Garmin | G1000: Cessna Citation Mustang | Garmin G1000: Cessna Citation Mustang G1000 Cockpit Reference Guide for Cessna Mustang

Garmin G1000: Cessna Citation Mustang G1000 Cockpit Reference Guide for Cessna Mustang
G1000
®
Integrated Flight Deck
Cockpit Reference Guide for the Cessna Citation Mustang
Flight Instruments
EICAS
Nav/Com/Transponder/Audio Panel
Automatic Flight Control System
GPS Navigation
Flight Planning
Procedures
Hazard Avoidance
Additional Features
Abnormal Operation
Annunciations & Alerts
Appendix
INDEx
Copyright © 2006-2010 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0435.20 or later for the Cessna
Citation Mustang. Some differences in operation may be observed when comparing the
information in this manual to earlier or later software versions.
Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.
Tel: 913/397.8200
Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: 503/391.3411
Fax 503/364.2138
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Southampton, SO40 9RB, U.K.
Tel: 44/0870.8501241
Fax: 44/0870.8501251
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: 886/02.2642.9199
Fax: 886/02.2642.9099
For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount
and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836.
Web Site Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied,
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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
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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.
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without the express permission of Garmin.
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XM Satellite Radio, Inc.; Honeywell® and Bendix/King® are registered trademarks of Honeywell
International, Inc.; CO Guardian is a trademark of CO Guardian, Inc.
June, 2010
190-00600-03 Rev. A
Printed in the U.S.A.
Warnings, Cautions & Notes
WARNING: Navigation and terrain separation must NOT be predicated upon
the use of the terrain avoidance feature. The terrain avoidance feature is NOT
intended to be used as a primary reference for terrain avoidance and does
not relieve the pilot from the responsibility of being aware of surroundings
during flight. The terrain avoidance feature is only to be used as an aid for
terrain avoidance. Terrain data is obtained from third party sources. Garmin
is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory
in nature and should not be relied upon as the sole source of obstacle and
terrain avoidance information. Always refer to current aeronautical charts
for appropriate minimum clearance altitudes.
WARNING: The altitude calculated by the GPS receivers is geometric height
above Mean Sea Level and could vary significantly from the altitude displayed
by pressure altimeters, such as the GDC 74B Air Data Computer, or other
altimeters in the aircraft. GPS altitude should never be used for vertical
navigation. Always use pressure altitude displayed by the PFD or other
pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in
the system must be updated regularly in order to ensure that the information
remains current. Pilots using any outdated database do so entirely at their
own risk.
WARNING: Do not use basemap (land and water data) information for
primary navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING: Traffic information shown on system displays is provided as an
aid in visually acquiring traffic. Pilots must maneuver the aircraft based upon
TCAS II Resolution Advisories (if installed), ATC guidance, or positive visual
acquisition of conflicting traffic.
WARNING: XM Weather should not be used for hazardous weather
penetration. Weather information provided by the GDL 69A is approved only
for weather avoidance, not penetration.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Warnings, Cautions & Notes
Warning: NEXRAD weather data is to be used for long-range planning
purposes only. Due to inherent delays in data transmission and the relative
age of the data, NEXRAD weather data should not be used for short-range
weather avoidance.
WARNING: The G1000 Integrated Flight Deck, as installed in the Cessna
Citation Mustang aircraft, has a very high degree of functional integrity.
However, the pilot must recognize that providing monitoring and/or selftest capability for all conceivable system failures is not practical. Although
unlikely, it may be possible for erroneous operation to occur without a fault
indication shown by the system. It is thus the responsibility of the pilot to
detect such an occurrence by means of cross-checking with all redundant or
correlated information available in the cockpit.
WARNING: For safety reasons, system operational procedures must be learned
on the ground.
WARNING: The United States government operates the Global Positioning
System and is solely responsible for its accuracy and maintenance. The
GPS system is subject to changes which could affect the accuracy and
performance of all GPS equipment. Portions of the system utilize GPS as a
precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs,
information presented by the system can be misused or misinterpreted and,
therefore, become unsafe.
WARNING: To reduce the risk of unsafe operation, carefully review and
understand all aspects of the G1000 Pilot’s Guide documentation and the
Cessna Citation Mustang Airplane Flight Manual. Thoroughly practice basic
operation prior to actual use. During flight operations, carefully compare
indications from the system to all available navigation sources, including
the information from other NAVAIDs, visual sightings, charts, etc. For safety
purposes, always resolve any discrepancies before continuing navigation.
WARNING: The illustrations in this guide are only examples. Never use
the system to attempt to penetrate a thunderstorm. Both the FAA Advisory
Circular, Subject: Thunderstorms, and the Aeronautical Information Manual
(AIM) recommend avoiding “by at least 20 miles any thunderstorm identified
as severe or giving an intense radar echo.”
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Warnings, Cautions & Notes
WARNING: Lamp(s) inside this product may contain mercury (HG) and must
be recycled or disposed of according to local, state, or federal laws. For
more information, refer to our website at www.garmin.com/aboutGarmin/
environment/disposal.jsp.
WARNING: Because of variation in the earth’s magnetic field, operating the
system within the following areas could result in loss of reliable attitude and
heading indications. North of 72° North latitude at all longitudes. South of
70° South latitude at all longitudes. North of 65° North latitude between
longitude 75° W and 120° W. (Northern Canada). North of 70° North latitude
between longitude 70° W and 128° W. (Northern Canada). North of 70° North
latitude between longitude 85° E and 114° E. (Northern Russia). South of
55° South latitude between longitude 120° E and 165° E. (Region south of
Australia and New Zealand).
WARNING: Do not use GPS to navigate to any active waypoint identified as
a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are
derived from an unknown map reference datum that may be incompatible
with the map reference datum used by GPS (known as WGS84) and may be
positioned in error as displayed.
CAUTION: The PFD and MFD displays use a lens coated with a special
anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive
cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTIREFLECTIVE COATING. It is very important to clean the lens using a clean,
lint-free cloth and an eyeglass lens cleaner that is specified as safe for antireflective coatings.
CAUTION: The system does not contain any user-serviceable parts. Repairs
should only be made by an authorized Garmin service center. Unauthorized
repairs or modifications could void both the warranty and the pilot’s authority
to operate this device under FAA/FCC regulations.
nOTE: All visual depictions contained within this document, including screen
images of the panel and displays, are subject to change and may not reflect
the most current system and databases. Depictions of equipment may differ
slightly from the actual equipment.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Warnings, Cautions & Notes
NOTE: This device complies with part 15 of the FCC Rules. Operation is
subject to the following two conditions: (1) this device may not cause harmful
interference, and (2) this device must accept any interference received,
including interference that may cause undesired operation.
NOTE: The data contained in the terrain and obstacle databases comes from
government agencies. Garmin accurately processes and cross-validates the
data, but cannot guarantee the accuracy and completeness of the data.
NOTE: This product, its packaging, and its components contain chemicals
known to the State of California to cause cancer, birth defects, or reproductive
harm. This notice is being provided in accordance with California’s Proposition
65. If you have any questions or would like additional information, please
refer to our web site at www.garmin.com/prop65.
NOTE: Interference from GPS repeaters operating inside nearby hangars can
cause an intermittent loss of attitude and heading displays while the aircraft
is on the ground. Moving the aircraft more than 100 yards away from the
source of the interference should alleviate the condition.
NOTE: Use of polarized eyewear may cause the flight displays to appear dim
or blank.
NOTE: The purpose of this Cockpit Reference Guide is to provide the pilot
a resource with which to find operating instructions on the major features
of the G1000 system more easily. It is not intended to be a comprehensive
operating guide. Complete operating procedures for the system are found
in the G1000 Integrated Flight Deck Pilot’s Guide.
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Warnings, Cautions & Notes
Blank Page
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Record of Revisions
Part Number
190-00600-00
Rev A
Change Summary
Initial release
Rev B
190-00600-01
Rev A
Added Additional Features section
Rev B
Added CAS INOP system messages
Rev C
Added COM 3 function for HF
Added TAS
Removed automatic Reversionary Mode operation
190-00600-02
Rev A
190-00600-03
Production release
Added Synthetic Vision
Added other GDU 9.01 parameters
Added GDU 10.01 parameters
Added GSD 41
Added GMA -20
Added new page navigation
TCAS II
Radar Altimeter
Added AOPA Airport Directory
Added dual navigation database capability
Added database synchronization
Revision Date of Revision Affected Pages
A
June, 2010
All
190-00600-03 Rev. A
Description
Production release
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
RR-1
Record of Revisions
Blank Page
RR-2
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Table of Contents
Flight Instruments. ............................................................................................................... 1
Selecting the Altimeter Barometric Pressure Setting....................................................... 1
Selecting Standard Barometric Pressure.............................................................................. 1
Change Altimeter Barometric Pressure Setting Units....................................................... 1
Synchronizing the Altimeter Barometric Pressure Settings............................................ 1
Synchronize CDI......................................................................................................................... 1
Change Navigation Sources.................................................................................................... 2
Enable/Disable OBS Mode While Navigating with GPS..................................................... 2
Generic Timer.............................................................................................................................. 2
Configure Vspeed Bugs Individually...................................................................................... 2
Turn Vspeed Bugs On or Off by Category............................................................................. 3
Set Barometric/Radar Altimeter (RA Optional) Minimum Descent Altitude................ 3
Displaying Wind Data............................................................................................................... 3
Engine Indication & Crew Alerting System........................................................ 5
Crew Alerting System (CAS).................................................................................................... 6
CAS Messages and Prioritization........................................................................................... 6
Nav/Com/Transponder/Audio Panel......................................................................... 7
Enter or Change Flight ID........................................................................................................ 7
ADF Tuning (Optional)............................................................................................................... 7
DME Tuning................................................................................................................................. 7
Enter a Transponder Code....................................................................................................... 8
Select Transponder Mode........................................................................................................ 8
Selecting a COM Radio............................................................................................................. 8
Selecting a NAV Radio.............................................................................................................. 9
NAV/COM Tuning........................................................................................................................ 9
Intercom System (ICS) Isolation........................................................................................... 10
Passenger Address (PA) System............................................................................................ 10
Clearance Recorder and Player............................................................................................ 11
Automatic Flight Control System........................................................................... 13
Flight Director Activation...................................................................................................... 13
Vertical Modes.......................................................................................................................... 14
Lateral Modes........................................................................................................................... 15
GPS Navigation......................................................................................................................... 17
Direct-to Navigation............................................................................................................... 17
Activate a Stored Flight Plan................................................................................................ 18
Activate a Flight Plan Leg...................................................................................................... 18
Stop Navigating a Flight Plan............................................................................................... 19
Vertical Navigation (VNAV)................................................................................................... 19
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
i
Table of Contents
Flight Planning....................................................................................................................... 21
Weight Planning....................................................................................................................... 21
Trip Planning............................................................................................................................. 21
Create a New User Waypoint Defined by Latitude & Longitude.................................. 23
Create a New User Waypoint Defined by Radials from Other Waypoints.................. 24
Create a New User Waypoint Defined by a Radial & Distance from Another
Waypoint.............................................................................................................................. 26
Delete a User Waypoint.......................................................................................................... 27
Create a New Flight Plan....................................................................................................... 28
Import a Flight Plan from an SD Card................................................................................. 29
Insert a Waypoint in the Active Flight Plan....................................................................... 29
Enter an Airway in a Flight Plan........................................................................................... 30
Invert An Active Flight Plan................................................................................................... 31
Remove a Departure, Arrival, Approach, or Airway from a Flight Plan...................... 31
Store a Flight Plan................................................................................................................... 32
Edit a Stored Flight Plan........................................................................................................ 32
Delete a Waypoint from the Flight Plan............................................................................. 32
Invert and Activate a Stored Flight Plan............................................................................ 33
Copy a Flight Plan.................................................................................................................... 33
Delete a Flight Plan................................................................................................................. 33
Graphical Flight Plan Creation.............................................................................................. 34
Export a Flight Plan to an SD Card...................................................................................... 34
Procedures................................................................................................................................. 35
Load and Activate a Departure Procedure........................................................................ 35
Activate A Departure Leg...................................................................................................... 35
Load An Arrival Procedure..................................................................................................... 35
Activate An Arrival Leg.......................................................................................................... 36
Load and/or Activate an Approach Procedure.................................................................. 36
Activate An Approach in the Active Flight Plan................................................................ 37
Activate a Vector to Final Approach Fix............................................................................. 37
Activate A Missed Approach in the Active Flight Plan.................................................... 38
Hazard Avoidance................................................................................................................. 39
Customizing the Hazard Displays on the Navigation Map............................................. 39
XM Weather (Subscription Optional).................................................................................. 39
Traffic Systems......................................................................................................................... 41
Terrain Awareness & Warning System (TAWS-B).............................................................. 45
Airborne Color Weather Radar............................................................................................. 47
Additional Features............................................................................................................ 51
Synthetic Vision (Optional).................................................................................................... 51
Terminal Procedure Charts.................................................................................................... 53
ii
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Table of Contents
AOPA Airport Directory.......................................................................................................... 55
XM® Radio Entertainment (Subscription Optional)......................................................... 55
Abnormal Operation.......................................................................................................... 59
Reversionary Mode................................................................................................................. 59
Abnormal COM Operation..................................................................................................... 59
Audio Panel Fail-safe Operation.......................................................................................... 59
Hazard Displays with Loss of GPS Position........................................................................ 60
Unusual Attitudes.................................................................................................................... 60
Dead Reckoning....................................................................................................................... 61
Annunciations & Alerts................................................................................................... 63
CAS Messages........................................................................................................................... 63
Comparator Annunciations.................................................................................................... 65
Reversionary Sensor Annunciations.................................................................................... 66
TAWS-B Alerts........................................................................................................................... 67
TCAS II Alerts and Annunciations......................................................................................... 68
Aural Alerts............................................................................................................................... 70
Flight Plan Import/Export Messages................................................................................... 70
MFD & PFD Message Advisories........................................................................................... 72
Database Message Advisories.............................................................................................. 73
GMA 1347D/1347D-20 Message Advisories........................................................................ 76
GIA 63W Message Advisories................................................................................................ 77
GSD 41 Message Advisories.................................................................................................. 79
GEA 71 Message Advisories................................................................................................... 80
GTX 33/33D Message Advisories........................................................................................... 80
GRS 77 Message Advisories................................................................................................... 81
GMU 44 Message Advisories................................................................................................. 82
GDL 69A Message Advisories................................................................................................ 83
GWX 68 Alert Messages.......................................................................................................... 83
GDC 74B Message Advisories................................................................................................ 84
GCU 475 Message Advisories................................................................................................ 84
GMC 710 Message Advisories............................................................................................... 85
Miscellaneous Message Advisories...................................................................................... 85
Appendix........................................................................................................................................ 91
PFD Softkey Map..................................................................................................................... 91
MFD Softkey Map.................................................................................................................... 99
Database Updates................................................................................................................. 101
Index..........................................................................................................................................Index-1
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
iii
Table of Contents
Blank Page
iv
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Flight Instruments
Flight
Instruments
Flight Instruments
Selecting the Altimeter Barometric Pressure Setting
EICAS
Turn the BARO Knob to select the desired setting.
Nav/Com/
XPDR/Audio
Selecting Standard Barometric Pressure
Press the BARO Knob.
2)
Press the ALT UNIT Softkey.
3)
Press the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Flight
Planning
Press the PFD Softkey to display the second-level softkeys.
GPS Nav
1)
AFCS
Change Altimeter Barometric Pressure Setting Units
Or:
4)
Procedures
Press the HPA Softkey to display the barometric pressure setting in
hectopascals.
Press the BACK Softkey to return to the top-level softkeys.
Hazard
Avoidance
Synchronizing the Altimeter Barometric Pressure Settings
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight BARO in the SYNCHRONIZATION
Window.
4)
Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
Abnormal
Operation
Select the AUX-SYSTEM SETUP Page on the MFD.
Additional
Features
1)
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window.
4)
Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Index
Select the AUX-SYSTEM SETUP Page on the MFD.
Appendix
1)
Annun/
Alerts
Synchronize CDI
1
Change Navigation Sources
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.
Flight
Planning
1)
Press the OBS Softkey to select OBS Mode.
2)
Turn the CRS Knob to select the desired course to/from the waypoint. Press
the CRS Knob to slew the CDI Course Pointer to a course bearing directly
to the waypoint.
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 large FMS Knob to highlight the desired Vspeed.
3) Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
1)
Enable/Disable OBS Mode While Navigating with GPS
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Flight Instruments
Index
speed has been changed from a default value, an asterisk appears next to
the speed).
2
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Flight Instruments
5)
Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
EICAS
Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field.
Flight
Instruments
4)
Turn Vspeed Bugs On or Off by Category
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.
AFCS
Press the TMR/REF Softkey.
Nav/Com/
XPDR/Audio
1)
GPS Nav
Set Barometric/Radar Altimeter (RA Optional) Minimum Descent
Altitude
Flight
Planning
1) Press the TMR/REF Softkey.
Turn the small FMS Knob clockwise to select BARO or RAD ALT.
4)
Press the ENT Key.
5)
Use the small FMS Knob to enter the desired altitude.
6)
Press the ENT Key.
7)
To remove the window, press the CLR Key or the TMR/REF Softkey.
Additional
Features
3)
Hazard
Avoidance
Turn the large FMS Knob to highlight the OFF/BARO/RAD ALT field to the
right of ‘Minimums’.
Procedures
2)
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.
Annun/
Alerts
1)
Abnormal
Operation
Displaying Wind Data
Appendix
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
3
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Flight Instruments
Blank Page
4
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
EICAS
5
2
6
1
EICAS
1
Flight
Instruments
Engine Indication & Crew Alerting System
Nav/Com/
XPDR/Audio
AFCS
5
7
GPS Nav
3
Flight
Planning
8
Procedures
6
2
Hazard
Avoidance
3
4
7
8
Abnormal
Operation
10
Additional
Features
9
10
3
Fuel Display
4
CAS Display
190-00600-03 Rev. A
5
6
7
Interstage Turbine
Temperature
Engine High Pressure
Turbine Rotation
Speed
Electrical Display
8
9
Cabin Pressure Altitude
and Change Rate
Trim Indicator
10
Flap Indicator
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Index
2
Engine Fan Rotation
Speed
Oil Pressure & Speed
Appendix
1
EIS Display (Reversionary Mode)
Annun/
Alerts
EICAS Display (Normal Mode)
5
Crew Alerting System (CAS)
NOTE: Refer to the Annunciations and Alerts section for specific CAS
messages.
EICAS
Flight
Instruments
EICAS
Nav/Com/
XPDR/Audio
NOTE: Refer to the Airplane Flight Manual (AFM) for emergency
procedures.
When CAS messages are present while in reversionary mode, the CAS Window appears on the display along with the flight instruments and EIS.
CAS Window
CAS Display
Normal Mode
Reversionary Mode
CAS Messages
CAS Messages and Prioritization
NOTE: Information on CAS messages in this pilot’s guide is always superseded
by the AFM.
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
NOTE: If there is a mismatch between databases or software on the PFDs,
CAS is inoperative.
Index
Appendix
• Warning (red) – Immediate crew awareness and action required; Master
Warning triggered
• Caution (yellow) – Immediate crew awareness and possible future corrective
action required; Master Caution triggered
• Advisory (white) – Crew awareness required and subsequent action may be
required
6
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Nav/Com/XPDR/Audio Panel
Flight
Instruments
Nav/Com/Transponder/Audio Panel
Enter or Change Flight ID
Press the TMR/REF Softkey, then turn the large FMS Knob to highlight the
Flight ID field.
EICAS
2)
Turn the small FMS Knob to enter the first character.
3)
Turn the large FMS Knob to select the next field.
Nav/Com/
XPDR/Audio
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.
AFCS
1)
GPS Nav
ADF Tuning (Optional)
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.
Additional
Features
Turn the small FMS Knob to enter the first digit of the desired ADF
frequency.
Hazard
Avoidance
2)
Procedures
Press the ADF/DME Softkey.
Flight
Planning
1)
Abnormal
Operation
10) Press the ENT Key to complete the selection.
DME Tuning
If two DMEs are installed, turn the large FMS to select the DME source
field.
3)
Turn the small FMS Knob to select the desired Nav radio.
4)
Press the ENT Key to complete the selection.
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Index
2)
Appendix
Press the ADF/DME Softkey.
Annun/
Alerts
1)
7
Enter a Transponder Code
1)
Press the XPDR Softkey (XPDR/TFC if the TCAS II option is available).
2)
Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
3)
Press the digit softkeys to enter the code in the code field. When entering
the code, the next key in sequence must be pressed within 10 seconds, or
the entry is cancelled and restored to the previous code. Five seconds after
the fourth digit has been entered, the transponder code becomes active.
Select Transponder Mode
With TCAS II Option
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
Press the XPDR/TFC Softkey.
2)
Press the MODE Softkey to display the transponder mode selection
softkeys.
3)
Press the desired transponder mode softkey (STBY, ON, or ALT).
Hazard
Avoidance
Without TCAS II Option
1)
Press the XPDR Softkey.
2)
If the aircraft is equipped with two transponders, press the XPDR1 or
XPDR2 Softkey to select the active transponder.
3)
Press the desired transponder mode softkey (STBY, ON, ALT, or GND).
Selecting a COM Radio
Abnormal
Operation
Additional
Features
1)
Transmit/Receive
Annun/
Alerts
Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (HF, if installed) on
the audio panel.
Appendix
Receive Only
Index
Press the COM1, COM2, or COM3 Key (HF, if installed) on the audio panel.
8
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Nav/Com/XPDR/Audio Panel
2)
Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or
deselect the navigation radio audio source. All radio keys can be selected
individually or together.
Nav/Com/
XPDR/Audio
To begin navigating using a navigation radio, press the CDI Softkey on the
PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).
EICAS
1)
Flight
Instruments
Selecting a NAV Radio
NAV/COM Tuning
Turn the respective tuning knobs to enter the desired frequency into the
standby frequency field. The large knob enters MHz and the small knob
enters kHz.
2)
Press the appropriate Frequency Transfer Key to place the frequency into
the active frequency field.
AFCS
1)
GPS Nav
Flight
Planning
Or:
Press the COM or NAV Key on the MFD/PFD Control Unit to select the
desired COM or NAV frequency box.
2)
Turn the FMS Knob to tune the desired frequency (large knob for MHz;
small knob for kHz).
3)
Press the Frequency Transfer Key to transfer the frequency to the active field.
Procedures
1)
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
9
Intercom System (ICS) Isolation
Pressing the INTR COM Key on either Audio Panel selects and deselects the
intercom on both Audio Panels. The annunciator is lit when the intercom is active.
The intercom connects the pilot and copilot together. Either the pilot or copilot may
select or deselect the intercom.
The MAN SQ Key allows either automatic or manual control of the intercom
squelch setting. Pressing the MAN SQ Key enables manual squelch control, indicated
by the MAN SQ annunciator.
•
When the MAN SQ Annunciator is extinguished (Automatic Squelch is on),
the ICS Knob controls only the volume (pressing the ICS Knob has no effect on the
VOL/SQ selection).
•
When the MAN SQ Annunciator is illuminated (Manual Squelch), the ICS
Knob controls either volume or squelch (selected by pressing the ICS Knob and
indicated by the VOL or SQ annunciation).
Cabin Address (GMA 1347D-20 only)
The CABIN Key initiates two way communication between the pilot or copilot and
the passengers in the cabin. The annunciator is lit when the cabin intercom is active
on either Audio Panel.
When the flight crew wants to communicate with the passengers, the pilot or
copilot presses the CABIN Key to signal that communication is desired. The cabin
signal must be acknowledged to begin intercom conversation.
When the passengers want to communicate with the pilot/copilot, they press the
“COCKPIT CALL” switch at their seat in the cabin. The CABIN annunciator flashes on
both Audio Panels to signal the pilot and copilot that cabin communication is desired.
The cockpit call signal must be acknowledged by pressing the CABIN Key to begin
intercom conversation.
Passenger Address (PA) System
A passenger address system is provided by pressing the PA Key to deliver messages
to the passengers. The message is heard by the other pilot on the cockpit speaker
(if selected on) or on the headset if the PA Key is enabled on both audio panels. PA
messages are one way from the flight deck to the passengers.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
10
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Nav/Com/XPDR/Audio Panel
Flight
Instruments
Clearance Recorder and Player
GMA 1347D
Press the REC Key to begin recording.
2)
Press the REC Key again to stop recording.
AFCS
1)
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
Procedures
2)
Flight
Planning
Press the PLAY Key once to play the latest recorded memory block.
GPS Nav
Play
1)
the previously recorded block.
GMA 1347D-20
Annun/
Alerts
Appendix
Index
11
Abnormal
Operation
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Additional
Features
COM audio is recorded automatically. Recorded audio is stored in separate memory
blocks. Once 2.5 minutes of recording time have been reached, the recorder begins
recording over the stored memory blocks, starting from the oldest block.
The PLAY Key controls the play function. The PLAY annunciator is illuminated to
indicate when play is in progress. The PLAY annunciator extinguishes after playback
is finished.
Pressing the PLAY Key once plays the latest recorded memory block and then
returns to normal operation. Pressing the PLAY Key again during play of a memory
block stops play. If a COM input signal is detected during play of a recorded memory
block, play is halted.
Hazard
Avoidance
NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio
to the Pilot. Pressing the play key on the Copilot’s Audio Panel plays recorded
audio to the Copilot.
190-00600-03 Rev. A
Nav/Com/
XPDR/Audio
Record
EICAS
NOTE: Only the audio for the selected COM MIC Key is recorded. Audio is
not recorded for COM3 MIC.
Pressing the PLAY Key twice within one-half second while audio is playing plays
the previous block of recorded audio. Each subsequent two presses of the PLAY Key
within one-half second backtracks through the recorded memory blocks to reach and
play any recorded block.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
12
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
AFCS
Modes Selected
HDG Key
Heading Select
HDG
Appendix
Approach**
PIT
PIT
GP
GS
PIT
Annun/
Alerts
APR Key
GPS
VOR
LOC
Pitch Hold (default)
Pitch Hold (default)
Glidepath
Glideslope
Pitch Hold (default)
Abnormal
Operation
Backcourse***
PIT
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
***The selected navigation receiver must have a valid LOC signal before BC Key press activates flight
director.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
13
Index
**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.
190-00600-03 Rev. A
Additional
Features
BC Key
Pitch Hold (default)
Hazard
Avoidance
Navigation**
GA Switch
ROL
ROL
ROL
TO
GA
ROL
ROL
ROL
GPS
VOR
LOC
BC
Procedures
NAV Key
FD Key
AP Key
CWS Button
Vertical
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Takeoff (on ground)
TO
Go Around
GA
Altitude Hold
ALT
Vertical Speed
VS
Vertical Path Tracking* VPTH
Flight
Planning
ALT Key
VS Key
VNV Key
Lateral
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
Takeoff (on ground)
Go Around
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
GPS Nav
Control Pressed
AFCS
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.
Nav/Com/
XPDR/Audio
Note: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.
EICAS
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.
Flight
Instruments
Automatic Flight Control System
Vertical Modes
Vertical Mode
EICAS
Flight
Instruments
AFCS
Selected Altitude
Armed
Altitude Hold
Vertical Speed
VNAV
VNAV Target
Altitude Armed
Takeoff
Appendix
Abnormal
Operation
Glidepath
Glideslope
Index
Control Annunciation
Holds the current aircraft pitch attitude;
may be used to climb/descend to the (default)
Selected Altitude
AFCS armed to capture the altitude
displayed in the Selected Altitude
*
window
Holds the current Altitude Reference
ALT Key
Maintains the current aircraft vertical
speed; may be used to climb/descend VS Key
to the Selected Altitude
Flight Level Change, Maintains the current aircraft airspeed
IAS Hold
(in IAS or Mach) while the aircraft is
FLC Key
Flight Level Change, climbing/descending to the Selected
Altitude
Mach Hold
Annun/
Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Pitch Hold
Description
Go Around
Captures and tracks the VNAV flight VNV
path
Key
AFCS armed to capture the altitude
displayed in the VNAV Target Altitude
**
window
Captures and tracks the WAAS
glidepath on approach
APR Key
Captures and tracks the ILS glideslope
on approach
Commands a constant pitch angle
and wings level on the ground in
preparation for takeoff
GA
Switch
Disengages the autopilot and
commands a constant pitch angle and
wings level in the air
PIT
ALTS
ALT
nnnnn ft
VS
nnnn fpm
FLC
nnn kt
FLC
M .nnn
VPTH
ALTV
GP
GS
TO
GA
* ALTS armed automatically when PIT, VS, FLC, or GA active, and under VPTH when Selected Altitude
is to be captured instead of VNAV Target Altitude
** ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of
Selected Altitude
14
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
AFCS
Lateral Mode
Roll Hold
Limits maximum commanded roll angle
Heading Select
Captures and tracks Selected Heading
HDG
GPS
Captures and tracks selected navigation
source (GPS, VOR, LOC)
NAV
Key
VOR
Flight
Planning
LOC
Captures and tracks a localizer signal
for backcourse approaches
BC Key
Procedures
BC
Hazard
Avoidance
GPS
Captures and tracks selected navigation
APR Key
source (GPS, VOR, LOC)
VAPP
Additional
Features
LOC
Annun/
Alerts
TO
GA
Switch
Appendix
Commands a constant pitch angle
and wings level on the ground in
preparation for takeoff
Disengages the autopilot and
commands a constant pitch angle and
wings level in the air
Abnormal
Operation
Go Around
*
GPS Nav
Takeoff
BANK
Key
HDG
Key
ROL
AFCS
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)
(default)
Nav/Com/
XPDR/Audio
Low Bank
Control Annunciation
EICAS
Description
Holds current aircraft roll attitude
or rolls wings level, depending on
commanded bank angle
GA
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Index
* No annunciation appears in the AFCS Status Box. The acceptable bank angle range is indicated in
green along the Roll Scale of the Attitude Indicator.
190-00600-03 Rev. A
Flight
Instruments
Lateral Modes
15
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
AFCS
Blank Page
16
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
GPS Navigation
Flight
Instruments
GPS Navigation
Direct-to Navigation
2)
3)
7)
10)
11)
Direct-to Navigation using the PFD
2)
5)
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
17
Index
6)
Appendix
4)
) on the PFD.
Turn the large FMS Knob to place the cursor in the desired selection field.
Turn the small FMS Knob to begin selecting the desired identifier, location,
etc.
Press the ENT Key.
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.
Turn the large FMS Knob counterclockwise to place the cursor over the
‘ALT’ altitude field.
Annun/
Alerts
3)
Press the Direct-to Key (
Abnormal
Operation
1)
Additional
Features
12)
Hazard
Avoidance
9)
Procedures
8)
Flight
Planning
6)
GPS Nav
5)
) Key on the MFD or MFD Controller.
Enter the waypoint identifier.
Press the ENT Key to confirm the identifier. The ‘Activate?’ field is
highlighted.
If no altitude constraint or course is desired, press the ENT Key to activate.
To enter an altitude constraint, proceed to step 5.
Turn the large FMS Knob counterclockwise to place the cursor over the
‘VNV’ altitude field.
Enter the desired altitude.
Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 9.
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Press the ENT Key. The cursor is now flashing in the VNV offset distance field.
Enter the desired offset distance before (-) the waypoint.
Press the ENT Key. The ‘Activate?’ field is highlighted.
Press the ENT Key to activate.
AFCS
4)
Press the Direct-to (
Nav/Com/
XPDR/Audio
1)
EICAS
Direct-to Navigation using the MFD
EICAS
Flight
Instruments
GPS Navigation
7)
Turn the small FMS Knob to enter the desired altitude constraint.
8)
Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 10.
9)
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Nav/Com/
XPDR/Audio
10) Press the ENT Key. The cursor is placed in the ‘OFFSET’ field.
11) Turn the small FMS Knob to enter the desired offset distance (-) from the
selected Direct-to.
AFCS
12) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to
highlight the ‘CRS’ field.
14) Press the ENT Key to highlight ‘ACTIVATE?’.
15) Press the ENT Key again to activate the Direct-to.
Activate a Stored Flight Plan
1)
Press the FPL Key on the MFD, or MFD Controller, and turn the small FMS
Knob to display the Flight Plan Catalog Page.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan
4)
Select the ACTIVE Softkey. The confirmation window is now displayed.
5)
With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel
the flight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and
press the ENT Key.
Activate a Flight Plan Leg
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
13) Turn the small FMS Knob to enter the desired course to the waypoint.
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 waypoint.
2)
Select the ACT LEG Softkey.
Appendix
or
Index
Press the MENU Key, select the ‘Activate Leg’ option from the page menu
and press the ENT Key. This step must be used when activating a leg from
the PFD.
3)
18
With ‘Activate’ highlighted, press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
GPS Navigation
Flight
Instruments
Stop Navigating a Flight Plan
2)
Press the MENU Key to display the Page Menu Window.
3)
Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT
Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan.
This will not delete the stored flight plan, only the active flight plan.
Vertical Navigation (VNAV)
AFCS
GPS Nav
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.
Nav/Com/
XPDR/Audio
Press the FPL Key to display the Active Flight Plan Page.
EICAS
1)
Flight
Planning
Procedures
Large White
Text
Large Light
Blue Text
Hazard
Avoidance
Small Light
Blue Text
Annun/
Alerts
Cross AT or ABOVE 5,000 ft
Abnormal
Operation
Small White Text
with Altitude
Restriction Bar
Additional
Features
Small Light
Blue Subdued
Text
Cross AT 2,300 ft
Appendix
Cross AT or BELOW 3,000 ft
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
19
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
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 flight path guidance outside the FAF. Note that these
altitudes will be displayed as small light blue text.
Altitudes that are designated for use in vertical navigation may also be made “nondesignated” by placing the cursor over the desired altitude and pressing the CLR Key.
The altitude is now displayed only as a reference. It will not be used to give vertical
flight path guidance. Other displayed altitudes may change due to re-calculations
or rendered invalid as a result of manually changing an altitude to a non-designated
altitude.
Light Blue Text
Light Blue
Subdued Text
Large Text Altitude calculated by
the system estimating
the altitude of the
aircraft as it passes
over the navigation
point. This altitude
is provided as a
reference and is not
designated to be used
in determining vertical
flight path guidance.
Altitude has been
entered by the pilot.
Altitude is designated
for use in giving
vertical flight path
guidance. Altitude
does not match the
published altitude in
navigation database or
no published altitude
exists.
The system cannot
use this altitude in
determining vertical
flight path guidance.
Small Text Altitude is not
designated to be used
in determining vertical
flight path guidance.
Altitude has been
retrieved from the
navigation database
and is provided as a
reference.
Altitude is designated
for use in giving vertical
flight path guidance.
Altitude has been
retrieved from the
navigation database
or has been entered by
the pilot and matches
a published altitude
in the navigation
database.
The system cannot
use this altitude in
determining vertical
flight path guidance.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
White Text
20
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Flight Planning
Flight
Instruments
Flight Planning
Weight Planning
EICAS
All procedures apply to the MFD unless otherwise stated.
Entering Weight Parameters
Procedures
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.
Additional
Features
Or:
Manually enter the desired fuel quantity.
6)
Press the FMS Knob to remove the cursor.
Abnormal
Operation
Enter the desired reserve fuel quantity.
Annun/
Alerts
Trip Planning
Turn the large FMS Knob to select the ‘AUX’ page group.
2)
Turn the small FMS Knob to select the Trip Planning Page.
3)
The current ‘page mode’ is displayed at the top of the page: ‘AUTOMATIC’
or ‘MANUAL’. To change the page mode, select the AUTO or MANUAL
Softkey.
21
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Appendix
1)
190-00600-03 Rev. A
Hazard
Avoidance
2)
5)
Flight
Planning
If necessary, press the FMS Knob to activate the cursor.
Press the ENT Key. The cursor is now in the ‘Fuel Reserves’ field.
GPS Nav
1)
4)
AFCS
Entering Fuel Parameters
Nav/Com/
XPDR/Audio
Turn the large FMS Knob to select the ‘AUX’ page group. Turn the small FMS
Knob to select the Weight Planning Page.
1) Select the EMPTY WT Softkey to place the cursor in the Basic Empty
Weight field.
2) Enter the desired aircraft empty weight.
3) Press the ENT Key. The cursor is now over the ‘Pilot & Stores’ field.
4) Enter the desired weight of Pilot & Stores.
5) Press the ENT Key.
6) Continue repeating these steps until all desired weights have been entered.
Flight Planning
Flight
Instruments
4)
For Direct-to planning:
a) Select the WPTS Softkey and verify that the starting waypoint field
indicates ‘P.POS’ (present position).
EICAS
b) If necessary, press the MENU Key and select ‘Set WPT to Present
Position’ to display ‘P.POS’.
Nav/Com/
XPDR/Audio
c) Press the ENT Key and the flashing cursor moves to the ending
waypoint field.
AFCS
d) Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.
Or:
GPS Nav
For point-to-point planning:
a) Enter the identifier of the starting waypoint.
Flight
Planning
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.
Procedures
d) Press the ENT Key to accept the waypoint.
Or:
Hazard
Avoidance
For flight plan leg planning:
a) Select the FPL Softkey (at the bottom of the display).
Additional
Features
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.
Annun/
Alerts
Abnormal
Operation
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’ displays the active flight plan. If an active flight plan
is selected, ‘REM’ will be an available option to display planning data
for the remainder of the flight plan.
Appendix
NOTE: The page mode must be set to ‘MANUAL’ to perform the following
steps.
5)
Turn the large FMS Knob to highlight the departure time (DEP TIME) field.
Index
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.
22
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Flight Planning
8)
The flashing cursor moves to the fuel flow field. Enter the fuel flow. Press
the ENT Key when finished. Note that in ‘automatic’ page mode, fuel flow
is provided by the system.
9)
The flashing cursor moves to the fuel onboard field. Modify the fuel onboard.
Press the ENT Key when finished. In ‘AUTOMATIC’ mode, fuel onboard is
provided by the entry made on the Weight Planning Page.
Hazard
Avoidance
Additional
Features
13) The flashing cursor moves to the air temperature (TOTAL AIR TEMP) field. Enter
the desired air temperature. Press the ENT Key when finished. Note that in
‘automatic’ page mode, air temperature is provided by the system outside
air temperature.
Procedures
12) The flashing cursor moves to the barometric setting (PRESSURE) field. Enter
the desired baro setting. Press the ENT Key when finished. Note that in
‘automatic’ page mode, the baro setting is provided by the setting entered
on the PFD.
Flight
Planning
11) The flashing cursor moves to the altitude (IND ALTITUDE) field. Enter the
altitude. Press the ENT Key when finished. Note that in ‘automatic’ page
mode, altitude is provided by the system.
GPS Nav
10) The flashing cursor moves to the calibrated airspeed (CALIBRATED AS) field.
Enter the calibrated airspeed. Press the ENT Key when finished. Note that
in ‘automatic’ page mode, calibrated airspeed is provided by the system.
AFCS
The flashing cursor moves to the ground speed (GS) field. Enter the ground
speed. Press the ENT Key when finished. Note that in ‘automatic’ page
mode, ground speed is provided by the system.
Nav/Com/
XPDR/Audio
7)
EICAS
Enter the departure time. Press the ENT Key when finished. Departure time
may be entered in local or UTC time, depending upon system settings.
Flight
Instruments
6)
Abnormal
Operation
Create a New User Waypoint Defined by Latitude & Longitude
Turn the large FMS Knob on the Control Unit to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Select the NEW Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
Annun/
Alerts
1)
Appendix
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
23
Flight Planning
Flight
Instruments
6)
The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
EICAS
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Nav/Com/
XPDR/Audio
With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
8)
Turn the small FMS Knob to select LAT/LON (latitude and longitude).
9)
Press the ENT Key.
Create a New User Waypoint Defined by Radials from Other
Waypoints
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
7)
AFCS
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
1)
Turn the large FMS Knob on the Control Unit to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Select the NEW Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
6)
The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
Abnormal
Operation
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Appendix
Annun/
Alerts
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
7)
With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
8)
Turn the small FMS Knob to select RAD/RAD (radial/radial).
9)
Press the ENT Key.
Index
10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first
waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:
24
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Flight Planning
b) Turn the large FMS Knob to select the desired waypoint.
EICAS
c) Press the ENT Key.
Flight
Instruments
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
Or:
AFCS
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
Nav/Com/
XPDR/Audio
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
c) Turn the large FMS Knob to select the desired waypoint.
GPS Nav
d) Press the ENT Key.
Or:
Procedures
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
Flight
Planning
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
12) Press the ENT Key.
Annun/
Alerts
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
Abnormal
Operation
d) Press the ENT Key.
Additional
Features
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Hazard
Avoidance
Or:
13) Repeat step 10 to enter the next waypoint name.
Index
15) Press the ENT Key.
16) Press the FMS Knob to remove the flashing cursor.
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Appendix
14) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field for the
second waypoint. Enter the desired radial from the reference waypoint.
25
Create a New User Waypoint Defined by a Radial & Distance from
Another Waypoint
1)
Turn the large FMS Knob on the MFD Control Unit to select the ‘WPT’ page
group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Select the NEW Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
6)
The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Flight Planning
Flight
Planning
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Hazard
Avoidance
Procedures
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
7)
With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
8)
Turn the small FMS Knob to select RAD/DIS (radial/distance).
9)
Press the ENT Key.
Additional
Features
10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first
waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:
Abnormal
Operation
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
Annun/
Alerts
b) Turn the large FMS Knob to select the desired waypoint.
c) Press the ENT Key.
Or:
Appendix
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Index
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
26
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Flight Planning
Flight
Instruments
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Or:
Nav/Com/
XPDR/Audio
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
EICAS
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
c) Turn the large FMS Knob to select the desired waypoint.
AFCS
d) Press the ENT Key.
Or:
GPS Nav
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
Flight
Planning
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Hazard
Avoidance
12) Press the ENT Key.
13) The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.
Additional
Features
14) Press the ENT Key.
15) Press the FMS Knob to remove the flashing cursor.
Abnormal
Operation
Delete a User Waypoint
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.
Index
27
Appendix
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Annun/
Alerts
1)
190-00600-03 Rev. A
Procedures
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
Create a New Flight Plan
NOTE: When creating a new flight plan in the Active Flight Plan Window,
the first leg is activated automatically after it is created.
EICAS
Flight
Instruments
Flight Planning
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Creating an active flight plan:
1) Press the FPL Key.
2) Press the FMS Knob to activate the cursor (only on MFD).
3) Turn the small FMS Knob to display the Waypoint Information Window.
(Turning it clockwise displays a blank Waypoint Information Window,
turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan,
nearest, recent, user, or airway waypoints).
4) Enter the identifier, facility, or city name of the departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key. The
active flight plan is modified as each waypoint is entered.
5) Repeat step numbers 3 and 4 to enter each additional flight plan waypoint.
6) When all waypoints have been entered, press the FMS Knob to remove the
cursor.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Creating a stored flight plan:
1) Press the FPL Key.
2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page.
3) Select the NEW Softkey; or press the MENU Key, highlight ‘Create New
Flight Plan’, and press the ENT Key to display a blank flight plan for the
first empty storage location.
4) Turn the small FMS Knob to display the Waypoint Information Window.
(Turning it clockwise displays a blank Waypoint Information Window,
turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan,
nearest, recent, user, or airway waypoints).
5) Enter the identifier, facility, or city name of the departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key.
6) Repeat step numbers 4 and 5 to enter each additional flight plan waypoint.
7) When all waypoints have been entered, press the FMS Knob to return to
the Flight Plan Catalog Page. The new flight plan is now in the list.
28
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Flight Planning
Insert the SD card containing the flight plan in the top card slot on the
MFD.
2)
Press the FPL Key on the Control Unit to display the Active Flight Plan Page
on the MFD.
3)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
4)
Press the FMS Knob to activate the cursor.
Nav/Com/
XPDR/Audio
5)
Turn either FMS Knob to highlight an empty or existing flight plan.
6)
Select the IMPORT Softkey.
AFCS
1)
EICAS
Flight
Instruments
Import a Flight Plan from an SD Card
Or:
8)
Press the ENT Key.
Hazard
Avoidance
Turn the small FMS Knob to highlight the desired flight plan for importing.
Procedures
7)
Flight
Planning
If an existing flight plan is selected, an ‘Overwrite existing flight plan? OK
or CANCEL’ prompt is displayed. Press the ENT Key to choose to overwrite
the selected flight plan and see a list of the available flight plans on the SD
card. If overwriting the existing flight plan is not desired, select ‘CANCEL’
using the FMS Knob, press the ENT Key, select another existing or empty
flight plan, and again select the IMPORT Softkey.
GPS Nav
If an empty flight plan is selected, a list of the available flight plans on the
SD card will be displayed.
Additional
Features
Insert a Waypoint in the Active Flight Plan
2)
If necessary, press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan waypoint. The
new waypoint is inserted before the highlighted waypoint.
4)
Turn the small FMS Knob. The Waypoint Information Window is now
displayed.
5)
Enter the new flight plan waypoint by one of the following:
Annun/
Alerts
Press the FPL Key to display the active flight plan.
Abnormal
Operation
1)
Appendix
a) Enter the user waypoint identifier, facility, or city.
b) Press the ENT Key.
Index
Or:
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
29
Flight Planning
Flight
Instruments
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
EICAS
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.
Nav/Com/
XPDR/Audio
d) Press the ENT Key.
Or:
AFCS
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
GPS Nav
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.
Flight
Planning
Or:
Procedures
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
d) Press the ENT Key.
6)
Press the ENT Key again to “accept” the waypoint.
Enter an Airway in a Flight Plan
1)
Press the FPL Key.
2)
Press the FMS Knob to activate the cursor (not required on the PFD).
3)
Turn the large FMS Knob to highlight the waypoint after the desired airway
entry point. If this waypoint is not a valid airway entry point, a valid entry
point should be entered at this time.
4)
Turn the small FMS Knob one click clockwise and select the LD AIRWY
Softkey, or press the MENU Key and select “Load Airway”. The Select
Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway”
menu item is available only when an acceptable airway entry waypoint has
been chosen (the waypoint ahead of the cursor position).
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
c) Turn the large FMS Knob to select the desired user waypoint.
30
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Flight Planning
Turn the FMS Knob to select the desired airway from the list, and press the
ENT Key. Low altitude airways are shown first in the list, followed by “all”
altitude airways, and then high altitude airways.
Flight
Instruments
6)
Turn the FMS Knob to select the desired airway exit point from the list, and
press the ENT Key. ‘LOAD?’ is highlighted.
EICAS
7)
Press the ENT Key. The system returns to editing the flight plan with the
new airway inserted.
Nav/Com/
XPDR/Audio
5)
Invert An Active Flight Plan
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.
Flight
Planning
2)
GPS Nav
Press the FPL Key to display the active flight plan.
AFCS
1)
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Or, for a stored flight plan:
Hazard
Avoidance
1)
Procedures
Remove a Departure, Arrival, Approach, or Airway from a Flight
Plan
Additional
Features
a) Press the MFD FPL Key and turn the small FMS Knob to select the
Flight Plan Catalog Page.
Abnormal
Operation
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.
Press the CLR Key to display a confirmation window.
4)
With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
31
Index
3)
Appendix
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.
Annun/
Alerts
2)
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 for the MFD and turn the small FMS Knob to display the
Flight Plan Catalog Page.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan.
4)
Select the EDIT Softkey.
5)
Turn the large FMS Knob to place the cursor in the desired location.
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
1)
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Flight Planning
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Additional
Features
Or, for a stored flight plan:
a) Press the FPL Key of the MFD and turn the small FMS Knob to select
the Flight Plan Catalog Page.
Abnormal
Operation
b) Press the FMS Knob to activate the cursor.
c) Turn the large FMS Knob to highlight the desired flight plan.
Index
Appendix
Annun/
Alerts
d) Select the EDIT Softkey.
32
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
190-00600-03 Rev. A
Flight Planning
Flight
Instruments
Invert and Activate a Stored Flight Plan
Press the FPL Key on the MFD or MFD Control Unit.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the desired flight plan.
5)
Select the INVERT Softkey. ‘Invert and activate stored flight plan?’ is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key. The selected flight plan is now
inverted and activated. The original flight plan remains intact in its flight plan
catalog storage location.
EICAS
1)
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Copy a Flight Plan
Press the FPL Key on the MFD or MFD Control Unit.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the flight plan to be copied.
5)
Select the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
Flight
Planning
1)
Procedures
Hazard
Avoidance
Additional
Features
Delete a Flight Plan
Press the FPL Key on the MFD or MFD Control Unit.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the flight plan to be deleted.
5)
Select the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
Abnormal
Operation
1)
Annun/
Alerts
Appendix
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
33
Graphical Flight Plan Creation
1)
Press the FPL Key to display the Active Flight Plan Page on the MFD.
2)
Press the Joystick to activate the map pointer. Use the Joystick to move
the pointer to the desired point on the map to be inserted as a waypoint in
the flight plan.
3)
The default insertion point is at the end of the flight plan. If the selected
waypoint is to be placed anywhere other than the end of the flight plan,
press the FMS Knob to activate the cursor. Waypoints are inserted ABOVE
the cursor. Turn the large FMS Knob to select the desired insertion point.
4)
Select the LD WPT Softkey. The selected waypoint is inserted at the selected
point. The default user waypoint naming is USR000, USR001, USR002, and
so on.
5)
To change the user waypoint name, follow the procedure for modifying a user
waypoint.
Export a Flight Plan to an SD Card
1)
Insert the SD card into the top card slot on the MFD.
2)
Press the FPL Key on the Contol Unit to display the Active Flight Plan Page
on the MFD.
3)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to highlight the flight plan to be exported.
6)
Select the EXPORT Softkey.
7)
Press the ENT Key to confirm the export.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Flight Planning
34
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Procedures
Flight
Instruments
Procedures
Load and Activate a Departure Procedure
EICAS
3)
Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a
list of available departures.
4)
Turn the large FMS Knob to highlight the desired departure.
5)
Press the ENT Key. A list of runways may be displayed for the departure. If
so, turn either FMS Knob to select the desired runway.
6)
Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a
list of available transitions.
7)
Turn the large FMS Knob to highlight the desired transition.
8)
Press the ENT Key.
9)
With ‘LOAD?’ highlighted, press the ENT Key. The departure is active when
the flight plan is active.
Flight
Planning
Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.
GPS Nav
2)
AFCS
Press the PROC Key.
Nav/Com/
XPDR/Audio
1)
Procedures
Hazard
Avoidance
Activate A Departure Leg
Press the FPL Key on the MFD or MFD Control Unit to display the active
flight plan.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the TO waypoint of the desired leg
within the departure.
4)
Select the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Additional
Features
1)
Abnormal
Operation
Annun/
Alerts
Load An Arrival Procedure
Appendix
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’.
3)
Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list
of available arrivals.
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
35
Index
1)
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Procedures
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 may be 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.
AFCS
11) The arrival becomes part of the active flight plan.
Activate An Arrival Leg
Procedures
Flight
Planning
GPS Nav
Turn the large FMS Knob to highlight the desired arrival.
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 TO waypoint of the desired leg
within the arrival.
4)
Select the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Load and/or Activate an Approach Procedure
Additional
Features
Hazard
Avoidance
4)
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.
Appendix
4)
Turn either FMS Knob to highlight the desired approach.
5)
Press the ENT Key. A list of available transitions for the selected approach
procedure is now displayed.
6)
Turn either FMS Knob to select the desired transition. The “Vectors”
option assumes vectors will be received to the final course segment of
Annun/
Alerts
1)
Index
Abnormal
Operation
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.
36
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Procedures
If desired, the DA/MDA for the selected approach procedure may be
entered and displayed on the PFD. Turn the small FMS Knob in the
direction of the green arrow to change the display from OFF to BARO or
optional RAD ALT.
9)
Press the ENT Key. The cursor moves to the altitude field. Turn the small
FMS Knob to enter the published DA/MDA for the selected approach
procedure.
AFCS
8)
Nav/Com/
XPDR/Audio
Press the ENT Key. The cursor moves to the MINIMUMS field.
EICAS
7)
Flight
Instruments
the approach and will provide navigation guidance relative to the final
approach course.
GPS Nav
10) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’
highlighted.
11) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.
Flight
Planning
Selecting ‘LOAD?’ enters the selected approach procedure into the active
flight plan, but is not currently active. Selecting ‘ACTIVATE?’ enters the
selected approach procedure into the active flight plan and activates the
first leg of the approach.
Procedures
12) Press the ENT Key.
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.
3)
Press the ENT Key.
Additional
Features
1)
Hazard
Avoidance
Activate An Approach in the Active Flight Plan
2)
Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’.
3)
Press the ENT Key.
4)
The final approach course becomes the active leg.
Appendix
Press the PROC Key.
Annun/
Alerts
1)
Abnormal
Operation
Activate a Vector to Final Approach Fix
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
37
Activate A Missed Approach in the Active Flight Plan
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Procedures
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’.
3)
Press the ENT Key. A confirmation window is displayed.
4)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Or:
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Press the go-around button.
38
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Hazard Avoidance
Flight
Instruments
Hazard Avoidance
Customizing the Hazard Displays on the Navigation Map
EICAS
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.
GPS Nav
XM Weather (Subscription Optional)
Select the NEXRAD or XM LTNG Softkey to display the desired weather.
Select the applicable softkey again to remove weather data from the
Navigation Map Page.
Additional
Features
2)
Hazard
Avoidance
Select the MAP Softkey.
Procedures
Displaying XM Weather on the Navigation Map Page
Display METAR and TAF information on the Airport Information Page
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).
Annun/
Alerts
Turn the large FMS Knob to select the WPT Page Group.
Abnormal
Operation
1)
Flight
Planning
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.
1)
AFCS
With the Navigation Map Page displayed, press the MENU Key to display
the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’
option.
Nav/Com/
XPDR/Audio
1)
Displaying Weather on the Weather Data Link Page
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.
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Index
Turn the large FMS Knob to select the Map Page Group.
Appendix
1)
39
Hazard Avoidance
Flight
Instruments
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.
Nav/Com/
XPDR/Audio
EICAS
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,
SIGMETs, PIREPs or AIREPs.
3)
Press the ENT Key to display pertinent information for the selected product.
Flight
Planning
GPS Nav
AFCS
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.
Procedures
Weather Products and Symbols
Turbulence
PIREPs
NEXRAD XM Lightning
Cloud Top
METARs Surface Analysis
SIGMETs/AIRMETs
County Warnings
Winds Aloft
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Echo Top (Cloud Top and Echo Top Mutually Exclusive)
Cyclone Warnings
City
Forecast
AIREPs
Cell Movement
Icing Potential
Freezing Levels
40
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Hazard Avoidance
Flight
Planning
Non-Threat Traffic
(intruder is beyond 5 nm and greater than 1200’ vertical separation)
GPS Nav
Description
AFCS
Traffic Symbol
Nav/Com/
XPDR/Audio
• If Traffic information Service (TIS) is configured, a STANDBY, OPERATE, and
TNA MUTE Softkey is displayed.
• If a Traffic Advisory System (TAS) is configured, a STANDBY, NORMAL, TEST,
and ALT MODE Softkey is displayed.
• If a TCAS II system is configured, a REL, ABS, TRC STBY, TA ONLY, TA/RA,
TEST, and ALT RNG Softkey is displayed.
EICAS
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.
Flight
Instruments
Traffic Systems
Procedures
Proximity Advisory (PA) (TAS and TCAS II only)
(intruder is within 5 nm and less than 1200’ vertical separation)
Traffic Advisory (TA)
(Potential collision area is within 20 to 48 seconds)
Hazard
Avoidance
Traffic Advisory Off Scale
Additional
Features
Resolution Advisory (RA) (TCAS II only)
(Potential collision area is within 15 to 35 seconds)
Abnormal
Operation
Resolution Advisory Off Scale (TCAS II only)
Traffic Symbol Description
Annun/
Alerts
Traffic Information Service (TIS)
NOTE: If the G1000 is configured to use an optional Traffic Advisory System
(TAS), TIS is not available for use.
Appendix
NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
41
Hazard Avoidance
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Traffic Map Page.
EICAS
3)
Select the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
4)
Select the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
5)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
AFCS
1)
Nav/Com/
XPDR/Audio
Flight
Instruments
Displaying Traffic on the Traffic Map Page
Flight
Planning
GPS Nav
Displaying Traffic on the Navigation Map
1)
Ensure TIS is operating. With the Navigation Map displayed, select the
MAP Softkey.
2)
Select the TRAFFIC Softkey. Traffic is now displayed on the map.
Procedures
Traffic Advisory System (TAS) (Optional)
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
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 NORMAL Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
4)
Select the ALT MODE Softkey to change the altitude volume. Select the
desired altitude volume by pressing the BELOW, NORMAL, ABOVE, or
UNREST (unrestricted) Softkey. The selection is displayed in the Altitude
Mode field.
5)
Select the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
6)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Index
System Self Test
42
1)
With the Traffic Map Page displayed, set the range to 2/6 nm.
2)
Select the STANDBY Softkey.
3)
Select the TEST Softkey.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Hazard Avoidance
Self test takes approximately eight seconds to complete. When completed
successfully, traffic symbols are displayed and a voice alert “TAS System Test
OK” is heard. If the self test fails, the system reverts to Standby Mode and
a voice alert “TAS System Test Fail” is heard.
EICAS
Displaying Traffic on the Navigation Map
Ensure TAS is operating.
2)
With the Navigation Map displayed, select the MAP Softkey.
3)
Select the TRAFFIC Softkey. Traffic is now displayed on the map.
Nav/Com/
XPDR/Audio
1)
AFCS
Traffic Collision Avoidance System (TCAS II) (Optional)
Flight
Planning
Procedures
WARNING: The TCAS II system is intended for advisory use only. TCAS II is
intended to help the pilot locate transponder-equipped traffic visually and
to provide advisory vertical maneuver guidance to avoid traffic. It is the
responsibility of the pilot to see and maneuver to avoid traffic, terrain, and
obstacles.
GPS Nav
NOTE: If the system is configured to use TIS, the optional TCAS II is not
available for use.
Hazard
Avoidance
System Test
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Traffic Map Page.
3)
Select the TEST Softkey. The aural annunciation “TCAS Test” will be
heard. A test pattern of traffic symbols is displayed on the Traffic Page
and inset map on the PFD. The VSI will display a red no descent indication
and a green climb indication of 2000 feet per min. and red from 2000
to 4000+. The pitch display will also display the appropriate indications
appropriate with the VSI. The self test takes approximately eight seconds
to complete, after which a voice alert “TCAS Test Passed” is heard. In the
event the system test fails, a voice alert “TCAS Test Failed” is heard and a
visual annunciation ‘TCAS FAIL’ appears on the PFD. In addition, a visual
annunciation ‘FAIL’ appears in the Operating Mode box on the Traffic Map
Page.
Annun/
Alerts
Appendix
Index
43
Abnormal
Operation
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Additional
Features
1)
190-00600-03 Rev. A
Flight
Instruments
4)
Hazard Avoidance
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Traffic Map Page.
EICAS
3)
Select the TA ONLY or TA/RA Softkey to begin displaying traffic. ‘TA/RA’ or
‘TA ONLY’ respectively, is displayed in the TCAS Mode field.
4)
Select the STANDBY Softkey to place the system in the Standby Mode.
‘TFC STBY’ will be displayed in the TCAS Mode field.
5)
Select the ABS (absolute) or REL (relative) Softkey to display intruder
altitude as an absolute altitude or an altitude relative to own aircraft
altitude.
6)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
GPS Nav
AFCS
1)
Nav/Com/
XPDR/Audio
Flight
Instruments
Displaying Traffic on the Traffic Map Page
Procedures
Flight
Planning
Changing the Altitude Range
1)
On the Traffic Page, select the ALT RNG Softkey.
2)
Select one of the following Softkeys:
Hazard
Avoidance
ABOVE: Displays non-threat and proximity traffic from 9900 feet above the
aircraft to 2700 feet below the aircraft. Typically used during climb phase
of flight.
Additional
Features
NORMAL: Displays non-threat and proximity traffic from 2700 feet above
the aircraft to 2700 feet below the aircraft. Typically used during enroute
phase of flight.
Abnormal
Operation
BELOW: Displays non-threat and proximity traffic from 2700 feet above the
aircraft to 9900 feet below the aircraft. Typically used during descent phase
of flight.
UNREST (unrestricted): All traffic is displayed.
Annun/
Alerts
3)
To return to the Traffic Page, select the BACK Softkey.
1)
Ensure TCAS II system is operating. With the Navigation Map displayed,
select the MAP Softkey.
2)
Select the TRAFFIC Softkey. Traffic will now be displayed on the map.
Index
Appendix
Displaying Traffic on the Navigation Map
44
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Hazard Avoidance
WARNING: The TAWS display shows supplemental information only. It should
not be used for navigation.
Nav/Com/
XPDR/Audio
NOTE: TAWS operation is only available when the system is configured for
a TAWS-B installation.
EICAS
NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.
Flight
Instruments
Terrain Awareness & Warning System (TAWS-B)
AFCS
Manual System Test
2)
Turn the small FMS Knob to select ‘Test TAWS System’.
3)
Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center
of the TAWS-B Page.
Flight
Planning
While the TAWS-B Page is displayed, press the MENU Key.
GPS Nav
1)
When all is in working order, “TAWS System Test, OK” is heard.
Procedures
Display Terrain and Obstacles on the TAWS-B Page
Turn the small FMS Knob to select the TAWS-B Page.
3)
If desired, select the VIEW Softkey to access the ARC and 360 softkeys.
When the ARC Softkey is selected, a radar-like 120° view is displayed.
Select the 360 Softkey to return to the 360° default display.
4)
Rotate the Joystick clockwise to increase the display range or rotate
counter-clockwise to decrease the display range.
Red
Terrain/Obstacle above or within 100’
below current aircraft altitude.
Yellow
Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.
Black
Terrain/Obstacle is more than 1000’
below aircraft altitude.
Appendix
Terrain/Obstacle Location
Annun/
Alerts
Color
Abnormal
Operation
2)
Additional
Features
Turn the large FMS Knob to select the Map Page Group.
Hazard
Avoidance
1)
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
45
Hazard Avoidance
EICAS
Flight
Instruments
Enable/Disable Aviation Data
1)
While the TAWS-B Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.
3)
Press the ENT Key.
Nav/Com/
XPDR/Audio
TAWS Inhibit
AFCS
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.
GPS Nav
Inhibit TAWS
While the TAWS-B Page is displayed, select the INHIBIT Softkey.
Procedures
Flight
Planning
Or:
1)
Press the MENU Key.
2)
Turn the small FMS Knob to select ‘Inhibit TAWS’.
3)
Press the ENT Key.
Hazard
Avoidance
Enable TAWS
While the TAWS-B Page is displayed, select the INHIBIT Softkey.
Abnormal
Operation
Additional
Features
Or:
1)
While the TAWS-B Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select ‘Enable TAWS’.
3)
Press the ENT Key.
1)
With the Navigation Map displayed, press the MAP Softkey.
2)
Select the TERRAIN Softkey. Terrain and obstacles will now be displayed
on the map.
Index
Appendix
Annun/
Alerts
Displaying Terrain and Obstacles on the Navigation Map
46
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Hazard Avoidance
AFCS
Displaying Weather on the Weather Radar Page
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Radar Page.
3)
Select the MODE Softkey.
4)
If the aircraft is on the ground, select the STANDBY Softkey to initiate the
one minute warm-up period. After the warm-up is complete, the radar will
enter the Standby Mode. After the aircraft is airborne, select the WEATHER
Softkey.
GPS Nav
1)
Hazard
Avoidance
Abnormal
Operation
If desired, select the VERTICAL Softkey for vertical scanning.
Additional
Features
6)
Adjusting Antenna Tilt
Index
47
Appendix
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Annun/
Alerts
Move the Joystick up or down to adjust the tilt of the antenna up or down. Monitor the displayed tilt value in the TILT field.
When scanning vertically, a Tilt Line may be displayed to aid in positioning the tilt
of the antenna. If the Tilt Line is not displayed, perform the following steps:
1) Press the MENU Key
2) Turn the large FMS Knob to select ‘Show Tilt Line’.
3) Press the ENT Key.
190-00600-03 Rev. A
Procedures
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.
Turn the Joystick to select the desired range.
Flight
Planning
Or:
5)
Nav/Com/
XPDR/Audio
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.
EICAS
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.
Flight
Instruments
Airborne Color Weather Radar
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Hazard Avoidance
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:
1) Press the MENU Key
2) Turn the large FMS Knob to select ‘Show Bearing Line’.
3) Press the ENT Key.
GPS Nav
Vertically Scan a Storm Cell
Hazard
Avoidance
Procedures
Flight
Planning
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.
Additional
Features
Adjusting Gain
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.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
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.
48
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Hazard Avoidance
Select the MODE Softkey.
2)
Select the GROUND Softkey to place the radar in Ground Map Mode.
3)
Select the BACK Softkey.
EICAS
1)
Flight
Instruments
Ground Mapping
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.
AFCS
1)
Hazard
Avoidance
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
49
Index
190-00600-03 Rev. A
Appendix
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.
Annun/
Alerts
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.
Abnormal
Operation
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.
Additional
Features
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.
Procedures
2)
Flight
Planning
To activate or deactivate the antenna stabilization, select the MODE
Softkey.
GPS Nav
Antenna Stabilization
1)
Nav/Com/
XPDR/Audio
Sector Scan
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Hazard Avoidance
Blank Page
50
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Additional Features
Flight
Instruments
Additional Features
Synthetic Vision (Optional)
Hazard
Avoidance
Additional
Features
Abnormal
Operation
3)
Press the SYN TERR Softkey.
4)
Press the BACK Softkey to return to the previous page.
Appendix
Press the SYN VIS Softkey.
Annun/
Alerts
2)
Procedures
Press the PFD Softkey.
Flight
Planning
Displaying Synthetic Terrain
1)
GPS Nav
Pathways
Flight Path Marker
Horizon Heading Marks
Terrain and Obstacle Alerting
Three-dimensional Traffic
Airport Signs
Runway Display
AFCS
•
•
•
•
•
•
•
Nav/Com/
XPDR/Audio
Synthetic Vision System (SVS) functionality is offered as an optional enhancement
to the G1000 Integrated Flight Deck.
SVS is primarily comprised of a computer-generated forward-looking, attitude
aligned view of the topography immediately in front of the aircraft from the pilot’s
perspective. SVS information is shown on the primary flight display (PFD).
SVS offers a three-dimensional view of terrain and obstacles. Terrain and
obstacles that pose a threat to the aircraft in flight are shaded yellow or red.
In addition to SVS enhancement to the PFD, the following feature enhancements
have been added to the PFD:
EICAS
WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. SVS is intended as an aid to situational
awareness only and may not provide either the accuracy or reliability upon
which to solely base decisions and/or plan maneuvers to avoid terrain,
obstacles, or traffic.
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
51
Additional Features
EICAS
NOTE: Pathways are not available when the cross-pointer (X-Pointer) flight
director format is selected.
Flight
Planning
GPS Nav
AFCS
NOTE: When the optional TCAS II system issues a Resolution Advisory (RA)
Pathways are automatically removed from the display. Pathways may again
be displayed by the pilot manually selecting Pathways.
Nav/Com/
XPDR/Audio
Flight
Instruments
Displaying Pathways
1)
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the PATHWAY Softkey.
5)
Press the BACK Softkey to return to the previous page.
Hazard
Avoidance
Procedures
Displaying Heading on the Horizon
1)
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the HRZN HDG Softkey.
5)
Press the BACK Softkey to return to the previous page.
1)
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the APTSIGNS Softkey.
5)
Press the BACK Softkey to return to the previous page.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Displaying Airport Signs
52
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Additional Features
NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may
be necessary to carry another source of charts on-board the aircraft.
EICAS
SafeTaxi®
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
53
Hazard
Avoidance
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Procedures
FliteCharts® resemble the paper version of AeroNav Services terminal procedures
charts. The charts are displayed with high-resolution and in color for applicable
charts. Current aircraft position is not displayed on FliteCharts.
Flight
Planning
FliteCharts® (Optional)
GPS Nav
ChartView resembles the paper version of Jeppesen terminal procedures charts.
The charts are displayed in full color with high-resolution. The MFD depiction shows
the aircraft position on the moving map in the plan view of most approach charts and
on airport diagrams.
The ChartView database is updated on a 14-day cycle. If the ChartView database
is not updated within 70 days of the expiration date, ChartView will no longer
function.
AFCS
ChartView (Optional)
Nav/Com/
XPDR/Audio
SafeTaxi® is an enhanced feature that gives greater map detail as the map range
is adjusted in on the airport. The airport display on the map reveals runways with
numbers, taxiways identifiers, and airport landmarks including ramps, buildings,
control towers, and other prominent features. Resolution is greater at lower map
ranges. The aircraft symbol provides situational awareness while taxiing.
Selecting the DCLTR Softkey (declutter) once removes the taxiway markings and
airport identification labels. Selecting the DCLTR Softkey twice removes VOR station
ID, the VOR symbol, and intersection names if within the airport plan view. Selecting
the DCLTR Softkey a third time removes the airport runway layout, unless the airport
in view is part of an active route structure. Selecting the DCLTR Softkey again cycles
back to the original map detail.
The SafeTaxi database contains detailed airport diagrams for selected airports.
These diagrams provide the pilot with situational awareness by displaying the aircraft
position in relation to taxiways, ramps, runways, terminals, and services. This
information should not be used by the pilot as the basis for maneuvering the aircraft
on the ground. This database is updated on a 56-day cycle.
190-00600-03 Rev. A
Flight
Instruments
Terminal Procedure Charts
The FliteCharts database contains procedure charts for the United States only.
This database is updated on a 28-day cycle. If not updated within 180 days of the
expiration date, FliteCharts will no longer function.
View Charts from the Navigation Map Page
EICAS
Flight
Instruments
Additional Features
Nav/Com/
XPDR/Audio
1)
Select the SHW CHRT Softkey when displayed.
Or:
AFCS
2)
GPS Nav
Move the map pointer to point to a desired point on the map and select the
SHW CHRT Softkey.
Select the DP, STAR, APR, WX, and NOTAM softkeys to access charts for
departures, arrivals, approaches, weather and NOTAMs Note that NOTAMS
are only available with ChartView.
3)
Select the GO BACK Softkey to return to the previous page.
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
View Charts from the Active Flight Plan Page
1)
While viewing the Active Flight Plan Page, press the FMS Knob to activate
the cursor.
2)
Turn the large FMS Knob to select the departure airport, destination
airport, departure, arrival, or approach.
3)
Select the SHW CHRT Softkey. The appropriate chart will be displayed, if
available for the item selected.
4)
Select the GO BACK Softkey to return to the previous page.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Change Day/Night View
54
1)
While viewing a chart press the MENU Key to display the Page Menu
OPTIONS.
2)
Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and
press the ENT Key.
3)
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.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Additional Features
7)
Press the FMS Knob when finished to remove the Chart Setup Menu.
EICAS
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.
Flight
Instruments
6)
AOPA Airport Directory
Nav/Com/
XPDR/Audio
AFCS
AOPA Airport Directory adds enhanced airport information when viewing airports
on the WPT-Airport Information Page.
This database is updated four times per year. Check fly.garmin.com for the current
database.
View Airport Directory Information
GPS Nav
Flight
Planning
While viewing the WPT-Airport Information Page, if necessary, select the
INFO-1 Softkey to change the softkey label to display INFO-2. AOPA
airport information is displayed on the right half of the display.
XM® Radio Entertainment (Subscription Optional)
2)
Turn the small FMS Knob to select the displayed AUX - XM Information
Page.
3)
Select the RADIO Softkey to show the XM Radio Page where audio
entertainment is controlled.
Abnormal
Operation
Turn the large FMS Knob to select the Auxiliary Page Group.
Additional
Features
1)
Hazard
Avoidance
Selecting the XM Radio Page
Procedures
The XM® Radio Page provides information and control of the audio entertainment
features of the XM Satellite Radio.
Active Channel and Channel List
Annun/
Alerts
Appendix
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.
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
55
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Additional Features
Selecting a Category
The Category Box of the XM Radio Page displays the currently selected category
of audio.
1) Select the CATGRY Softkey on the XM Radio Page.
2) Select the CAT + and CAT - softkeys to cycle through the categories.
Or:
Turn the small FMS Knob to display the ‘Categories’ list. Highlight the
desired category with the small FMS Knob.
3) Press the ENT Key.
Flight
Planning
GPS Nav
Select an Available Channel within the Selected Category
1)
While on the XM Radio Page, select the CHNL Softkey.
2)
Select the CH + Softkey to go up through the list in the Channel Box, or
move down the list with the CH – Softkey.
Or:
Procedures
Press the FMS Knob to highlight the channel list and turn the large FMS
Knob to scroll through the channels.
Hazard
Avoidance
3)
With the desired channel highlighted, press the ENT Key.
Annun/
Alerts
Abnormal
Operation
Additional
Features
Entering a Channel Directly
1)
While on the XM Radio Page, select the CHNL Softkey.
2)
Select the DIR CH Softkey. The channel number in the Active Channel Box
is highlighted.
3)
Select the numbered softkeys located on the bottom of the display to
directly select the desired channel number.
4)
Press the ENT Key to activate the selected channel.
Assigning Channel Presets
Index
Appendix
Up to 15 channels from any category can be assigned a preset number.
1) On the XM Radio Page, with the desired channel active, select the
PRESETS Softkey to access the first five preset channels (PS1 - PS5).
2) Select the MORE Softkey to access the next five channels (PS6 – PS10),
and again to access the last five channels (PS11 – PS15). Selecting the
MORE Softkey repeatedly cycles through the preset channels.
56
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Additional Features
4)
Select the SET Softkey on the desired channel number to save the channel
as a preset.
EICAS
Select any one of the (PS1 - PS15) softkeys to assign a number to the
active channel.
Flight
Instruments
3)
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
57
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Additional Features
Blank Page
58
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Abnormal Operation
Flight
Instruments
Abnormal Operation
Reversionary Mode
Additional
Features
Abnormal
Operation
59
Index
If there is a failure of one Audio Panel, the remaining Audio Panel does not have
access to the other side’s COM or NAV. For example, if the pilot side Audio Panel
Appendix
NOTE: Audio is not available on the speakers in case of an Audio Panel and
its cross-side GIA unit simultaneous failure.
Annun/
Alerts
If there is a failure of both Audio Panels, a fail-safe circuit connects the pilot’s headset
and microphone directly to the COM1 transceiver and the copilot’s headset directly to
the COM2 transceiver. Audio is not available on the speakers. If there is a failure of one
Audio Panel, that side only has access to their respective on-side fail-safe COM.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Hazard
Avoidance
Audio Panel Fail-safe Operation
190-00600-03 Rev. A
Procedures
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.
Flight
Planning
Abnormal COM Operation
GPS Nav
NOTE: The Cessna Citation Mustang Airplane Flight Manual (AFM) always
takes precedence over the information found in this section.
AFCS
• 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.
Nav/Com/
XPDR/Audio
Manual activation of reversionary display mode is accomplished by pressing the
DISPLAY BACKUP Button on the appropriate audio panel.
EICAS
If the system detects a failure in the MFD, PFD1 will enter reversionary
mode automatically. Reversionary mode must be entered manually in the case
of PFD1 or PFD2 failure.. In reversionary mode, critical flight instrumentation is
combined with engine instrumentation on the remaining display.
fails, the copilot side Audio Panel has access to all the radios except for COM1 and
NAV1. In this case, the copilot can receive the audio from NAV2 and operate COM2
for transmission/reception.
In addition, if there is a failure of one Audio Panel, the following functions are no
longer available on the failed side; NAV/ILS audio, speaker, cockpit/cockpit-passengers
intercom, aural warning alerts on headset, entertainment inputs, and digital recording
radio. Also, if a stereo headset is in use, and an Audio Panel fails, only the left channel
will be heard in the headphones.
Hazard Displays with Loss of GPS Position
If GPS position is lost, or becomes invalid, selected hazards being displayed on the
Navigation Map Page are removed until GPS position is again established.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Abnormal Operation
Loss of Hazard Functions with Loss of GPS
Position
Unusual Attitudes
The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary
functions are displayed in these situations.
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
Command Bars
• Inset Map
• Temperatures
• DME Information
Window
• Wind Data
• Selected Heading Box
• Selected Course Box
• Transponder Status
Box
60
• System Time
• PFD Setup Menu
• Windows displayed in
the lower right corner
of the PFD:
– Timer/References
– Nearest Airports
– Flight Plan
– Messages
– Procedures
– ADF/DME Tuning
• Barometric Minimum
Descent Altitude Box
• Glideslope, Glidepath, and Vertical
Deviation Indicators
• Altimeter Barometric
Setting
• Selected Altitude
• VNV Target Altitude
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Abnormal Operation
Flight
Instruments
EICAS
Nav/Com/
XPDR/Audio
Extreme Pitch Indication
Abnormal
Operation
Annun/
Alerts
Appendix
Index
61
Additional
Features
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Hazard
Avoidance
190-00600-03 Rev. A
Procedures
DR Mode is indicated on the G1000 by the appearance of the letters ‘DR’
superimposed in yellow over the ‘own aircraft’ symbol as shown in the following
figure. In addition, ‘DR’ is prominently displayed, also in yellow, on the HSI slightly
above and to the right of the aircraft symbol on the CDI as shown in the following
figure. The CDI deviation bar is displayed in yellow, but will be removed from the
display after 20 minutes. Lastly, but at the same time, a ‘GPS NAV LOST’ alert message
appears on the PFD.
Normal navigation using GPS/WAAS source data resumes automatically once a
valid GPS solution is restored.
It is important to note that estimated navigation data supplied by the G1000 in
DR Mode may become increasingly unreliable and must not be used as a sole means
of navigation. If, while in DR Mode, airspeed and/or heading data is also lost or
not available, the DR function may not be capable of estimating your position and,
consequently, the system may display a path that is different than the actual movement
of the aircraft. Estimated position information displayed by the G1000 through
DR while there is no heading and/or airspeed data available should not be used for
navigation.
Flight
Planning
NOTE: Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic
(OCN) phase of flight. In all other phases, an invalid GPS solution produces
a “NO GPS POSITION” annunciation on the map and the G1000 stops
navigating in GPS Mode.
GPS Nav
While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS
solution or is unable to calculate a GPS position, the system automatically reverts to
Dead Reckoning (DR) Mode. In DR Mode, the G1000 uses its last-known position
combined with continuously updated airspeed and heading data (when available) to
calculate and display the aircraft’s current estimated position.
AFCS
Dead Reckoning
DR Mode is inherently less accurate than the standard GPS/WAAS Mode due to the
lack of satellite measurements needed to determine a position. Changes in wind speed
and/or wind direction compounds the relative inaccuracy of DR Mode. Because of this
degraded accuracy, the crew must maintain position awareness using other navigation
equipment until GPS-derived position data is restored.
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Abnormal Operation
As a result of operating in DR Mode, all GPS-derived data is computed based upon
an estimated position and is displayed as yellow text on the display to denote degraded
navigation source information. This data includes the following:
•
•
•
•
•
•
Additional
Features
Abnormal
Operation
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
Current Track Indicator
All Bearing Pointer Distances
Active Flight Plan distances, bearings, and ETE values
Also, while the G1000 is in DR Mode, the autopilot will couple to GPS for up to 20
minutes. TAWS is also disabled. Additionally, the accuracy of all nearest information
(airports, airspaces, and waypoints) is questionable. Finally, airspace alerts continue
to function, but with degraded accuracy.
Index
Appendix
Annun/
Alerts
Symbolic Aircraft
(Map pages and Inset Map)
Dead Reckoning Indications
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
CDI ‘DR’ Indication on PFD
62
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Annunciations & Alerts
Flight
Instruments
Annunciations & Alerts
CAS Messages
EICAS
Messages
Caution
AFT DOOR
Tailcone baggage door not fully secured
Start control circuit breaker (located in aft j-box) tripped
AFT JBOX LMT L-R*
Current limiter blown (located in aft j-box)
ANTISKID FAIL
Antiskid Control Unit cannot perform anti-skid functions
Overheated NiCad battery (optional)
BATT TEMP FAIL
Battery temperature sensor failure
CABIN ALT
CABIN DOOR
GPS Nav
CABIN ALT
AFCS
AFT JBOX CB L-R*
BATTERY O’TEMP BATTERY O’TEMP
CABIN ALT
Description
Advisory
Nav/Com/
XPDR/Audio
Warning
Cabin altitude potentially unsafe
Cabin door not fully secured
CHECK DOORS
DUCT O’HEAT L-R*
Flight
Planning
A door monitor has not been properly tested or has failed
CVR FAIL
Cockpit voice Recorder has failed
Duct temperature too high or sensor disconnected
Procedures
ENG A/I COLD L-R* ENG A/I COLD L-R* Engine anti-ice system ON and inlet temperature is cold
ENG CTRL SYS L-R*
FADEC has a fault that requires maintenance
ENGINE FAIL L-R*
An engine has failed
F/W SHUTOFF L-R*
FDR FAIL
Hazard
Avoidance
Fuel firewall shutoff valve fully closed
Flight Data Recorder is not recording data
FLAPS FAIL
Additional
Features
A flap system failure has occurred.
Electric fuel boost pump ON. Caution condition is displayed
FUEL BOOST L-R* FUEL BOOST L-R*
when the boost pump is operating in abnormal conditions.
FUEL FLTR BP L-R*
Engine fuel filter impending bypass switch closed
FUEL LO INOP L-R* Fuel low level function failure
Abnormal
Operation
FUEL LVL LO L-R*
Fuel level in tank is too low
FUEL PRES LO L-R*
Fuel pressure too low
FUEL TRANSFER Fuel transfer valve open
GEN OFF L-R*
One or both electrical generators offline
HYD PRESS LO
Hydraulic system pressure too low
HYD PUMP ON
Hydraulic pump running too long
Appendix
MFD COLD
NOSE DOOR L-R*
Annun/
Alerts
GEN OFF L-R
MFD temperature is below -20° C
One or both nose baggage doors not fully secured
NO TIRE SPINDOWN Antiskid control spindown function not working
OIL PRESS LO L-R*
190-00600-03 Rev. A
Index
Oil pressure less than redline low limit
OXYGEN OFF
Oxygen supply off
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
63
Annunciations & Alerts
Flight
Instruments
Messages
EICAS
Warning
Advisory
P/S HTR L-R*
P/S HTR L-R*
No current detected to pitot static heater
PRESS CTRL
PRESS CTRL
Pressure controller loss of integrity
PRESS OFF
Air Source Selector switch in OFF or fresh air position
Nav/Com/
XPDR/Audio
SPD BRK EXTEND Speed brakes extended
STALL WARN FAIL
Failure detected in stall warning system
STALL WARN HI
AFCS
STALL WARN HTR
Stall warning system on ice-contaminated schedule
No power delivered to stall warning vane heater
SURFACE DE-ICE De-ice boots inflating/deflating as designed
T2 HTR FAIL L-R*
TAIL CONE BLD LK
T2 probe heater failure
Tailcone temp high, possible bleed air leak.
TAIL DE-ICE FAIL
Flight
Planning
GPS Nav
Description
Caution
De-ice system not operating normally
W/S A/I FAIL L-R*
W/S A/I FAIL L-R* Loss of power to windshield heater
W/S O’HEAT L-R*
WING DE-ICE FAIL
W/S O’HEAT L-R* Windshield anti-ice power ON; temperature too high
De-ice system operating abnormally
WOW MISCOMPARE
Gear on-ground inputs do not agree
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
*Only affected side displayed (L, R, or L-R) in a CAS message; applicable CAS messages listed here
display L-R for example.
64
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Annunciations & Alerts
ALT MISCOMP
Condition
Nav/Com/
XPDR/Audio
Comparator
Window Text
EICAS
Note that operating the system in the vicinity of metal buildings or other metal
structures can cause sensor differences that may result in nuisance miscompare
annunciations during start up, shut down, or while taxiing.
Flight
Instruments
Comparator Annunciations
Difference in altitude sensors is > 200 ft.
If both airspeed sensors detect < 35 knots, this is inhibited.
If either airspeed sensor detects > 35 knots, and the difference in sensors is >
15 kts.
Difference in pitch sensors is > 5 degrees.
ROL MISCOMP
Difference in roll sensors is > 6 degrees.
ALT NO COMP
No data from one or both altitude sensors.
IAS NO COMP
No data from one or both airspeed sensors.
HDG NO COMP
No data from one or both heading sensors.
PIT NO COMP
No data from one or both pitch sensors.
ROL NO COMP
No data from one or both roll sensors..
Hazard
Avoidance
PIT MISCOMP
Procedures
Difference in heading sensors is > 10 degrees.
Flight
Planning
HDG MISCOMP
GPS Nav
If either airspeed sensor detects > 80 knots, and the difference in sensors is
> 10 kts.
AFCS
IAS MISCOMP
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
65
Reversionary Sensor Annunciations
Reversionary
Sensor Window
Text
EICAS
Flight
Instruments
Annunciations & Alerts
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 ON AHRS2
Both PFDs are displaying data from the number two Attitude & Heading
Reference System.
BOTH ON GPS1
BOTH ON GPS2
USING ADC1
USING ADC2
USING AHRS1
USING AHRS2
USING GPS1
USING GPS2
Both PFDs are displaying data from the number one GPS receiver.
Both PFDs are displaying data from the number two GPS receiver.
PFD2 is displaying data from the #1 Air Data Computer.
PFD1 is displaying data from the #2 Air Data Computer.
PFD2 is displaying data from the #1 AHRS.
PFD1 is displaying data from the #2 AHRS.
PFD2 is displaying data from the #1 GPS.
PFD1 is displaying data from the #2 GPS.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
BOTH ON ADC1
BOTH ON ADC2
BOTH ON AHRS1
Condition
66
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Annunciations & Alerts
Alert Type
MFD
Pop-Up Alert
Aural Message
EICAS
PFD/MFD
TAWS-B Page
Annunciation
Flight
Instruments
TAWS-B Alerts
“Pull Up”
Reduced Required
Terrain Clearance
Warning (RTC)
“Terrain, Terrain; Pull Up,
Pull Up”
Imminent Terrain
Impact Warning (ITI)
“Terrain, Terrain; Pull Up,
Pull Up”
Reduced Required
Obstacle Clearance
Warning (ROC)
“Obstacle, Obstacle; Pull
Up, Pull Up”
Imminent Obstacle
Impact Warning
(IOI)
““Obstacle, Obstacle; Pull
Up, Pull Up”
Reduced Required
Terrain Clearance
Caution (RTC)
“Caution, Terrain; Caution,
Terrain”
Imminent Terrain
Impact Caution (ITI)
“Caution, Terrain; Caution,
Terrain”
Reduced Required
Obstacle Clearance
Caution (ROC)
“Caution, Obstacle;
Caution, Obstacle”
Imminent Obstacle
Impact Caution (IOI)
“Caution, Obstacle;
Caution, Obstacle”
Premature Descent
Alert Caution (PDA)
“Too Low, Terrain”
Additional
Features
Abnormal
Operation
Appendix
“Don’t Sink”
Annun/
Alerts
Negative Climb
Rate Caution (NCR)
Hazard
Avoidance
“Sink Rate”
Procedures
“Five-Hundred”
Excessive Descent
Rate Caution (EDR)
Flight
Planning
None
GPS Nav
None
AFCS
Altitude Callout
“500”
Nav/Com/
XPDR/Audio
Excessive Descent
Rate Warning (EDR)
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
67
Annunciations & Alerts
PFD/MFD
Alert
Annunciation
TAWS-B Page
Annunciation
Aural
Message
TAWS TEST
None
None
“TAWS System
Test OK”
None
None
TERRAIN DATABASE FAILURE
None
TAWS-B System Test Fail
TAWS FAIL
“TAWS System
Failure”
Terrain or Obstacle database
unavailable or invalid, invalid
software configuration, system
audio fault
TAWS FAIL
“TAWS System
Failure”
NO GPS POSITION
“TAWS Not
Available”
None
“TAWS Not
Available”
Alert Type
System Test in Progress
System Test Pass
None
TAWS Alerting is disabled
MFD Terrain or Obstacle
database unavailable or invalid.
TAWS operating with PFD
Terrain or Obstacle databases
None
No GPS position
Excessively degraded GPS
signal, Out of database
coverage area
TCAS II Alerts and Annunciations
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
TAWS-B System Status Annunciations
PFD Mode
Annunciation
MFD Traffic Map Page
Mode Annunciation
TCAS II Self-test
Initiated (TEST)
None
TEST
(‘TEST MODE’ also shown in
white on top center of page)
Traffic Advisory and
Resolution Advisory
(TA/RA)
None
TA/RA
Index
Appendix
Annun/
Alerts
Mode
68
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Traffic
Display
Status Icon
(Other Maps)
190-00600-03 Rev. A
Annunciations & Alerts
Mode
MFD Traffic Map Page
Mode Annunciation
EICAS
Traffic Advisory Only
(TA ONLY)
Traffic
Display
Status Icon
(Other Maps)
Flight
Instruments
PFD Mode
Annunciation
TA ONLY
in air
Nav/Com/
XPDR/Audio
on ground
TCAS II Standby
(TFC STBY)
STANDBY or STANDBY*
(also shown in white in
center of page)
AFCS
FAIL
TCAS II Failed
GPS Nav
* Annunciation appears yellow while in flight.
TCAS II Modes
Description
Procedures
NO DATA
Flight
Planning
Traffic Map Page
Annunciation
Data is not being received from the TCAS II unit
FAILED
Hazard
Avoidance
Data is being received from the TCAS II unit, but the unit is selfreporting a failure
DATA FAILED
Incorrect data format received from the TCAS II unit
Description
Abnormal
Operation
Traffic Status Banner
Annunciation
Additional
Features
TCAS II Failure Annunciations
A Resolution Advisory is outside the selected display range*.
Annunciation is removed when traffic comes within the selected
display range
TA OFF SCALE
A Traffic Advisory is outside the selected display range*.
Annunciation is removed when traffic comes within the selected
display range.
RA X.X ± XX ↕
System cannot determine bearing of Resolution Advisory**.
Annunciation indicates distance in nm, altitude separation in hundreds
of feet, and altitude trend arrow (climbing/descending).
69
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Appendix
190-00600-03 Rev. A
Annun/
Alerts
RA OFF SCALE
Traffic Status Banner
Annunciation
Description
TA X.X ± XX ↕
System cannot determine bearing of Traffic Advisory**.
Annunciation indicates distance in nm, altitude separation in hundreds
of feet, and altitude trend arrow (climbing/descending).
EICAS
Flight
Instruments
Annunciations & Alerts
AFCS
Nav/Com/
XPDR/Audio
TRFC FAIL
NO TCAS DATA
TCAS II unit has failed (unit is self-reporting a failure or sending
incorrectly formatted data)
Data is not being received from the TCAS II unit
*Shown as symbol on Traffic Map Page
**Shown in center of Traffic Map Page
Aural Alerts
Aural Alert
“Vertical track”
Additional
Features
Hazard
Avoidance
“Traffic”
“TIS not available”
The aircraft is one minute from Top of Descent. Issued only when vertical
navigation is enabled.
The Traffic Information Service (TIS) has issued a Traffic Advisory alert
The aircraft is outside the Traffic Information Service (TIS) coverage area (not
available when a TAS system is installed).
Flight Plan Import/Export Messages
In some circumstances, some messages may appear in conjunction with others.
Flight Plan Import/Export
Results
Abnormal
Operation
Annun/
Alerts
Appendix
Index
Description
“Minimums, minimums” The aircraft has descended below the preset minimum descent altitude or
decision altitude.
Procedures
Flight
Planning
GPS Nav
TCAS II Traffic Status Annunciations
Description
‘Flight plan successfully imported.’
A flight plan file stored on the SD card was successfully
imported as a stored flight plan.
‘File contained user waypoints only.
User waypoints imported successfully. No stored flight plan data was
modified.’
The file stored on the SD card did not contain a flight plan,
only user waypoints. These waypoints have been saved to the
system user waypoints. No flight plans stored in the system
have been modified.
‘No flight plan files found to import.’
The SD card contains no flight plan data.
‘Flight plan import failed.’
Flight plan data was not successfully imported from the SD card.
70
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Annunciations & Alerts
Description
‘File contained user waypoints only.’
The file stored on the SD card did not contain a flight plan,
only user waypoints. One or more of these waypoints did not
import successfully.
‘Too many points. Flight plan truncated.’
The flight plan on the SD card contains more waypoints than
the system can support. The flight plan was imported with as
many waypoints as possible.
‘Some waypoints not loaded. Waypoints locked.’
The flight plan on the SD card contains one or more waypoints
that the system cannot find in the navigation database. The
flight plan has been imported, but must be edited within the
system before it can be activated for use.
‘User waypoint database full. Not all
loaded.’
The flight plan file on the SD card contains user waypoints.
The quantity of stored user waypoints has exceeded system
capacity, therefore not all the user waypoints on the SD card
have been imported. Any flight plan user waypoints that were
not imported are locked in the flight plan. The flight plan must
be edited within the system before it can be activated for use.
Nav/Com/
XPDR/Audio
Some flight plan waypoints were successfully imported from
the SD card, however others had errors and were not imported.
A partial stored flight plan now exists in the system.
EICAS
‘Flight plan partially imported.’
Flight
Instruments
Flight Plan Import/Export
Results
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
‘One or more user waypoints renamed.’ One or more imported user waypoints were renamed when
imported due to naming conflicts with waypoints already
existing in the system.
‘Flight plan export failed.’
The stored flight plan was not successfully exported to the SD
card. The SD card may not have sufficient available memory or
the card may have been removed prematurely.
Abnormal
Operation
The stored flight plan was successfully exported to the SD card.
Additional
Features
‘Flight plan successfully exported.’
Annun/
Alerts
Appendix
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
71
MFD & PFD Message Advisories
Message
Comments
DATA LOST – Pilot stored data was The pilot profile data was lost. System reverts
lost. Recheck settings.
to default pilot profile and settings. The pilot
may reconfigure the MFD & PFDs with preferred
settings, if desired.
XTALK ERROR – A flight display
The MFD and PFDs are not communicating with
crosstalk error has occurred.
each other. The system should be serviced.
PFD1 SERVICE – PFD1 needs
service. Return unit for repair.
PFD2 SERVICE – PFD2 needs
The PFD and/or MFD self-test has detected a
service. Return unit for repair.
problem. The system should be serviced.
MFD1 SERVICE – MFD1 needs
service. Return unit for repair.
MANIFEST – PFD1 software
mismatch, communication halted.
MANIFEST – PFD2 software
The PFD and/or MFD has incorrect software
mismatch, communication halted. installed. The system should be serviced.
MANIFEST – MFD1 software
mismatch, communication halted.
PFD1 CONFIG – PFD1 config error.
The PFD configuration settings do not match
Config service req’d.
backup configuration memory. The system
PFD2 CONFIG – PFD2 config error. should be serviced.
Config service req’d.
MFD1 CONFIG – MFD1 config
The MFD configuration settings do not match
error. Config service req’d.
backup configuration memory. The system
should be serviced.
SW MISMATCH – GDU software
The MFD and PFDs have different software
version mismatch. Xtalk is off.
versions installed. The system should be
serviced.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
72
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Annunciations & Alerts
Comments
EICAS
The PFD and/or MFD is overheating and is
reducing power consumption by dimming the
display. If problem persists, the system should
be serviced.
Nav/Com/
XPDR/Audio
AFCS
A key is stuck on the PFD and/or MFD bezel.
Attempt to free the stuck key by pressing it
several times. The system should be serviced if
the problem persists.
GPS Nav
Flight
Planning
The PFD1 configuration module backup memory
has failed. The system should be serviced.
Procedures
The PFD1 voltage is low. The system should be
serviced.
The PFD2 voltage is low. The system should be
serviced.
The MFD voltage is low. The system should be
serviced.
Hazard
Avoidance
Additional
Features
Message
PFD1 COOLING – PFD1 has poor
cooling. Reducing power usage.
PFD2 COOLING – PFD2 has poor
cooling. Reducing power usage.
MFD1 COOLING – MFD1 has poor
cooling. Reducing power usage.
PFD1 KEYSTK – PFD1 [key name]
Key is stuck.
PFD2 KEYSTK – PFD2 [key name]
Key is stuck.
MFD1 KEYSTK – MFD [key name]
Key is stuck.
CNFG MODULE – PFD1
configuration module is
inoperative.
PFD1 VOLTAGE – PFD1 has low
voltage. Reducing power usage
PFD2 VOLTAGE – PFD2 has low
voltage. Reducing power usage
MFD1 VOLTAGE – MFD1 has low
voltage. Reducing power usage
Flight
Instruments
MFD & PFD Message Advisories (Cont.)
Abnormal
Operation
Database Message Advisories
The MFD and/or PFD detected a failure in the
navigation database. Attempt to reload the
navigation database. If problem persists, the
system should be serviced.
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Appendix
190-00600-03 Rev. A
Comments
Annun/
Alerts
Message
MFD1 DB ERR – MFD1 navigation
database error exists.
PFD1 DB ERR – PFD1 navigation
database error exists.
PFD2 DB ERR – PFD2 navigation
database error exists.
73
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
Database Message Advisories (Cont.)
Message
MFD1 DB ERR – MFD1 basemap
database error exists.
PFD1 DB ERR – PFD1 basemap
database error exists.
PFD2 DB ERR – PFD2 basemap
database error exists.
MFD1 DB ERR – MFD1 terrain
database error exists.
PFD1 DB ERR – PFD1 terrain
database error exists.
PFD2 DB ERR – PFD2 terrain
database error exists.
MFD1 DB ERR – MFD1 terrain
database missing.
PFD1 DB ERR – PFD1 terrain
database missing.
PFD2 DB ERR – PFD2 terrain
database missing.
MFD1 DB ERR – MFD1 obstacle
database error exists.
PFD1 DB ERR – PFD1 obstacle
database error exists.
PFD2 DB ERR – PFD2 obstacle
database error exists.
MFD1 DB ERR – MFD1 obstacle
database missing.
PFD1 DB ERR – PFD1 obstacle
database missing.
PFD2 DB ERR – PFD2 obstacle
database missing.
74
Comments
The MFD and/or PFD detected a failure in the
basemap database.
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 system should be
serviced.
The terrain database is present on another LRU,
but is missing on the specified LRU.
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 system should be serviced.
The obstacle database is present on another LRU,
but is missing on the specified LRU.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Annunciations & Alerts
Comments
EICAS
The MFD and/or PFD detected a failure in the
airport terrain database. Ensure that the data
card is properly inserted. Replace data card. If
problem persists, the system should be serviced.
Nav/Com/
XPDR/Audio
AFCS
The airport terrain database is present on
another LRU, but is missing on the specified LRU.
GPS Nav
Flight
Planning
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
The MFD detected a failure in the ChartView
database (optional feature). Ensure that the data
card is properly inserted. Replace data card. If
problem persists, the system should be serviced.
MFD1 DB ERR – MFD1 FliteCharts The MFD detected a failure in the FliteCharts
database error exists.
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the system should be serviced.
MFD1 DB ERR – MFD1 Airport
The MFD detected a failure in the Airport Directory
Directory database error exists.
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the system should be serviced.
Hazard
Avoidance
The MFD and/or PFD detected a failure in the
Safe Taxi database. Ensure that the data card is
properly inserted. Replace data card. If problem
persists, the system should be serviced.
Procedures
Message
MFD1 DB ERR – MFD1 airport
terrain database error exists.
PFD1 DB ERR – PFD1 airport
terrain database error exists.
PFD2 DB ERR – PFD2 airport
terrain database error exists.
MFD1 DB ERR – MFD1 airport
terrain database missing.
PFD1 DB ERR – PFD1 airport
terrain database missing.
PFD2 DB ERR – PFD2 airport
terrain database missing.
MFD1 DB ERR – MFD1 Safe Taxi
database error exists.
PFD1 DB ERR – PFD1 Safe Taxi
database error exists.
PFD2 DB ERR – PFD2 Safe Taxi
database error exists.
MFD1 DB ERR – MFD1 Chartview
database error exists.
Flight
Instruments
Database Message Advisories (Cont.)
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
75
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
Database Message Advisories (Cont.)
Message
DB MISMATCH – Navigation
database mismatch. Xtalk is off.
Comments
The PFDs and MFD have different navigation
database versions or types (Americas, European,
etc.) installed. Crossfill is off. Install correct
navigation database version or type in all displays.
DB MISMATCH – Terrain database The PFDs and MFD have different terrain database
mismatch.
versions or types installed. Install correct terrain
database version or type in all displays.
DB MISMATCH – Obstacle
The PFDs and MFD have different obstacle
database mismatch.
database installed. Install correct obstacle
database in all displays.
DB MISMATCH – Airport Terrain
The PFDs and MFD have different airport terrrain
database mismatch.
databases installed. Install correct airport terrain
database in all displays.
NAV DB UPDATED – Active
System has updated the active navigation
navigation database updated.
database from the standby navigation database.
TERRAIN DSP – [PFD1, PFD2 or
One of the terrain, airport terrain, or obstacle
MFD1] Terrain awareness display
databases required for TAWS in the specified PFD
unavailable.
or MFD is missing or invalid.
GMA 1347D/1347D-20 Message Advisories
Message
Comments
GMA1 FAIL – GMA1 is inoperative. The audio panel self-test has detected a failure.
GMA2 FAIL – GMA2 is inoperative. The audio panel is unavailable. The system
should be serviced.
GMA XTALK – GMA crosstalk error An error has occurred in transferring data
has occurred.
between the two GMAs. The system should be
serviced.
GMA1 CONFIG – GMA1 config
The audio panel configuration settings do not
error. Config service req’d.
match backup configuration memory. The system
GMA2 CONFIG – GMA2 config
should be serviced.
error. Config service req’d.
76
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Annunciations & Alerts
The audio panel self-test has detected a problem
in the unit. Certain audio functions may still be
available, and the audio panel may still be usable.
The system should be serviced when possible.
AFCS
GPS Nav
Comments
Flight
Planning
The GIA1 and/or GIA2 configuration settings do
not match backup configuration memory. The
system should be serviced.
Procedures
The GIA1 and/or GIA2 have an error in the audio
configuration. The system should be serviced.
Additional
Features
Abnormal
Operation
The GIA1 and/or GIA2 temperature is too low
to operate correctly. Allow units to warm up to
operating temperature.
Annun/
Alerts
The GIA1 and/or GIA2 temperature is too
high. If problem persists, the system should be
serviced.
Appendix
Index
The GIA1 and/or GIA2 self-test has detected
a problem in the unit. The system should be
serviced.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Hazard
Avoidance
190-00600-03 Rev. A
The audio panel has incorrect software installed. The
system should be serviced.
Nav/Com/
XPDR/Audio
GIA 63W Message Advisories
Message
GIA1 CONFIG – GIA1 config error.
Config service req’d.
GIA2 CONFIG – GIA2 config error.
Config service req’d.
GIA1 CONFIG – GIA1 audio config
error. Config service req’d.
GIA2 CONFIG – GIA2 audio config
error. Config service req’d.
GIA1 COOLING – GIA1
temperature too low.
GIA2 COOLING – GIA2
temperature too low.
GIA1 COOLING – GIA1 over
temperature.
GIA2 COOLING – GIA2 over
temperature.
GIA1 SERVICE – GIA1 needs
service. Return the unit for repair.
GIA2 SERVICE – GIA2 needs
service. Return the unit for repair.
Comments
EICAS
Message
MANIFEST – GMA1 software
mismatch, communication halted.
MANIFEST – GMA2 software
mismatch, communication halted.
GMA1 SERVICE – GMA1 needs
service. Return unit for repair.
GMA2 SERVICE – GMA2 needs
service. Return unit for repair.
Flight
Instruments
GMA 1347D/1347D-20 Message Advisories (Cont.)
77
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
GIA 63W Message Advisories (Cont.)
Message
HW MISMATCH – GIA hardware
mismatch. GIA1 communication halted.
HW MISMATCH – GIA hardware
mismatch. GIA2 communication halted.
MANIFEST – GIA1 software
mismatch, communication halted.
MANIFEST – GIA2 software
mismatch, communication halted.
MANIFEST – GFC software
mismatch, communication halted.
COM1 TEMP – COM1 over temp.
Reducing transmitter power.
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
COM1 SERVICE – COM1 needs
service. Return unit for repair.
COM2 SERVICE – COM2 needs
service. Return unit for repair.
COM1 PTT – COM1 push-to-talk key
is stuck.
COM2 PTT – COM2 push-to-talk key
is stuck.
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.
78
Comments
A GIA mismatch has been detected, where
only one is WAAS capable.
The GIA1 and/or GIA 2 has incorrect software
installed. The system should be serviced.
Incorrect servo software is installed, or gain
settings are incorrect.
The system has detected an over temperature
condition in COM1 and/or COM2. The
transmitter is operating at reduced power. If the
problem persists, the system should be serviced.
The system has detected a failure in COM1
and/or COM2. COM1 and/or COM2 may still
be usable. The system should be serviced when
possible.
The COM1 and/or COM2 external push-to-talk
switch is stuck in the enable (or “pressed”)
position. Press the PTT switch again to cycle its
operation. If the problem persists, the system
should be serviced.
GPS integrity is insufficient for the current
phase of flight.
Loss of GPS navigation due to insufficient
satellites.
Loss of GPS navigation due to position error.
Loss of GPS navigation due to GPS failure.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Annunciations & Alerts
Comments
Abort approach due to loss of GPS navigation.
EICAS
Vertical guidance generated by WAAS is
unavailable, use LNAV only minimums.
Displayed after passing the first waypoint of a true
north approach when the nav angle is set to ‘AUTO’.
AFCS
GPS Nav
A failure has been detected in the GPS1 and/
or GPS2 receiver. The receiver may still be
available. The system should be serviced.
Additional
Features
Abnormal
Operation
A failure has been detected in glideslope
receiver 1 and/or receiver 2. The receiver may
still be available. The system should be serviced
when possible.
Hazard
Avoidance
G/S1 SERVICE – G/S1 needs
service. Return unit for repair.
G/S2 SERVICE – G/S2 needs
service. Return unit for repair.
Procedures
G/S2 FAIL – G/S2 is inoperative.
Flight
Planning
A failure has been detected in the NAV1 and/
or NAV2 receiver. The receiver may still be
available. The system should be serviced.
A failure has been detected in glideslope
receiver 1 and/or receiver 2. The system should
be serviced.
GSD 41 Message Advisories
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Appendix
190-00600-03 Rev. A
Comments
GSD1 and the CDU have different copies of
the GSD1 configuration.
GSD1 is reporting a low temperature
condition.
GSD1 is reporting an over-temperature
condition.
Annun/
Alerts
Message
GSD1 CONFIG – GSD1 config error.
Config service req’d.
GSD1 COOLING – GSD1 temperature
too low.
GSD1 COOLING – GSD1 over
temperature.
Nav/Com/
XPDR/Audio
Message
ABORT APR – Loss of GPS
navigation. Abort approach.
APR DWNGRADE – Approach
downgraded.
TRUE APR – True north approach.
Change HDG reference to TRUE.
GPS1 SERVICE – GPS1 needs
service. Return unit for repair.
GPS2 SERVICE – GPS2 needs
service. Return unit for repair.
NAV1 SERVICE – NAV1 needs
service. Return unit for repair.
NAV2 SERVICE – NAV2 needs
service. Return unit for repair.
G/S1 FAIL – G/S1 is inoperative.
Flight
Instruments
GIA 63W Message Advisories (Cont.)
79
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
GSD 41 Message Advisories (Cont.)
Message
GSD1 SERVICE – GSD1 needs service.
Return unit for repair.
MANIFEST – GSD1 software
mismatch. Communication halted.
Comments
GSD1 is reporting an internal error condition.
The GSD may still be usable.
GSD1 has incorrect software installed. The
system should be serviced.
GEA 71 Message Advisories
Message
Comments
GEA1 CONFIG – GEA1 config error. The GEA1 configuration settings do not match
Config service req’d.
those of backup configuration memory. The
system should be serviced.
GEA2 CONFIG – GEA2 config error. The GEA2 configuration settings do not match
Config service req’d.
those of backup configuration memory. The
system should be serviced.
MANIFEST – GEA1 software
The #1 GEA 71 has incorrect software installed.
mismatch, communication halted. The system should be serviced.
MANIFEST – GEA2 software
The #2 GEA 71 has incorrect software installed.
mismatch, communication halted. The system should be serviced.
GTX 33/33D Message Advisories
Message
XPDR1 CONFIG – XPDR1 config
error. Config service req’d.
XPDR2 CONFIG – XPDR2 config
error. Config service req’d.
MANIFEST – GTX1 software
mismatch, communication halted.
MANIFEST – GTX2 software
mismatch, communication halted.
XPDR1 SRVC – XPDR1 needs
service. Return unit for repair.
80
Comments
The transponder configuration settings do not
match those of backup configuration memory.
The system should be serviced.
The transponder configuration settings do not
match those of backup configuration memory.
The system should be serviced.
The transponder has incorrect software installed.
The system should be serviced.
The transponder has incorrect software installed.
The system should be serviced.
The #1 transponder should be serviced when
possible.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Annunciations & Alerts
Comments
The #2 transponder should be serviced when
possible.
There is no communication with the #1
transponder.
There is no communication with the #2
transponder.
EICAS
Nav/Com/
XPDR/Audio
Message
XPDR2 SRVC – XPDR2 needs
service. Return unit for repair.
XPDR1 FAIL – XPDR1 is
inoperative.
XPDR2 FAIL – XPDR2 is
inoperative.
Flight
Instruments
GTX 33/33D Message Advisories (Cont.)
AFCS
GRS 77 Message Advisories
81
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Appendix
190-00600-03 Rev. A
Annun/
Alerts
AHRS1 GPS – AHRS1 not receiving
backup GPS information.
Abnormal
Operation
AHRS2 GPS – AHRS2 not receiving
any GPS information.
Additional
Features
AHRS1 GPS – AHRS1 not receiving
any GPS information.
Hazard
Avoidance
AHRS2 GPS – AHRS2 using backup
GPS source.
Procedures
AHRS1 GPS – AHRS1 using backup
GPS source.
Flight
Planning
AHRS2 TAS – AHRS2 not receiving
valid airspeed.
Comments
The #1 AHRS is not receiving true airspeed from
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed.
The system should be serviced.
The #2 AHRS is not receiving true airspeed from
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed.
The system should be serviced.
The #1 AHRS is using the backup GPS path.
Primary GPS path has failed. The system should
be serviced when possible.
The #2 AHRS is using the backup GPS path.
Primary GPS path has failed. The system should
be serviced when possible.
The #1 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
system should be serviced.
The #2 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
system should be serviced.
The #1 AHRS is not receiving backup GPS
information. The system should be serviced.
GPS Nav
Message
AHRS1 TAS – AHRS1 not receiving
valid airspeed.
GRS 77 Message Advisories (CONT.)
Message
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 Magneticfield model needs update.
AHRS2 SRVC – AHRS2 Magneticfield model needs update.
GEO LIMITS – AHRS1 too far
North/South, no magnetic compass.
GEO LIMITS – AHRS2 too far
North/South, no magnetic compass.
MANIFEST – GRS1 software
mismatch, communication halted.
MANIFEST – GRS2 software
mismatch, communication halted.
Comments
The #2 AHRS is not receiving backup GPS
information. The system should be serviced.
The #1 AHRS is operating exclusively in no-GPS
mode. The system should be serviced.
The #2 AHRS is operating exclusively in no-GPS
mode. The system should be serviced.
The #1 AHRS and #2 AHRS magnetic model
database versions do not match.
The #1 AHRS earth magnetic field model is out of
date. Update magnetic field model when practical.
The #2 AHRS earth magnetic field model is out of
date. Update magnetic field model when practical.
The aircraft is outside geographical limits for
approved AHRS operation. Heading is flagged
as invalid.
The #1 AHRS has incorrect software installed.
The system should be serviced.
The #2 AHRS has incorrect software installed.
The system should be serviced.
GMU 44 Message Advisories
Message
HDG FAULT – AHRS1
magnetometer fault has occurred.
HDG FAULT – AHRS2
magnetometer fault has occurred.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
82
Comments
A fault has occurred in the #1 GMU 44.
Heading is flagged as invalid. The AHRS uses
GPS for backup mode operation. The system
should be serviced.
A fault has occurred in the #2 GMU 44.
Heading is flagged as invalid. The AHRS uses
GPS for backup mode operation. The system
should be serviced.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Annunciations & Alerts
Comments
EICAS
The GMU 44 has incorrect software installed.
The system should be serviced.
Nav/Com/
XPDR/Audio
Message
MANIFEST – GMU1 software
mismatch, communication halted.
MANIFEST – GMU2 software
mismatch, communication halted.
Flight
Instruments
GMU 44 Message Advisories (Cont.)
GDL 69A Message Advisories
Flight
Planning
Procedures
MANIFEST – GDL software
mismatch, communication halted.
Comments
GDL 69 configuration settings do not match
those of backup configuration memory. The
system should be serviced.
A failure has been detected in the GDL 69. The
receiver is unavailable. The system should be
serviced
The GDL 69 has incorrect software installed.
The system should be serviced.
GPS Nav
GDL69 FAIL – GDL 69 has failed.
AFCS
Message
GDL69 CONFIG – GDL 69 config
error. Config service req’d.
83
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Appendix
190-00600-03 Rev. A
Annun/
Alerts
GWX SERVICE – GWX needs
service. Return unit for repair.
MANIFEST – GWX software
mismatch, communication halted.
WX ALERT – Possible severe
weather ahead.
Abnormal
Operation
GWX FAIL – GWX is inoperative.
Comments
GWX 68 configuration settings do not match
those of the GDU configuration. The system
should be serviced.
The GDU is not recieving status packet from the
GWX 68 or the GWX 68 is reporting a fault.
The GWX 68 radar system should be serviced.
A failure has been detected in the GWX 68. The
GWX 68 may still be usable.
The GWX 68 has incorrect software installed.
The system should be serviced.
Possible severe weather detected within +/- 10
degrees of the aircraft heading at a range of 80
to 320 nm.
Additional
Features
Message
GWX CONFIG – GWX config error.
Config service req’d.
Hazard
Avoidance
GWX 68 Alert Messages
GDC 74B Message Advisories
Message
ADC1 ALT EC – ADC1 altitude error
correction is unavailable.
ADC2 ALT EC – ADC2 altitude error
correction is unavailable.
ADC1 AS EC – ADC1 airspeed error
correction is unavailable.
ADC2 AS EC – ADC2 airspeed error
correction is unavailable.
MANIFEST – GDC1 software
mismatch, communication halted.
MANIFEST – GDC2 software
mismatch, communication halted.
Comments
GDC1 or GDC2 is reporting that the altitude
error correction is unavailable.
GDC1 or GDC2 is reporting that the airspeed
error correction is unavailable.
The GDC 74B has incorrect software installed.
The system should be serviced.
GCU 475 Message Advisories
Message
GCU CNFG – GCU Config error.
Config service req’d.
GCU FAIL – GCU is inoperative.
MANIFEST – GCU software
mismatch, communication halted.
GCU KEYSTK – GCU [key name]
Key is stuck.
Comments
GCU 475 configuration settings do not match
those of backup configuration memory. The
system should be serviced.
A failure has been detected in the GCU 475.
The GCU 475 is unavailable.
The GCU 475 has incorrect software installed.
The system should be serviced.
A key is stuck on the GCU 475 bezel. Attempt
to free the stuck key by pressing it several times.
The system should be serviced if the problem
persists.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
84
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Annunciations & Alerts
AFCS
GPS Nav
MANIFEST – GMC software
mismatch. Communication halted.
GMC KEYSTK – GMC [key name]
Key is stuck.
Nav/Com/
XPDR/Audio
GMC FAIL – GMC is inoperative.
Comments
GMC 710 configuration settings do not match
those of backup configuration memory. The
system should be serviced.
A failure has been detected in the GMC 710.
The GMC 710 is unavailable.
The GMC 710 has incorrect software installed.
The system should be serviced.
A key is stuck on the GMC 710 bezel. Attempt
to free the stuck key by pressing it several
times. The system should be serviced if the
problem persists.
EICAS
Message
GMC CONFIG – GMC Config error.
Config service req’d.
Flight
Instruments
GMC 710 Message Advisories
Flight
Planning
Miscellaneous Message Advisories
Comments
Upon power-up, the system detects that a
stored flight plan waypoint is locked. This
occurs when a navigation 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 – Flight plan
The system has detected that a waypoint
waypoint moved.
coordinate has changed due to a new
navigation database update. Verify that stored
flight plans contain correct waypoint locations.
TIMER EXPIRD – Timer has expired. The system notifies the pilot that the timer has
expired.
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Hazard
Avoidance
190-00600-03 Rev. A
Procedures
Message
FPL WPT LOCK – Flight plan
waypoint is locked.
85
Miscellaneous Message Advisories (Cont.)
Message
DB CHANGE – Database changed.
Verify user modified procedures.
DB CHANGE – Database changed.
Verify stored airways.
FPL TRUNC – Flight plan has been
truncated.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
LOCKED FPL – Cannot navigate
locked flight plan.
WPT ARRIVAL – Arriving at
waypoint -[xxxx]
STEEP TURN – Steep turn ahead.
INSIDE ARSPC – Inside airspace.
ARSPC AHEAD – Airspace ahead
less than 10 minutes.
ARSPC NEAR – Airspace near and
ahead.
86
Comments
This occurs when a stored flight plan contains
procedures that have been manually edited.
This alert is issued only after a navigation
database update. Verify that the user-modified
procedures in stored flight plans are correct and
up to date.
This occurs when a stored flight plan contains
an airway that is no longer consistent with the
navigation database. This alert is issued only
after a navigation database update. Verify use
of airways in stored flight plans and reload
airways as needed.
This occurs when a newly installed navigation
database eliminates an obsolete approach
or arrival used by a stored flight plan. The
obsolete procedure is removed from the flight
plan. Update flight plan with current arrival or
approach.
This occurs when the pilot attempts to activate
a stored flight plan that contains locked
waypoint. Remove locked waypoint from flight
plan. Update flight plan with current waypoint.
Arriving at waypoint [xxxx], where [xxxx] is the
waypoint name.
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.
Special use airspace is near and ahead of the
aircraft position.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Annunciations & Alerts
Bad parallel track geometry.
Procedures
Invalid leg type for parallel offset.
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
IAF waypoint for parallel offset has been
passed.
The current vertical waypoint can not be
reached within the maximum flight path angle
and vertical speed constraints. The system
automatically transitions to the next vertical
waypoint.
The lateral flight plan contains a procedure
turn, vector, or other unsupported leg type
prior to the active vertical waypoint. This
prevents vertical guidance to the active vertical
waypoint.
The current track angle error exceeds the limit,
causing the vertical deviation to go invalid.
Hazard
Avoidance
VNV – Unavailable. Excessive track
angle error.
Flight
Planning
VNV – Unavailable. Unsupported
leg type in flight plan.
GPS Nav
PTK FAIL – Parallel track unavailable:
bad geometry.
PTK FAIL – Parallel track unavailable:
invalid leg type.
PTK FAIL – Parallel track unavailable:
past IAF.
UNABLE V WPT – Can’t reach
current vertical waypoint.
AFCS
SLCT NAV – Select NAV on CDI for
approach.
Nav/Com/
XPDR/Audio
SLCT FREQ – Select appropriate
frequency for approach.
Comments
Special use airspace is within 2 nm of the
aircraft position.
The system notifies the pilot that the loaded
approach is not active. Activate approach
when required.
The system notifies the pilot to load the
approach frequency for the appropriate NAV
receiver. Select the correct frequency for the
approach.
The system notifies the pilot to set the CDI to
the correct NAV receiver. Set the CDI to the
correct NAV receiver.
EICAS
Message
ARSPC NEAR – Airspace near – less
than 2 nm.
APR INACTV – Approach is not
active.
Flight
Instruments
Miscellaneous Message Advisories (Cont.)
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
87
Miscellaneous Message Advisories (Cont.)
VNV – Unavailable. Excessive
crosstrack error.
VNV – Unavailable. Parallel course
selected.
NO WGS84 WPT – Non WGS 84
waypoint for navigation -[xxxx]
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
TRAFFIC FAIL – Traffic device has
failed.
FAILED PATH – A data path has
failed.
MAG VAR WARN – Large magnetic
variance. Verify all course angles.
SVS – SVS DISABLED: Out of
available terrain region.
SVS – SVS DISABLED: Terrain DB
resolution too low.
SCHEDULER [#] – <message>.
CHECK CRS – Database course for
LOC1 / [LOC ID] is [CRS]°.
CHECK CRS – Database course for
LOC2 / [LOC ID] is [CRS]°.
[PFD1, PFD2, or MFD1] CARD
1 REM – Card 1 was removed.
Reinsert card.
88
The current crosstrack exceeds the limit,
causing vertical deviation to go invalid.
A parallel course has been selected, causing
the vertical deviation to go invalid.
The position of the selected waypoint [xxxx]
is not calculated based on the WGS84 map
reference datum and may be positioned in
error as displayed. Do not use GPS to navigate
to the selected non-WGS84 waypoint.
The system is no longer receiving data from
the traffic system. The traffic device should be
serviced.
A data path connected to the GDU, GSD 41,
GSD 69A, or the GIA 63/W has failed.
The GDU’s internal model cannot determine
the exact magnetic variance for geographic
locations near the magnetic poles. Displayed
magnetic course angles may differ from the
actual magnetic heading by more than 2°.
Synthetic Vision is disabled because the aircraft
is not within the boundaries of the installed
terrain database.
Synthetic Vision is disabled because a terrain
database of sufficient resolution (9 arc-second
or better) is not currently installed.
Message criteria entered by the user.
Selected course for LOC1 differs from published
localizer course by more than 10 degrees.
Selected course for LOC2 differs from published
localizer course by more than 10 degrees.
The SD card was removed from the top card
slot of the specified PFD or MFD. The SD card
needs to be reinserted.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Annunciations & Alerts
Nav/Com/
XPDR/Audio
The SD card was removed from the bottom
card slot of the specified PFD or MFD. The SD
card needs to be reinserted.
The SD card in the top card slot of the specified
PFD or MFD contains invalid data.
The SD card in the bottom card slot of the
specified PFD or MFD contains invalid data.
EICAS
[PFD1, PFD2, or MFD1] CARD
2 REM – Card 2 was removed.
Reinsert card.
[PFD1, PFD2, or MFD1] CARD 1
ERR – Card 1 is invalid.
[PFD1, PFD2, or MFD1] CARD 2
ERR – Card 2 is invalid.
Flight
Instruments
Miscellaneous Message Advisories (Cont.)
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
89
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
Blank Page
90
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Appendix
Flight
Instruments
Appendix
PFD Softkey Map
EICAS
ADF/DME
Nav/Com/
XPDR/Audio
AFCS
Top Level PFD Softkeys
GPS Nav
(optional TCAS II)
(optional TCAS II)
TRFC/MAP
XPDR/TFC
ADF/DME
Flight
Planning
Procedures
TRFC-1
Hazard
Avoidance
Select the BACK Softkey to return
to the top-level softkeys.
TRFC-2
Annun/
Alerts
OFF
Pressing the INSET Softkey Displays Inset Map
in the PFD lower left corner. The TRFC/MAP
Softkey is displayed when the TCAS II option
is installed. Pressing the TRFC/MAP Softkey
displays the Inset Map showing Traffic Map Page.
Removes Inset Map
Abnormal
Operation
INSET or
TRFC/MAP
Additional
Features
Inset Map Softkeys
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Index
190-00600-03 Rev. A
Appendix
DCLTR (3) 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
91
Appendix
EICAS
Flight
Instruments
TRAFFIC
Nav/Com/
XPDR/Audio
TOPO
TERRAIN
AFCS
NEXRAD
GPS Nav
XM LTNG
Cycles through traffic display options:
TRFC-1: Traffic displayed on inset map
TRFC-2: Traffic Map Page is displayed in the
inset map window
Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation scale on Inset Map
Displays terrain information on Inset Map (not
available with TAWS-A)
Displays NEXRAD weather and coverage
information on Inset Map (optional feature)
Displays XM lightning information on Inset Map
(optional feature)
Flight
Planning
ADF/DME
Procedures
Press the BACK Softkey to
return to the top level softkeys.
ADC1
ADC2
AHRS2
BACK
MSG
Hazard
Avoidance
Sensor Softkeys
ADC1
Displays softkeys for selecting the #1 and #2 AHRS
and Air Data Computers
Selects the #1 Air Data Computer
ADC2
Selects the #2 Air Data Computer
AHRS1
Selects the #1 AHRS
AHRS2
Selects the #2 AHRS
SENSOR
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
AHRS1
92
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Appendix
Flight
Instruments
ADF/DME
DME
ALT UNIT
NAV2
GPS
GPS
OFF
OFF
IN
AFCS
METERS
Select the BACK Softkey
to return to the top-level softkeys
Nav/Com/
XPDR/Audio
NAV1
EICAS
SYN VIS
HPA
GPS Nav
SYN TERR HRZN HDG APTSIGNS
Flight
Planning
PATHWAY
PFD Configuration Softkeys
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Appendix
190-00600-03 Rev. A
Annun/
Alerts
DFLTS
HRZN HDG Displays compass heading along the
Zero-Pitch line
APTSIGNS Displays position markers for airports
within approximately 15 nm of the
current aircraft position. Airport
identifiers are displayed when the
airport is within approximately 9 nm.
Resets PFD to default settings, including changing units to standard
Abnormal
Operation
SYN TERR
Additional
Features
PATHWAY
Hazard
Avoidance
SYN VIS
Displays second-level softkeys for
additional PFD configurations
Displays the softkeys for enabling or
disabling Synthetic Vision features
Displays rectangular boxes representing
the horizontal and vertical flight path
of the active flight plan
Enables synthetic terrain depiction
Procedures
PFD
93
Appendix
Flight
Instruments
WIND
EICAS
OPTN 1
OPTN 2
Nav/Com/
XPDR/Audio
OPTN 3
OFF
GPS Nav
AFCS
DME
BRG1
Procedures
Flight
Planning
BRG2
Hazard
Avoidance
ALT UNIT
Additional
Features
METERS
IN
Abnormal
Operation
HPA
OBS
CDI
Index
Appendix
Annun/
Alerts
STD BARO
94
Displays softkeys to select wind data
parameters
Wind direction arrows with headwind
and crosswind components
Wind direction arrow and speed
Wind direction arrow with direction
and speed
Information not displayed
Displays the DME information window
Cycles the Bearing 1 Information
Window through NAV1 or GPS/
waypoint identifier and GPS-derived
distance information.
Cycles the Bearing 2 Information
Window through NAV2 or GPS/
waypoint identifier and GPS-derived
distance information.
Displays softkeys for setting the
altimeter and BARO settings to metric
units
When enabled, displays altimeter and
selected altitude 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)
Selects OBS mode on the CDI when
navigating by GPS (only available with
active leg)
Cycles through GPS, VOR1 (LOC1),
and VOR2 (LOC2) navigation sources
on the CDI
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Appendix
Flight
Instruments
Displays the ADF/DME Tuning
Window, providing ADF tuning
capability (when installed) and
allowing selection of the NAV source
for tuning each DME
ADF/DME
EICAS
Nav/Com/
XPDR/Audio
ADF/DME
AFCS
Press the BACK Softkey to return
to the top-level softkeys.
MSG
GPS Nav
Selecting BACK returns to the previous softkey level.
Flight
Planning
MSG
Procedures
Transponder Softkeys
XPDR2
Selects the #2 transponder as active.
STBY
Selects Standby Mode (transponder does
not reply to any interrogations)
Selects Mode A (transponder replies to
identification 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. Not
available with TCAS II option.
95
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Appendix
190-00600-03 Rev. A
Annun/
Alerts
GND
Abnormal
Operation
ALT
Additional
Features
ON
Hazard
Avoidance
XPDR1
Displays transponder mode selection
softkeys
Selects the #1 transponder as active.
XPDR
Appendix
BKSP
Removes numbers entered, one at a time
Flight
Instruments
EICAS
CODE
TMR/REF
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Displays Timer/References Window
NRST
Displays Nearest Airports Window
MSG
Displays Messages Window
IDENT
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
0—7
Automatically enters the VFR code (1200 in
the U.S.A. only). Not available when TCAS
II option is installed.
Displays transponder code selection softkeys 0-7
Use numbers to enter code
VFR
PFD
OBS
CDI
(optional)
ADF/DME XPDR/TFC
IDENT
Procedures
TRFC/MAP SENSOR
TMR/REF
NRST
MSG
Press the BACK Softkey to return
to the top-level softkeys.
XPDR2
MODE
TCAS
CODE
BACK
IDENT
Hazard
Avoidance
XPDR1
MSG
Additional
Features
Selecting BACK returns to the
previous softkey level.
REL
ABS
ALT RNG
TEST
BACK
MSG
Abnormal
Operation
Selecting BACK returns to the
previous softkey level.
ABOVE NORMAL BELOW UNREST
BACK
MSG
Annun/
Alerts
Selecting BACK returns to the
previous softkey level.
STBY
ON
ALT
TA ONLY
BACK
TA/RA
MSG
Appendix
Selecting BACK returns to the
previous softkey level.
0
1
2
3
4
5
6
7
IDENT
BKSP
BACK
MSG
Index
Transponder/Traffic Softkeys with TCAS II Option
96
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Appendix
XPDR1
Appendix
Index
97
Annun/
Alerts
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Abnormal
Operation
190-00600-03 Rev. A
Additional
Features
BACK
Hazard
Avoidance
TA/RA
Procedures
TA ONLY
Flight
Planning
ALT
GPS Nav
ON
AFCS
STBY
Nav/Com/
XPDR/Audio
MODE
EICAS
XPDR2
Displays the transponder and
TCAS II selection softkeys
Selects the #2 transponder as
active.
Selects the #2 transponder as
active.
Displays transponder mode
selection softkeys
Selects transponder Standby
Mode (transponder does not
reply to any interrogations).
When the transponder is set to
standby, the TCAS II system is
also set to standby.
Activates transponder
(transponder replies to
identification interrogations).
When the transponder is set to
ON, the TCAS II system is set
to standby.
Altitude Reporting Mode
(transponder replies to
identification and altitude
interrogations). When the
transponder is set to ALT,
the TCAS II system is set to
standby.
Activates the TCAS II system
in TA Only Mode and sets the
transponder to ALT
Activates the TCAS II system
in TA/RA Mode and sets the
transponder to ALT
Returns to the previous softkey
level
Flight
Instruments
XPDR/TFC
Appendix
Flight
Instruments
TCAS
EICAS
REL
Nav/Com/
XPDR/Audio
ABS
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
ALT RNG
Abnormal
Operation
TEST
BACK
Annun/
Alerts
CODE
Appendix
0—7
Index
IDENT
98
Displays the TCAS control
softkeys
Displays intruder altitude as
altitude relative to own aircraft
altitude
Displays intruder MSL altitude
Displays the altitude display
range softkeys
Displays non-threat traffic from
ABOVE
9900 feet above the aircraft to
2700 feet below the aircraft.
Typically used during climb
phase of flight.
NORMAL Displays non-threat traffic from
2700 feet above the aircraft to
2700 feet below the aircraft.
Typically used during enroute
phase of flight.
BELOW Displays non-threat traffic from
2700 feet above the aircraft to
9900 feet below the aircraft. Typically used during descent
phase of flight.
UNREST All traffic is displayed
Activates Test Mode and
displays test intruder symbols
Returns to the previous softkey
level
Displays transponder code
selection softkeys 0-7
Use numbers to enter code
Activates the Special Position
Identification (SPI) pulse for
18 seconds, identifying the
transponder return on the ATC
screen
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Appendix
IDENT
Flight
Planning
(optional)
CAS ↑
CAS ↓
DCLTR
MAP
GPS Nav
MFD Softkey Map
AFCS
MSG
Nav/Com/
XPDR/Audio
NRST
EICAS
TMR/REF
Flight
Instruments
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
BKSP
SHW CHRT
Procedures
DCLTR-1
DCLTR-2
TOPO
TERRAIN
AIRWAYS
(optional)
(optional)
NEXRAD
XM LTNG
BACK
Additional
Features
TRAFFIC
Select the BACK Softkey on this level to
return to the top softkey level.
Hazard
Avoidance
DCLTR-3
AIRWY ON
Abnormal
Operation
AIRWY LO
AIRWAY HI
Annun/
Alerts
MFD Softkeys
Appendix
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
99
CAS ↑
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
CAS ↓
MAP
TRAFFIC Displays traffic information on Navigation Map
Displays topographical data (e.g., coastlines,
terrain, rivers, lakes) and elevation scale on
Navigation Map
TERRAIN Displays terrain information on Navigation Map
TOPO
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Appendix
DCLTR (3)
SHW CHRT
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
AIRWAYS 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
NEXRAD Displays NEXRAD weather and coverage
information on Navigation Map (optional feature)
XM LTNG Displays XM lightning information on Navigation
Map (optional feature)
Returns to top-level softkeys
BACK
100
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
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Appendix
EICAS
Nav/Com/
XPDR/Audio
The 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 navigation and Jeppesen ChartView database updates. Not all SD cards are
compatible with the G1000. Use only SD cards supplied by Garmin or the aircraft
manufacturer.
Information regarding the various databases may be viewed on the AUX-System
Status Page.
Flight
Instruments
Database Updates
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Display Database
Selection Softkey
AUX-System Status Page
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
101
The Display Database Selection Softkey is used to place the cursor in the Database
Window. Upon first press of the Display Database Selection Softkey, the softkey will
change to a selected state (black text on gray background) and the cursor will appear
in the Database Window. At this point the user can scroll through all databases in
the Database Window to view status information. If the Display Database Selection
Softkey is selected repeatedly, the softkey will switch between PFD1, PFD2, and MFD1.
Database status information in the Database Window will reflect the database of the
selected PFD or MFD.
Unselected
Garmin Databases
The following databases are stored on Supplemental Data Cards provided by
Garmin:
• Expanded basemap
• Terrain
• Airport terrain
Hazard
Avoidance
• Obstacle
• SafeTaxi
• FliteCharts
• Airport Directory
(AOPA)
After subscribing to the desired database product updates, these updated databases
are copied to each Supplemental Data Card for each display (the card that contains the
FliteCharts or ChartView database resides in the MFD). Since these databases are not
stored internally in the displays, these Supplemental Data Cards must remain in the
bottom card slot of each display.
Abnormal
Operation
Additional
Features
PFD1 DB Selected
Annun/
Alerts
NOTE: The data contained in the terrain and obstacle databases comes from
government agencies. Garmin accurately processes and cross-validates the
data, but cannot guarantee the accuracy and completeness of the data.
Obtaining Garmin Database Updates
The Garmin database updates can be obtained by following the instructions
detailed in the ‘Aviation Databases’ section of the Garmin website (fly.garmin.com).
Once the updated files have been downloaded from the website, a PC equipped with
Index
Appendix
MFD1 DB Selected
Display Database Selection Softkey
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Appendix
102
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Appendix
Abnormal
Operation
Annun/
Alerts
Appendix
Index
103
Additional
Features
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Hazard
Avoidance
190-00600-03 Rev. A
Procedures
Loading the Garmin database updates:
1) With system power OFF, remove the MFD database card from the bottom
card slot of the MFD.
2) Update the Garmin databases on the MFD card.
3) Insert the MFD database card into the bottom card slot of the MFD.
Flight
Planning
In some cases it may be necessary to obtain an unlock code from Garmin in order
to make the database product functional. It may also be necessary to have the system
configured by a Garmin authorized service facility in order to use some database
features.
GPS Nav
Loading Updated Databases
AFCS
The ChartView database should be copied to the Supplemental Data Card which
will reside in the bottom card slot on the MFD. The navigation database is be loaded
from the Jeppesen or user supplied SD data card. Contact Jeppesen (www.jeppesen.
com) for subscription and update information.
The navigation database is loaded from an SD card inserted into the top card slot
of each displayed. The database is copied from the SD card in the top card slot to the
display’s internal memory.
Nav/Com/
XPDR/Audio
Note: The Jeppesen aviation navigation database is now referred to as the
‘navigation database’. Previously this database had been referred to as the
‘aviation database’.
EICAS
Jeppesen Databases
Flight
Instruments
an appropriate SD card reader is used to unpack and copy the new databases onto the
appropriate Supplemental Data Cards. Equipment required to perform the update is
as follows:
• Windows-compatible PC computer (Windows 2000 or XP recommended)
• SD Card Reader: SanDisk SDDR-93, SanDisk SDDR-99, Verbatim #96504, or
equivalent
• Updated database obtained from the Garmin website
• Existing Supplemental Database SD Card (010-00330-41, -42, or -43) from the
MFD. The supplemental data card from the MFD should be used because all
databases (except the active navigation database) are required to reside on this
card.
Appendix
Apply power to the system, check that the databases are initialized
and displayed on the power-up screen. When updating the terrain and
FliteCharts databases, a ‘Verifying’ message may be seen. If this message is
present, wait for the system to finish loading before proceeding to step 5.
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
4)
Procedures
Blank Page
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Database Information on the Power-up Screen
5)
Acknowledge the Power-up Page agreement by pressing the ENT Key or
the right most softkey.
6)
Turn the large FMS Knob to select the AUX Page group on the MFD.
7)
Turn the small FMS Knob to select the System Status Page.
8)
Make sure the SYNC DBS Softkey is in the enabled state.
9)
Monitor the Sync Status in the Database Window. Wait for all databases to
complete synching, indicated by ‘Complete’ being displayed.
10) Remove and reapply power to the system.
Annun/
Alerts
11) Turn the large FMS Knob to select the AUX Page group on the MFD.
12) Turn the small FMS Knob to select the System Status Page.
Index
Appendix
13) Select the Display Database Selection Softkey to show database information
for each display (MFD1 DB, PFD1 DB). Verify the correct database cycle
information is shown for each database for each display.
104
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Appendix
Flight
Instruments
Canceling an automatic database synchronization:
1) While synchronization is in progress, select the SYNC DBS Softkey to
disable (Figure B-2) automatic database synchronization.
2) Acknowledge the cancelation by pressing the ENT Key.
EICAS
With the G1000 system OFF, insert the SD card containing the new
navigation database version into the top card slot of the MFD (label of SD
card facing left).
Turn the G1000 system ON. A prompt similar to the following illustration is
displayed:
3)
Procedures
2)
Flight
Planning
Copy the new navigation database to an SD card obtained from Garmin, or
the aircraft manufacturer.
GPS Nav
1)
AFCS
NOTE: Loading the Jeppesen navigation database prior to its effective date
will result in the expiration date on the power-up screen and the effective
date on the AUX-System Status Page being displayed in yellow.
Nav/Com/
XPDR/Audio
Loading the Jeppesen navigation database:
Hazard
Avoidance
Additional
Features
Navigation Database Load Prompt
Abnormal
Operation
5)
After the update completes, the display starts in normal mode.
6)
Turn the G1000 system OFF and remove the SD card from the top card slot.
7)
Repeat steps 2 through 6 for PFD1.
8)
Repeat steps 2 through 6 for PFD2.
9)
Apply power to the system and press the ENT Key to acknowledge the
startup screen.
Appendix
Select the YES Softkey to update the navigation database in the MFD.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Index
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
190-00600-03 Rev. A
Annun/
Alerts
4)
105
Appendix
Flight
Instruments
11) Turn the small FMS Knob to select the System Status Page.
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
12) Select the Display Database Selection Softkey to show navigation database
information for each display (MFD1 DB, PFD1 DB, PFD2 DB).
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Check Database Cycle Number (MFD shown)
106
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Index
E
Edit a flight plan 32
Engine display 5
F
Procedures
Hazard
Avoidance
Flight Director 13
Flight ID 7
Flight path marker 51
FliteCharts® 53
Frequency Transfer 9
Additional
Features
G
Gain 48
Cabin pressure altitude 5
CDI 1, 2, 9, 87
Channel Presets 56
ChartView 53
Clearance player 11
Clearance Recorder 11
Code selection softkeys 8
COM 8, 9, 11, 59
Crew Alerting System (CAS)
Messages 6–7
HF 8
Horizon heading 51
Horizontal scan 48
Annun/
Alerts
H
Abnormal
Operation
C
I
Appendix
Inhibit 46
Inhibit TAWS 46
Inset Map 91, 92
Intercom isolation 10
IOI 67
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Index
190-00600-03 Rev. A
Flight
Planning
Barometric Altitude Minimums 3
Barometric pressure 94
Bearing line 48, 49
GPS Nav
B
AFCS
Databases 101
Database synchronization 105
Database updates 101, 102, 103
DCLTR Softkey 53
Dead Reckoning 61
Declutter 100
Declutter 60, 91
Designated altitudes 20
Direct-to 17
DME 7, 9
DR mode 61, 62
Nav/Com/
XPDR/Audio
Activate a flight plan 18
Active Channel 55
ADF 7, 9
AHRS 81, 82, 84, 85
Airport Signs 51, 52
Airways 100
Air Data Computer 66
Alert messages 83
ALT 42
Altimeter setting 1
Altitude mode 42
Altitude volume 42
Antenna stabilization 49
Antenna tilt 47
AOPA’s Airport Directory 55
Attitude & Heading Reference System
66
Audio Panel 59
Audio panel controls
NAV1, NAV2 9
EICAS
D
Flight
Instruments
A
Index-1
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Index
J
S
Jeppesen 53
SafeTaxi® 51, 53
Sector scan 49
Secure Digital (SD) cards 101
Sensor 66
STAB 49
Standby 47
Store Flight Plan 32
Supplemental Data Card 102, 103
SVS 51, 88
Synthetic Vision System 51
M
Map panning 40
Message advisories 72–79, 81–89
METAR 39
Minimums 70
MISCOMP 65
Mode S 95
Multi Function Display (MFD)
Softkeys 99
N
NAV 9
NAV1 2, 9
NAV2 2, 9
Navigation database 19, 20, 71, 73,
76, 85, 86
NEXRAD 39, 40, 92, 100
O
OBS 2
Obstacles 76, 78
Overspeed Protection 14
P
Pathways 51, 52
PIT 65
Play 11
R
Resolution Advisory 41, 52
Reversionary mode 59
Reversionary Mode
EICAS 5
ROC 67
Index-2
T
TAF 39
TAS 42, 43, 81
TAWS 45, 46, 67
TAWS-A 67, 92
TAWS-B 45
TCAS II 8, 43, 44, 52, 91, 95, 96, 97
Terrain 45, 76, 92, 100
Tilt line 47
Timer 2, 85
Topographical data 92, 100
Traffic 39, 42, 44, 100
Traffic advisory 41
Traffic Advisory 41
Traffic map page 42, 43, 44
Transponder 7, 8, 95, 96, 97, 98, 99
V
Vertical speed guidance 20
Vertical track 70
VNV 17, 60, 87, 88
Vspeed 2
W
WAAS 78
WATCH® 49
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Index
Flight
Instruments
Waypoint Selection Submenu 28
Weather Attenuated Color Highlight 49
Weather data link page 39
Weather radar 47
Wind data 94
EICAS
Nav/Com/
XPDR/Audio
X
XM lightning 92, 100
XM weather 39
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Index-3
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Index
Blank Page
Index-4
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p: 913.397.8200 f: 913.397.8282
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
p: 503.391.3411 f: 503.364.2138
Garmin (Europe) Ltd
Liberty House, Bulls Copse Road
Hounsdown Business Park
Southampton, SO40 9RB, U.K.
p: 44/0870.8501241 f: 44/0870.8501251
Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p: 886/2.2642.9199 f: 886/2.2642.9099
www.garmin.com
© 2006-2010 Garmin Ltd. or its subsidiaries
190-00600-03 Rev. A
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