Garmin M20M, M20R Reference Guide

®

G1000

Cockpit Reference Guide for the Cessna Citation Mustang

Integrated Flight Deck

FLIGHT INSTRUMENTS

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, 2007 Garmin Ltd. or its subsidiaries. All rights reserved.

This manual reflects the operation of System Software version 0435.09 or later for the Cessna
Citation Mustang. Some differences in operation may be observed when comparing the information
in this manual to earlier or later software versions.

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

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

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

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

Web Site Address: www.garmin.com

Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted,
disseminated, downloaded or stored in any storage medium, for any purpose without the express
written permission of Garmin. Garmin hereby grants permission to download a single copy of this
manual and of any revision to this manual onto a hard drive or other electronic storage medium to
be viewed for personal use, provided that such electronic or printed copy of this manual or revision
must contain the complete text of this copyright notice and provided further that any unauthorized
commercial distribution of this manual or any revision hereto is strictly prohibited.

Garmin® and G1000® are registered trademarks of Garmin Ltd. or its subsidiaries. WATCH™,
FliteCharts™, and SafeTaxi™ are trademarks of Garmin Ltd. or its subsidiaries. These trademarks
may not be used without the express permission of Garmin.

NavData® is a registered trademark of Jeppesen, Inc.; XM® is a registered trademark of XM
Satellite Radio, Inc.

May, 2007 190-00600-01 Rev. C Printed in the U.S.A.

Warnings, Cautions & Notes

WARNING: Navigation and terrain separation must NOT be predicated upon
the use of the terrain function. The G1000 Terrain Proximity 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 Proximity feature is only to be used as an aid for terrain
avoidance and is not certified for use in applications requiring a certified
terrain awareness system. Terrain data is obtained from third party sources.
Garmin is not able to independently verify the accuracy of the terrain data.

WARNING: The displayed minimum safe altitudes (MSAs) are only advisory
in nature and should not be relied upon as the sole source of obstacle and
terrain avoidance information. Always refer to current aeronautical charts
for appropriate minimum clearance altitudes.

WARNING: The altitude calculated by G1000 GPS receivers is geometric
height above Mean Sea Level and could vary significantly from the altitude
displayed by pressure altimeters, such as the GDC 74B Air Data Computer,
or other altimeters in aircraft. GPS altitude should never be used for vertical
navigation. Always use pressure altitude displayed by the G1000 PFD or
other pressure altimeters in aircraft.

WARNING: Do not use outdated database information. Databases used in
the G1000 system must be updated regularly in order to ensure that the
information remains current. Pilots using any outdated database do so
entirely at their own risk.

WARNING: Do not use basemap (land and water data) information for
primary navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered as an aid to
enhance situational awareness.

WARNING: Traffic information shown on the G1000 Multi Function Display
is provided as an aid in visually acquiring traffic. Pilots must maneuver
the aircraft based only upon ATC guidance or positive visual acquisition of
conflicting traffic.

WARNING: XM Weather should not be used for hazardous weather
penetration. Weather information provided by the GDL 69A is approved only

for weather avoidance, not penetration.

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

Warnings, Cautions & Notes

WARNING: NEXRAD weather data is to be used for long-range planning
purposes only. Due to inherent delays in data transmission and the relative
age of the data, NEXRAD weather data should not be used for short-range

weather avoidance.

WARNING: The Garmin G1000, as installed in the Cessna Citation Mustang
aircraft, has a very high degree of functional integrity. However, the pilot
must recognize that providing monitoring and/or self-test capability for all
conceivable system failures is not practical. Although unlikely, it may be
possible for erroneous operation to occur without a fault indication shown
by the G1000. It is thus the responsibility of the pilot to detect such an
occurrence by means of cross-checking with all redundant or correlated
information available in the cockpit.

WARNING: For safety reasons, G1000 operational procedures must be learned
on the ground.

WARNING: The United States government operates the Global Positioning
System and is solely responsible for its accuracy and maintenance. The GPS
system is subject to changes which could affect the accuracy and performance
of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a
precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs,
information presented by the G1000 can be misused or misinterpreted and,
therefore, become unsafe.

WARNING: To reduce the risk of unsafe operation, carefully review and
understand all aspects of the G1000 Pilot’s Guide documentation and the
Cessna Citation Mustang Airplane Flight Manual. Thoroughly practice basic
operation prior to actual use. During flight operations, carefully compare
indications from the G1000 to all available navigation sources, including
the information from other NAVAIDs, visual sightings, charts, etc. For safety
purposes, always resolve any discrepancies before continuing navigation.

WARNING: The illustrations in this guide are only examples. Never use
the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory
Circular, Subject: Thunderstorms, and the Aeronautical Information Manual
(AIM) recommend avoiding “by at least 20 miles any thunderstorm identified
as severe or giving an intense radar echo.”

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Warnings, Cautions & Notes

CAUTION: The GDU 1040A PFDs and GDU 1500 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 ANTI-REFLECTIVE 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 anti-reflective coatings.

CAUTION: The Garmin G1000 does not contain any user-serviceable parts.
Repairs should only be made by an authorized Garmin service center.
Unauthorized repairs or modifications could void both the warranty and the
pilot’s authority to operate this device under FAA/FCC regulations.

NOTE: All visual depictions contained within this document, including screen
images of the G1000 panel and displays, are subject to change and may not
reflect the most current G1000 system. Depictions of equipment may differ
slightly from the actual equipment.

NOTE: This device complies with part 15 of the FCC Rules. Operation is
subject to the following two conditions: (1) this device may not cause harmful
interference, and (2) this device must accept any interference received,
including interference that may cause undesired operation.

NOTE: 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: 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.

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

Part Number Change Summary

190-00600-00

Rev A

Initial release

Rev B

Added Additional Features section

190-00600-01

Rev A

Rev B

Production release

Added CAS INOP system messages

Revision Date of Revision Affected Pages Description

C May, 2007 Pages 6

Pages 36, 37
Page 51

Added COM 3 function for HF.
Added TAS.
Removed automatic Reversionary
Mode operation.

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Table of Contents

Flight Instruments ....................................................................................................................... 1

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

Selecting Standard Barometric Pressure (29.92 in Hg) .................................................... 1

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

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

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

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

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

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

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

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

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

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

Nav/Com/Transponder/Audio Panel ................................................................................... 5

Enter or Change Flight ID ....................................................................................................... 5

ADF Tuning (Optional) .............................................................................................................. 5

DME Tuning ................................................................................................................................ 5

Enter a Transponder Code ...................................................................................................... 6

Selecting a COM Radio ............................................................................................................ 6

Selecting a NAV Radio ............................................................................................................. 6

NAV/COM Tuning ....................................................................................................................... 6

Digital Clearance Recorder and Player ................................................................................ 7

Automatic Flight Control System ....................................................................................... 9

Flight Director Activation ....................................................................................................... 9

Vertical Modes ......................................................................................................................... 10

Lateral Modes .......................................................................................................................... 11

GPS Navigation ........................................................................................................................... 13

Direct-to Navigation .............................................................................................................. 13

Activate a Stored Flight Plan ............................................................................................... 14

Activate a Flight Plan Leg ..................................................................................................... 14

Stop Navigating a Flight Plan .............................................................................................. 15

Vertical Navigation ................................................................................................................. 15

Flight Planning ............................................................................................................................ 17

Weight Planning ...................................................................................................................... 17

Trip Planning ............................................................................................................................ 17

Create a New User Waypoint ............................................................................................... 19

Delete a User Waypoint ......................................................................................................... 20

Create a New Flight Plan ...................................................................................................... 20

Insert a Waypoint in the Active Flight Plan ...................................................................... 21

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Table of Contents

Enter an Airway in a Flight Plan .......................................................................................... 22

Invert An Active Flight Plan .................................................................................................. 23

Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 23

Store a Flight Plan .................................................................................................................. 24

Edit a Stored Flight Plan ....................................................................................................... 24

Delete a Waypoint from the Flight Plan ............................................................................ 24

Invert and Activate a Stored Flight Plan ........................................................................... 25

Copy a Flight Plan ................................................................................................................... 25

Delete a Flight Plan ................................................................................................................ 25

Graphical Flight Plan Creation ............................................................................................. 26

Procedures ..................................................................................................................................... 27

Load and Activate a Departure Procedure ....................................................................... 27

Activate A Departure Leg ..................................................................................................... 27

Load An Arrival Procedure .................................................................................................... 27

Activate An Arrival Leg ......................................................................................................... 28

Load and/or Activate an Approach Procedure ................................................................. 28

Activate An Approach in the Active Flight Plan ............................................................... 29

Activate a Vector to Final Approach Fix ............................................................................ 29

Activate A Missed Approach in the Active Flight Plan ................................................... 29

Hazard Avoidance ......................................................................................................................31

Customizing the Hazard Displays on the Navigation Map ............................................ 31

XM Weather (Optional) .......................................................................................................... 31

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

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

Airborne Color Weather Radar ............................................................................................ 41

Additional Features .................................................................................................................. 47

SafeTaxi™ ................................................................................................................................ 47

ChartView ................................................................................................................................. 47

FliteCharts™ ............................................................................................................................ 47

View Charts from the Navigation Map Page .................................................................... 47

View Charts from the Active Flight Plan Page ................................................................. 48

Change Day/Night View ........................................................................................................48

XM® Radio Entertainment .................................................................................................... 49

Abnormal Operation ................................................................................................................ 51

Reversionary Mode ................................................................................................................ 51

Abnormal COM Operation .................................................................................................... 51

Hazard Displays with Loss of GPS Position ....................................................................... 51

Unusual Attitudes ................................................................................................................... 52

Dead Reckoning ...................................................................................................................... 53

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Table of Contents

Annunciations & Alerts ........................................................................................................... 55

CAS Messages .......................................................................................................................... 55

Appendix ......................................................................................................................................... 79

PFD Softkey Map .................................................................................................................... 79

MFD Softkey Map ................................................................................................................... 84

SD Card Use .............................................................................................................................. 86

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

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Flight Instruments

FLIGHT INSTRUMENTS

SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING

Turn the BARO Knob to select the desired setting.

SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)

1)

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

2)

Press the STD BARO Softkey.

OR

Push the BARO Knob to select standard pressure.

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

1)

Press the MENU Key to display the PFD Setup Menu.

2)

Turn the

3)

Turn the

4)

Press the MENU Key to remove the window.

large

FMS Knob to highlight the ‘Baro Sync’ ON/OFF field.

small

FMS Knob clockwise to ON or counterclockwise to OFF.

SYNCHRONIZE CDI

1)

Press the MENU Key to display the PFD Setup Menu.

2)

Turn the large FMS Knob to highlight ‘CDI SYNC OFF’.

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Flight Instruments

3)

Turn the small FMS Knob in the direction of the green arrowhead to select
ON.

4)

Press the MENU Key to remove the window.

CHANGE NAVIGATION SOURCES

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
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 a CRS Knob to select the desired course to/from the waypoint. Press a
CRS Knob to synchronize the Selected Course with the bearing to the next

waypoint.

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
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

1)

Press the TMR/REF Softkey.

2)

Turn the

2

large

FMS Knob to highlight the desired Vspeed.

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

3)

Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
speed has been changed from a default value, an asterisk appears next to
the speed).

4)

Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field

5)

Turn the

6)

To remove the window, press the CLR Key or the TMR/REF Softkey.

small

FMS Knob clockwise to ON or counterclockwise to OFF.

TURN VSPEED BUGS ON OR OFF BY CATEGORY

1)

Press the TMR/REF Softkey.

2)

Press the MENU Key.

3)

Turn the FMS Knob to highlight the desired option.

4)

Press the ENT Key. Press the TMR/REF Softkey to remove the window.

SET BAROMETRIC MINIMUM DESCENT ALTITUDE

1)

Press the TMR/REF Softkey.

2)

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

3)

Turn the small FMS Knob clockwise to BARO.

4)

Press the ENT Key.

5)

Use the small FMS Knob to enter the desired altitude.

6)

Press the ENT Key.

7)

To remove the window, press the CLR Key or the TMR/REF Softkey.

Flight Instruments

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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Flight Instruments

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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)

1)

Press the ADF/DME Softkey.

2)

Turn the small FMS Knob to enter the first digit of the desired ADF
frequency.

3)

Turn the large FMS Knob to select the next desired field.

4)

Turn the small FMS Knob to enter the desired number.

5)

Repeat steps 3 and 4 until the desired ADF frequency is entered.

6)

Press the ENT Key to accept the new frequency.

7)

Press the ENT Key again to transfer the frequency to the active field.

8)

Turn the large FMS Knob to select the MODE field.

9)

Turn the small FMS Knob to select ANT, ADF, ADF/BFO, or ANT/BFO.

10)

Press the ENT Key to complete the selection.

Nav/Com/XPDR/Audio Panel

DME TUNING

1)

Press the ADF/DME or DME Softkey.

2)

Turn the large FMS to select the DME source field.

3)

Turn the small FMS Knob to select the desired DME tuning.

4)

Press the ENT Key to complete the selection.

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Nav/Com/XPDR/Audio Panel

ENTER A TRANSPONDER CODE

1)

Press the XPDR Softkey to display the transponder mode selection softkeys.

2)

Press the XPDR1 or XPDR2 Softkey to select the active transponder.

3)

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

4)

Press the digit softkeys to enter the code in the code field. When entering
the code, the next key in sequence must be pressed within 10 seconds, or
the entry is cancelled and restored to the previous code. Five seconds after
the fourth digit has been entered, the transponder code becomes active.

SELECTING A COM RADIO

Transmit

Press the COM1 MIC, COM2 MIC
the audio panel.

Receive

Press the COM1, COM2

, or

, or

COM3 MIC Key (HF, if installed) on

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

SELECTING A NAV RADIO

1)

Press the CDI Softkey to select NAV1 (VOR1/LOC1) or NAV2 (VOR2/LOC2).

2)

Pressing the NAV1, NAV2, DME, or ADF Key selects and deselects the
navigation radio audio source. All radio keys can be selected individually or
together.

NAV/COM TUNING

1)

Press the small tuning knob to select the desired radio for tuning.

2)

Turn the respective tuning knobs to enter the desired frequency into the
standby frequency field. The large knob enters MHz and the small knob
enters kHz.

3)

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

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Nav/Com/XPDR/Audio Panel

DIGITAL CLEARANCE RECORDER AND PLAYER

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

COM 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.

Key is recorded. Audio is

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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 flight director 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

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

ALT Key

Takeoff (on ground)

Go Around (in air)

TO

GA

Roll Hold (default) ROL Altitude Hold ALT

Takeoff (on ground)

Go Around (in air)TOGA

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

GPS

APR Key Approach**

VOR

Pitch Hold (default) PIT

LOC

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.

BC

***The selected navigation receiver must have a valid LOC signal before

director.

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Key press activates flight

9

AFCS

VERTICAL MODES

Vertical Mode Description Control Annunciation

Holds the current aircraft pitch attitude;

Pitch Hold

Selected Altitude
Capture

Altitude Hold Holds the current Altitude Reference ALT Key ALT nnnnn FT

Vertical Speed

Flight Level Change,
IAS Hold

Flight Level Change,
Mach Hold

Vertical Path
Tracking

VNV Target Altitude
Capture

Glidepath

Glideslope

Takeoff (on ground)

Go Around (in air)

* ALTS armed automatically when PIT, VS, FLC, TO, or GA active, and under VPTH when Selected

Altitude is to be captured instead of VNV Target Altitude

** ALTV armed automatically under VPTH when VNV Target Altitude is to be captured instead of

Selected Altitude

may be used to climb/descend to the
Selected Altitude

Captures the Selected Altitude

Maintains the current aircraft vertical
speed; may be used to climb/descend
to the Selected Altitude

Maintains the current aircraft airspeed
(in IAS or Mach) while the aircraft is
climbing/descending to the Selected
Altitude

Captures and tracks descent legs of an
active vertical profile

Captures the Vertical Navigation (VNV)
Target Altitude

Captures and tracks the WAAS
glidepath on approach

Captures and tracks the ILS glideslope
on approach

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

FLC nnn KT

FLC Key

FLC M .nnn

VNV

Key

VPTH

** ALTV

GP

APR Key

GS

TO

GA

Switch

GA

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190-00600-01 Rev. C

AFCS

LATERAL MODES

Lateral Mode Description Control Annunciation

Holds current aircraft roll attitude

Roll Hold

Low Bank

Heading Select

Navigation, GPS Arm/
Capture/Track

Navigation, VOR Enroute
Arm/Capture/Track

Navigation, LOC Arm/
Capture/Track
(No Glideslope)

Backcourse Arm/Capture/
Track

Approach, GPS Arm/
Capture/Track

Approach, VOR Arm/
Capture/Track

Approach, ILS Arm/
Capture/Track
(Glideslope Mode
automatically armed)

Takeoff (on ground)

Go Around (in 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.

or rolls wings level, depending
on commanded bank angle

Limits maximum commanded
roll angle

Captures and tracks Selected
Heading

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

Captures and tracks a localizer
signal for backcourse approaches

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

Disengages autopilot and
commands a constant pitch
angle and wings level in
preparation for takeoff

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

(default) ROL

BANK

Key

HDG

Key

*

HDG

GPS

NAV

VOR

Key

LOC

BC Key BC

GPS

VAPP

APR Key

LOC

TO

GA

Switch

GA

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AFCS

Roll Hold Mode (ROL)

Bank Angle Flight Director Response

< 6 deg Rolls wings level

6 to 30 deg Maintains current aircraft roll attitude

> 30 deg Limits bank to 30 degrees

Roll Hold Mode Responses

12

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

GPS NAVIGATION

DIRECT-TO NAVIGATION

Direct-to Navigation from the MFD

1)

Press the Direct-to

2)

Enter the destination waypoint identifier.

3)

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

4)

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

5)

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

6)

Enter the desired altitude.

7)

Press the ENT Key. The option to select MSL or AGL is now displayed.

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 (-) or after (+) the waypoint.

11)

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

12)

Press the ENT Key to activate.

( )

Key.

GPS Navigation

Direct-to Navigation from the PFD

1)

Press the Direct-to Key

2)

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

3)

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

4)

Press the ENT Key.

5)

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

6)

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

7)

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

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

( )

.

13

GPS Navigation

8)

Press the ENT Key. The option to select MSL or AGL is now displayed.

9)

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

10)

Press the ENT Key. The cursor is placed in the ‘VNV’ offset distance field.

11)

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

the selected Direct-to.

12)

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

highlight the ‘COURSE’ 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 again to activate the Direct-to.

ACTIVATE A STORED FLIGHT PLAN

1)

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

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight the desired flight plan

4)

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

5)

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

ACTIVATE A FLIGHT PLAN LEG

1)

From the Active Flight Plan Page, press the FMS Knob to activate the cursor
and turn the large FMS Knob to highlight the desired destination waypoint.

2)

Select the ACT LEG Softkey.

OR

3)

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.

4)

With ‘Activate’ highlighted, press the ENT Key.

14

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

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

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

190-00600-01 Rev. C

Small Light

Blue Text

Small Light

Blue Subdued

Text

Small White Text

with Altitude

Restriction Bar

Stay AT or ABOVE 5,000 ft

Stay AT 2,300 ft

Stay AT or BELOW 3,000 ft

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

15

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 or
approach for giving vertical speed and deviation guidance. Note that these altitudes
will be displayed as blue text up to, but not including the FAF. The FAF will always be
a “reference only” altitude and cannot be designated, unless the selected approach does
not provide vertical guidance. In this case, the FAF altitude can be designated.

Altitudes that have been designated for use in vertical guidance may also be made
“non-designated” by placing the cursor over the desired altitude and pressing the CLR
Key. The altitude is now displayed only as a reference. It will not be used to give
vertical guidance. Other displayed altitudes may change due to re-calculations or
rendered invalid as a result of manually changing an altitude to a non-designated
altitude.

White Text Light Blue Text Light Blue

Subdued Text

Large Text

Small Text

16

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
speed and deviation
guidance.

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

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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

Altitude is designated
for use in giving vertical
speed and deviation
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
speed and deviation
guidance.

The system cannot
use this altitude in
determining vertical
speed and deviation
guidance.

190-00600-01 Rev. C

Flight Planning

FLIGHT PLANNING

WEIGHT PLANNING

All procedures apply to the MFD unless otherwise stated.

Entering Weight Parameters

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

FMS

Knob to select the first rectangular page icon.

1)

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

FMS

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

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

1)

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

2)

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

3)

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

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

17

Flight Planning

4)

For Direct-to planning:

a)

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

b)

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

c)

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

d)

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

OR

5)

For point-to-point planning:

a)

Enter the identifier of the starting waypoint.

b)

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

c)

Again, enter the identifier of the ending waypoint.

d)

Press the ENT Key to accept the waypoint.

OR

6)

For flight plan leg planning:

a)

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

b)

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

c)

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

d)

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’ will display 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.

18

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

7)

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

190-00600-01 Rev. C

Flight Planning

8)

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

9)

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

10)

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.

11)

The flashing cursor moves to the calibrated airspeed field. Enter a calibrated

airspeed. Press the ENT Key when finished.

CREATE A NEW USER WAYPOINT

1)

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

2)

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

3)

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

4)

Enter the desired waypoint name.

5)

Press the ENT Key.

6)

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

a)

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

b)

Turn the large FMS Knob to select the desired waypoint.

c)

Press the ENT Key.

OR

a)

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

b)

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

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

OR

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

19

Flight Planning

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.

7)

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

8)

Press the ENT Key.

9)

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

10)

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

waypoint, if desired.

11)

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.

CREATE A NEW FLIGHT PLAN

Using the MFD

1)

Press the FPL Key.

2)

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

3)

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

20

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

Flight Planning

4)

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

5)

Enter the identifier of the departure waypoint.

6)

Press the ENT Key.

7)

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

8)

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

Using the PFD

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

using the PFD.

NOTE: After the first leg is entered (using the PFD only) it is immediately

activated.

1)

Press the FPL Key.

2)

Press the FMS Knob to activate the cursor.

3)

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

4)

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

5)

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

6)

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

7)

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

8)

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

INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN

1)

Press the FPL Key to display the active flight plan.

2)

Press the FMS Knob to activate the cursor.

3)

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

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

21

Flight Planning

4)

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

5)

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

a)

Enter the user waypoint identifier, facility, or city.

b)

Press the ENT Key.

OR

a)

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

b)

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

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

OR

a)

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

b)

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

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

ENTER AN AIRWAY IN A FLIGHT PLAN

1)

Press the FPL Key to display the active flight plan or display a stored flight
plan.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight the waypoint before which the airway
will be entered.

4)

Enter the desired airways entry point. When the first alphanumeric key is
pressed, the Waypoint Information Window will be displayed.

5)

Press the ENT Key.

6)

Enter the desired airway identifier. When the first alphanumeric key is
pressed, the Waypoint Information Window will be displayed.

7)

Press the LD AIRWY Softkey.

22

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

Flight Planning

8)

Turn either FMS Knob to scroll through the list of available exit points.

9)

With the desired exit point highlighted, press the ENT Key.

10)

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

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.

a)

Press the FMS Knob to activate the cursor.

OR

a)

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.

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

23

Flight Planning

STORE A FLIGHT PLAN

1)

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

2)

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

3)

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

EDIT A STORED FLIGHT PLAN

1)

Press the FPL Key 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.

6)

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

24

1)

Press the FPL Key to display the active flight plan.

a)

Press the FMS Knob to activate the cursor.

OR

a)

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.

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

190-00600-01 Rev. C

INVERT AND ACTIVATE A STORED FLIGHT PLAN

1)

Press the FPL Key.

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?’ will be
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.

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.

Flight Planning

DELETE A FLIGHT PLAN

1)

Press the FPL Key.

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.

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

25

Flight Planning

GRAPHICAL FLIGHT PLAN CREATION

1)

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

2)

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

3)

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

4)

Select the LD WPT Softkey. The selected waypoint will be 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.

FMS Knob to activate the cursor. Waypoints are inserted

ABOVE

26

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

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

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 will be active
when the flight plan is active.

FMS Knob to select the desired runway.

Procedures

ACTIVATE A DEPARTURE LEG

1)

Press the FPL Key to display the active flight plan.

2)

Press the FMS Knob to activate the cursor.

3)

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

4)

Select the ACT LEG Softkey. A confirmation window showing the selected
leg will be 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.

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

27

Procedures

4)

Turn the large FMS Knob to highlight the desired arrival.

5)

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 is displayed for the selected arrival.

8)

Turn the large FMS Knob to highlight the desired runway.

9)

Press the ENT Key.

10)

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

11)

The arrival will become 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)

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

4)

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

5)

With ‘ACTIVATE’ highlighted, press the ENT Key.

LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE

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.

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 the either FMS Knob to highlight the desired approach.

The WAAS channel and ID for the selected approach procedure are
displayed in the ‘APPROACH CHANNEL’ field.

5)

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

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

6)

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

7)

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

8)

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

Selecting ‘LOAD?’ will enter the selected approach procedure into the
active flight plan, but will not be currently active. Selecting ‘ACTIVATE?’
will enter the selected approach procedure into the active flight plan and
immediately activate it.

9)

Press the ENT Key.

ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN

1)

Press the PROC Key.

2)

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

3)

Press the ENT Key. A confirmation window will be displayed.

4)

With ‘ACTIVATE’ highlighted, press the ENT Key.

Procedures

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)

A direct-to vector is established to the final approach fix.

ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN

1)

Press the PROC Key.

2)

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

3)

Press the ENT Key. A confirmation window will be displayed.

4)

With ‘ACTIVATE’ highlighted, press the ENT Key.

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Procedures

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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
option.

2)

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

3)

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

XM WEATHER (OPTIONAL)

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

Menu. The cursor flashes on the ‘Map Setup’

1)

Press the MAP Softkey.

2)

Press the NEXRAD or XM LTNG Softkey to display the desired weather.
Press 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.

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Hazard Avoidance

4)

Select the LEGEND Softkey to view the legends for the selected products.
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,
or SIGMETs.

3)

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

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

Weather Products and Symbols

Echo Top (Cloud Top and Echo Top Mutually Exclusive)

NEXRAD

32

Cell Movement

XM Lightning

Cloud Top

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

SIGMETs/AIRMETs

City Forecast

METARs

Freezing Levels

Surface Analysis

Winds Aloft

Cyclone Warnings

County Warnings

190-00600-01 Rev. C

Weather Product Age

Hazard Avoidance

Weather Product

Expires After

(minutes)

Refresh Rate

(minutes)

SIGMETs/AIRMETs 60 12
City Forecasts
County Warnings
Cyclone Warnings
Echo Tops
Freezing Levels
METARs

90 12
60 5
60 12
30 7.5
60 12

90 12
Lightning 30 5
NEXRAD 30 5
Cell Movement 30 1.25
Surface Analysis

60 12
TFRs 60 12
Winds Aloft
TAFs
Clouds Tops

60 12

60 12

60 15

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Hazard Avoidance

TRAFFIC SYSTEMS

• If Traffic information Service (TIS) is configured, a STANDBY, OPERATE, and
TNA MUTE Softkey will be displayed.

• If a Traffic Advisory System (TAS) is configured, a STANDBY, OPERATE, TEST,
and ALT MODE Softkey will be displayed.

TAS Symbol Description

Non-Threat Traffic

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

Proximity Advisory (PA)

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

Traffic Advisory (TA)

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

Traffic Advisory Off Scale

Traffic Symbol Description

Traffic Information Service (TIS)

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

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

Operating

Mode

Traffic Advisory,

Off Scale Aircraft

is Out of Range,

200’ Above and

Descending

Display

of System

Status

Hazard Avoidance

Non-Threat
Traffic

Proximity
Advisory, 1700’
Above and
Descending

Mutes “TIS Not
Available” Voice
Alert

Traffic Advisory, Aircraft

is 400’ Below and

Climbing

Non-Bearing Traffic (System is Unable to

Determine Bearing), Aircraft Distance is 8.0

nm, 1100’ Above and Descending

Traffic Map Page - TIS

Displaying Traffic on the Traffic Map Page

1)

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

2)

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

3)

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

4)

Select the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ will be 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, press the
MAP Softkey.

2)

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

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Hazard Avoidance

Traffic Advisory System (TAS) (Optional)

Operating

Mode

Traffic Advisory,

Off Scale Aircraft

is Out of Range,

200’ Above and

Descending

Non-Threat
Traffic

Proximity
Advisory, 1700’
Above and
Descending

Traffic Advisory, Aircraft

is 400’ Below and

Climbing

Non-Bearing Traffic (System is Unable to

Determine Bearing), Aircraft Distance is 8.0

nm, 1100’ Above and Descending

Traffic Map Page - TAS

System Self Test

1)

Set the range to 2/6 nm.

2)

Press the STANDBY Softkey.

3)

Press the TEST Softkey.

4)

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

Displaying Traffic on the Traffic Map Page

1)

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

2)

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

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190-00600-01 Rev. C

Hazard Avoidance

3)

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

4)

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

5)

Press the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ will be displayed in the Traffic Mode field.

6)

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

Displaying Traffic on the Navigation Map

1)

Ensure the KTA 870 system is operating. With the Navigation Map
displayed, press the MAP Softkey.

2)

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

TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY

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

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

Manual System Test

1)

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

2)

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

3)

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

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

Display Terrain on the TAWS Page

1)

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

2)

Turn the small FMS Knob to select the TAWS Page.

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Hazard Avoidance

Potential Impact Point

Unlighted Obstacle

Projected Flight Path

1000'

100' Threshold

3)

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

4)

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

Color Terrain/Obstacle Location

Red

Yellow

Black

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

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

Terrain/Obstacle is more than 1000’

below aircraft altitude.

Unlighted Obstacle
(Height is less than
1000’ AGL)

Lighted Obstacle
(Height is less
than 1000’ AGL)

Unlighted Obstacle
(Height is greater
than 1000’ AGL)

Lighted Obstacle
(Height is greater
than 1000’ AGL)

TAWS Colors & Symbols

Imminent Terrain Impact (ITI) and Imminent Obstacle Impact (IOI)

Phase of Flight Level Flight Descending

38

Enroute 700 ft 500 ft

Terminal 350 ft 300 ft

Approach 150 ft 100 ft

Departure 100 ft 100 ft

Terrain & Obstacle Clearance Thresholds for Alerting

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

Potential
Impact
Points

Premature Descent Alert (PDA)

700

600

500

400

300

200

100

Height Above Terrain (Feet)

Distance From Destination Airport (nm)

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15

“Too Low, Terrain”“Too Low, Terrain”

Runway

Threshold

6000

5500

5000

4500

4000

3500

3000

2500

2000

1500

1000

500

0

2000 4000 6000 8000 10000 12000

"PULL UP""PULL UP"

"SINK RA

TE"

Descent Rate

Height Above Terrain (Feet)

PDA Alerting

Excessive Descent Rate Alert (EDR)

Hazard Avoidance

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Excessive Descent Rate Alerting

39

Hazard Avoidance

1000

800

600

400

200

Height Above Terrain (Feet)

Altitude Loss (Feet)

0 20 40 60 80 100 120 140

“DON’T SINK”“DON’T SINK”

1000

900

800

700

600

500

400

300

200

100

Height Above Terrain (Feet)

Sink Rate (Feet Per Minute)

0

“DON’T SINK”“DON’T SINK”

500 1000 1500 2500 35002000 3000 4000

Negative Climb Rate After Takeoff Alert (NCR)

The purpose of the Negative Climb Rate After Takeoff alert is to provide suitable
alerts to the pilot when the system determines that the aircraft is losing altitude (closing
upon terrain) after takeoff. The aural message “Don’t Sink” is given for NCR alerts,
accompanied by an annunciation and a pop-up terrain alert on the display.

Negative Climb Rate (NCR) Alerting

“Five-Hundred” Aural Alert

The purpose of the aural alert message “Five-hundred” is to provide an advisory
alert to the aircrew that the aircraft is five-hundred feet above terrain. When the aircraft
descends within 500 feet of terrain, the aural message “Five-hundred” is heard.

Enable/Disable Aviation Data

1)

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

2)

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

3)

40

Press the ENT Key.

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

Hazard Avoidance

TAWS Inhibit

Inhibit TAWS

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

OR

1)

Press the MENU Key.

2)

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

3)

Press the ENT Key.

Enable TAWS

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

OR

1)

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

2)

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

3)

Press the ENT Key.

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.

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.

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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Hazard Avoidance

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.

Weather Mode

Color

BLACK < 23 dBZ < .01 in./hr.

GREEN 23 dBZ to < 32 dBZ .01 - 0.1 in./hr.

YELLOW 32 dBZ to < 41 dBZ 0.1 - 0.5 in./hr.

RED 41 dBZ to < 50 dBZ 0.5 - 2 in./hr.

MAGENTA 50 dBZ and greater > 2 in./hr.

Intensity

Approx.

Rainfall Rate

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.

Adjusting Antenna Bearing

Move the

Joystick

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

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

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:

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

Hazard Avoidance

1)

Press the MENU Key

2)

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

3)

Press the ENT Key.

Vertically Scan a Storm Cell

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

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

2)

Select the VERTICAL Softkey. A vertical ‘slice’ of the selected area will now
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
to return to the Horizontal Scan view and repeat the previous steps.

Adjusting Gain

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.

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.

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43

Hazard Avoidance

4)

Press the FMS Knob to activate the cursor.

5)

Turn the large FMS Knob to place the cursor in the ‘TILT’ field.

6)

Adjust the antenna tilt angle by turning the small FMS Knob to position the
ground returns as desired.

7)

Press the FMS Knob to remove the cursor.

Ground Map

Mode Color

BLACK 0 dB

LIGHT BLUE > 0 dB to < 9 dB

YELLOW 9 dB to < 18 dB

MAGENTA 18 dB to < 27 dB

BLUE 27 dB and greater

Intensity

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.

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.

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Hazard Avoidance

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.

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Hazard Avoidance

Blank Page

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

Additional Features

ADDITIONAL FEATURES

NOTE: The availability of SafeTaxi™, ChartView, or FliteCharts™ in electronic
form does not preclude the requirement to carry paper charts aboard the
aircraft. See AC 120-76A for more information.

SAFETAXI™

SafeTaxi™ is an enhanced feature that gives greater map detail when zooming in on
airports at close range. The airport display on the map reveals runways with numbers,
taxiways with identifying letters/numbers, and airport landmarks including ramps,
buildings, control towers, and other prominent features. Resolution is greater at lower
map ranges. When the aircraft location is within the screen boundary, including within
SafeTaxi ranges, an airplane symbol is shown on any of the navigation map views for
enhanced position awareness.

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

CHARTVIEW

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

FLITECHARTS™

FliteCharts™ resemble the paper version of National Aeronautical Charting Office
(NACO) terminal procedures charts. The charts are displayed with high-resolution
and in color for applicable charts.

VIEW CHARTS FROM THE NAVIGATION MAP PAGE

1)

Press the SHW CHRT Softkey while viewing the navigation map. This will
display the airport diagram for the closest airport, if available.

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47

Additional Features

OR

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

2)

Press the DP, STAR, APR, WX, and NOTAM softkeys to access charts for
departures, arrivals, approaches, weather and NOTAMs.

3)

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

VIEW CHARTS FROM THE ACTIVE FLIGHT PLAN PAGE

1)

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

2)

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

3)

Press the SHW CHRT Softkey. The appropriate chart will be displayed, if
available for the item selected.

4)

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

CHANGE DAY/NIGHT VIEW

48

1)

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

2)

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

3)

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

4)

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

5)

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

6)

In Auto Mode, turn the large FMS Knob to select the percentage field and
change percentage with the small FMS Knob. The percentage of change is
the day/night crossover point based on backlighting intensity.

7)

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

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

Additional Features

XM® RADIO ENTERTAINMENT

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

Selecting the XM Radio Page

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)

Press 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.

Selecting a Category

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

1)

Select the CATGRY Softkey on the XM Radio Page.

2)

Press the CAT + and CAT - Softkeys to cycle through the categories.

OR

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

3)

Press the ENT Key.

Select an Available Channel within the Selected Category

1)

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

2)

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

OR

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

3)

With the desired channel highlighted, press the ENT Key.

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Additional Features

Entering a Channel Directly

1)

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

2)

Press the DIR CH Softkey. The channel number in the Active Channel Box
will be highlighted.

3)

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

4)

Press the ENT Key to activate the selected channel.

Assigning Channel Presets

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

1)

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

2)

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

3)

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

4)

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

Adjusting Volume

Radio volume is controlled at each passenger station.

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Abnormal Operation

ABNORMAL OPERATION

REVERSIONARY MODE

Reversionary Mode is a mode of operation in which all important flight information
is presented identically on at least one of the remaining displays. Flight parameters are
presented in the same format as in normal mode.

Reversionary display mode can be manually activated by the pilot.

• 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 Citation Mustang Airplane Flight Manual (AFM) always takes
precedence over the information found in this section.

ABNORMAL COM OPERATION

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

HAZARD DISPLAYS WITH LOSS OF GPS POSITION

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

Loss of Hazard Functions with Loss of GPS

Position

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Abnormal Operation

UNUSUAL ATTITUDES

The PFD will ‘declutter’ when the aircraft enters an unusual attitude. Only the

primary functions will be displayed in these situations.

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

are disabled) when the aircraft experiences unusual attitudes:

• Traffic Annunciations

• AFCS Annunciations

• Flight director Com

-

mand Bars

• Inset Map

• Temperatures

• DME Information
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

Extreme Pitch Indication

• Glideslope, Glide

­path, and Vertical
Deviation Indicators

• Altimeter Barometric
Setting

• Selected Altitude

• VNV Target Altitude

52

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

Abnormal Operation

DEAD RECKONING

While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS
solution or is unable to calculate a GPS position, the system will automatically revert
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 will only function in Enroute (ENR) or Oceanic
(OCN) phase of flight. In all other phases, an invalid GPS solution will produce
a “NO GPS POSITION” annunciation on the map and the G1000 will stop
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’ will be prominently displayed, also in yellow, on the HSI
slightly above and to the right of the aircraft symbol on the CDI as shown in the
following figure. Also, the CDI deviation bar is removed from the display. Lastly, but
at the same time, a ‘GPS NAV LOST’ alert message will appear on the PFD.

Normal navigation using GPS/WAAS source data will resume 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 accurately tracking your estimated
position and, consequently, the system may display a path that is different than the
actual movement of the aircraft. Estimated position information displayed by the
G1000 through DR while there is no heading and/or airspeed data available should
not be used for navigation.

DR Mode is inherently less accurate than the standard GPS/WAAS Mode due to the
lack of satellite measurements needed to determine a position. Changes in wind speed
and/or wind direction will compound 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.

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

53

Abnormal Operation

CDI ‘DR’ Indication on PFD

Symbolic Aircraft

(Map pages and Inset Map)

Dead Reckoning Indications

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

• Navigation Status Box fields except Active Leg, TAS, and DTK

• GPS Bearing Pointer

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

• Track Bug

• All Bearing Pointer Distances

• Active Flight Plan distances, bearings, and ETE values

Also, while the G1000 is in DR Mode, the autopilot will not couple to GPS, and
both TAWS and Terrain Proximity will be disabled. Additionally, the accuracy of all
nearest information (airports, airspaces, and waypoints) will be questionable. Finally,
airspace alerts will continue to function, but with degraded accuracy.

54

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

CAS MESSAGES

Annunciations & Alerts

ANNUNCIATIONS & ALERTS

Messages

Warning

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

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

ENGINE FAIL L-R* An engine has failed

GEN OFF L-R GEN OFF L-R*

Caution Advisory

AFT DOOR

AFT JBOX CB L-R*

AFT JBOX LMT L-R*

ANTISKID FAIL

BATT TEMP FAIL Battery temperature sensor failure X X

CABIN DOOR Cabin door not fully secured X

CHECK DOORS

DUCT O’HEAT L-R*

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

ENG CTRL SYS L-R*

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

FLAPS FAIL A flap system failure has occurred. X

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

FUEL FLTR BP L-R*

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

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

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

FUEL TRANSFER Fuel transfer valve open X

HYD PRESS LO Hydraulic system pressure too low X X

HYD PUMP ON Hydraulic pump running too long X X

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

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

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

One or both electrical generators
offline

Description

Inhibits

ESI

TOPI

AIR

LOPI

X X X X

X X

ESDI

X X

EMER

X

X

X

X

X

X

GND

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

55

Annunciations & Alerts

Messages

Warning

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

TAIL CONE BLD LK

Caution Advisory

NOSE DOOR L-R*

NO TIRE SPINDOWN

OXYGEN OFF Oxygen supply off X X X

P/S HTR L-R*

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

PRESS OFF

SPD BRK EXTEND Speed brakes extended X

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

STALL WARN HI

STALL WARN HTR

SURFACE DE-ICE

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

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

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

W/S O’HEAT L-R* W/S O’HEAT L-R*

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

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

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

No current detected to pitot static
heater

Air Source Selector switch in OFF or
fresh air position

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

Tailcone temp high, possible bleed
air leak.

Windshield anti-ice power ON;
temperature too high

Description

Inhibits

ESI

TOPI

AIR

LOPI

X X

X X

X X

X X

X X X

ESDI

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

EMER

X

X

X

X

GND

56

Name Inhibit

EMER Emergency Bus Mode Inhibit

ESI Engine Start Inhibit

TOPI Takeoff Operation Phase Inhibit

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

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

COMPARATOR ANNUNCIATIONS

Annunciations & Alerts

Comparator

Window Text

ALT MISCOMP

IAS MISCOMP

HDG MISCOMP

PIT MISCOMP

ROLL MISCOMP

ALT NO COMP
IAS NO COMP

HDG NO COMP

PIT NO COMP

ROLL 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 > 10 kts.

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

Difference in heading sensors is > 6 degrees.

Difference in pitch sensors is > 5 degrees.

Difference in roll sensors is > 6 degrees.

No data from one or both altitude sensors.

No data from one or both airspeed sensors.

No data from one or both heading sensors.

No data from one or both pitch sensors.

No data from one or both roll sensors..

REVERSIONARY SENSOR ANNUNCIATIONS

Reversionary

Sensor Window

Text

BOTH ON ADC1
BOTH ON ADC2

BOTH ON AHRS1

BOTH ON AHRS2

BOTH ON GPS1
BOTH ON GPS2

XSIDE ADC

XSIDE AHRS

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.

The PFD displaying this annunciation is displaying data from the cross-side Air Data
Computer.

The PFD displaying this annunciation is displaying data from the cross-side Attitude &
Heading Reference System.

Condition

Condition

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

57

Annunciations & Alerts

G1000 SYSTEM FAILURE ANNUNCIATIONS

GIA 63W
Integrated

Avionics

Units

GEA 71

Engine

Airframe

Unit

OR

GIA 63W

Integrated

Avionics

Unit

FADEC

GDC 74B Air Data

Computer

G1000 System Failure Annunciations

GIA 63W

Integrated

Avionics

Units

GDC 74B Air

Data Computer

GRS 77 AHRS

OR

GMU 44

Magnetometer

GIA 63W
Integrated

Avionics

Units

GTX 33/33D

Transponder

OR

GIA 63W

Integrated

Avionics

Units

58

System

Annunciation

Red ‘X’

Messages Window

Message Softkey

Annunciation

G1000 System Messages

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

MFD & PFD Message Advisories

Message Comments

DATA LOST

– Pilot stored data was

lost. Recheck settings.

XTALK ERROR

– A flight display

crosstalk error has occurred.

PFD1 SERVICE

– PFD1 needs

service. Return unit for repair.

PFD2 SERVICE

– PFD2 needs

service. Return unit for repair.

MFD1 SERVICE

– MFD1 needs

service. Return unit for repair.

MANIFEST

– PFD1 software

mismatch, communication halted.

MANIFEST

– PFD2 software

mismatch, communication halted.

MANIFEST

– MFD1 software

mismatch, communication halted.

PFD1 CONFIG

– PFD1 config error.

Config service req’d.

PFD2 CONFIG

– PFD2 config error.

Config service req’d.

MFD1 CONFIG

– MFD1 config error.

Config service req’d.

SW MISMATCH

– GDU software

version mismatch. Xtalk is off.

CAS INOP

– No Dispatch. Software

correction required.

Annunciations & Alerts

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

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

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

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

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

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

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

The MFD and/or PFDs have a software
mismatch. The G1000 system should be
serviced.

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

59

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 G1000
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 G1000 system should be
serviced if the problem persists.

Key is stuck.

CNFG MODULE

configuration module is inoperative.

– PFD1

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

PFD1 VOLTAGE

voltage. Reducing power usage

PFD2 VOLTAGE

voltage. Reducing power usage

MFD1 VOLTAGE

voltage. Reducing power usage

– PFD1 has low

– PFD2 has low

– MFD1 has low

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

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

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

Database Message Advisories

Message Comments

MFD1 DB ERR

– MFD1 aviation

database error exists.

PFD1 DB ERR

– PFD1 aviation

database error exists.

PFD2 DB ERR

– PFD2 aviation

database error exists.

60

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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

190-00600-01 Rev. C

Database Message Advisories (Cont.)

Message Comments

MFD1 DB ERR

– MFD1 basemap

database error exists.

PFD1 DB ERR

– PFD1 basemap

database error exists.

PFD2 DB ERR

– PFD2 basemap

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

database error exists.

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 terrain

– PFD1 terrain

– PFD2 terrain

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

database error exists.

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 obstacle

– PFD1 obstacle

– PFD2 obstacle

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

database error exists.

MFD1 DB ERR

terrain database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 airport

– PFD1 airport terrain

– PFD2 airport terrain

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

database error exists.

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 Safe Taxi

– PFD1 Safe Taxi

– PFD2 Safe Taxi

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

database error exists.

Annunciations & Alerts

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

61

Annunciations & Alerts

Database Message Advisories (Cont.)

Message Comments

MFD1 DB ERR

database error exists.

– MFD1 Chartview

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

MFD1 DB ERR

database error exists.

– MFD1 FliteCharts

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

DB MISMATCH

version mismatch. Xtalk is off.

– Aviation database

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

DB MISMATCH

type mismatch. Xtalk is off.

– Aviation database

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

DB MISMATCH

version mismatch.

– Terrain database

The PFD and MFD have different terrain
database versions installed. Install correct
terrain database version in both displays.

DB MISMATCH

type mismatch.

– Terrain database

The PFD and MFD have different terrain
database types installed. Install correct
terrain database type in both displays.

DB MISMATCH

version mismatch.

– Obstacle database

The PFD and MFD have different obstacle
database versions installed. Install correct
obstacle database version in both displays.

DB MISMATCH

database mismatch.

– Airport Terrain

The PFD and MFD have different airport terrain
databases installed. Install correct airport
terrain database in both displays.

CAS INOP

– No Dispatch. Database

correction required.

The MFD and/or PFDs have an aviation
database mismatch. Load the same aviation
database version in the MFD and both PFDs.

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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

GMA 1347D Message Advisories

Message Comments

GMA1 FAIL
GMA2 FAIL

GMA XTALK

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

– GMA crosstalk error

has occurred.

GMA1 CONFIG

– GMA1 config

error. Config service req’d.

GMA2 CONFIG

– GMA2 config

error. Config service req’d.

MANIFEST

mismatch, communication halted.

MANIFEST

mismatch, communication halted.

GMA1 SERVICE

service. Return unit for repair.

GMA2 SERVICE

service. Return unit for repair.

– GMA1 software

– GMA2 software

– GMA1 needs

– GMA2 needs

Annunciations & Alerts

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

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

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

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

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

GIA 63W Message Advisories

Message Comments

GIA1 CONFIG

– GIA1 config error.

Config service req’d.

GIA2 CONFIG

– GIA2 config error.

Config service req’d.

GIA1 CONFIG

– GIA1 audio config

error. Config service req’d.

GIA2 CONFIG

– GIA2 audio config

error. Config service req’d.

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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

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

63

Annunciations & Alerts

GIA 63W Message Advisories (Cont.)

Message Comments

GIA1 COOLING

too low.

– GIA1 temperature

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

GIA2 COOLING

– GIA2 temperature

to operating temperature.

too low.

GIA1 COOLING

temperature.

– GIA1 over

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

GIA2 COOLING

– GIA2 over

should be 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 G1000 system

GIA2 SERVICE

– GIA2 needs

should be serviced.

service. Return the unit for repair.

HW MISMATCH

– GIA hardware
mismatch. GIA1 communication
halted.

HW MISMATCH

– GIA hardware

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

mismatch. GIA2 communication
halted.

MANIFEST

mismatch, communication halted.

– GIA1 software

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

MANIFEST

– GIA2 software

serviced.

mismatch, communication halted.

COM1 TEMP

Reducing transmitter power.

COM2 TEMP

Reducing transmitter power.

– COM1 over temp.

– COM2 over temp.

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

COM1 SERVICE

service. Return unit for repair.

COM2 SERVICE

service. Return unit for repair.

– COM1 needs

– COM2 needs

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

64

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

GIA 63W Message Advisories (Cont.)

Message Comments

COM1 PTT

is stuck.

COM2 PTT

is stuck.

– COM1 push-to-talk key

– COM2 push-to-talk key

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

COM1 RMT XFR

transfer key is stuck.

COM2 RMT XFR

transfer key is stuck.

– COM1 remote

– COM2 remote

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

LOI

– GPS integrity lost. Crosscheck

with other NAVS.

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.

ABORT APR

– Loss of GPS

navigation. Abort approach.

APR DWNGRADE

– Approach

downgraded.

TRUE APR

– True north approach.

Change HDG reference to TRUE.

GPS integrity is insufficient for the current
phase of flight.

Loss of GPS navigation due to insufficient
satellites.

Loss of GPS navigation due to position error.

Loss of GPS navigation due to GPS failure.

Abort approach due to loss of GPS
navigation.

Use LNAV minima when approach is
downgraded.

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

GPS1 SERVICE

service. Return unit for repair.

GPS2 SERVICE

service. Return unit for repair.

– GPS1 needs

– GPS2 needs

A failure has been detected in the GPS1
and/or GPS2 receiver. The receiver may still
be available. The G1000 system should be
serviced.

Annunciations & Alerts

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

65

Annunciations & Alerts

GIA 63W Message Advisories (Cont.)

Message Comments

NAV1 SERVICE

service. Return unit for repair.

NAV2 SERVICE

service. Return unit for repair.

NAV1 RMT XFR

transfer key is stuck.

NAV2 RMT XFR

transfer key is stuck.

– NAV1 needs

– NAV2 needs

– NAV1 remote

– NAV2 remote

A failure has been detected in the NAV1
and/or NAV2 receiver. The receiver may still
be available. The G1000 system should be
serviced.

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

G/S1 FAIL

G/S2 FAIL

G/S1 SERVICE

Return unit for repair.

G/S2 SERVICE

Return unit for repair.

– G/S1 is inoperative. A failure has been detected in glideslope

– G/S2 is inoperative.

– G/S1 needs service.

receiver 1 and/or receiver 2. The G1000
system should be serviced.

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

– G/S2 needs service.

still be available. The G1000 system should
be serviced when possible.

GEA 71 Message Advisories

Message Comments

GEA1 CONFIG

– GEA1 config error.

Config service req’d.

GEA2 CONFIG

– GEA2 config error.

Config service req’d.

MANIFEST

– GEA1 software

mismatch, communication halted.

MANIFEST

– GEA2 software

mismatch, communication halted.

66

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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

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

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

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

190-00600-01 Rev. C

GTX 33 & GTX 33D Message Advisories

Message Comments

XPDR1 CONFIG

error. Config service req’d.

– XPDR1 config

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

XPDR2 CONFIG

error. Config service req’d.

– XPDR2 config

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

MANIFEST

mismatch, communication halted.

– GTX1 software

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

MANIFEST

mismatch, communication halted.

– GTX2 software

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

XPDR1 SRVC

service. Return unit for repair.

XPDR2 SRVC

service. Return unit for repair.

XPDR1 FAIL

– XPDR1 needs

The #1 transponder should be serviced when
possible.

– XPDR2 needs

The #2 transponder should be serviced when
possible.

– XPDR1 is inoperative. There is no communication with the #1

transponder.

XPDR2 FAIL

– XPDR2 is inoperative. There is no communication with the #2

transponder.

Annunciations & Alerts

GRS 77 Message Advisories

Message Comments

AHRS1 TAS

– AHRS1 not receiving

airspeed.

AHRS2 TAS

– AHRS2 not receiving

airspeed.

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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

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

67

Annunciations & Alerts

GRS 77 Message Advisories (Cont.)

Message Comments

AHRS1 GPS

– AHRS1 using backup

GPS source.

AHRS2 GPS

– AHRS2 using backup

GPS source.

AHRS1 GPS

– AHRS1 not receiving

any GPS information.

AHRS2 GPS

– AHRS2 not receiving

any GPS information.

AHRS1 GPS

– AHRS1 not receiving

backup GPS information.

AHRS2 GPS

– AHRS2 not receiving

backup GPS information.

AHRS1 GPS

– AHRS1 operating

exclusively in no-GPS mode.

AHRS2 GPS

– AHRS2 operating

exclusively in no-GPS mode.

AHRS MAG DB

– AHRS magnetic

model database version mismatch.

AHRS1 SRVC

– AHRS1 Magnetic-

field model needs update.

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

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

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

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

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

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

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

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

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

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

68

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

GRS 77 Message Advisories (Cont.)

Message Comments

AHRS2 SRVC

field model needs update.

– AHRS2 Magnetic-

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

GEO LIMITS

South, no magnetic compass.

– AHRS1 too far North/

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

GEO LIMITS

– AHRS2 too far North/

flagged as invalid.

South, no magnetic compass.

MANIFEST

mismatch, communication halted.

MANIFEST

mismatch, communication halted.

– GRS1 software

– GRS2 software

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

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

GMU 44 Message Advisories

Message Comments

HDG FAULT

fault has occurred.

– AHRS1 magnetometer

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

HDG FAULT

fault has occurred.

– AHRS2 magnetometer

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

MANIFEST

mismatch, communication halted.

MANIFEST

– GMU1 software

– GMU2 software

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

mismatch, communication halted.

Annunciations & Alerts

GDL 69A Message Advisories

Message Comments

GDL69 CONFIG

– GDL 69 config

error. Config service req’d.

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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

69

Annunciations & Alerts

GDL 69A Message Advisories (Cont.)

Message Comments

GDL69 FAIL

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

69. The receiver is unavailable. The G1000
system should be serviced

MANIFEST

mismatch, communication halted.

– GDL software

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

GDC 74B Message Advisories

Message Comments

ADC1 ALT EC

correction is unavailable.

ADC2 ALT EC

– ADC1 altitude error

– ADC2 altitude error

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

correction is unavailable.

ADC1 AS EC

correction is unavailable.

ADC2 AS EC

– ADC1 airspeed error

– ADC2 airspeed error

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

correction is unavailable.

MANIFEST

mismatch, communication halted.

MANIFEST

– GDC1 software

– GDC2 software

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

mismatch, communication halted.

GCU 475 Message Advisories

Message Comments

GCU CNFG

– GCU config error.

Config service req’d.

GCU FAIL

MANIFEST

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

– GCU software

mismatch, communication halted.

70

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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

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

The G1000 system should be serviced.

190-00600-01 Rev. C

GCU 475 Message Advisories (Cont.)

Message Comments

GCU KEYSTK

is stuck.

– GCU [key name] Key

A key is stuck on the GCU 475 bezel.
Attempt to free the stuck key by pressing it
several times. The G1000 system should be
serviced if the problem persists.

GMC 710 Message Advisories

Message Comments

GMC CONFIG

Config service req’d.

GMC FAIL

– GMC config error.

Error in the configuration of the GMC 710.

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

The GMC 710 is unavailable.

MANIFEST

mismatch, communication halted.

– GMC software

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

GMC KEYSTK

Key is stuck.

– GMC [key name]

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

Annunciations & Alerts

GWX 68 Alert Messages

Message Comments

GWX CONFIG

– GWX config error.

Config service req’d.

GWX FAIL

GWX SERVICE

– GWX is inoperative. The GDU is not receiving status packet from

– GWX needs

service. Return unit for repair.

MANIFEST

– GWX software

mismatch, communication halted.

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

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

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

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

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

71

Annunciations & Alerts

GWX 68 Alert Messages (Cont.)

Message Comments

WX ALERT

– Possible severe weather

ahead.

Miscellaneous Message Advisories

Message Comments

FPL WPT LOCK

waypoint is locked.

– Flight plan

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

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

FPL WPT MOVE

waypoint moved.

– Flight plan

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

TIMER EXPIRD

expired.

DB CHANGE

changed. Verify user modified
procedures.

– Timer has

– Database

The system notifies the pilot that the timer has
expired.

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

DB CHANGE

changed. Verify stored airways.

– Database

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

The GWX 68 indicates severe weather within
±10 degrees of the aircraft heading at a
range of 80 to 320 nm.

72

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

Miscellaneous Message Advisories (Cont.)

Message Comments

FPL TRUNC

been truncated.

– Flight plan has

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

LOCKED FPL

navigate locked flight plan.

– Cannot

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

WPT ARRIVAL

waypoint -[xxxx]

STEEP TURN

ahead.

INSIDE ARSPC

airspace.

ARSPC AHEAD

ahead less than 10 minutes.

– Arriving at

– Steep turn

– Inside

– Airspace

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

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

The aircraft is inside the airspace.

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

ARSPC NEAR

and ahead.

ARSPC NEAR

– less than 2 nm.

LEG UNSMOOTH

leg will not be smooth.

– Airspace near

– Airspace near

– Flight plan

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

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

The approaching flight plan waypoints are too
close to allow for smooth turns. Prepare for
steep turns ahead and expect noticeable course
deviations.

APR INACTV

active.

– Approach is not

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

SLCT FREQ

– Select appropriate

frequency for approach.

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

Annunciations & Alerts

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

73

Annunciations & Alerts

Miscellaneous Message Advisories (Cont.)

Message Comments

SLCT NAV

for approach.

– Select NAV on CDI

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

PTK FAIL

unavailable: bad geometry.

PTK FAIL

unavailable: invalid leg type.

PTK FAIL

unavailable: past IAF.

UNABLE V WPT

current vertical waypoint.

– Parallel track

– Parallel track

– Parallel track

– Can’t reach

Bad parallel track geometry.

Invalid leg type for parallel offset.

IAF waypoint for parallel offset has been passed.

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

VNV

– Unavailable. Unsupported

leg type in flight plan.

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

VNV

– Unavailable. Excessive

crosstrack error.

VNV

– Unavailable. Excessive

track angle error.

VNV

– Unavailable. Parallel course

selected.

NO WGS84 WPT

– Non WGS 84

waypoint for navigation -[xxxx]

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

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

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

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

TRAFFIC FAIL

failed.

STRMSCP FAIL

failed.

FAILED PATH

failed.

– Traffic device has

– Stormscope has

– A data path has

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

Stormscope has failed. The G1000 system
should be serviced.

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

74

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

Annunciations & Alerts

Miscellaneous Message Advisories (Cont.)

Message Comments

SCHEDULER [#]
MAG VAR WARN

magnetic variance. Verify all course
angles.

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

– Large

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

AFCS ALERTS

Condition Description

Pitch Failure Pitch axis control failure. AP is inoperative.

Roll Failure Roll axis control failure. AP is inoperative.

MET Switch Stuck, or
Pitch Trim Axis Control
Failure

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

Emergency Descent
Mode

Elevator Mistrim Up A condition has developed causing the pitch servo to

Elevator Mistrim Down A condition has developed causing the pitch servo to

Aileron Mistrim Left A condition has developed causing the roll servo to

Aileron Mistrim Right A condition has developed causing the roll servo to

Rudder Mistrim Left A condition has developed causing the yaw servo to

Rudder Mistrim Right A condition has developed causing the yaw servo to provide a

Preflight Test Performing preflight system test. Upon completion of the

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

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

provide a sustained force in the nose up direction.

provide a sustained force in the nose down direction.

provide a sustained left force.

provide a sustained right force.

provide a sustained force.

sustained force.

test, the aural alert will be heard.

Preflight system test has failed.

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

75

Annunciations & Alerts

TAWS ALERTS SUMMARY

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)

76

PFD/MFD

TAWS Page

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

MFD

Pop-Up Alert

or

or

or

or

or

or

or

Aural Message

“Pull Up”

“Terrain, Terrain; Pull Up, Pull

*

Up”*

“Terrain Ahead, Pull Up;

Terrain Ahead, Pull Up”

Terrain Ahead, Pull Up; Ter-

rain Ahead, Pull Up”

*

“Terrain, Terrain; Pull Up, Pull

Up”*

“Obstacle, Obstacle; Pull Up,

*

*

*

*

*

Pull Up”*

“Obstacle Ahead, Pull Up;

Obstacle Ahead, Pull Up”

“Obstacle Ahead, Pull Up;

Obstacle Ahead, Pull Up”

“Obstacle, Obstacle; Pull Up,

Pull Up”*

“Caution, Terrain; Caution,

Terrain”*

“Terrain Ahead; Terrain

Ahead”

“Terrain Ahead; Terrain

Ahead”

“Caution, Terrain; Caution,

Terrain”*

“Caution, Obstacle; Caution,

Obstacle”*

“Obstacle Ahead; Obstacle

Ahead”

190-00600-01 Rev. C

or

or

or

or

or

or

or

Annunciations & Alerts

Alert Type

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 Page

None None “Five-Hundred”

MFD

Pop-Up Alert

or

or

Aural Message

“Obstacle Ahead; Obstacle

Ahead”

*

“Caution, Obstacle; Caution,

*

or

Obstacle”*

“Too Low, Terrain”

“Sink Rate”

“Don’t Sink”*

or

“Too Low, Terrain”

* Mustang default configuration

TAWS STATUS ANNUNCIATIONS

PFD/MFD

Alert Type

TAWS Page

Annuncia-

tion

TAWS System Test Fail None “TAWS System Failure”

MFD

Pop-Up Alert

Aural Message

TAWS Alerting is disabled

No GPS position or excessively
degraded GPS signal

System Test in progress None None

System Test pass

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

None None “TAWS System Test OK”

None None

None “TAWS Not Available”

“TAWS Available” will be

heard when sufficient GPS

signal is re-established.

77

Annunciations & Alerts

OTHER G1000 AURAL ALERTS

Aural Alert Description

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

altitude.

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

navigation is enabled.

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

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

78

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

PFD SOFTKEY MAP

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

Appendix

APPENDIX

Top Level PFD Softkeys

INSET

OFF

DCLTR (3)

190-00600-01 Rev. C

Inset Map Softkeys

Displays Inset Map in PFD lower left corner

Removes Inset Map

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

DCLTR (No Declutter): All map features

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

active flight plan

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

79

Appendix

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

BACK

MSG

ADC2

ADC1

AHRS1

AHRS2

SENSOR

TRAFFIC

TOPO

TERRAIN

NEXRAD

XM LTNG

ADC1

ADC2

AHRS1

AHRS2

Displays traffic information on Inset Map

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

Displays terrain information on Inset Map

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

Displays XM lightning information on Inset
Map (optional feature)

Sensor Softkeys

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

Selects the #1 Air Data Computer

Selects the #2 Air Data Computer

Selects the #1 AHRS

Selects the #2 AHRS

80

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

PFD Configuration Softkeys

Select the STD BARO or
BACK Softkey to return to

the top-level softkeys

FD FRMT

ALT UNIT

METERS IN HPA

SNGL CUE

X POINTR

Appendix

PFD

190-00600-01 Rev. C

Displays second-level softkeys for ad­ditional PFD configurations

FD FRMT

Displays the softkeys for selecting the
two flight director formats

SNGL CUE

Selects the single cue flight director
format

X POINTR

Selects the cross pointer flight director
format

DFLTS

WIND

Resets PFD to default settings, including
changing units to standard

Displays softkeys to select wind data
parameters

OPTN 1

OPTN 2

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Longitudinal and lateral components

Total direction and speed

81

Appendix

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

Press the IDENT or BACK Softkey to return
to the top-level softkeys.

MSG

MSG

BRG1

BRG2

ALT UNIT

STD BARO

OPTN 3

OFF

METERS

IN

HPA

Total direction with head and crosswind
speed components

Information not displayed

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

information, and ADF/frequency.

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

information, and ADF/frequency.

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

When enabled, displays altimeter in
meters

Press to display the BARO setting as
inches of mercury

Press to display the BARO setting as
hectopacals

Sets barometric pressure to 29.92 in Hg
(1013 hPa)

82

Transponder Softkeys

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C

Appendix

XPDR

IDENT

TMR/REF

NRST

MSG

XPDR1

XPDR2

STBY

ON

ALT

GND

VFR

CODE

0 — 7

BKSP

Displays transponder mode selection
softkeys

Selects the #1 transponder as active

Selects the #2 transponder as active

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

Selects Mode A (transponder replies to
interrogations)

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

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

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

Displays transponder code selection soft­keys 0-7

Use numbers to enter code

Removes numbers entered, one at a time

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

Displays Timer/References Window

Displays Nearest Airports Window

Displays Messages Window

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

83

Appendix

MAP

DCLTR

TRAFFIC

TOPO

BACK

TERRAIN

DCLTR-2

DCLTR-3

DCLTR-1

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

NEXRAD

XM LTNG

(optional)(optional)

CAS ↓

CAS ↑

SHW CHRT

CHKLIST

(optional)(optional)

AIRWAYS

AIRWY LO

AIRWAY HI

AIRWY ON

MFD SOFTKEY MAP

MFD Softkeys

CAS ↑

CAS ↓

MAP

84

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

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

Enables second-level Navigation Map softkeys

TRAFFIC

TOPO

TERRAIN

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

Displays traffic information on Navigation Map

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

Displays terrain information on Navigation Map

190-00600-01 Rev. C

Appendix

DCLTR (3)

SHW CHRT

CHKLIST

AIRWAYS

NEXRAD

XM LTNG

BACK

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

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

Displays XM lightning information on Navigation
Map (optional feature)

Returns to top-level softkeys

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

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

flight plan

When available, displays optional airport and
terminal procedure charts

When available, displays optional checklists

190-00600-01 Rev. C

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

85

Appendix

SD CARD USE

The G1000 System uses Secure Digital (SD) cards to load and store various types of
data. For basic flight operations, SD cards are required for database storage as well as
Jeppesen aviation and ChartView database updates.

Jeppesen Databases

The Jeppesen aviation database is updated on a 28-day cycle. 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.

Both these databases are provided directly from Jeppesen. The ChartView database
should be copied to the Garmin supplied Supplemental Data Card which will reside
in the bottom card slot on the MFD. The aviation database may be installed from the
Jeppesen supplied SD data card or copied to one of the Garmin supplied Supplemen­tal Data Cards. Contact Jeppesen (www.jeppesen.com) for subscription and update
information.

The aviation database may be programmed to only one of the Supplemental Data
Cards. This card must then be used to update the PFDs and the MFD.

NOTE: After the aviation database is installed, the card may be removed
after loading the update to each LRU.

Updating the Jeppesen aviation database:

1)

With the G1000 System OFF, insert the SD card containing the aviation
database update into the top card slot of the first PFD to be updated (Label
of SD card facing left).

2)

Turn the G1000 System ON. A prompt similar to the following is displayed
in the upper left corner of the PFD:

Database Update Prompt

86

Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang

190-00600-01 Rev. C