Garmin | G1000: Cessna Citation Mustang | Garmin G1000: Cessna Citation Mustang G1000 CRG for Cessna Citation Mustang

Garmin G1000: Cessna Citation Mustang G1000 CRG for Cessna Citation 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 © 2006-2011, 2016 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0413.28 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.
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190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Honeywell International, Inc.; CO Guardian is a trademark of CO Guardian, Inc.
AC-U-KWIK® is a registered trademark of Penton Business Media Inc.
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively
“AOPA”) expressly disclaim all warranties, with respect to the AOPA information included in this
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consequential damages that result from the use or inability to use the software or related
documentation, even if AOPA or an AOPA authorized representative has been advised of the
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in the datasets. Some jurisdictions do not allow the limitation or exclusion of implied warranties
or liability for incidental or consequential damages so the above limitations or exclusions may not
apply to licensee.
Printed in the U.S.A.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Warnings, Cautions & Notes
WARNING: Do not use the terrain avoidance feature as the sole means of
navigation and terrain separation. The terrain avoidance feature is only to
be used as and aid to terrain avoidance. Garmin obtains terrain database
content from third party sources and is not able to independently verify the
accuracy of the terrain data.
WARNING: Do not rely on the displayed minimum safe altitude (MSAs) as
the sole source of obstacle and terrain avoidance information. The displayed
minimum safe altitudes (MSAs) are only advisory in nature. Always refer to
current aeronautical charts for appropriate minimum clearance altitudes.
WARNING: Do not use GPS-derived geometric altitude for compliance with air
traffic control altitude requirements in the National Airspace System (NAS) or
internationally. The primary barometric altimeter must be used for compliance
with all air traffic control altitude regulations, requirements, instructions, and
clearance.
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.
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 only an aid to
enhance situational awareness.
WARNING: Do not rely solely upon the display of traffic information for
collision avoidance maneuvering. The traffic display does not provide collision
avoidance resolution advisories and does not under any circumstances or
conditions relieve the pilot’s responsibility to see and avoid other aircraft.
WARNING: Do not rely solely upon the display of traffic information to
accurately depict all of the traffic within range of the aircraft. Due to lack
of equipment, poor signal reception, and/or inaccurate information from
aircraft or ground stations, traffic may be present that is not represented on
the display.
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Warnings, Cautions & Notes
WARNING: Do not use data link weather information for maneuvering in,
near or around areas of hazardous weather. Information contained within data
link weather products may not accurately depict current weather conditions.
WARNING: Do not use the indicated data link weather product age to
determine the age of the weather information shown by the data link weather
product. Due to time delays inherent in gathering and processing weather
data for data link transmission, the weather information shown by the data
link weather product may be older than the indicated weather product age.
WARNING: Do not rely on information from the lightning detection system
display as the sole basis for hazard weather avoidance. Range limitations
and interference may cause the system to display inaccurate or incomplete
information. Refer to the documentation from the lightning detection system
manufacturer for detailed information about the system.
WARNING: The Garmin system, as installed in this aircraft, has a very
high degree of functional integrity. However, the pilot must recognize that
providing monitoring and/or self-test capability for all conceivable system
failures is not practical.
WARNING: Do not use the system until carefully reviewing, and gaining
a thorough understanding of all aspects of the system’s Pilot’s Guide
documentation and the Airplane Flight Manual. Do not attempt to learn
system operational procedures while the aircraft is in the air. 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.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Warnings, Cautions & Notes
WARNING: To reduce the risk of unsafe operation, carefully review and
understand all aspects of the Pilot’s Guide documentation and the 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: Do not use the system to attempt to penetrate a thunderstorm.
The illustrations in this guide are only examples. Both the FAA Advisory
Circular, Subject: Thunderstorms, and the Aeronautical Information Manual
(AIM) recommend avoiding any thunderstorm identified as severe of giving
intense radar echo by at least 20 miles.
WARNING: Lamp(s) inside this product 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.
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Warnings, Cautions & Notes
WARNING: Do not use a QFE altimeter setting with this system. System
functions will not operate properly with a QFE altimeter setting. Use only
a QNH altimeter setting for height above mean sea level, or the standard
pressure setting, as applicable.
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: Do not rely upon data link services to provide Temporary Flight
Restriction (TFR) information. Always confirm TFR information through official
sources such as Flight Service Stations or Air Traffic Control.
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.
NOTE: This device complies with part 15 of the FCC Rules. Operation is
subject to the following two conditions: (1) this device may not cause harmful
interference, and (2) this device must accept any interference received,
including interference that may cause undesired operation.
NOTE: This product, its packaging, and its components contain chemicals
known to the State of California to cause cancer, birth defects, or reproductive
harm. This notice is being provided in accordance with California’s Proposition
65. If you have any questions or would like additional information, please
refer to our web site at www.garmin.com/prop65.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Warnings, Cautions & Notes
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: Garmin requests the flight crew report any observed discrepancies
related to database information. These discrepancies could come in the form
of an incorrect procedure; incorrectly identified terrain, obstacles and fixes; or
any other displayed item used for navigation or communication if the air or
on the ground. Go to FlyGarmin.com and select Aviation Data Error Report.
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 Pilot’s Guide for this aircraft.
NOTE: The FAA has asked Garmin to remind pilots who fly with Garmin
database-dependent avionics of the following:
• It is the pilot’s responsibility to remain familiar with all FAA regulatory
and advisory guidance and information related to the use of databases in
the National Airspace System.
• Garmin equipment will only recognize and use databases that are
obtained from Garmin or Jeppesen. Databases obtained from Garmin
or Jeppesen are assured compliance with all data quality requirements
(DQRs) by virtue of a Type 2 Letter of Authorization (LOA) from the FAA. A
copy of the Type 2 LOA is available for each database and can be viewed
at http://fly.garmin.com by selecting ‘Type 2 LOA Status.’
• Use of a current Garmin or Jeppesen database in your Garmin equipment
is required for compliance with established FAA regulatory guidance, but
does not constitute authorization to fly any and all terminal procedures
that may be presented by the system. It is the pilot’s responsibility to
operate in accordance with established AFM(S) and regulatory guidance or
limitations as applicable to the pilot, the aircraft, and installed equipment.
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Warnings, Cautions & Notes
NOTE: The pilot/operator must review and be familiar with Garmin’s database
exclusion list as discussed in SAIB CE-14-04 to determine what data may be
incomplete. The database exclusion list can be viewed at www.flygarmin.
com by selecting ‘Database Exclusions List.’
NOTE: The pilot/operator must have access to Garmin and Jeppesen database
alerts and consider their impact on the intended aircraft operation. The
database alerts can be viewed at www.flygarmin.com by selecting ‘Aviation
Database Alerts.’
NOTE: If the pilot/operator wants or needs to adjust the database, contact
Garmin Product Support to coordinate the revised DQRs.
NOTE: Garmin requests the flight crew report any observed discrepancies
related to database information. These discrepancies could come in the form
of an incorrect procedure; incorrectly identified terrain, obstacles and fixes;
or any other displayed item used for navigation or communication in the air
or on the ground. Go to FlyGarmin.com and select ‘Report An Aviation Data
Error Report.’
NOTE: Operate G1000 system power through at least one cycle in a period
of four days of continuous operation to avoid an autonomous system reboot.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
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
190-00600-04
190-00600-05 Rev. C
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
Added GDU 12.02 parameters
Added Profile View
Added MV DB update procedure
Updated Database update procedures
Updated XM WX weather product symbols
Flight Plan Enhancements
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
RR-1
Record of Revisions
Part Number
190-00600-05
Rev A
Rev B
Change Summary
Added GDU 15.12 parameters
Added Temperature Compensated Altitudes
Added User Defined Holds
Updated Weather Radar information
Added AC-U-KWIK Airport Directory capability
Updated CAS Messages
Added ADS-B out
Updated Transponder information
Added Visual Reporting Points
Clerical
Revision Date of Revision Affected Pages
C
August, 2016
Page 43
RR-2
Description
Added Temperature Compensation
to the Load And/Or Activate An
Approach Procedure
Page 51
Added Displaying a Weather Radar
Overlay on the Navigation Map
Pages 110 & 111
Added WX RADAR Softkey to the MFD
Softkey Map and associated table
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Table of Contents
Flight Instruments........................................................................................................................ 1
Selecting the Altimeter Barometric Pressure Setting....................................................... 1
Selecting Standard Barometric Pressure (29.92 IN HG).................................................... 1
Change Altimeter Barometric Pressure Setting Units....................................................... 1
Synchronizing the Altimeter Barometric Pressure Settings............................................ 1
Synchronize CDI......................................................................................................................... 1
Change Navigation Sources.................................................................................................... 2
Enable/Disable OBS Mode While Navigating with GPS..................................................... 2
Generic Timer.............................................................................................................................. 2
Configure Vspeed Bugs Individually...................................................................................... 2
Turn Vspeed Bugs On Or Off By Category............................................................................ 3
Set Minimum Descent Altitude/Decision Height................................................................ 3
Displaying Wind Data............................................................................................................... 3
Engine Indication & Crew Alerting System.................................................................... 5
Crew Alerting System (CAS).................................................................................................... 6
CAS Messages............................................................................................................................. 6
Nav/Com/Transponder/Audio Panel.................................................................................... 7
Enter Or Change Flight ID........................................................................................................ 7
ADF Tuning (Optional)............................................................................................................... 7
DME Tuning (Optional).............................................................................................................. 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............................................................................................. 9
Clearance Recorder And Player............................................................................................ 10
Automatic Flight Control System...................................................................................... 11
Flight Director Activation...................................................................................................... 11
Vertical Modes.......................................................................................................................... 12
Lateral Modes........................................................................................................................... 13
GPS Navigation............................................................................................................................ 15
Direct-to Navigation............................................................................................................... 15
Activate A Stored Flight Plan................................................................................................ 16
Activate A Flight Plan Leg..................................................................................................... 16
Stop Navigating A Flight Plan............................................................................................... 17
Vertical Navigation (VNAV)................................................................................................... 18
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
i
Table of Contents
Flight Planning............................................................................................................................. 21
Weight Planning....................................................................................................................... 21
Trip Planning............................................................................................................................. 21
Selecting A VRP (Visual Reporting Point)........................................................................... 23
Create A User Waypoint Defined By Latitude & Longitude............................................ 24
Create A User Waypoint Defined By Radials From Other Waypoints........................... 24
Create A User Waypoint Defined By A Radial & Distance From Another Waypoint. 26
Create A User Waypoint Using The Map Pointer............................................................... 28
Delete A User Waypoint......................................................................................................... 28
Create A Flight Plan................................................................................................................. 29
Import A Flight Plan From An SD Card................................................................................ 30
Insert A Waypoint in the Active Flight Plan....................................................................... 31
Enter An Airway In A Flight Plan.......................................................................................... 32
User-Defined Holding Patterns............................................................................................. 33
Invert An Active Flight Plan................................................................................................... 36
Remove A Departure, Arrival, Approach, Or Airway From A Flight Plan..................... 36
Store A Flight Plan................................................................................................................... 37
Edit A Stored Flight Plan ....................................................................................................... 37
Delete A Waypoint From the Flight Plan............................................................................ 37
Invert And Activate A Stored Flight Plan........................................................................... 38
Copy A Flight Plan................................................................................................................... 38
Delete A Flight Plan................................................................................................................. 39
Graphical Flight Plan Creation.............................................................................................. 39
Export A Flight Plan To An SD Card...................................................................................... 39
Procedures...................................................................................................................................... 41
Load And Activate A Departure Procedure........................................................................ 41
Activate A Departure Leg...................................................................................................... 41
Load An Arrival Procedure..................................................................................................... 42
Activate An Arrival Leg.......................................................................................................... 42
Load And/Or Activate An Approach Procedure................................................................. 43
Activate An Approach In the Active Flight Plan................................................................ 44
Activate A Vector to Final Approach Fix............................................................................. 44
Activate A Missed Approach In the Active Flight Plan.................................................... 44
Temperature Compensated Altitude................................................................................... 45
Hazard Avoidance....................................................................................................................... 47
Customizing the Hazard Displays on the Navigation Map............................................. 47
SiriusXM Weather (Subscription Optional)........................................................................ 47
Airborne Color Weather Radar............................................................................................. 50
Traffic Systems......................................................................................................................... 54
Terrain Awareness & Warning System (TAWS-B).............................................................. 58
ii
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Table of Contents
Additional Features................................................................................................................... 61
Synthetic Vision (Optional).................................................................................................... 61
Terminal Procedure Charts.................................................................................................... 63
Airport Directory..................................................................................................................... 65
SiriusXM® Radio Entertainment (Subscription Optional)............................................... 65
Abnormal Operation................................................................................................................. 69
Reversionary Mode................................................................................................................. 69
Abnormal COM Operation..................................................................................................... 69
Audio Panel Fail-safe Operation.......................................................................................... 69
Hazard Displays with Loss of GPS Position........................................................................ 70
Unusual Attitudes.................................................................................................................... 70
Dead Reckoning....................................................................................................................... 71
Annunciations & Alerts............................................................................................................ 73
CAS Messages........................................................................................................................... 73
Comparator Annunciations.................................................................................................... 76
Reversionary Sensor Annunciations.................................................................................... 76
TAWS-B Alerts........................................................................................................................... 77
TCAS II Alerts and Annunciations......................................................................................... 79
Aural Alerts............................................................................................................................... 81
Flight Plan Import/Export Messages................................................................................... 81
G1000 System Message Advisories...................................................................................... 82
Appendix........................................................................................................................................ 101
PFD Softkey Map................................................................................................................... 101
MFD Softkey Map.................................................................................................................. 110
Loading Updated Databases............................................................................................... 112
Index............................................................................................................................................Index-1
190-00600-05 Rev. C
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
190-00600-05 Rev. C
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 (29.92 IN HG)
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.
190-00600-05 Rev. C
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 a CRS Knob to select the desired course to/from the waypoint. Press
the CRS Knob to synchronize the Selected Course with the bearing to the
next waypoint.
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
190-00600-05 Rev. C
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 MINIMUM DESCENT ALTITUDE/DECISION HEIGHT
Flight
Planning
1) Press the TMR/REF Softkey.
Turn the large FMS Knob to highlight the Minimums field.
3)
Turn the small FMS Knob to select BARO, TEMP COMP, or RAD ALT
(optional). OFF is selected by default. Press the ENT Key or turn the large
FMS Knob to highlight the next field.
4)
Use the small FMS Knob to enter the desired altitude. When BARO and
TEMP COMP are selected, values from zero to 16,000 feet may be entered.
When RAD ALT is selected, values from zero to 2,500 feet may be entered.
5)
If TEMP COMP was selected, press the ENT Key or turn the large FMS
Knob to highlight the next field and then enter the destination airport
temperature (-59˚C to 59˚C). The temperature compensated altitude
minimum is displayed below the previously enter minimum altitude value.
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
Procedures
2)
Additional
Features
Abnormal
Operation
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.
Appendix
Press the PFD Softkey.
Annun/
Alerts
1)
Hazard
Avoidance
DISPLAYING WIND DATA
Index
190-00600-05 Rev. C
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
190-00600-05 Rev. C
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
190-00600-05 Rev. C
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
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 (amber) – 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
190-00600-05 Rev. C
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 (OPTIONAL)
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.
190-00600-05 Rev. C
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
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
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, or ALT).
Hazard
Avoidance
Procedures
With TCAS II Option
1)
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).
SELECTING A COM RADIO
Transmit/Receive
Abnormal
Operation
Additional
Features
1)
Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (if installed) on the
audio panel.
Annun/
Alerts
Receive Only
Index
Appendix
Press the COM1, COM2, or COM3 Key (if installed) on the audio panel.
8
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
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)
Flight
Planning
Annun/
Alerts
Appendix
Index
9
Abnormal
Operation
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Additional
Features
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 selected on both audio panels. PA
messages are one way from the flight deck to the passengers.
Hazard
Avoidance
Passenger Address (PA) System
Procedures
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).
190-00600-05 Rev. C
GPS Nav
INTERCOM SYSTEM (ICS) ISOLATION
CLEARANCE RECORDER AND PLAYER
GMA 1347D
NOTE: Only the audio for the selected COM MIC Key is recorded. Audio is
not recorded for COM3 MIC.
EICAS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
AFCS
Nav/Com/
XPDR/Audio
Record
Press the REC Key to begin recording.
2)
Press the REC Key again to stop recording.
Flight
Planning
GPS Nav
Play
1)
Press the PLAY Key once to play the latest recorded memory block.
2)
Press the PLAY Key once while playing to stop.
3)
Press the PLAY Key twice quickly while playing to begin playing the
previously recorded block. Each subsequent two presses will skip back to
the previously recorded block.
Procedures
GMA 1347D-20
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.
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
1)
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.
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.
10
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
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
11
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.
190-00600-05 Rev. C
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 SBAS 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
12
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
AFCS
Description
Holds current aircraft roll attitude
or rolls wings level, depending on
commanded bank angle
Roll Hold
Heading Select
Captures and tracks Selected Heading
GPS
Captures and tracks selected navigation
source (GPS, VOR, LOC)
NAV
Key
VOR
LOC
BC Key
BC
Hazard
Avoidance
Captures and tracks a localizer signal
for backcourse approaches
Procedures
GPS
Captures and tracks selected navigation
APR Key
source (GPS, VOR, LOC)
Additional
Features
VAPP
Abnormal
Operation
LOC
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
Annun/
Alerts
Go Around
HDG
Flight
Planning
Takeoff
*
GPS Nav
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)
BANK
Key
HDG
Key
ROL
AFCS
Limits maximum commanded roll angle
(default)
Nav/Com/
XPDR/Audio
Low Bank
Control Annunciation
EICAS
Lateral Mode
Flight
Instruments
LATERAL MODES
GA
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.
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
13
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
14
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
GPS Navigation
Flight
Instruments
GPS NAVIGATION
DIRECT-TO NAVIGATION
2)
3)
7)
10)
11)
Direct-to Navigation using the PFD
2)
5)
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
15
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 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
Appendix
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)
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the destination waypoint for the
desired leg.
Or:
Index
Use the Joystick to place the Quick Select Box on the destination waypoint
for the desired leg.
16
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
GPS Navigation
‘Activate Leg’, and press the ENT Key. A confirmation window is displayed
with ‘ACTIVATE’ highlighted.
5)
Press the FMS Knob to remove the flashing cursor, if required.
Nav/Com/
XPDR/Audio
Press the ENT Key to activate the flight plan leg. To cancel, press the CLR
Key, or highlight ‘CANCEL’ and press the ENT Key.
EICAS
4)
Flight
Instruments
3) Press the ACT LEG Softkey (MFD only); or press the MENU Key, highlight
STOP NAVIGATING A FLIGHT PLAN
Press the FPL Key to display the Active Flight Plan Page.
2)
Press the MENU Key to display the Page Menu Window.
3)
Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT
Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan.
This will not delete the stored flight plan, only the active flight plan.
AFCS
1)
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
17
VERTICAL NAVIGATION (VNAV)
The navigation database only contains altitudes for procedures that call for “Cross
at” altitudes. If the procedure states “Expect to cross at,” the altitude is not in the
database. In this case the altitude may be entered manually.
NOTE: Temperature Compensated (TEMP COMP) altitudes are depicted as
slanted text.
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
GPS Navigation
GPS Nav
Large White
Text
Flight
Planning
Insertion
Point
Indicator
Large Light
Blue Text
Small Light
Blue Text
Procedures
Quick
Select
Box
Small Light
Blue Subdued
Text
Additional
Features
Hazard
Avoidance
Small White Text
with Altitude
Restriction Bar
Cross AT or ABOVE 5,000 ft
Abnormal
Operation
Cross AT 2,300 ft
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.
Index
Appendix
Annun/
Alerts
Cross AT or BELOW 3,000 ft
18
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
GPS Navigation
Light Blue
Subdued Text
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.
Flight
Planning
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.
GPS Nav
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.
AFCS
Large
Text
Nav/Com/
XPDR/Audio
Light Blue Text
EICAS
White Text
Flight
Instruments
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.
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
NOTE: Making course changes greater than 90° during a descent with vertical
guidance may cause excessive and rapid movement of the vertical deviation
indicator, and SVT Pathways.
Appendix
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
19
The system updates vertical path guidance continuously using ground speed and
the calculated distance to the Bottom of Descent (BOD). Due to turn anticipation
guidance (turn-smoothing), distance to the BOD can be affected by course changes
greater than approximately 5 degrees. Ground speed can be affected by factors such as
shifts in wind direction, aircraft power management, pitch angle, and course changes.
Abrupt and/or substantial changes to either the distance to the BOD, ground speed, or
both can cause similarly abrupt/substantial changes in vertical path guidance.
Because of turn-smoothing, changes to both distance to the BOD and ground speed
tend to be more extreme when the BOD is also a waypoint that marks a large course
change. These speed and distance changes will be accounted for in the computed
required vertical path and reflected in the vertical guidance indications.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
GPS Navigation
20
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
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)
190-00600-05 Rev. C
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
190-00600-05 Rev. C
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.
2)
Press the ENT Key.
3)
Press the FMS Knob to remove the flashing cursor.
Annun/
Alerts
With the VRP Information Page displayed, enter the identifier or the name
of the VRP in the VRP Box.
Abnormal
Operation
1)
2)
Press the ENT Key or turn either FMS Knob to select an identifier in the
Nearest VRP Box.
3)
Press the FMS Knob to remove the flashing cursor.
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Index
With the Nearest VRP Page displayed, press the FMS Knob.
Appendix
Or:
1)
Additional
Features
SELECTING A VRP (VISUAL REPORTING POINT)
Hazard
Avoidance
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)
23
CREATE A USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE
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’.
7)
With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
8)
Turn the small FMS Knob to select LAT/LON (latitude and longitude).
9)
Press the ENT Key.
CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
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.
1)
Turn the large FMS Knob on the MFD Control Unit to select the ‘WPT’ page
group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Select the NEW Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
6)
The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
24
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Flight Planning
8)
Turn the small FMS Knob to select RAD/RAD (radial/radial).
9)
Press the ENT Key.
Nav/Com/
XPDR/Audio
With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
EICAS
7)
Flight
Instruments
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.
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:
GPS Nav
b) Turn the large FMS Knob to select the desired waypoint.
AFCS
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
c) Press the ENT Key.
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Flight
Planning
Or:
Procedures
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
Hazard
Avoidance
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Abnormal
Operation
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
Additional
Features
Or:
c) Turn the large FMS Knob to select the desired waypoint.
Annun/
Alerts
d) Press the ENT Key.
Or:
Appendix
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.
Index
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
25
Flight Planning
Flight
Instruments
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
12) Press the ENT Key.
EICAS
13) Repeat step 10 to enter the next waypoint name.
15) Press the ENT Key.
16) Press the FMS Knob to remove the flashing cursor.
CREATE A 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.
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
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.
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Appendix
Annun/
Alerts
Abnormal
Operation
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.
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:
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
26
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Flight Planning
Flight
Instruments
b) Turn the large FMS Knob to select the desired waypoint.
c) Press the ENT Key.
Or:
Nav/Com/
XPDR/Audio
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
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:
Flight
Planning
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
GPS Nav
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.
Procedures
d) Press the ENT Key.
Or:
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
Additional
Features
c) Turn the large FMS Knob to select the desired waypoint.
Hazard
Avoidance
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
d) Press the ENT Key.
12) Press the ENT Key.
Annun/
Alerts
13) The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.
Abnormal
Operation
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
14) Press the ENT Key.
Appendix
15) Press the FMS Knob to remove the flashing cursor.
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
27
CREATE A USER WAYPOINT USING THE MAP POINTER
1)
Press the Joystick to activate the panning function and pan to the map
location of the desired user waypoint.
2)
Press the ENT Key. The User Waypoint Information Page is displayed with
the captured position.
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Flight Planning
3)
Enter a user waypoint name (up to six characters).
4)
Press the ENT Key to accept the selected name.
5)
If desired, define the type and location (i.e., LAT/LON, RAD/RAD or RAD/
DIS) of the waypoint.
6)
Press the ENT Key to accept the new waypoint.
7)
If desired, change the storage method of the waypoint to “TEMPORARY” or
“NORMAL” by moving the cursor to “TEMPORARY” and selecting the ENT
Key to check or uncheck the box.
8)
Press the FMS Knob to remove the flashing cursor.
9)
Press the GO BACK Softkey to return to the map page.
DELETE A USER WAYPOINT
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
NOTE: If the pointer has highlighted a map database feature, one of three
things happens upon pressing the ENT Key: 1) information about the selected
feature is displayed instead of initiating a new waypoint, 2) a menu pops up
allowing a choice between ‘Review Airspaces’ or ‘Create User Waypoint’, or
3) a new waypoint is initiated with the default name being the selected map
item.
28
1)
Turn the large FMS Knob to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’
field.
5)
Turn the small FMS Knob to highlight the desired waypoint.
6)
Select the DELETE Softkey.
7)
The message ‘Would you like to delete the user waypoint?’ is displayed. With
‘YES’ highlighted, press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Flight Planning
NOTE: When creating a flight plan in the Active Flight Plan Window, the first
leg is activated automatically after it is created.
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
29
Flight
Planning
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
GPS Nav
190-00600-05 Rev. C
AFCS
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.
Nav/Com/
XPDR/Audio
Creating an active flight plan using the cursor:
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.
EICAS
Creating an active flight plan using the Quick Select Box (MFD only):
1) Press the FPL Key.
2) Begin entering the identifier of the departure waypoint using the MFD
Control Unit’s alphanumeric keys. The Waypoint Information Window is
displayed as the identifier is entered.
3) Press the ENT Key. The Quick Select Box moves to the next empty field.
4) Repeat steps 2 and 3 to enter each additional flight plan waypoint. The
active flight plan is modified as each waypoint is entered.
Flight
Instruments
CREATE A FLIGHT PLAN
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.
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Flight Planning
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
IMPORT A FLIGHT PLAN FROM AN SD CARD
1)
Insert the SD card containing the flight plan in the top card slot on the
MFD.
2)
Press the FPL Key on the MFD Control Unit to display the Active Flight Plan
Page on the MFD.
3)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
4)
Press the FMS Knob to activate the cursor.
5)
Turn either FMS Knob to highlight an empty or existing flight plan.
6)
Select the IMPORT Softkey.
Additional
Features
If an empty flight plan is selected, a list of the available flight plans on the
SD card will be displayed.
Or:
7)
Turn the small FMS Knob to highlight the desired flight plan for importing.
8)
Press the ENT Key.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
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.
30
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Flight Planning
Flight
Instruments
INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN
Insert waypoint using the Quick Select Box:
Press the FPL Key on the MFD Control Unit to display the active flight plan.
2)
Use the Joystick to move the Insertion Point Indicator to the location for
the new waypoint in the flight plan list.
3)
Begin entering the identifier of the new waypoint using the MFD Control
Unit’s alphanumeric keys. The Waypoint Information Window is displayed
as the identifier is entered.
4)
Press the ENT Key.
EICAS
1)
Nav/Com/
XPDR/Audio
AFCS
Insert waypoint using the cursor:
2)
If necessary, press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to move cursor and Insertion Point Indicator
(small light blue triangle) to the desired insertion point in the flight plan.
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:
Flight
Planning
Press the FPL Key on the MFD Control Unit to display the active flight plan.
Procedures
Hazard
Avoidance
a) Enter the user waypoint identifier, facility, or city.
b) Press the ENT Key.
b) Turn the small FMS Knob to the right to display the ‘NRST’ airport
waypoints to the aircraft’s current position.
Annun/
Alerts
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
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 ‘RECENT’
waypoints.
Appendix
Or:
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Abnormal
Operation
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Additional
Features
Or:
190-00600-05 Rev. C
GPS Nav
1)
31
Flight Planning
d) Press the ENT Key.
e) Press the ENT Key again to “accept” the waypoint.
ENTER AN AIRWAY IN A FLIGHT PLAN
Enter airway using the Quick Select Box:
1)
Press the FPL Key on the MFD Control Unit to display the active flight plan.
2)
Use the Joystick to move the Insertion Point Indicator to the desired entry
point in the flight plan list.
3)
Begin entering the identifier of the airway entry waypoint using the MFD
Control Unit’s alphanumeric keys. The Waypoint Information Window is
displayed as the identifier is entered.
4)
Press the ENT Key. The Quick Select Box and Insertion Point Indicator are
now located following the newly entered waypoint.
5)
Press the MENU Key and select “Load Airway” (required on the PFD). The
Select Airway Page is displayed. The “Load Airway” menu item is available
only when an acceptable airway entry waypoint has been entered in step 3
(the waypoint ahead of the Insertion Point Indicator).
6)
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.
7)
Turn the FMS Knob to select the desired airway exit point from the list, and
press the ENT Key. ‘LOAD?’ is highlighted.
8)
Press the ENT Key. The system returns to editing the flight plan with the
new airway inserted.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
c) Turn the large FMS Knob to select the desired waypoint.
Index
Appendix
Annun/
Alerts
Enter airway using the cursor:
1) Press the FPL Key on the MFD Control Unit.
2) Press the FMS Knob to activate the cursor (not required on the PFD).
3) Turn the large FMS Knob to move the cursor and Insertion Point Indicator
(small light blue triangle) to the desired waypoint insertion point in the
flight plan. If this waypoint is not a valid airway entry point, a valid entry
point should be entered at this time.
32
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Flight Planning
Turn the small FMS Knob one click clockwise and press the LD AIRWY
Softkey, or press the MENU Key and select “Load Airway” (required on
the PFD). The Select Airway Page is displayed. The LD AIRWY Softkey
or the “Load Airway” menu item is available only when an acceptable
airway entry waypoint has been chosen (the waypoint ahead of the cursor
position).
5)
Turn the FMS Knob to select the desired airway from the list, and press the
ENT Key. Low altitude airways are shown first in the list, followed by “all”
altitude airways, and then high altitude airways.
Nav/Com/
XPDR/Audio
6)
Turn the FMS Knob to select the desired airway exit point from the list, and
press the ENT Key. ‘LOAD?’ is highlighted.
AFCS
7)
Press the ENT Key. The system returns to editing the flight plan with the
new airway inserted only when an acceptable airway entry waypoint
has been entered in step 3 (the waypoint ahead of the Insertion Point
Indicator).
8)
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.
9)
Turn the FMS Knob to select the desired airway exit point from the list, and
press the ENT Key. ‘LOAD?’ is highlighted.
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Appendix
Index
33
Annun/
Alerts
Creating a User-Defined Hold at an Active Flight Plan Waypoint:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
2) Use the Joystick to move the Quick Select Box around the waypoint for
the hold.
3) Press the MENU Key, highlight ‘Hold At Waypoint’, and press the ENT Key.
The HOLD AT window appears with the course field highlighted.
4) Use the FMS Knobs to edit the entry course, and press the ENT Key.
Abnormal
Operation
A holding pattern can be defined at any active flight plan waypoint, or at the aircraft
present position.
Additional
Features
USER-DEFINED HOLDING PATTERNS
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
EICAS
10) Press the ENT Key. The system returns to editing the flight plan with the
new airway inserted.
190-00600-05 Rev. C
Flight
Instruments
4)
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Flight Planning
5)
Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course
direction, and press the ENT Key.
6)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
7)
Use the FMS Knobs to edit the length, and press the ENT Key.
8)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
9)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key. (Note: Using the keypad to enter a two digit value
for hours requires using the FMS Knob to access the leftmost hours digit.)
GPS Nav
10) Press the ENT Key while ‘LOAD?’ is highlighted to add the hold into the
flight plan.
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
Creating a User-Defined Hold at the Aircraft Present Position:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
2) Press the MENU Key, highlight ‘Hold At Present Position’, and press the
ENT Key. The HOLD AT window appears with the Length mode highlighted.
3) If desired, use the FMS Knobs to edit the entry course, and press the ENT
Key.
4) Us the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course
direction, and press the ENT Key.
5) Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
6) Use the FMS Knobs to edit the length, and press the ENT Key.
7) Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
8) Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key. (Note: Using the keypad to enter a two digit value
for hours requires using the FMS Knob to access the leftmost hours digit.)
9) Press the ENT Key while ‘ACTIVATE?’ is highlighted to immediately activate
the hold.
Index
Creating a User-Defined Hold at a Direct-To Waypoint:
1) Press a Direct-to Key and set up the direct-to waypoint as desired, but
select ‘HOLD?’ instead of ‘ACTIVATE?’ when finished (MFD or PFD).
34
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Flight Planning
Use the FMS Knobs to edit the entry course, and press the ENT Key.
3)
Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course
direction, and press the ENT Key.
4)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
5)
Use the FMS Knobs to edit the length, and press the ENT Key.
6)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
7)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key. (Note: Using the keypad to enter a two digit value
for hours requires using the FMS Knob to access the leftmost hours digit.)
8)
Press the ENT Key while ‘ACTIVATE?’ is highlighted to activate the Direct To
with the user-defined hold defined at the Direct To waypoint. (If the directto waypoint is part of the active flight plan, the HOLD is inserted into the
active flight plan. If the direct-to waypoint is not part of the active flight
plan, an off-route direct-to hold is created.)
Flight
Instruments
2)
EICAS
Nav/Com/
XPDR/Audio
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Removing a User-Defined Hold (Created at an Active Flight Plan
Waypoint):
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
2) Use the Joystick to move the Quick Select Box around the ‘HOLD’
waypoint.
AFCS
Removing a User-Defined Hold (Created at the Aircraft Present
Position):
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
2) Use the Joystick to move the Quick Select Box around PPOS-H waypoint.
3) Press the CLR Key. A “Remove Holding Pattern?” confirmation window is
displayed.
4) Select ‘OK’ and press the ENT Key. The holding pattern is removed from
the active flight plan. Select ‘CANCEL’ and press the ENT Key to cancel the
removal of the holding pattern.
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
35
3)
Press the CLR Key. A ‘Remove Holding Pattern?’ confirmation window is
displayed.
4)
Select ‘OK’ and press the ENT Key. The holding pattern is removed from
the active flight plan. Select ‘CANCEL’ and press the ENT Key to cancel the
removal of the holding pattern.
INVERT AN ACTIVE FLIGHT PLAN
1)
Press the FPL Key to display the active flight plan.
2)
Press the MENU Key to display the Page Menu.
3)
Turn the large FMS Knob to highlight ‘Invert Flight Plan’.
4)
Press the ENT Key. The original flight plan remains intact in its flight plan
catalog storage location.
5)
With ‘OK’ highlighted, press the ENT Key to invert the flight plan.
REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT
PLAN
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Flight Planning
Additional
Features
Hazard
Avoidance
Remove using the Quick Select Box (active flight plan only):
1)
Press the FPL Key on the MFD Control Unit to display the active flight plan.
2)
Use the Joystick to move the Quick Select Box around the desired
procedure name or airway in the flight plan.
3)
Press the CLR Key to display a confirmation window.
4)
With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Remove using the cursor:
1) Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Or, for a stored flight plan:
a) Press the FPL Key on the MFD Control Unit and turn the small FMS
Knob to select the Flight Plan Catalog Page.
b) Press the FMS Knob to activate the cursor.
c) Turn the large FMS Knob to highlight the desired flight plan.
d) Press the EDIT Softkey.
36
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Flight Planning
Press the CLR Key to display a confirmation window.
4)
With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.
STORE A FLIGHT PLAN
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.
GPS Nav
After creating a flight plan on either the PFD or MFD, it may be saved by
pressing the MENU Key.
EDIT A STORED FLIGHT PLAN
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.
Procedures
Press the FPL Key for the MFD and turn the small FMS Knob to display the
Flight Plan Catalog Page.
Hazard
Avoidance
Additional
Features
DELETE A WAYPOINT FROM THE FLIGHT PLAN
Press the FPL Key on the MFD Control Unit to display the active flight plan.
2)
Use the Joystick to move the Quick Select Box around the desired
waypoint to be deleted.
3)
Press the CLR Key to display a confirmation window.
4)
With ‘OK’ highlighted, press the ENT Key to remove the selected waypoint.
Annun/
Alerts
1)
Abnormal
Operation
Delete using the Quick Select Box (active flight plan only):
Index
37
Appendix
Delete using the cursor:
1) Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Flight
Planning
1)
190-00600-05 Rev. C
AFCS
1)
Nav/Com/
XPDR/Audio
3)
EICAS
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.
Flight
Instruments
2)
Flight Planning
Flight
Instruments
Or, for a stored flight plan:
a) Press the FPL Key on the MFD Control Unit and turn the small FMS
Knob to select the Flight Plan Catalog Page.
EICAS
b) Press the FMS Knob to activate the cursor.
c) Turn the large FMS Knob to highlight the desired flight plan.
AFCS
Nav/Com/
XPDR/Audio
d) Press the EDIT Softkey.
2)
Turn the large FMS Knob to highlight the waypoint to be deleted.
3)
4)
Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation window.
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.
When all changes have been made, press the FMS Knob to remove the cursor.
GPS Nav
5)
1)
Press the FPL Key on the 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.
Press the FPL Key on the 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.
Annun/
Alerts
1)
Appendix
COPY A FLIGHT PLAN
Index
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
INVERT AND ACTIVATE A STORED FLIGHT PLAN
38
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Flight Planning
Press the FPL Key on the 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.
AFCS
EICAS
1)
Nav/Com/
XPDR/Audio
Flight
Instruments
DELETE A FLIGHT PLAN
GPS Nav
GRAPHICAL FLIGHT PLAN CREATION
Press the FPL Key to display the Active Flight Plan Page on the MFD.
2)
Use the Joystick to move the Insertion Point Indicator to the desired
waypoint entry point in the flight plan list.
3)
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.
4)
Select the LD WPT Softkey. The selected waypoint is inserted at the selected
point. The default user waypoint naming is USR000, USR001, USR002, and
so on.
5)
To change the user waypoint name, follow the procedure for modifying a user
waypoint.
Flight
Planning
1)
Additional
Features
Abnormal
Operation
Press the FPL Key on the Control Unit to display the Active Flight Plan Page
on the MFD.
3)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
4)
Press the FMS Knob to activate the cursor.
5)
Turn 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.
Appendix
2)
Annun/
Alerts
Insert the SD card into the top card slot on the MFD.
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Hazard
Avoidance
1)
190-00600-05 Rev. C
Procedures
EXPORT A FLIGHT PLAN TO AN SD CARD
39
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
Blank Page
40
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
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’.
Hazard
Avoidance
Activate leg using the Quick Select Box:
2)
Use the Joystick to move the Quick Select Box to the TO waypoint of the
desired leg within the departure.
3)
Press the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
4)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Appendix
Index
41
Annun/
Alerts
Activate leg using the cursor:
1) Press the FPL Key on the 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.
Abnormal
Operation
Press the FPL Key on the MFD Control Unit to display the active flight plan.
Additional
Features
1)
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Procedures
ACTIVATE A DEPARTURE LEG
190-00600-05 Rev. C
GPS Nav
2)
AFCS
Press the PROC Key.
Nav/Com/
XPDR/Audio
1)
Press the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.
AFCS
GPS Nav
Flight
Planning
Procedures
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’.
3)
Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list
of available arrivals.
4)
Turn the large FMS Knob to highlight the desired arrival.
5)
Press the ENT Key. A list of transitions is displayed for the selected arrival.
6)
Turn either FMS Knob to select the desired transition.
7)
Press the ENT Key. A list of runways 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.
11) The arrival becomes part of the active flight plan.
ACTIVATE AN ARRIVAL LEG
Activate Arrival using the Quick Select Box:
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
4)
LOAD AN ARRIVAL PROCEDURE
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Procedures
1)
Press the FPL Key on the MFD Control Unit to display the active flight plan.
2)
Use the Joystick to move the Quick Select Box to the TO waypoint of the
desired leg within the arrival.
3)
Press the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
4)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Index
Appendix
Activate Arrival using the cursor:
1) Press the FPL Key on the MFD Control Unit to display the active flight plan.
2) Press the FMS Knob to activate the cursor.
42
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Procedures
4)
Press the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘SELECT APPROACH’.
3)
Press the ENT Key. A list of available approaches for the destination airport
is displayed.
4)
Turn either FMS Knob to highlight the desired approach.
5)
Press the ENT Key. A list of available transitions for the selected approach
procedure is now displayed.
6)
Turn either FMS Knob to select the desired transition. The “Vectors”
option assumes vectors will be received to the final course segment of
the approach and will provide navigation guidance relative to the final
approach course.
7)
Press the ENT Key. The cursor moves to the MINIMUMS field.
8)
If desired, the DA/MDA for the selected approach procedure may be
entered and displayed on the PFD. Turn the small FMS Knob in the
direction of the green arrow to change the display from OFF to BARO, TEMP
COMP, 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.
GPS Nav
1)
AFCS
NOTE: If certain GPS parameters (SBAS, RAIM, etc.) are not available, some
published approach procedures for the desired airport may not be displayed
in the list of available approaches.
Nav/Com/
XPDR/Audio
LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE
EICAS
Turn the large FMS Knob to highlight the TO waypoint of the desired leg
within the arrival.
Flight
Instruments
3)
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
10) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’
highlighted.
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
43
Procedures
Flight
Instruments
11) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.
12) Press the ENT Key.
ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.
3)
Press the ENT Key.
Procedures
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’.
3)
Press the ENT Key.
4)
The final approach course becomes the active leg.
ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN
Abnormal
Operation
Additional
Features
Hazard
Avoidance
1)
ACTIVATE A VECTOR TO FINAL APPROACH FIX
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
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.
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
Press the go-around button.
44
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Procedures
When temperature compensated altitude is enabled for the loaded approach, the
altitudes associated with the approach waypoints are displayed in slanted text.
Flight
Instruments
TEMPERATURE COMPENSATED ALTITUDE
EICAS
Nav/Com/
XPDR/Audio
AFCS
Altitudes Displayed With
Temperature Compensation
GPS Nav
Altitudes Displayed Without
Temperature Compensation
Procedures
Use the small FMS Knob to select the temperature at the <airport>. The
5)
Press the ENT Key. ‘ACTIVATE COMPENSATION?’ is highlighted.
6)
Press the ENT Key. The compensated altitudes for the approach are
Additional
Features
compensated altitude is computed as the temperature is selected.
Abnormal
Operation
shown in the flight plan.
Annun/
Alerts
Disabling temperature compensated altitude:
1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is
displayed.
2) Turn the FMS Knob to highlight ‘Temperature Compensation’.
3) Press the ENT Key. The TEMPERATURE COMPENSATION Window is
displayed.
4) Press the ENT Key. ‘CANCEL COMPENSATION?’ is highlighted.
Appendix
Press the ENT Key. The temperature compensated altitude at the FAF
is cancelled.
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
45
Index
5)
Hazard
Avoidance
4)
Flight
Planning
Enabling temperature compensated altitude:
1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is
displayed.
2) Turn the FMS Knob to highlight ‘Temperature Compensation’.
3) Press the ENT Key. The TEMPERATURE COMPENSATION Window is
displayed.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Procedures
Blank Page
46
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Hazard Avoidance
Flight
Instruments
HAZARD AVOIDANCE
EICAS
WARNING: Do not use the indicated data link weather product age to
determine the age of the weather information shown by the data link weather
product. Due to time delays inherent in gathering and processing weather
data for data link transmission, the weather information shown by the data
link weather product may be older than the indicated weather product age.
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.
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.
Flight
Planning
1)
Additional
Features
Annun/
Alerts
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.
Abnormal
Operation
2)
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).
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Index
Turn the large FMS Knob to select the WPT Page Group.
Appendix
1)
Hazard
Avoidance
Displaying SiriusXM Weather on the Navigation Map Page
Select the MAP Softkey.
Procedures
SIRIUSXM WEATHER (SUBSCRIPTION OPTIONAL)
1)
GPS Nav
CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP
Nav/Com/
XPDR/Audio
WARNING: Do not use data link weather information for maneuvering in,
near or around areas of hazardous weather. Information contained within
data link weather products may not accurately depict current weather conditions.
47
Hazard Avoidance
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Data Link Page.
3)
Select the available softkeys to select the desired XM weather product.
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
Flight
Instruments
Displaying Weather on the Weather Data Link Page
GPS Nav
AFCS
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.
Procedures
Flight
Planning
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.
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Enabling/disabling winds aloft data display in Profile View:
1)
Select the Navigation Map Page.
2)
Press the MENU Key.
3)
With Map Setup highlighted, press the ENT Key
4)
Turn the small FMS Knob to select the Profile Group and press the ENT Key
5)
Turn the large FMS Knob to select ‘Profile Winds’.
6)
7)
Turn the small FMS Knob to select ‘On’ or ‘Off’.
Press the FMS Knob or CLR Key to return to the Navigation Map Page with
the changed settings.
Index
Appendix
NOTE: NEXRAD data cannot be displayed at the same time as terrain, echo
tops, turbulence, or icing data is displayed.
48
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Hazard Avoidance
Wx Product
Status Icons
Flight
Instruments
SiriusXM Weather Products and Symbols
Description
EICAS
NEXRAD - Available for the US and Canada. The age of the displayed data
for each is shown at the right.
Nav/Com/
XPDR/Audio
ECHO TOP - The age of the displayed data is shown at the right. Not
displayed when CLOUD TOP is displayed.
AFCS
CLOUD TOP - The age of the displayed data is shown at the right. Not
displayed when ECHO TOP is displayed.
GPS Nav
XM LIGHTNING - The age of the displayed data is shown at the right.
CELL MOVEMENT - The age of the displayed data is shown at the right.
Abnormal
Operation
Annun/
Alerts
WINDS ALOFT - Available for the US and Canada. The age of the displayed
data for each is shown at the right. The altitude selection is shown at the
bottom.
Additional
Features
FREEZING LEVEL - The age of the displayed data is shown at the right.
Hazard
Avoidance
SURFACE ANALYSIS with CITY FORECAST - The upper symbol depicts
Surface Analysis. The lower symbol depicts City Forecast. The age of the
displayed data for each is shown at the right. The selected forecast period is
shown at the bottom.
Procedures
METAR - Available for the US and Canada. The age of the displayed data for
each is shown at the right.
Flight
Planning
SIGMET & AIRMET - The age of the displayed data for each is shown at the
right.
COUNTY WARNING - The age of the displayed data is shown at the right.
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Index
AIREP - The age of the displayed data is shown at the right.
Appendix
CYCLONE WARNING - The age of the displayed data is shown at the right.
49
Hazard Avoidance
Flight
Instruments
Wx Product
Status Icons
Description
EICAS
PIREP - The age of the displayed data is shown at the right. Urgent Pireps
are displayed in yellow.
Nav/Com/
XPDR/Audio
TURBULENCE - The age of the displayed data is shown at the right. The
altitude selection is shown at the bottom.
AFCS
ICING POTENTIAL - The age of the displayed data is shown at the right.
The altitude selection is shown at the bottom.
TFR- Depicted as an area outlined in yellow
AIRBORNE COLOR WEATHER RADAR
WARNING: Begin transmitting only when it is safe to do so. If it is desired to
transmit while the aircraft is on the ground, no personnel or objects should
be within 11 feet of the antenna.
Procedures
Flight
Planning
GPS Nav
No Status Icon
Additional
Features
Hazard
Avoidance
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.
Weather Mode Color
Annun/
Alerts
Abnormal
Operation
Black
Green
Yellow
Red
Magenta
Approximate
Precipitation Rate (in/hr.)
< 23 dBZ
< .01.
23 dBZ to < 32 dBZ
.01 - 0.1.
32 dBZ to < 41 dBZ
0.1 - 0.5
41 dBZ to < 50 dBZ
0.5 - 2
50 dBZ and greater
>2
Intensity
Index
Appendix
Precipitation Intensity Levels
50
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Hazard Avoidance
Flight
Instruments
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.
EICAS
1)
Nav/Com/
XPDR/Audio
AFCS
Or:
Turn the Joystick to select the desired range.
6)
If desired, select the VERTICAL Softkey for vertical scanning.
Flight
Planning
5)
GPS Nav
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.
Displaying a Weather Radar Overlay on the Navigation Map
2)
Press the MAP Softkey.
3)
Press the WX RADAR Softkey.
Hazard
Avoidance
Select the Navigation Map Page.
Procedures
1)
Adjusting Antenna Tilt
Additional
Features
Abnormal
Operation
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.
Appendix
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
51
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.
52
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Hazard Avoidance
Black
Yellow
Magenta
AFCS
Blue
0 dB
> 0 dB to < 9 dB
9 dB to < 18 dB
18 dB to < 27 dB
27 dB and greater
Nav/Com/
XPDR/Audio
Light blue
Intensity
EICAS
Ground Map
Mode Color
Flight
Instruments
Ground Mapping
Ground Target Return Intensity Levels
3)
Select the BACK Softkey.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to place the cursor in the TILT field.
6)
Adjust the antenna tilt angle by turning the small FMS Knob to display
ground returns at the desired distance.
7)
Press the FMS Knob to remove the cursor.
Hazard
Avoidance
Select the GROUND Softkey to place the radar in Ground Map Mode.
Procedures
2)
Flight
Planning
Select the MODE Softkey.
GPS Nav
1)
Sector Scan
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.
Appendix
Press the FMS Knob to display the cursor.
Annun/
Alerts
2)
Abnormal
Operation
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.
Additional
Features
1)
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
53
Hazard Avoidance
1)
To activate or deactivate the antenna stabilization, select the MODE
Softkey.
2)
Select the STAB ON Softkey to activate antenna stabilization or select
the STAB OFF Softkey to deactivate. The current stabilization condition is
shown in the upper right of the weather radar display.
Weather Attenuated Color Highlight (WATCH®)
To activate or deactivate the WATCH® feature, select the WATCH Softkey. This
feature is only available in the Horizontal Scan Mode.
Weather Alert
To activate or deactivate Weather Alert, select the WX ALRT Softkey. Activating
and deactivating will also enable or inhibit the alert on the PFD.
Automatic Standby
When the weather radar system is in the Weather or Ground Map Mode, upon
landing the system will automatically switch to Standby Mode.
TRAFFIC SYSTEMS
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Antenna Stabilization
Additional
Features
WARNING: Traffic information shown on system displays is provided as an
aid in visually acquiring traffic. Traffic avoidance maneuvers are based upon
TCAS II Resolution Advisories (if installed), ATC guidance, or positive visual
acquisition of conflicting traffic.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
• 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.
54
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Hazard Avoidance
Description
Flight
Instruments
Traffic Symbol
Non-Threat Traffic
(intruder is beyond 5 nm and greater than 1200’ vertical separation)
EICAS
Proximity Advisory (PA) (TAS and TCAS II only)
(intruder is within 5 nm and less than 1200’ vertical separation)
Nav/Com/
XPDR/Audio
Traffic Advisory (TA)
(Potential collision area is within 20 to 48 seconds)
Traffic Advisory Off Scale
AFCS
GPS Nav
Resolution Advisory (RA) (TCAS II only)
(Potential collision area is within 15 to 35 seconds)
Resolution Advisory Off Scale (TCAS II only)
Flight
Planning
Traffic Symbol Description
Displaying Traffic on the Traffic Map Page
Turn the small FMS Knob to select the Traffic Map Page.
3)
Select the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
4)
Select the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
5)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Appendix
2)
Annun/
Alerts
Turn the large FMS Knob to select the Map Page Group.
Abnormal
Operation
1)
Additional
Features
NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.
Hazard
Avoidance
NOTE: If the G1000 is configured to use an optional Traffic Advisory System
(TAS), TIS is not available for use.
Procedures
Traffic Information Service (TIS)
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
55
Hazard Avoidance
EICAS
Flight
Instruments
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.
Nav/Com/
XPDR/Audio
Traffic Advisory System (TAS) (Optional)
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.
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Displaying Traffic on the Traffic Map Page
1)
With the Traffic Map Page displayed, set the range to 2/6 nm.
2)
Select the STANDBY Softkey.
3)
Select the TEST Softkey.
4)
Self test takes approximately eight seconds to complete. When completed
successfully, traffic symbols are displayed and a voice alert “TAS System Test
OK” is heard. If the self test fails, the system reverts to Standby Mode and
a voice alert “TAS System Test Fail” is heard.
Annun/
Alerts
Abnormal
Operation
Additional
Features
System Self Test
Index
Appendix
Displaying Traffic on the Navigation Map
56
1)
Ensure TAS is operating.
2)
With the Navigation Map displayed, select the MAP Softkey.
3)
Select the TRAFFIC Softkey. Traffic is now displayed on the map.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Hazard Avoidance
EICAS
NOTE: If the system is configured to use TIS, the optional TCAS II is not
available for use.
Flight
Instruments
Traffic Collision Avoidance System (TCAS II) (Optional)
System Test
Nav/Com/
XPDR/Audio
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.
Hazard
Avoidance
Displaying Traffic on the Traffic Map Page
Procedures
Turn the small FMS Knob to select the Traffic Map Page.
Flight
Planning
2)
GPS Nav
Turn the large FMS Knob to select the Map Page Group.
AFCS
1)
2)
Turn the small FMS Knob to select the Traffic Map Page.
3)
Select the TA ONLY or TA/RA Softkey to begin displaying traffic. ‘TA/RA’ or
‘TA ONLY’ respectively, is displayed in the TCAS Mode field.
4)
Select the STANDBY Softkey to place the system in the Standby Mode.
‘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.
Abnormal
Operation
Turn the large FMS Knob to select the Map Page Group.
Additional
Features
1)
Annun/
Alerts
Appendix
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
57
Hazard Avoidance
1)
On the Traffic Page, select the ALT RNG Softkey.
2)
Select one of the following Softkeys:
EICAS
Flight
Instruments
Changing the Altitude Range
Nav/Com/
XPDR/Audio
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.
AFCS
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.
GPS Nav
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.
Flight
Planning
3)
Procedures
Displaying Traffic on the Navigation Map
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.
TERRAIN AWARENESS & WARNING SYSTEM (TAWS-B)
Additional
Features
Hazard
Avoidance
To return to the Traffic Page, select the BACK Softkey.
Abnormal
Operation
WARNING: The TAWS display shows supplemental information only. It should
not be used for navigation.
Annun/
Alerts
NOTE: Terrain data is not displayed when the aircraft is outside the installed
terrain database coverage area.
Index
Appendix
NOTE: TAWS operation is only available when the system is configured for
a TAWS-B installation.
58
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Hazard Avoidance
While the TAWS-B Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select ‘Test TAWS System’.
3)
Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center
of the TAWS-B Page.
EICAS
1)
Flight
Instruments
Manual System Test
Nav/Com/
XPDR/Audio
When all is in working order, “TAWS System Test, OK” is heard.
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.
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.
Additional
Features
Red
Hazard
Avoidance
Terrain/Obstacle Location
Procedures
Color
Flight
Planning
2)
GPS Nav
Turn the large FMS Knob to select the Map Page Group.
AFCS
1)
Abnormal
Operation
On the TAWS-B Page only, a gray shade of
purple indicates no terrain data is available.
Enable/Disable Aviation Data
2)
Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.
3)
Press the ENT Key.
Appendix
While the TAWS-B Page is displayed, press the MENU Key.
Annun/
Alerts
1)
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
59
Hazard Avoidance
Flight
Instruments
TAWS Inhibit
Nav/Com/
XPDR/Audio
EICAS
NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active
waypoint in a GPS SBAS approach, a LOW ALT annunciation may appear on
the PFD next to the altimeter if the current aircraft altitude is at least 164
feet below the prescribed altitude at the Final Approach Fix.
Inhibit TAWS
While the TAWS-B Page is displayed, select the INHIBIT Softkey.
GPS Nav
AFCS
Or:
1)
Press the MENU Key.
2)
Turn the small FMS Knob to select ‘Inhibit TAWS’.
3)
Press the ENT Key.
Flight
Planning
Enable TAWS
While the TAWS-B Page is displayed, select the INHIBIT Softkey.
Hazard
Avoidance
Procedures
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.
3)
Terrain and obstacles may be displayed in the Profile View by selecting the
PROFILE Softkey.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Displaying Terrain and Obstacles on the Navigation Map
60
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
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 Technology (SVT) functionality is offered as an optional
enhancement to the G1000 Integrated Flight Deck.
SVT 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. SVT information is shown on the primary flight display (PFD).
SVT offers a three-dimensional view of terrain and obstacles. Terrain and
obstacles that pose a threat to the aircraft in flight are shaded amber or red.
In addition to SVT 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. SVT 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
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
61
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
62
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
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.
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
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.
GPS Nav
ChartView (Optional)
AFCS
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.
Nav/Com/
XPDR/Audio
SafeTaxi®
EICAS
NOTE: Do not maneuver the aircraft based solely upon the geo-referenced
aircraft symbol.
Flight
Instruments
TERMINAL PROCEDURE CHARTS
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
63
FliteCharts® (Subscription Optional)
FliteCharts® resemble the paper version of AeroNav Services terminal procedures
charts. The charts are displayed with high-resolution and in color for applicable
charts. The MFD depiction shows the aircraft position on the moving map in the plan
view of most approach charts and on airport diagrams.
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
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Additional Features
1)
Select the SHW CHRT Softkey when displayed.
GPS Nav
Or:
Flight
Planning
2)
Procedures
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.
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
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
Change Day/Night View
64
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.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Additional Features
Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’
Options.
6)
In Auto Mode, turn the large FMS Knob to select the percentage field and
change percentage with the small FMS Knob. The percentage of change is
the day/night crossover point based on backlighting intensity.
7)
Press the FMS Knob when finished to remove the Chart Setup Menu.
AFCS
AIRPORT DIRECTORY
Flight
Planning
View Airport Directory Information
Procedures
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.
Selecting the XM Radio Page
3)
Select the RADIO Softkey to show the XM Radio Page where audio
entertainment is controlled.
Annun/
Alerts
Turn the small FMS Knob to select the displayed AUX - XM Information
Page.
Abnormal
Operation
2)
Appendix
Active Channel and Channel List
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
65
Index
The Active Channel Box on the XM Radio Page displays the currently selected
channel. The Channels List Box of the XM Radio Page shows a list of the available
channels for the selected category.
190-00600-05 Rev. C
Additional
Features
The XM® Radio Page provides information and control of the audio entertainment
features of the SiriusXM Satellite Radio.
Hazard
Avoidance
SIRIUSXM® RADIO ENTERTAINMENT (SUBSCRIPTION OPTIONAL)
Turn the large FMS Knob to select the Auxiliary Page Group.
GPS Nav
The AOPA or AC-U-KWIK Airport Directory adds enhanced airport information
when viewing airports on the WPT-Airport Information Page.
The Airport Directory databases are revised every 56 days. Check fly.garmin.
com for the current database.
1)
Nav/Com/
XPDR/Audio
5)
EICAS
Turn the small FMS Knob to choose between the ‘On’ and ‘Off’ Full Screen
Options.
Flight
Instruments
4)
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.
1)
While on the XM Radio Page, select the CHNL Softkey.
2)
Select the CH + Softkey to go up through the list in the Channel Box, or
move down the list with the CH – Softkey.
Flight
Planning
GPS Nav
Select an Available Channel within the Selected Category
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.
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.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Entering a Channel Directly
66
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Additional Features
EICAS
Nav/Com/
XPDR/Audio
AFCS
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.
3) Select any one of the (PS1 - PS15) softkeys to assign a number to the
active channel.
4) Select the SET Softkey on the desired channel number to save the channel
as a preset.
Flight
Instruments
Assigning Channel Presets
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
67
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
68
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Abnormal Operation
Flight
Instruments
ABNORMAL OPERATION
REVERSIONARY MODE
Flight
Planning
Procedures
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.
Hazard
Avoidance
AUDIO PANEL FAIL-SAFE OPERATION
Abnormal
Operation
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
69
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.
Additional
Features
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.
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
70
• 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
190-00600-05 Rev. C
Abnormal Operation
Flight
Instruments
EICAS
Nav/Com/
XPDR/Audio
Extreme Pitch Indication
Abnormal
Operation
Annun/
Alerts
Appendix
Index
71
Additional
Features
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Hazard
Avoidance
190-00600-05 Rev. C
Procedures
DR Mode is indicated on the G1000 by the appearance of the letters ‘DR’
superimposed in amber over the ‘own aircraft’ symbol as shown in the following
figure. In addition, ‘DR’ is prominently displayed, also in amber, 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 amber, 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/SBAS 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/SBAS 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 amber 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
72
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Annunciations & Alerts
Flight
Instruments
ANNUNCIATIONS & ALERTS
CAS MESSAGES
EICAS
Warning Messages
Nav/Com/
XPDR/Audio
AFCS
Annunciation Text
Desription
Overheated NiCad battery (optional)
BATTERY O’TEMP
Cabin altitude is high
CABIN ALT
An engine has failed
ENGINE FAIL L-R*
One or both generators are offline
GEN OFF L-R
Left engine oil pressure low
OIL PRESS LO L-R*
Tail cone temp high, possible bleed air leak
TAIL CONE BLD LK
*Only affected side displayed (L, R, or L-R) in a CAS message; applicable CAS
messages listed here display L-R for example.
GPS Nav
Flight
Planning
Procedures
Caution Messages
Tailcone baggage door not fully secured
Start control circuit breaker (located in aft j-box) tripped
Current limiter blown (located in aft j-box)
Antiskid Control Unit cannot perform anti-skid
functions
Overheated NiCad battery (optional)
Annun/
Alerts
Battery temperature sensor failure
Cabin altitude potentially unsafe
Cabin door not fully secured
A door monitor has not been properly tested or has
failed
Duct temperature too high or sensor disconnected
Appendix
Index
190-00600-05 Rev. C
ADS-B has failed
Abnormal
Operation
DUCT O’HEAT L-R*
ENG A/I COLD L-R*
Description
Additional
Features
BATTERY O’TEMP
BATTERY TEMP FAIL
CABIN ALT
CABIN DOORS
CHECK DOORS
Hazard
Avoidance
Annunciation Text
ADS-B FAIL
AFT DOOR
AFT JBOX CB L-R*
AFT JBOX LMT L-R*
ANTISKID FAIL
Engine anti-ice system ON and inlet temperature is cold
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
73
Annunciations & Alerts
EICAS
Flight
Instruments
Annunciation Text
ENG CTRL SYS L-R*
F/W SHUTOFF L/R*
FLAPS FAIL
Nav/Com/
XPDR/Audio
FUEL BOOST L-R*
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
FUEL FILTER BP L-R*
FUEL LVL LO L-R*
FUEL PRES LO L-R*
GEN OFF L-R*
HYD PRESS LO
HYD PUMP ON
NOSE DOOR L-R*
OXYGEN OFF
P/S HTR L-R*
PRESS CTRL
STALL WARN FAIL
STALL WARN HTR
T2 HTR FAIL L-R*
TAIL DE-ICE FAIL
W/S A/I FAIL L-R*
W/S O’HEAT L-R*
WING DE-ICE FAIL
WOW MISCOMPARE
XPDR 1 FAIL
XPDR 2 FAIL
XPDR 1-2 FAIL
XPDR STANDBY
Description
FADEC has a fault that requires maintenance
Fuel firewall shutoff valve fully closed
A flap system failure has occurred
Electric fuel boost pump ON. Caution condition
is displayed when the boost pump is operating in
abnormal conditions
Engine fuel filter impending bypass switch closed
Fuel level in tank is too low
Fuel pressure too low
One or both electrical generators offline
Hydraulic system pressure too low
Hydraulic pump running too long
One or both nose baggage doors not fully secured
Oxygen supply off
No current detected to pitot static heater
Pressure controller loss of integrity
Failure detected in stall warning system
No power delivered to stall warning vane heater
T2 probe heater failure
De-ice system not operating normally
Loss of power to windshield heater
Windshield anti-ice power ON; temperature too high
De-ice system operating abnormally
Gear on-ground inputs do not agree
Transponder 1 has failed
Transponder 2 has failed
Transponder 1 and/or 2 has failed
Transponder is in Standby Mode
Index
*Only affected side displayed (L, R, or L-R) in a CAS message; applicable CAS
messages listed here display L-R for example.
74
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Annunciations & Alerts
Flight
Instruments
Advisory Messages
Electric fuel boost pump ON. Caution condition is
displayed when the boost pump is operating in abnormal
conditions.
AFCS
Fuel low level function failure
Fuel transfer valve open
GPS Nav
MFD temperature is below -20° C
Antiskid control spindown function not working
No current detected to pitot static heater
Flight
Planning
Pressure controller loss of integrity
Air Source Selector switch in OFF or fresh air position
Procedures
Speed brakes extended
Stall warning system on ice-contaminated schedule
Hazard
Avoidance
De-ice boots inflating/deflating as designed
Loss of power to windshield heater
Windshield anti-ice power ON; temperature too high
Additional
Features
FUEL LO INOP L-R*
FUEL TRANSFER
MFD COLD
NO TIRE SPINDOWN
P/S HTR L-R*
PRESS CTRL
PRESS OFF
SPD BRK EXTEND
STALL WARN HI
SURFACE DE-ICE
W/S A/I FAIL L-R*
W/S O’HEAT L-R*
Nav/Com/
XPDR/Audio
FUEL BOOST L-R*
EICAS
Annunciation Text
Description
Cabin altitude potentially unsafe
CABIN ALT
Cockpit voice Recorder has failed
CVR FAIL
ENGINE A/I COLD L-R* Engine anti-ice system ON and inlet temperature is cold
*Only affected side displayed (L, R, or L-R) in a CAS message; applicable CAS
messages listed here display L-R for example.
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
75
COMPARATOR ANNUNCIATIONS
Note that operating the system in the vicinity of metal buildings or other metal
structures can cause sensor differences that may result in nuisance miscompare
annunciations during start up, shut down, or while taxiing.
Comparator
Window Text
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
ALT MISCOMP
Difference in altitude sensors is > 200 ft.
AFCS
If both airspeed sensors detect < 35 knots, this is inhibited.
IAS MISCOMP
If either airspeed sensor detects > 35 knots, and the difference in sensors is >
15 kts.
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
If either airspeed sensor detects > 80 knots, and the difference in sensors is
> 10 kts.
HDG MISCOMP
Difference in heading sensors is > 10 degrees.
PIT MISCOMP
Difference in pitch sensors is > 5 degrees.
ROL MISCOMP
Difference in roll sensors is > 6 degrees.
VDI MISCOMP
Difference in temperature compensated altitudes is > 50 ft.
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..
VDI NO COMP
No temperature compensated altitude data available.
REVERSIONARY SENSOR ANNUNCIATIONS
Reversionary
Sensor Window
Text
Annun/
Alerts
Abnormal
Operation
Condition
Appendix
BOTH ON ADC1
BOTH ON ADC2
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.
Index
BOTH ON AHRS1
Condition
76
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Annunciations & Alerts
Both PFDs are displaying data from the number two Attitude & Heading
Reference System.
Both PFDs are displaying data from the number one GPS receiver.
Nav/Com/
XPDR/Audio
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.
AFCS
PFD2 is displaying data from the #1 AHRS.
PFD1 is displaying data from the #2 AHRS.
GPS Nav
BOTH ON GPS1
BOTH ON GPS2
USING ADC1
USING ADC2
USING AHRS1
USING AHRS2
USING GPS1
USING GPS2
Condition
EICAS
BOTH ON AHRS2
Flight
Instruments
Reversionary
Sensor Window
Text
PFD2 is displaying data from the #1 GPS.
PFD1 is displaying data from the #2 GPS.
Flight
Planning
TAWS-B ALERTS
PFD/MFD
TAWS-B Page
Annunciation
MFD
Pop-Up Alert
Procedures
Alert Type
Aural Message
“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”
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00600-05 Rev. C
Hazard
Avoidance
Excessive Descent
Rate Warning (EDR)
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
77
Alert Type
Additional
Features
Abnormal
Operation
Annun/
Alerts
MFD
Pop-Up Alert
Aural Message
“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”
Altitude Callout
“500”
None
None
“Five-Hundred”
Excessive Descent
Rate Caution (EDR)
“Sink Rate”
Negative Climb
Rate Caution (NCR)
“Don’t Sink”
TAWS-B System Status Annunciations
Alert Type
PFD/MFD
Alert
Annunciation
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
TAWS-B System Test Fail
None
TAWS-B Page
Annunciation
Aural
Message
TAWS TEST
None
None
“TAWS System
Test OK”
None
None
TERRAIN DATABASE FAILURE
None
TAWS FAIL
“TAWS System
Failure”
Index
Appendix
PFD/MFD
TAWS-B Page
Annunciation
Imminent Terrain
Impact Caution (ITI)
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
78
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Annunciations & Alerts
TAWS FAIL
“TAWS System
Failure”
NO GPS POSITION
“TAWS Not
Available”
None
“TAWS Not
Available”
AFCS
Excessively degraded GPS
signal, Out of database
coverage area
Nav/Com/
XPDR/Audio
Aural
Message
GPS Nav
TCAS II ALERTS AND ANNUNCIATIONS
TEST
(‘TEST MODE’ also shown in
white on top center of page)
Traffic Advisory and
Resolution Advisory
(TA/RA)
None
TA/RA
Traffic Advisory Only
(TA ONLY)
TA ONLY
on ground
in air
Abnormal
Operation
TCAS II Standby
(TFC STBY)
Additional
Features
None
Hazard
Avoidance
TCAS II Self-test
Initiated (TEST)
Traffic
Display
Status Icon
(Other Maps)
Annun/
Alerts
STANDBY or STANDBY*
(also shown in white in
center of page)
FAIL
TCAS II Failed
Procedures
MFD Traffic Map Page
Mode Annunciation
Flight
Planning
PFD Mode
Annunciation
Mode
EICAS
TAWS-B Page
Annunciation
Terrain or Obstacle database
unavailable or invalid, invalid
software configuration, system
audio fault
No GPS position
Flight
Instruments
PFD/MFD
Alert
Annunciation
Alert Type
Appendix
* Annunciation appears amber while in flight.
TCAS II Modes
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
79
Annunciations & Alerts
Flight
Instruments
Traffic Map Page
Annunciation
EICAS
NO DATA
DATA FAILED
Data is not being received from the TCAS II unit
Data is being received from the TCAS II unit, but the unit is selfreporting a failure
Incorrect data format received from the TCAS II unit
TCAS II Failure Annunciations
Traffic Status Banner
Annunciation
GPS Nav
A Resolution Advisory is outside the selected display range*.
Annunciation is removed when traffic comes within the selected
display range
Flight
Planning
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).
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).
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
TCAS II Traffic Status Annunciations
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
RA OFF SCALE
Procedures
Description
Hazard
Avoidance
AFCS
Nav/Com/
XPDR/Audio
FAILED
Description
80
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Annunciations & Alerts
Aural Alert
Flight
Instruments
AURAL ALERTS
Description
“Vertical track”
EICAS
“Minimums, minimums” The aircraft has descended below the preset minimum descent altitude or
decision altitude.
“Traffic”
Nav/Com/
XPDR/Audio
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
“TIS not available”
AFCS
The aircraft is outside the Traffic Information Service (TIS) coverage area (not
available when a TAS system is installed).
FLIGHT PLAN IMPORT/EXPORT MESSAGES
Description
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.
‘Flight plan partially imported.’
Some flight plan waypoints were successfully imported from
the SD card, however others had errors and were not imported.
A partial stored flight plan now exists in the system.
‘File contained user waypoints only.’
The file stored on the SD card did not contain a flight plan,
only user waypoints. One or more of these waypoints did not
import successfully.
Abnormal
Operation
‘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.
Annun/
Alerts
Index
81
Appendix
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Hazard
Avoidance
190-00600-05 Rev. C
Procedures
‘Flight plan successfully imported.’
Additional
Features
Flight
Planning
Flight Plan Import/Export
Results
GPS Nav
In some circumstances, some messages may appear in conjunction with others.
Flight Plan Import/Export
Results
‘User waypoint database full. Not all
loaded.’
Description
The flight plan file on the SD card contains user waypoints.
The quantity of stored user waypoints has exceeded system
capacity, therefore not all the user waypoints on the SD card
have been imported. Any flight plan user waypoints that were
not imported are locked in the flight plan. The flight plan must
be edited within the system before it can be activated for use.
‘One or more user waypoints renamed.’ One or more imported user waypoints were renamed when
imported due to naming conflicts with waypoints already
existing in the system.
‘Flight plan successfully exported.’
The stored flight plan was successfully exported to the SD card.
‘Flight plan export failed.’
The stored flight plan was not successfully exported to the SD
card. The SD card may not have sufficient available memory or
the card may have been removed prematurely.
G1000 SYSTEM MESSAGE ADVISORIES
Message
ABORT APR – Loss of GPS
navigation. Abort approach.
ADC1 ALT EC – ADC1 altitude error
correction is unavailable.
ADC1 AS EC – ADC1 airspeed error
correction is unavailable.
ADC2 ALT EC – ADC2 altitude error
correction is unavailable.
ADC2 AS EC – ADC2 airspeed error
correction is unavailable.
AHRS MAG DB – AHRS magnetic
model database version mismatch.
AHRS1 CAL – AHRS1 calibration
version error. Srvc req’d.
AHRS1 CONFIG – AHRS1 config
error. Config service req’d.
Comments
Abort approach due to loss of GPS navigation.
GDC1 s reporting that the altitude error correction
is unavailable.
GDC1 is reporting that the airspeed error
correction is unavailable.
GDC2 is reporting that the altitude error correction
is unavailable.
GDC2 is reporting that the airspeed error
correction is unavailable.
The #1 AHRS and #2 AHRS magnetic model
database versions do not match.
The #1 AHRS calibration version error. The system
should be serviced.
The #1 AHRS config version error. 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
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Annunciations & Alerts
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
AHRS2 GPS – AHRS2 operating
exclusively in no-GPS mode.
AHRS2 GPS – AHRS2 not receiving
backup GPS information.
AHRS2 GPS – AHRS2 using backup
GPS source.
AFCS
AHRS2 CAL – AHRS2 calibration
version error. Srvc req’d.
AHRS2 CONFIG – AHRS2 config
error. Config service req’d.
AHRS2 GPS – AHRS2 not receiving
any GPS information.
Nav/Com/
XPDR/Audio
AHRS1 SRVC – AHRS1 Magneticfield model needs update.
AHRS1 TAS – AHRS1 not receiving
valid airspeed.
EICAS
AHRS1 GPS – AHRS1 operating
exclusively in no-GPS mode.
AHRS1 GPS – AHRS1 using backup
GPS source.
Comments
The #1 AHRS is operating exclusively in no-GPS
mode. The system should be serviced.
The #1 AHRS is not receiving backup GPS information.
The system should be serviced.
The #1 AHRS is not receiving any or any useful GPS
information. Check AFMS limitations. The system
should be serviced.
The #1 AHRS is operating exclusively in no-GPS
mode. 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 #1 AHRS earth magnetic field model is out of
date. Update magnetic field model when practical.
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 calibration version error. The system
should be serviced.
The #2 AHRS config version error. 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 #2 AHRS is operating exclusively in no-GPS
mode. The system should be serviced.
Ther #2 AHRS is not receiving backup GPS information.
The system should be serviced.
The #2 AHRS is using the backup GPS path.
Primary GPS path has failed. The system should be
serviced when possible.
Flight
Instruments
Message
AHRS1 GPS – AHRS1 operating
exclusively in no-GPS mode.
AHRS1 GPS – AHRS1 not receiving
backup GPS information.
AHRS1 GPS – AHRS1 not receiving
any GPS information.
Index
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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
83
Message
AHRS2 SRVC – AHRS2 Magneticfield model needs update.
AHRS2 TAS – AHRS2 not receiving
valid airspeed.
APR ADVISORY – SBAS VNAV not
available. Using Baro VNAV.
APR DWNGRADE – Approach
downgraded.
APR INACTV – Approach is not
active.
Comments
The #2 AHRS earth magnetic field model is out of
date. Update magnetic field model when practical.
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.
SBAS VNAV not available. Check GPS signal.
Vertical guidance generated by SBAS is unavailable,
use LNAV only minimums.
The system notifies the pilot that the loaded
approach is not active. Activate approach when
required.
ARSPC AHEAD – Airspace ahead
Special use airspace is ahead of aircraft. The
less than 10 minutes.
aircraft will penetrate the airspace within 10
minutes.
ARSPC NEAR – Airspace near and
Special use airspace is near and ahead of the
ahead.
aircraft position.
ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the aircraft
than 2 nm.
position.
BARO MISMATCH – Correct baro
mismatch for VNAV guidance.
Altimeter setting is not the same on the PFD1 and
PFD2. Synchronize settings for VNAV guidance
CHECK CRS – Database course for
LOC1 / [LOC ID] is [CRS]°.
CHECK CRS – Database course for
LOC2 / [LOC ID] is [CRS]°.
COM1 PTT – COM1 push-to-talk key
is stuck.
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 COM1 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.
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
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190-00600-05 Rev. C
Annunciations & Alerts
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
DB CHANGE – Database changed.
Verify user modified procedures.
The pilot profile data was lost. System reverts
to default pilot profile and settings. The pilot
may reconfigure the MFD & PFDs with preferred
settings, if desired.
This occurs when a stored flight plan contains
procedures that have been manually edited. This
alert is issued only after an navigation database
update. Verify that the user-modified procedures in
stored flight plans are correct and up to date.
Nav/Com/
XPDR/Audio
DATA LOST – Pilot stored data was
lost. Recheck settings.
EICAS
Comments
The system has detected a failure in COM1. COM1
may still be usable. The system should be serviced
when possible.
COM1 TEMP – COM1 over temp.
The system has detected an over temperature
Reducing transmitter power.
condition in COM1. The transmitter is operating at
reduced power. If the problem persists, the system
should be serviced.
COM2 PTT – COM2 push-to-talk key The COM2 external push-to-talk switch is stuck in the
is stuck.
enable (or “pressed”) position. Press the PTT switch
again to cycle its operation. If the problem persists, the
system should be serviced.
COM2 SERVICE – COM2 needs
The system has detected a failure in COM2. COM2
service. Return unit for repair.
may still be usable. The system should be serviced
when possible.
COM2 TEMP – COM2 over temp.
The system has detected an over temperature
Reducing transmitter power.
condition in COM2. The transmitter is operating at
reduced power. If the problem persists, the system
should be serviced.
CNFG MODULE – PFD1
The PFD1 configuration module backup memory
configuration module is inoperative. has failed. The system should be serviced.
Flight
Instruments
Message
COM1 SERVICE – COM1 needs
service. Return unit for repair.
Annun/
Alerts
Appendix
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
85
Message
DB CHANGE – Database changed.
Verify stored airways.
Comments
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.
DB MISMATCH – Navigation
The PFDs and MFD have different navigation
database mismatch. Xtalk is off.
database versions or types (Americas, European,
etc.) installed. Crossfill is off. Install correct
navigation database version or type in all displays.
DB MISMATCH – Obstacle database The PFDs and MFD have different obstacle
mismatch.
database installed. Install correct obstacle
database in all displays.
DB MISMATCH – Standby
The PFDs and MFD have different standby
Navigation database mismatch.
navigation database versions or regions installed.
Check the AUX-SYSTEM STATUS Page to determine
versions or regions. Also, check the AUX-SYSTEM
STATUS Page for a database synchronization
function not completed. After synchronization is
complete, power must be turned off, then on.
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.
FAILED PATH – A data path has
failed.
FPL TRUNC – Flight plan has been
truncated.
A data path connected to the GDU, GSD 41, or the
GIA 63/W has failed.
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.
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
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Annunciations & Alerts
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
A failure has been detected in glideslope receiver
1. The system should be serviced.
G/S1 SERVICE – G/S1 needs service. A failure has been detected in glideslope receiver
Return unit for repair.
1. The receiver may still be available. The system
should be serviced when possible.
G/S2 FAIL – G/S2 is inoperative.
A failure has been detected in glideslope receiver
2. The system should be serviced.
G/S2 SERVICE – G/S2 needs service. A failure has been detected in glideslope receiver
Return unit for repair.
2. The receiver may still be available. The system
should be serviced when possible.
GCU CNFG – GCU Config error.
GCU 475 configuration settings do not match
Config service req’d.
those of backup configuration memory. The system
should be serviced.
GCU FAIL – GCU is inoperative.
A failure has been detected in the GCU 475. The
GCU 475 is unavailable.
Nav/Com/
XPDR/Audio
G/S1 FAIL – G/S1 is inoperative.
EICAS
FPL WPT MOVE – Flight plan
waypoint moved.
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.
The system has detected that a waypoint
coordinate has changed due to a new navigation
database update. Verify that stored flight plans
contain correct waypoint locations.
Flight
Instruments
Message
FPL WPT LOCK – Flight plan
waypoint is locked.
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
87
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
Message
Comments
GCU KEYSTK – GCU [key name] Key A key is stuck on the GCU 475 bezel. Attempt to
is stuck.
free the stuck key by pressing it several times. The
system should be serviced if the problem persists.
GCU MANIFEST – GCU software
The GCU 475 has incorrect software installed. The
mismatch, communication halted.
system should be serviced.
GDC1 MANIFEST – GDC1 software
mismatch, communication halted.
The GDC 74B has incorrect software installed. The
GDC2 MANIFEST – GDC2 software system should be serviced.
mismatch, communication halted.
GDL69 CONFIG – GDL 69 config
GDL 69 configuration settings do not match those
error. Config service req’d.
of backup configuration memory. The system
should be serviced.
GDL69 FAIL – GDL 69 has failed.
A failure has been detected in the GDL 69. The
receiver is unavailable. The system should be
serviced
GDL69 MANIFEST – GDL69
The GDL 69 has incorrect software installed. The
software mismatch, communication
system should be serviced.
halted.
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.
GEA1 MANIFEST – GEA1 software The #1 GEA 71 has incorrect software installed.
mismatch, communication halted.
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.
GEA2 MANIFEST – GEA2 software The #2 GEA 71 has incorrect software installed.
mismatch, communication halted.
The system should be serviced.
GEO LIMITS – AHRS1 too far North/
The aircraft is outside geographical limits for
South, no magnetic compass.
approved AHRS operation. Heading is flagged as
GEO LIMITS – AHRS2 too far North/ invalid.
South, no magnetic compass.
GFC MANIFEST – GFC software
Incorrect servo software is installed, or gain
mismatch, communication halted.
settings are incorrect.
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Annunciations & Alerts
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
89
Procedures
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Flight
Planning
190-00600-05 Rev. C
GPS Nav
GIA2 COOLING – GIA2 over
temperature.
GIA2 MANIFEST – GIA2 software
mismatch, communication halted.
GIA2 SERVICE – GIA2 needs service.
Return the unit for repair.
GMA XTALK – GMA crosstalk error
has occurred.
GMA1 CONFIG – GMA1 config
error. Config service req’d.
AFCS
GIA2 CONFIG – GIA2 audio config
error. Config service req’d.
GIA2 COOLING – GIA2 temperature
too low.
Nav/Com/
XPDR/Audio
GIA1 MANIFEST – GIA1 software
mismatch, communication halted.
GIA1 SERVICE – GIA1 needs service.
Return the unit for repair.
GIA2 CONFIG – GIA2 config error.
Config service req’d.
EICAS
GIA1 CONFIG – GIA1 audio config
error. Config service req’d.
GIA1 COOLING – GIA1 over
temperature.
GIA1 COOLING – GIA1 temperature
too low.
Comments
The GIA1 configuration settings do not match
backup configuration memory. The system should
be serviced.
The GIA2 have an error in the audio configuration.
The system should be serviced.
The GIA1 temperature is too high. If problem
persists, the system should be serviced.
The GIA1 temperature is too low to operate
correctly. Allow units to warm up to operating
temperature.
The GIA1 has incorrect software installed. The
system should be serviced.
The GIA1 self-test has detected a problem in the
unit. The system should be serviced.
The GIA2 configuration settings do not match
backup configuration memory. The system should
be serviced.
The GIA2 have an error in the audio configuration.
The system should be serviced.
The GIA2 temperature is too low to operate
correctly. Allow units to warm up to operating
temperature.
The GIA2 temperature is too high. If problem
persists, the system should be serviced.
The GIA 2 has incorrect software installed. The
system should be serviced.
The GIA2 self-test has detected a problem in the
unit. The system should be serviced.
An error has occurred in transferring data between
the two GMAs. The system should be serviced.
The audio panel configuration settings do not
match backup configuration memory. The system
should be serviced.
Flight
Instruments
Message
GIA1 CONFIG – GIA1 config error.
Config service req’d.
Message
GMA1 FAIL – GMA1 is inoperative.
Comments
The audio panel self-test has detected a failure.
The audio panel is unavailable. The system should
be serviced.
GMA1 MANIFEST – GMA1 software The audio panel has incorrect software installed.
mismatch, communication halted.
The system should be serviced.
GMA1 SERVICE – GMA1 needs
The audio panel self-test has detected a problem
service. Return unit for repair.
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.
GMA2 CONFIG – GMA2 config
The audio panel configuration settings do not
error. Config service req’d.
match backup configuration memory. The system
should be serviced.
GMA2 FAIL – GMA2 is inoperative. The audio panel self-test has detected a failure.
The audio panel is unavailable. The system should
be serviced.
GMA2 MANIFEST – GMA2 software The audio panel has incorrect software installed.
mismatch, communication halted.
The system should be serviced.
GMA2 SERVICE – GMA2 needs
The audio panel self-test has detected a problem
service. Return unit for repair.
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.
GMC CONFIG – GMC Config error.
Error in the configuration of the GMC 710.
Config service req’d.
GMC FAIL – GMC is inoperative.
A failure has been detected in the GMC 710. The
GMC 710 is unavailable.
GMC KEYSTK – GMC [key name]
A key is stuck on the GMC 710 bezel. Attempt to
Key is stuck.
free the stuck key by pressing it several times. The
system should be serviced if the problem persists.
GMC MANIFEST – GMC software
The GMC 710 has incorrect software installed. The
mismatch. Communication halted. 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
90
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Annunciations & Alerts
The GMU 44 has incorrect software installed. The
system should be serviced.
EICAS
Loss of GPS navigation due to insufficient satellites.
Nav/Com/
XPDR/Audio
Loss of GPS navigation due to position error.
AFCS
Loss of GPS navigation due to GPS failure.
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.
Flight
Planning
The #1 AHRS has incorrect software installed. The
system should be serviced.
The #2 AHRS has incorrect software installed. The
system should be serviced.
GSD1 and the CDU have different copies of the
GSD1 configuration.
Procedures
Hazard
Avoidance
GSD1 is reporting a low temperature condition.
Additional
Features
GSD1 is reporting an over-temperature condition.
Abnormal
Operation
GSD1 has incorrect software installed. The system
should be serviced.
GSD1 is reporting an internal error condition. The
GSD may still be usable.
The transponder has incorrect software installed.
The system should be serviced.
The transponder has incorrect software installed.
The system should be serviced.
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Annun/
Alerts
190-00600-05 Rev. C
Comments
Flight
Instruments
Message
GMU1 MANIFEST – GMU1 software
mismatch, communication halted.
GMU2 MANIFEST – GMU2 software
mismatch, communication halted.
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.
GPS1 SERVICE – GPS1 needs
service. Return unit for repair.
GPS2 SERVICE – GPS2 needs
service. Return unit for repair.
GRS1 MANIFEST – GRS1 software
mismatch, communication halted.
GRS2 MANIFEST – GRS2 software
mismatch, communication halted.
GSD1 CONFIG – GSD1 config
error. Config service req’d.
GSD1 COOLING – GSD1
temperature too low.
GSD1 COOLING – GSD1 over
temperature.
GSD1 MANIFEST – GSD1 software
mismatch. Communication halted.
GSD1 SERVICE – GSD1 needs
service. Return unit for repair.
GTX1 MANIFEST – GTX1 software
mismatch, communication halted.
GTX2 MANIFEST – GTX2 software
mismatch, communication halted.
91
Message
GWX CONFIG – GWX config error.
Config service req’d.
Comments
GWX 68 configuration settings do not match those
of the GDU configuration. The system should be
serviced.
GWX FAIL – GWX is inoperative.
The GDU is not recieving status packet from the
GWX 68 or the GWX 68 is reporting a fault. The
GWX 68 radar system should be serviced.
GWX MANIFEST – GWX software
The GWX 68 has incorrect software installed. The
mismatch, communication halted.
system should be serviced.
GWX SERVICE – GWX needs service. A failure has been detected in the GWX 68. The
Return unit for repair.
GWX 68 may still be usable.
HDG FAULT – AHRS1 magnetometer A fault has occurred in the #1 GMU 44. Heading is
fault has occurred.
flagged as invalid. The AHRS uses GPS for backup
mode operation. The system should be serviced.
HDG FAULT – AHRS2 magnetometer A fault has occurred in the #2 GMU 44. Heading is
fault has occurred.
flagged as invalid. The AHRS uses GPS for backup
mode operation. The system should be serviced.
HW MISMATCH – GIA hardware
mismatch. GIA1 communication
halted.
A GIA mismatch has been detected, where only
one is SBAS capable.
HW MISMATCH – GIA hardware
mismatch. GIA2 communication
halted.
HOLD EXPIRED – Holding EFC time
The time for the holding EFC has expired.
expired.
INSIDE ARSPC – Inside airspace.
The aircraft is inside the airspace.
LOCKED FPL – Cannot navigate
locked flight plan.
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.
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
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Annunciations & Alerts
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
The MFD is overheating and is reducing power
consumption by dimming the display. If problem
persists, the system should be serviced.
MFD1 CONFIG – MFD1 config error. The MFD configuration settings do not match
Config service req’d.
backup configuration memory. 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.
MFD1 DB ERR – MFD1 basemap
The MFD detected a failure in the basemap
database error exists.
database.
MFD1 DB ERR – MFD1 Chartview
The MFD detected a failure in the ChartView
database error exists.
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 navigation The MFD detected a failure in the navigation
database error exists.
database. Attempt to reload the navigation
database. If problem persists, the system should
be serviced.
Nav/Com/
XPDR/Audio
MFD1 COOLING – MFD1 has poor
cooling. Reducing power usage.
EICAS
Comments
GPS integrity is insufficient for the current phase
of flight.
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°.
Flight
Instruments
Message
LOI – GPS integrity lost. Crosscheck
with other NAVS.
LRG MAG VAR – Verify all course
angles.
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
93
Message
MFD1 DB ERR – MFD1 obstacle
database error exists.
MFD1 DB ERR – MFD1 obstacle
database missing.
MFD1 DB ERR – MFD1 Safe Taxi
database error exists.
MFD1 DB ERR – MFD1 Safe Taxi
database error exists.
MFD1 DB ERR – MFD1 terrain
database error exists.
MFD1 DB ERR – MFD1 terrain
database missing.
MFD1 KEYSTK – MFD [key name]
Key is stuck.
MFD1 MANIFEST – MFD1 software
mismatch, communication halted.
MFD1 SERVICE – MFD1 needs
service. Return unit for repair.
MFD1 VOLTAGE – MFD1 has low
voltage. Reducing power usage
Comments
The MFD 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.
The MFD 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.
The MFD 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.
The MFD 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.
A key is stuck on the MFD bezel. Attempt to free
the stuck key by pressing it several times. The
system should be serviced if the problem persists.
The MFD has incorrect software installed. The
system should be serviced.
The MFD self-test has detected a problem. The
system should be serviced.
The MFD voltage is low. 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
94
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Annunciations & Alerts
Comments
[PFD1, PFD2, or MFD1] CARD 1
ERR – Card 1 is invalid.
[PFD1, PFD2, or MFD1] CARD
1 REM – Card 1 was removed.
Reinsert card.
[PFD1, PFD2, or MFD1] CARD 2
ERR – Card 2 is invalid.
[PFD1, PFD2, or MFD1] CARD
2 REM – Card 2 was removed.
Reinsert card.
PFD1 COOLING – PFD1 has poor
cooling. Reducing power usage.
The SD card in the top card slot of the specified
PFD or MFD contains invalid data.
The SD card was removed from the top card slot of
the specified PFD or MFD. The SD card needs to be
reinserted.
The SD card in the bottom card slot of the specified
PFD or MFD contains invalid data.
The SD card was removed from the bottom card
slot of the specified PFD or MFD. The SD card
needs to be reinserted.
The PFD is overheating and is reducing power
consumption by dimming the display. If problem
persists, the system should be serviced.
The PFD configuration settings do not match
backup configuration memory. The system should
be serviced.
The PFD detected a failure in the basemap
database.
Flight
Instruments
Message
NAV1 SERVICE – NAV1 needs
service. Return unit for repair.
NAV2 SERVICE – NAV2 needs
service. Return unit for repair.
NAV DB UPDATED – Active
navigation database updated.
NO NAV CAPTURE – Intercept
angle too large for LOC/BC capture.
EICAS
A failure has been detected in the NAV1 and/or
NAV2 receiver. The receiver may still be available.
The system should be serviced.
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
95
Hazard
Avoidance
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Procedures
190-00600-05 Rev. C
Flight
Planning
PFD1 DB ERR – PFD1 basemap
database error exists.
GPS Nav
PFD1 CONFIG – PFD1 config error.
Config service req’d.
AFCS
The maximum intercept angle for LOC/BC
capture is 105 degrees. This message informs
the pilot that the capture will not occur if the
limit is exceeded..
NON WGS84 WPT – Do not use GPS The position of the selected waypoint [xxxx] is not
for navigation to [xxxx]
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 nonWGS84 waypoint.
Nav/Com/
XPDR/Audio
System has updated the active navigation database
from the standby navigation database.
Message
PFD1 DB ERR – PFD1 navigation
database error exists.
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
PFD1 DB ERR – PFD1 obstacle
database error exists.
PFD1 DB ERR – PFD1 obstacle
database missing.
PFD1 DB ERR – PFD1 Safe Taxi
database error exists.
PFD1 DB ERR – PFD1 terrain
database error exists.
PFD1 DB ERR – PFD1 terrain
database missing.
PFD1 COOLING – PFD1 has poor
cooling. Reducing power usage.
PFD1 CONFIG – PFD1 config error.
Config service req’d.
PFD1 KEYSTK – PFD1 [key name]
Key is stuck.
PFD1 MANIFEST – PFD1 software
mismatch, communication halted.
PFD1 SERVICE – PFD1 needs
service. Return unit for repair.
96
Comments
The PFD detected a failure in the navigation
database. Attempt to reload the navigation
database. If problem persists, the system should
be serviced.
The 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.
The 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.
The 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 PFD is overheating and is reducing power
consumption by dimming the display. If problem
persists, the system should be serviced.
The PFD configuration settings do not match
backup configuration memory. The system should
be serviced.
A key is stuck on the PFD bezel. Attempt to free
the stuck key by pressing it several times. The
system should be serviced if the problem persists.
The PFD has incorrect software installed. The
system should be serviced.
The PFD self-test has detected a problem. The
system should be serviced.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Annunciations & Alerts
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Hazard
Avoidance
190-00600-05 Rev. C
Procedures
PFD2 DB ERR – PFD2 terrain
database missing.
PFD2 KEYSTK – PFD2 [key name]
Key is stuck.
Flight
Planning
PFD2 DB ERR – PFD2 terrain
database error exists.
GPS Nav
PFD2 DB ERR – PFD2 obstacle
database missing.
PFD2 DB ERR – PFD2 Safe Taxi
database error exists.
AFCS
PFD2 DB ERR – PFD2 obstacle
database error exists.
Nav/Com/
XPDR/Audio
PFD2 DB ERR – PFD2 basemap
database error exists.
PFD2 DB ERR – PFD2 navigation
database error exists.
EICAS
PFD2 CONFIG – PFD2 config error.
Config service req’d.
Comments
The PFD1 voltage is low. The system should be
serviced.
The PFD is overheating and is reducing power
consumption by dimming the display. If problem
persists, the system should be serviced.
The PFD configuration settings do not match
backup configuration memory. The system should
be serviced.
The PFD detected a failure in the basemap
database.
The PFD detected a failure in the navigation
database. Attempt to reload the navigation
database. If problem persists, the system should
be serviced.
The 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.
The 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.
The 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.
A key is stuck on the PFD bezel. Attempt to free
the stuck key by pressing it several times. The
system should be serviced if the problem persists.
Flight
Instruments
Message
PFD1 VOLTAGE – PFD1 has low
voltage. Reducing power usage
PFD2 COOLING – PFD2 has poor
cooling. Reducing power usage.
97
Message
PFD2 MANIFEST – PFD2 software
mismatch, communication halted.
PFD2 SERVICE – PFD2 needs
service. Return unit for repair.
PFD2 VOLTAGE – PFD2 has low
voltage. Reducing power usage
Comments
The PFD has incorrect software installed. The
system should be serviced.
The PFD self-test has detected a problem. The
system should be serviced.
The PFD2 voltage is low. The system should be
serviced.
SCHEDULER [#] – <message>.
SLCT FREQ – Select appropriate
frequency for approach.
Message criteria entered by the user.
The system notifies the pilot to load the approach
frequency for the appropriate NAV receiver. Select
the correct frequency for the approach.
The Navigation angle is non-magnetic. Select the
MAGNETIC NAV ANGLE display units.
The system notifies the pilot to set the CDI to the
correct NAV receiver. Set the CDI to the correct
NAV receiver.
The Navigation angle is magnetic. Select the
alternate NAV ANGLE display units.
A steep turn is 15 seconds ahead. Prepare to turn.
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 (4.9 arc-second or
better) is not currently installed.
The MFD and PFDs have different software versions
installed. The system should be serviced.
SLCT MAG – Select MAGNETIC
NAV ANGLE display units.
SLCT NAV – Select NAV on CDI for
approach.
SLCT NON-MAG – Select alternate
NAV ANGLE display units.
STEEP TURN – Steep turn ahead.
SVS – SVS DISABLED: Out of
available terrain region.
SVS – SVS DISABLED: Terrain DB
resolution too low.
SW MISMATCH – GDU software
version mismatch. Xtalk is off.
TERRAIN AUD CFG – Trn
Awareness audio config error.
Service req’d.
Terrain audio alerts are not configured properly.
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
98
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Annunciations & Alerts
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Appendix
190-00600-05 Rev. C
Annun/
Alerts
Possible severe weather detected within +/- 10
degrees of the aircraft heading at a range of 80 to
320 nm.
Abnormal
Operation
WX ALERT – Possible severe
weather ahead.
Additional
Features
The current track angle error exceeds the limit,
causing the vertical deviation to go invalid.
The current crosstrack exceeds the limit, causing
vertical deviation to go invalid.
A parallel course has been selected, causing the
vertical deviation to go invalid.
Hazard
Avoidance
VNV – Unavailable. Excessive
track angle error.
VNV – Unavailable. Excessive
crosstrack error.
VNV – Unavailable. Parallel course
selected.
Procedures
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.
Flight
Planning
VNV – Unavailable. Unsupported
leg type in flight plan.
GPS Nav
UNABLE V WPT – Can’t reach
current vertical waypoint.
The current VNAV is not supported, the Flight
Director has reverted to PIT mode.
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.
AFCS
UNABLE PATH - Revert to PIT.
Nav/Com/
XPDR/Audio
TRN AUD FAIL – Trn Awareness
audio source unavailable.
TRUE APR – True north approach.
Change HDG reference to TRUE.
EICAS
TRAFFIC FAIL – Traffic device has
failed.
Comments
One of the terrain, or obstacle databases required
for TAWS in the specified PFD or MFD is missing or
invalid.
The system notifies the pilot that the timer has
expired.
The system is no longer receiving data from the
traffic system. The traffic device should be serviced.
The audio source for terrain awareness is offline.
Check GIA1 or GIA 2.
Displayed after passing the first waypoint of a true
north approach when the nav angle is set to ‘AUTO’.
Flight
Instruments
Message
TERRAIN DSP – [PFD1, PFD2 or
MFD1] Terrain awareness display
unavailable.
TIMER EXPIRD – Timer has expired.
99
Message
WPT ARRIVAL – Arriving at
waypoint -[xxxx]
Comments
Arriving at waypoint [xxxx], where [xxxx] is the
waypoint name.
XPDR1 CONFIG – XPDR1 config
error. Config service req’d.
The transponder configuration settings do not
match those of backup configuration memory. The
system should be serviced.
XPDR1 CTRL FAIL – XPDR1 not
receiving control information.
Transponder #1 is not receiving data from the
display units. The transponder will continue to
operate in the mode reported on the display, but
changes to mode and code are not possible. The
system should be serviced.
The Transponder 1 should be serviced when
possible.
The transponder configuration settings do not
match those of backup configuration memory. The
system should be serviced.
Transponder #2 is not receiving data from the
display units. The transponder will continue to
operate in the mode reported on the display, but
changes to mode and code are not possible. The
system should be serviced.
The Transponder 1 and/or 2 should be serviced
when possible.
The MFD and PFDs are not communicating with
each other. The system should be serviced.
XPDR1 SRVC – XPDR1 needs
service. Return unit for repair.
XPDR2 CONFIG – XPDR2 config
error. Config service req’d.
XPDR2 CTRL FAIL – XPDR2 not
receiving control information.
XPDR2 SRVC – XPDR2 needs
service. Return unit for repair.
XTALK ERROR – A flight display
crosstalk error 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
100
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Appendix
Flight
Instruments
APPENDIX
PFD SOFTKEY MAP
EICAS
ADF/DME
Nav/Com/
XPDR/Audio
CDI
CDI (NAV1)
CDI (NAV2)
AFCS
CDI (GPS)
Top Level PFD Softkeys
GPS Nav
(optional TCAS II)
(optional TCAS II)
TRFC/MAP
XPDR/TFC
ADF/DME
Flight
Planning
NEXRAD
TRFC-1
METAR
Procedures
WX LGND
TRFC-2
Level 1
Level 2
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
Annun/
Alerts
Appendix
OFF
Description
Abnormal
Operation
INSET or
TRFC/
MAP
Additional
Features
INSET Map Softkeys
Hazard
Avoidance
Select the BACK Softkey to return
to the top-level softkeys.
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
101
Level 1
Level 2
Description
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
WX LGND Displays icon and age on the Inset Map for the
selected weather products (optional)
Cycles through traffic display options:
TRAFFIC
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, terTOPO
rain, rivers, lakes) and elevation scale on Inset Map
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Appendix
Procedures
TERRAIN
Hazard
Avoidance
NEXRAD
XM LTNG
Abnormal
Operation
Additional
Features
METAR
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)
Displays METAR flags on airport symbols shown on
the Inset Map (optional)
Annun/
Alerts
ADF/DME
Press the BACK Softkey to
return to the top level softkeys.
Appendix
ADC1
ADC2
AHRS1
AHRS2
BACK
MSG
Index
Sensor Softkeys
102
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Appendix
Level 2
Description
Selects the #2 Air Data Computer
AHRS1
Selects the #1 AHRS
AHRS2
Selects the #2 AHRS
Nav/Com/
XPDR/Audio
ADC2
AFCS
ADF/DME
DME
GPS Nav
SYN VIS
ALT UNIT
GPS
GPS
OFF
OFF
METERS
Select the BACK Softkey
to return to the top-level softkeys
Procedures
NAV2
Flight
Planning
NAV1
EICAS
ADC1
Displays softkeys for selecting the #1 and #2 AHRS
and Air Data Computers
Selects the #1 Air Data Computer
SENSOR
Flight
Instruments
Level 1
IN
HPA
Hazard
Avoidance
Additional
Features
PATHWAY
SYN TERR HRZN HDG APTSIGNS
Level 2
Level 3
PFD
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
103
Index
PATHWAY
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
Appendix
SYN VIS
Description
Annun/
Alerts
Level 1
Abnormal
Operation
PFD Configuration Softkeys
Level 1
Level 2
Level 3
SYN TERR
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Appendix
DFLTS
Procedures
Flight
Planning
GPS Nav
WIND
Hazard
Avoidance
OFF
Abnormal
Operation
Additional
Features
DME
BRG1
Annun/
Alerts
BRG2
Appendix
ALT UNIT
METERS
Index
Enables synthetic terrain depiction
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
Displays softkeys to select wind data
parameters
Wind direction arrows with headwind
OPTN 1
and crosswind components
Wind direction arrow and speed
OPTN 2
OPTN 3
IN
104
Description
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
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Appendix
Level 2
Level 3
Description
Flight
Instruments
Level 1
Press to display the BARO setting as
hectopacals
HPA
GPS Nav
ADF/DME
AFCS
CDI
Nav/Com/
XPDR/Audio
OBS
EICAS
Flight
Planning
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
Displays the ADF/DME Tuning
Window, providing ADF tuning
capability (when installed) and
allowing selection of the NAV source
for tuning each DME
STD BARO
Procedures
ADF/DME
Hazard
Avoidance
Press the BACK Softkey to return
to the top-level softkeys.
MSG
Additional
Features
MSG
Level 1
Level 2
Level 3
Description
Selects the #2 transponder as active.
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Index
XPDR2
Appendix
XPDR1
Displays transponder mode selection
softkeys
Selects the #1 transponder as active.
XPDR
Annun/
Alerts
Transponder Softkeys
Abnormal
Operation
Selecting BACK returns to the previous softkey level.
105
Level 1
Level 2
Level 3
ALT
VFR
0—7
Airborne - (Green mode indication)
Generates Mode A, Mode C, and Mode
S replies as well as transmissions of
acquisition and extended squitters,
including ADS-B out.
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
BKSP
Removes numbers entered, one at a time
ON
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
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
Abnormal
Operation
Additional
Features
CODE
Index
Appendix
Annun/
Alerts
Description
Selects Standby Mode (transponder does
not reply to any interrogations)
Selects Mode A (transponder replies to
identification interrogations)
On Ground - (White mode indication)
Generates Mode S replies to discrete
interrogations as well as transmission
of acquisition and extended squitters,
including ADS-B out. Mode A, Mode C,
and Mode S all-call replies are inhibited
STBY
EICAS
Flight
Instruments
Appendix
106
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Appendix
PFD
OBS
CDI
(optional)
ADF/DME XPDR/TFC
IDENT
TMR/REF
NRST
MSG
XPDR1
XPDR2
MODE
TCAS
CODE
BACK
IDENT
MSG
REL
ABS
ALT RNG
TEST
BACK
MSG
AFCS
Selecting BACK returns to the
previous softkey level.
ABOVE NORMAL BELOW
UNREST
BACK
MSG
GPS Nav
Selecting BACK returns to the
previous softkey level.
STBY
ON
ALT
TA ONLY
TA/RA
BACK
MSG
Flight
Planning
Selecting BACK returns to the
previous softkey level.
1
3
2
4
5
6
7
IDENT
BKSP
BACK
MSG
Procedures
0
Transponder/Traffic Softkeys with TCAS II Option
Level 2
Level 3
XPDR1
STBY
107
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Appendix
190-00600-05 Rev. C
Annun/
Alerts
MODE
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.
Abnormal
Operation
XPDR2
Description
Additional
Features
XPDR/TFC
Level 4
Hazard
Avoidance
Level 1
Nav/Com/
XPDR/Audio
Selecting BACK returns to the
previous softkey level.
EICAS
Press the BACK Softkey to return
to the top-level softkeys.
Flight
Instruments
TRFC/MAP SENSOR
Level 1
Level 2
Level 3
ON
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Appendix
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
ALT
Abnormal
Operation
TA ONLY
Annun/
Alerts
TA/RA
Appendix
BACK
TCAS
Index
REL
108
Level 4
Description
Activates transponder
(transponder replies to
identification interrogations).
When the transponder is set to
ON, the TCAS II system is set
to standby.
On Ground - (White mode
indication)
Generates Mode S replies to
discrete interrogations as well
as transmission of acquisition
and extended squitters,
including ADS-B out. Mode A,
Mode C, and Mode S all-call
replies are inhibited
Airborne - (Green mode
indication)
Generates Mode A, Mode C,
and Mode S replies as well as
transmissions of acquisition
and extended squitters,
including ADS-B out.
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
Displays the TCAS control
softkeys
Displays intruder altitude as
altitude relative to own aircraft
altitude
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Appendix
Level 2
Level 3
ABS
ALT RNG
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
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
GPS Nav
0—7
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
AFCS
CODE
Displays intruder MSL altitude
Nav/Com/
XPDR/Audio
BACK
Description
EICAS
TEST
Level 4
Flight
Instruments
Level 1
Annun/
Alerts
Appendix
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
109
Level 1
Level 2
Level 3
Level 4
Nav/Com/
XPDR/Audio
BKSP
Procedures
Flight
Planning
GPS Nav
AFCS
IDENT
TMR/REF
NRST
MSG
MFD SOFTKEY MAP
(optional)
CAS ↑
CAS ↓
DCLTR
MAP
Additional
Features
Hazard
Avoidance
Description
Activates the Special Position
Identification (SPI) pulse for
18 seconds, identifying the
transponder return on the ATC
screen
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
IDENT
EICAS
Flight
Instruments
Appendix
SHW CHRT
DCLTR-1
Abnormal
Operation
DCLTR-2
DCLTR-3
Annun/
Alerts
TRAFFIC
PROFILE
TOPO
TERRAIN
AIRWAYS
Select the BACK Softkey on this level to
return to the top softkey level.
(optional) (optional) (optional)
NEXRAD
XM LTNG
LEGEND
METAR
WX RADAR
BACK
Appendix
AIRWY ON
AIRWY LO
Index
AIRWAY HI
MFD Softkeys
110
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Appendix
Level 2
CAS ↑
Description
Flight
Instruments
Level 1
CAS ↓
Nav/Com/
XPDR/Audio
MAP
EICAS
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
Displays/removes Profile View on Navigation Map
Page
Displays topographical data (e.g., coastlines,
terrain, rivers, lakes) and elevation scale on
Navigation Map
Displays terrain information on Navigation Map
TOPO
TERRAIN
Displays airways on the map; cycles through the
following:
AIRWAYS: No airways are displayed
AIRWY ON: All airways are displayed
AIRWY LO: Only low altitude airways are
displayed
AIRWY HI: Only high altitude airways are
displayed
Displays NEXRAD weather and coverage
NEXRAD
information on Navigation Map (optional feature)
XM LTNG Displays XM lightning information on Navigation
Map (optional feature)
Displays METAR flags on airport symbols shown on
METAR
the Navigation Map (optional)
Displays the legend for the selected weather
LEGEND
products. Available only when NEXRAD, XM LTNG,
PROFILE and/or METAR softkeys are selected.
WX RADAR Displays Airborne Weather Radar information on
the Navigation Map
Returns to top-level softkeys
BACK
Flight
Planning
PROFILE
GPS Nav
Displays traffic information on Navigation Map
AFCS
TRAFFIC
AIRWAYS
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
111
Hazard
Avoidance
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Procedures
190-00600-05 Rev. C
Level 1
DCLTR (3)
SHW
CHRT
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
CAUTION: Never disconnect power to the system when loading a database.
Power interruption during the database loading process could result in
maintenance being required to reboot the system.
NOTE: When loading database updates, the ‘DB Mismatch’ message will
be displayed until database synchronization is complete, followed by turning
system power off, then on. Synchronization can be monitored on the AUXSYSTEM STATUS Page.
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Description
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.
If an error occurs during synchronization, an error message will be displayed,
followed by the affected display in the Sync Status section of the Database Window. If
synchronization completes on one display, but an error occurs on another, the error
message will be displayed with the affected displays listed after it. When an error
message is displayed, the problem must be corrected before synchronization can be
completed. A power cycle is required to restart synchronization when ‘Card Full’ or
‘Err’ is shown.
Index
Appendix
Level 2
LOADING UPDATED DATABASES
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Appendix
112
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Appendix
Flight
Instruments
Error Message
Description
Canceled
Database synchronization has been canceled by removing the
bottom SD card in display being updated
Card Full
SD card does not contain sufficient memory
Err
Displayed for all other errors that may cause the synchronization
process to be halted
Timeout
System timed-out prior to the database transfer completing
EICAS
Nav/Com/
XPDR/Audio
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.
4)
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.
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)
Monitor the Sync Status in the Database Window. Wait for all databases to
complete synching, indicated by ‘Complete’ being displayed.
9)
Remove and reapply power to the system.
GPS Nav
1)
AFCS
Loading Garmin Database Updates
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
11) Turn the small FMS Knob to select the System Status Page.
Annun/
Alerts
Appendix
12) Press the Display Database Selection Softkey to show database information
for each display (MFD1 DB, PFD1 DB, PFD2 DB). Verify the correct
database cycle information is shown for each database for each display.
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
113
Loading the Jeppesen Navigation Database as the Active Navigation
Database
The Jeppesen Navigation Database that is loaded to internal memory as the active
database will be used by the system.
NOTE: Loading the Jeppesen navigation database as the active 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 amber.
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Appendix
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
NOTE: After the navigation database is loaded or copied, the top SD card
may be removed.
1)
With the system OFF, insert the SD card containing the new navigation database
version into the top card slot of the display (PFD1, PFD2 or MFD) to be updated
(label of SD card facing left).
2)
Turn the system ON. A prompt is displayed in the upper left corner of the
display:
3)
4)
Press the NO Softkey to proceed to loading the active database.
A prompt similar to the following is displayed. Press the YES Softkey to update
the active navigation database.
5)
After the update completes, the display starts in normal mode.
6)
Turn the system OFF and remove the SD card from the top card slot.
7)
Repeat steps 1 through 6 for the other displays (PFD1, PFD2 or MFD).
8)
Apply power to the system and press the ENT Key to acknowledge the startup
screen.
9)
Turn the large FMS Knob to select the AUX Page group on the MFD.
Annun/
Alerts
10) Turn the small FMS Knob to select the System Status Page.
Index
Appendix
11) Press the Display Database Selection Softkey to show active navigation
database information for each display (MFD1 DB, PFD1 DB, PFD2 DB). Verify
the correct active navigation database cycle information is shown for each
display.
114
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Appendix
EICAS
The purpose of the Standby Navigation Database is to allow the loading of the
next cycle of the Jeppesen Navigation Database to the bottom SD card, prior to its
effective date. (The Jeppesen Navigation Database is available from Jeppesen seven
days prior to its effective date.)
Flight
Instruments
Loading the Jeppesen Navigation Database as the Standby Navigation
Database
Nav/Com/
XPDR/Audio
NOTE: After the navigation database is loaded or copied, the top SD card
may be removed.
AFCS
With the system OFF, insert the SD card containing the new navigation
database version into the top card slot of the MFD.
2)
Verify that an SD card is inserted in the bottom slot of each PFD and the
MFD.
3)
Turn the system ON. A prompt is displayed.
4)
Press the YES Softkey. The navigation database is copied to the SD card in
the bottom card slot of the MFD.
5)
After the navigation database files are copied to the bottom SD card, press
any key to continue, as instructed.
Again, press any key to continue as instructed on the display.
9)
Turn the large FMS Knob to select the AUX Page group on the MFD.
Abnormal
Operation
Press the ENT Key to acknowledge the startup screen.
Additional
Features
8)
Hazard
Avoidance
Press the NO Softkey. The display now starts in normal mode. Since the
database effective date is not yet valid, it should not be loaded as the
active database. The display now starts in normal mode. Do not remove
power while the display is starting.
Procedures
7)
Flight
Planning
6)
GPS Nav
1)
10) Turn the small FMS Knob to select the System Status Page.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
115
Index
190-00600-05 Rev. C
Appendix
NOTE: During the synchronization process, version differences between
standby navigation databases will exist. This will result in the system
displaying a ‘DB Mismatch’ alert for the standby navigation databases. This
alert will remain until the next power cycle.
Annun/
Alerts
11) The new database is copied to the SD card in the bottom card slot of each
PFD. Progress can be monitored in the SYNC STATUS field. When copying
is finished, ‘Complete’ is displayed.
Appendix
Flight
Instruments
12) Turn system power OFF.
13) Remove the SD card from the top card slot of the MFD.
14) Turn system power ON.
EICAS
15) Press the ENT Key to acknowledge the startup screen.
16) Turn the large FMS Knob to select the AUX Page group on the MFD.
Nav/Com/
XPDR/Audio
17) Turn the small FMS Knob to select the System Status Page.
Magnetic Field Variation Database Update
At startup, the system compares this version of the MV DB with that presently being
used by each AHRS (GRS1 and GRS2). If the system determines the MV DB needs
to be updated, a prompt is displayed on the Navigation Map Page, as shown in the
following figure. Note, in the following example, GRS1 is the first AHRS to indicate
an update is available. In actuality, this is dependent on which AHRS is the first to
report status to the system. GRS2 may be displayed before GRS1. The order is not
important, only that both AHRS be updated.
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
18) Press the Display Database Selection Softkey to show standby navigation
database information for each display (MFD1 DB, PFD1 DB, PFD2 DB).
Verify the correct standby navigation database cycle information is shown
for each display.
Abnormal
Operation
GRS1 Magnetic Field Variation Database Update Prompt
Index
Appendix
Annun/
Alerts
Loading the magnetic field variation database update:
1) With ‘OK’ highlighted, as shown in the previous figure, press the ENT Key
on the MFD. A progress monitor is displayed as shown in the following
figure.
116
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Appendix
Flight
Instruments
EICAS
Nav/Com/
XPDR/Audio
2)
AFCS
Uploading Database to GRS1
GPS Nav
When the upload is complete, the prompt for the next GRS upload is
displayed, as seen in the following figure.
Flight
Planning
Procedures
GRS2 Magnetic Field Variation Database Update Prompt
Additional
Features
With ‘OK’ highlighted, press the ENT Key on the MFD. A progress monitor
is displayed as shown in the following figure. When the upload is complete,
the system is ready for use.
Hazard
Avoidance
3)
Abnormal
Operation
Annun/
Alerts
Appendix
Uploading Database to GRS2
Index
190-00600-05 Rev. C
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
117
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Appendix
Blank Page
118
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Index
D
DB Mismatch 112, 115
DCLTR Softkey 63
Dead Reckoning 71
Declutter 70, 102, 112
Designated altitudes 19
Direct-to 15
DME 7, 9
DR mode 71, 72
GPS Nav
Flight
Planning
Procedures
E
Edit a flight plan 37
Engine display 5
Hazard
Avoidance
F
Additional
Features
Flight Director 11
Flight ID 7
Flight path marker 61
FliteCharts® 63, 64
Frequency Transfer 9
Abnormal
Operation
G
Annun/
Alerts
Gain 52
Ground mapping 53
Cabin pressure altitude 5
CDI 1, 2, 9, 98
Channel Presets 67
Horizon heading 61
Horizontal scan 52
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Index
H
Appendix
C
190-00600-05 Rev. C
AFCS
Barometric Altitude Minimums 3
Barometric pressure 105
Bearing line 52, 53
Nav/Com/
XPDR/Audio
B
EICAS
Activate a flight plan 16
Active Channel 65
Active database 114
Active Navigation Database 114
AC-U-KWIK Airport Directory 65
ADF 7, 9
AHRS 77, 83, 84, 87, 88, 90, 92, 103,
116
AIREP 49
AIRMET 48, 49
Airport Directory 65
Airport Signs 61, 62
Airways 111
Air Data Computer 76
ALT 56
Altimeter setting 1
Altitude mode 56
Altitude volume 56
Antenna stabilization 54
Antenna tilt 51
AOPA Airport Directory 65
Attitude & Heading Reference System
76, 77
Audio Panel 69
Audio panel controls
NAV1, NAV2 9
ChartView 63
Clearance player 10
Clearance Recorder 10
Code selection softkeys 8
COM 8, 9, 10, 69
Crew Alerting System (CAS)
Messages 6–7
Flight
Instruments
A
Index-1
I
P
Inhibit 60
Inhibit TAWS 60
Inset Map 101, 102
Intercom isolation 9
IOI 77, 78
Pathways 61, 62
PIREP 50
PIT 76
Play 10
Profile View 111
J
Q
Jeppesen 63
Quick Select Box 18, 29, 31, 32, 33, 35,
36, 37, 41, 42
M
Magnetic Field Variation Database 116,
117
Map panning 48
Message advisories 82
METAR 47, 48, 49, 102, 111
Minimums 81
MISCOMP 76
Multi Function Display (MFD)
Softkeys 110
N
NAV 9
NAV1 2, 9
NAV2 2, 9
Navigation database 18, 19, 81, 85,
86, 87, 93, 96, 97
Nearest
VRP 23
NEXRAD 47, 102, 111
O
OBS 2
Obstacles 86, 92
Overspeed Protection 12
R
Resolution Advisory 55, 62
Reversionary mode 69
Reversionary Mode
EICAS 5
ROC 77, 78
S
SafeTaxi® 61, 63
SBAS 12, 43, 60, 71, 72, 84, 92
Sector scan 53
Sensor 76
SIGMET 48, 49
STAB 54
Standby 51
Standby Navigation Database 115
Store Flight Plan 37
SVS 98
SVT 61
Synchronization 113
SYNC Status 115
Synthetic Vision System 61
T
TAF 47
TAS 56, 83, 84
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Index
Index-2
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-05 Rev. C
Index
Flight
Instruments
TAWS 58, 59, 60, 77
TAWS-A 77, 102
TAWS-B 58
TCAS II 8, 57, 58, 62, 101, 106, 107,
108
TEMP COMP 18
Terrain 58, 86, 102, 111
TFR 48, 50
Tilt line 51
Timer 2, 99
Topographical data 102, 111
Traffic 47, 55, 57, 111
Traffic Advisory 55
Traffic map page 55, 56, 57, 58
Transponder 7, 8, 105, 106, 107, 108,
109, 110
EICAS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
V
Procedures
Vertical speed guidance 19
Vertical track 81
VNV 15, 70, 99
VRP 23
Vspeed 2
Hazard
Avoidance
Additional
Features
W
Abnormal
Operation
WATCH® 54
Waypoint Selection Submenu 29, 30
Weather Attenuated Color Highlight 54
Weather data link page 48
Weather radar 50
Weather Radar Overlay 51, 111
Wind data 104
Annun/
Alerts
Appendix
X
XM lightning 102, 111
Index
190-00600-05 Rev. C
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
190-00600-05 Rev. C
Garmin International, Inc.
1200 East 151st Street
Olathe, Kansas 66062, U.S.A.
Tel: 913.397.8200
Fax: 913.397.8282
Aircraft On Ground (AOG) Hotline: 913.397.0836
Aviation Dealer Technical Support: 888.606.5482
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Tel: 503.581.8101
Fax 503.364.2138
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
Tel: +44 (0) 238 052 4000
Fax: +44 (0) 238 052 4004
Aviation Support: +44 (0) 370 850 1243
Garmin Corporation
No. 68, Zhangshu 2nd Road
Xizhi District, New Taipei City, Taiwan
Tel: 34-93-357-2608
Fax: 34-93-429-4484
www.garmin.com
© 2006-2011, 2016 Garmin Ltd. or its subsidiaries
190-00600-05 Rev. C
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