.’

The flight plan on the SD card contains one or more waypoints
that the system cannot find in the navigation database. The
flight plan has been imported, but must be edited within the
system before it can be activated for use.

‘User waypoint database full. Not all
loaded.’

The flight plan file on the SD card contains user waypoints.
The quantity of stored user waypoints has exceeded system
capacity, therefore not all the user waypoints on the SD card
have been imported. Any flight plan user waypoints that were
not imported are locked in the flight plan. The flight plan must
be edited within the system before it can be activated for use.

‘One or more user waypoints renamed.’ One or more imported user waypoints were renamed when

imported due to naming conflicts with waypoints already
existing in the system.

‘Flight plan successfully exported.’ The stored flight plan was successfully exported to the SD card.

‘Flight plan export failed.’ The stored flight plan was not successfully exported to the SD

card. The SD card may not have sufficient available memory or
the card may have been removed prematurely.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

190-00600-03 Rev. A 71

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Alerts Appendix Index

Annun/

Annunciations & Alerts

MFD & PFD MESSAGE ADVISORIES

Flight

InstrumentsEICAS

DATA LOST

Message Comments

– Pilot stored data was

lost. Recheck settings.

XTALK ERROR

Nav/Com/

XPDR/AudioAFCSGPS Nav

– 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.

Flight

PlanningProcedures

MANIFEST

– PFD1 software

mismatch, communication halted.

MANIFEST

– PFD2 software

mismatch, communication halted.

MANIFEST

Hazard

mismatch, communication halted.

Avoidance

PFD1 CONFIG

– MFD1 software

– PFD1 config error.

Config service req’d.

Features

Additional

PFD2 CONFIG

– PFD2 config error.

Config service req’d.

MFD1 CONFIG

Abnormal

Operation

– MFD1 config

error. Config service req’d.

AlertsAppendixIndex

Annun/

SW MISMATCH

– GDU software

version mismatch. Xtalk is off.

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 system should be serviced.

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

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

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

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

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

72

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Annunciations & Alerts

MFD & PFD MESSAGE ADVISORIES (CONT.)

Message Comments

PFD1 COOLING

cooling. Reducing power usage.

PFD2 COOLING

cooling. Reducing power usage.

MFD1 COOLING

– PFD1 has poor

– PFD2 has poor

– MFD1 has poor

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

cooling. Reducing power usage.

PFD1 KEYSTK

Key is stuck.

PFD2 KEYSTK

Key is stuck.

MFD1 KEYSTK

– PFD1 [key name]

– PFD2 [key name]

– MFD [key name]

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

Key is stuck.

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 system should be serviced.

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

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

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

DATABASE MESSAGE ADVISORIES

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Message Comments

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 navigation

– PFD1 navigation

– PFD2 navigation

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

database error exists.

190-00600-03 Rev. A 73

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Alerts Appendix Index

Annun/

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEICAS

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

Nav/Com/

PFD2 DB ERR

XPDR/AudioAFCSGPS Nav

database error exists.

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

database error exists.

Flight

PlanningProcedures

MFD1 DB ERR

database missing.

PFD1 DB ERR

database missing.

PFD2 DB ERR

Hazard

database missing.

Avoidance

MFD1 DB ERR

database error exists.

Features

Additional

PFD1 DB ERR

database error exists.

PFD2 DB ERR

Abnormal

Operation

database error exists.

MFD1 DB ERR

AlertsAppendixIndex

Annun/

database missing.

PFD1 DB ERR

database missing.

PFD2 DB ERR

database missing.

Message Comments

– MFD1 basemap

– PFD1 basemap

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

– PFD2 basemap

– MFD1 terrain

The MFD and/or PFD detected a failure in the

– PFD1 terrain

terrain database. Ensure that the terrain card
is properly inserted in display. Replace terrain
card. If problem persists, the system should be

– PFD2 terrain

serviced.

– MFD1 terrain

– PFD1 terrain

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

– PFD2 terrain

– MFD1 obstacle

The MFD and/or PFD detected a failure in the

– PFD1 obstacle

obstacle database. Ensure that the data card is
properly inserted. Replace data card. If problem

– PFD2 obstacle

persists, the system should be serviced.

– MFD1 obstacle

– PFD1 obstacle

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

– PFD2 obstacle

74

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Message Comments

MFD1 DB ERR

terrain database error exists.

PFD1 DB ERR

terrain database error exists.

PFD2 DB ERR

– MFD1 airport

– PFD1 airport

– PFD2 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 system should be serviced.

terrain database error exists.

MFD1 DB ERR

– MFD1 airport

terrain database missing.

PFD1 DB ERR

– PFD1 airport

terrain database missing.

PFD2 DB ERR

– PFD2 airport

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

terrain database missing.

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 system should be serviced.

database error exists.

MFD1 DB ERR

database error exists.

– MFD1 Chartview

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

MFD1 DB ERR

database error exists.

– MFD1 FliteCharts

The MFD detected a failure in the FliteCharts
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the system should be serviced.

MFD1 DB ERR

Directory database error exists.

– MFD1 Airport

The MFD detected a failure in the Airport Directory
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the 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

190-00600-03 Rev. A 75

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEICAS

DB MISMATCH

database mismatch. Xtalk is off.

Message Comments

– Navigation

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

DB MISMATCH

Nav/Com/

XPDR/AudioAFCSGPS Nav

mismatch.

– Terrain database

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

DB MISMATCH

database mismatch.

– Obstacle

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

DB MISMATCH

database mismatch.

Flight

PlanningProcedures

NAV DB UPDATED

navigation database updated.

TERRAIN DSP

MFD1] Terrain awareness display
unavailable.

Hazard

Avoidance

– Airport Terrain

– Active

– [PFD1, PFD2 or

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

System has updated the active navigation
database from the standby navigation database.

One of the terrain, airport terrain, or obstacle
databases required for TAWS in the specified PFD
or MFD is missing or invalid.

GMA 1347D/1347D-20 MESSAGE ADVISORIES

Features

Additional

Abnormal

Operation

GMA1 FAIL
GMA2 FAIL

Message Comments

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

GMA XTALK

AlertsAppendixIndex

Annun/

has occurred.

GMA1 CONFIG

error. Config service req’d.

GMA2 CONFIG

error. Config service req’d.

76

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

– GMA crosstalk error

– GMA1 config

– GMA2 config

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

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

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

190-00600-03 Rev. A

Annunciations & Alerts

GMA 1347D/1347D-20 MESSAGE ADVISORIES (CONT.)

Message Comments

MANIFEST – GMA1 software

mismatch, communication halted.

MANIFEST – GMA2 software

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

mismatch, communication halted.

GMA1 SERVICE – GMA1 needs

service. Return unit for repair.

GMA2 SERVICE – GMA2 needs

service. Return unit for repair.

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 system should be serviced when possible.

GIA 63W MESSAGE ADVISORIES

Message Comments

GIA1 CONFIG

Config service req’d.

– GIA1 config error.

The GIA1 and/or GIA2 configuration settings do
not match backup configuration memory. The

GIA2 CONFIG

– GIA2 config error.

system should be serviced.

Config service req’d.

GIA1 CONFIG

error. Config service req’d.

GIA2 CONFIG

– GIA1 audio config

– GIA2 audio config

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

error. Config service req’d.

GIA1 COOLING

temperature too low.

– GIA1

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

GIA2 COOLING

– GIA2

operating temperature.

temperature too low.

GIA1 COOLING

temperature.

– GIA1 over

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

GIA2 COOLING

– GIA2 over

serviced.

temperature.

GIA1 SERVICE

service. Return the unit for repair.

– GIA1 needs

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

GIA2 SERVICE

– GIA2 needs

serviced.

service. Return the unit for repair.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00600-03 Rev. A 77

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEICAS

HW MISMATCH

Message Comments

– GIA hardware

mismatch. GIA1 communication halted.

HW MISMATCH

– GIA hardware

mismatch. GIA2 communication halted.

Nav/Com/

XPDR/AudioAFCSGPS Nav

MANIFEST

– GIA1 software

mismatch, communication halted.

MANIFEST

– GIA2 software

mismatch, communication halted.

MANIFEST

– GFC software

mismatch, communication halted.

COM1 TEMP

– COM1 over temp.

Reducing transmitter power.

Flight

PlanningProcedures

COM2 TEMP

– COM2 over temp.

Reducing transmitter power.

COM1 SERVICE

– COM1 needs

service. Return unit for repair.

COM2 SERVICE

Hazard

service. Return unit for repair.

Avoidance

COM1 PTT

is stuck.

Features

Additional

COM2 PTT

– COM2 needs

– COM1 push-to-talk key

– COM2 push-to-talk key

is stuck.

Abnormal

Operation

LOI

– GPS integrity lost. Crosscheck

with other NAVS.

AlertsAppendixIndex

Annun/

GPS NAV LOST

– Loss of GPS

navigation. Insufficient satellites.

GPS NAV LOST

– Loss of GPS

navigation. Position error.

GPS NAV LOST

– Loss of GPS

navigation. GPS fail.

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

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

Incorrect servo software is installed, or gain
settings are incorrect.

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 system should be serviced.

The system has detected a failure in COM1
and/or COM2. COM1 and/or COM2 may still
be usable. The 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 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.

78

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-03 Rev. A

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Message Comments

ABORT APR

navigation. Abort approach.

APR DWNGRADE

downgraded.

TRUE APR

Change HDG reference to TRUE.

GPS1 SERVICE

service. Return unit for repair.

– Loss of GPS

– Approach

– True north approach.

– GPS1 needs

Abort approach due to loss of GPS navigation.

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

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

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

GPS2 SERVICE

– GPS2 needs

available. The 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 system should be serviced.

service. Return unit for repair.

G/S1 FAIL

– G/S1 is inoperative.

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

G/S2 FAIL

– G/S2 is inoperative.

be serviced.

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

G/S1 SERVICE

service. Return unit for repair.

G/S2 SERVICE

service. Return unit for repair.

– G/S1 needs

– G/S2 needs

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

GSD 41 MESSAGE ADVISORIES

Message Comments

GSD1 CONFIG

Config service req’d.

GSD1 COOLING

too low.

GSD1 COOLING

temperature.

190-00600-03 Rev. A 79

– GSD1 config error.

GSD1 and the CDU have different copies of
the GSD1 configuration.

– GSD1 temperature

GSD1 is reporting a low temperature
condition.

– GSD1 over

GSD1 is reporting an over-temperature
condition.

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Annunciations & Alerts

GSD 41 MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEICAS

GSD1 SERVICE

Message Comments

– GSD1 needs service.

Return unit for repair.

MANIFEST

– GSD1 software

mismatch. Communication halted.

Nav/Com/

XPDR/AudioAFCSGPS Nav

GEA 71 MESSAGE ADVISORIES

Message Comments

GEA1 CONFIG

– GEA1 config error.

Config service req’d.

GEA2 CONFIG

– GEA2 config error.

Config service req’d.

Flight

PlanningProcedures

MANIFEST

– GEA1 software

mismatch, communication halted.

MANIFEST

– GEA2 software

mismatch, communication halted.

Hazard

Avoidance

GTX 33/33D MESSAGE ADVISORIES

GSD1 is reporting an internal error condition.
The GSD may still be usable.

GSD1 has incorrect software installed. The
system should be serviced.

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

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

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

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

Features

Additional

XPDR1 CONFIG

– XPDR1 config

error. Config service req’d.

Message Comments

Abnormal

Operation

XPDR2 CONFIG

– XPDR2 config

error. Config service req’d.

AlertsAppendixIndex

Annun/

MANIFEST

– GTX1 software

mismatch, communication halted.

MANIFEST

– GTX2 software

mismatch, communication halted.

XPDR1 SRVC

– XPDR1 needs

service. Return unit for repair.

80

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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

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

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

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

The #1 transponder should be serviced when
possible.

190-00600-03 Rev. A

Annunciations & Alerts

GTX 33/33D MESSAGE ADVISORIES (CONT.)

Message Comments

XPDR2 SRVC

service. Return unit for repair.

XPDR1 FAIL

inoperative.

XPDR2 FAIL

inoperative.

– XPDR2 needs

– XPDR1 is

– XPDR2 is

The #2 transponder should be serviced when
possible.

There is no communication with the #1
transponder.

There is no communication with the #2
transponder.

GRS 77 MESSAGE ADVISORIES

Message Comments

AHRS1 TAS

valid airspeed.

– AHRS1 not receiving

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 system should be serviced.

AHRS2 TAS

valid airspeed.

– AHRS2 not receiving

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 system should be serviced.

AHRS1 GPS

GPS source.

– AHRS1 using backup

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

AHRS2 GPS

GPS source.

– AHRS2 using backup

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

AHRS1 GPS

any GPS information.

– AHRS1 not receiving

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

AHRS2 GPS

any GPS information.

– AHRS2 not receiving

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

AHRS1 GPS

backup GPS information.

– AHRS1 not receiving

The #1 AHRS is not receiving backup GPS
information. The 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

190-00600-03 Rev. A 81

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Annunciations & Alerts

GRS 77 MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEICAS

AHRS2 GPS

Message Comments

– AHRS2 not receiving

backup GPS information.

AHRS1 GPS

– AHRS1 operating

exclusively in no-GPS mode.

Nav/Com/

AHRS2 GPS

XPDR/AudioAFCSGPS Nav

– AHRS2 operating

exclusively in no-GPS mode.

AHRS MAG DB

– AHRS magnetic

model database version mismatch.

AHRS1 SRVC

– AHRS1 Magnetic-

field model needs update.

AHRS2 SRVC

field model needs update.

Flight

PlanningProcedures

GEO LIMITS

– AHRS2 Magnetic-

– AHRS1 too far

North/South, no magnetic compass.

GEO LIMITS

– AHRS2 too far

North/South, no magnetic compass.

MANIFEST

Hazard

mismatch, communication halted.

Avoidance

MANIFEST

mismatch, communication halted.

Features

Additional

– GRS1 software

– GRS2 software

GMU 44 MESSAGE ADVISORIES

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

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

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

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

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 system should be serviced.

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

Abnormal

Operation

HDG FAULT

magnetometer fault has occurred.

AlertsAppendixIndex

Annun/

HDG FAULT

Message Comments

– AHRS1

– AHRS2

magnetometer fault has occurred.

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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

190-00600-03 Rev. A

Annunciations & Alerts

GMU 44 MESSAGE ADVISORIES (CONT.)

Message Comments

MANIFEST

mismatch, communication halted.

MANIFEST

– GMU1 software

– GMU2 software

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

mismatch, communication halted.

GDL 69A MESSAGE ADVISORIES

Message Comments

GDL69 CONFIG

error. Config service req’d.

– GDL 69 config

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

GDL69 FAIL

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

receiver is unavailable. The system should be
serviced

MANIFEST

mismatch, communication halted.

– GDL software

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

GWX 68 ALERT MESSAGES

Instruments EICAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Message Comments

GWX CONFIG

Config service req’d.

– GWX config error.

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

GWX FAIL

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

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

GWX SERVICE

service. Return unit for repair.

MANIFEST

mismatch, communication halted.

WX ALERT

weather ahead.

– GWX needs

– GWX software

– Possible severe

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

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

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

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

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 system should be serviced.

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

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

The 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 system should be serviced if the problem
persists.

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190-00600-03 Rev. A