Garmin Cessna Citation Mustang Reference Guide

®
G1000
Cockpit Reference Guide for the Cessna Citation Mustang
Integrated Flight Deck
FLIGHT INSTRUMENTS
EICAS
NAV/COM/TRANSPONDER/AUDIO PANEL
AUTOMATIC FLIGHT CONTROL SYSTEM
FLIGHT PLANNING
PROCEDURES
HAZARD AVOIDANCE
ADDITIONAL FEATURES
ABNORMAL OPERATION
ANNUNCIATIONS & ALERTS
APPENDIX
INDEX
Copyright © 2006-2010 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0435.20 or later for the Cessna Citation Mustang. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions.
Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A. Tel: 503/391.3411 Fax 503/364.2138
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Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan Tel: 886/02.2642.9199 Fax: 886/02.2642.9099
For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836.
Web Site Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin® is a registered trademark of Garmin Ltd. or its subsidiaries. WATCH®, FliteCharts®, and SafeTaxi® are trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin.
NavData® is a registered trademark of Jeppesen, Inc.; and XM® is a registered trademark of XM Satellite Radio, Inc.; Honeywell® and Bendix/King® are registered trademarks of Honeywell International, Inc.; CO Guardian is a trademark of CO Guardian, Inc.
June, 2010 190-00600-03 Rev. A Printed in the U.S.A.
Warnings, Cautions & Notes
WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from third party sources. Garmin is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical charts for appropriate minimum clearance altitudes.
WARNING: The altitude calculated by the GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74B Air Data Computer, or other altimeters in the aircraft. GPS altitude should never be used for vertical navigation. Always use pressure altitude displayed by the PFD or other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in the system must be updated regularly in order to ensure that the information remains current. Pilots using any outdated database do so entirely at their own risk.
WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness.
WARNING: Traffic information shown on system displays is provided as an aid in visually acquiring traffic. Pilots must maneuver the aircraft based upon TCAS II Resolution Advisories (if installed), ATC guidance, or positive visual acquisition of conflicting traffic.
WARNING: XM Weather should not be used for hazardous weather penetration. Weather information provided by the GDL 69A is approved only
for weather avoidance, not penetration.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Warnings, Cautions & Notes
WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for short-range
weather avoidance.
WARNING: The G1000 Integrated Flight Deck, as installed in the Cessna Citation Mustang aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self­test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the system. It is thus the responsibility of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated information available in the cockpit.
WARNING: For safety reasons, system operational procedures must be learned on the ground.
WARNING: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or misinterpreted and, therefore, become unsafe.
WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000 Pilot’s Guide documentation and the Cessna Citation Mustang Airplane Flight Manual. Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the system to all available navigation sources, including the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation.
WARNING: The illustrations in this guide are only examples. Never use the system to attempt to penetrate a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo.”
190-00600-03 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Warnings, Cautions & Notes
WARNING: Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/aboutGarmin/ environment/disposal.jsp.
WARNING: Because of variation in the earth’s magnetic field, operating the system within the following areas could result in loss of reliable attitude and heading indications. North of 72° North latitude at all longitudes. South of 70° South latitude at all longitudes. North of 65° North latitude between longitude 75° W and 120° W. (Northern Canada). North of 70° North latitude between longitude 70° W and 128° W. (Northern Canada). North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia). South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand).
WARNING: Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned in error as displayed.
CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI­REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti­reflective coatings.
CAUTION: The system does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations.
NOTE: All visual depictions contained within this document, including screen images of the panel and displays, are subject to change and may not reflect the most current system and databases. Depictions of equipment may differ slightly from the actual equipment.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Warnings, Cautions & Notes
NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) this device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation.
NOTE: The data contained in the terrain and obstacle databases comes from government agencies. Garmin accurately processes and cross-validates the data, but cannot guarantee the accuracy and completeness of the data.
NOTE: This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition
65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65.
NOTE: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition.
NOTE: Use of polarized eyewear may cause the flight displays to appear dim or blank.
NOTE: The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide. Complete operating procedures for the system are found in the G1000 Integrated Flight Deck Pilot’s Guide.
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Warnings, Cautions & Notes
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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
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Record of Revisions
Part Number Change Summary
190-00600-00
Rev A
Initial release
Rev B
Added Additional Features section
190-00600-01
Rev A
Rev B
Rev C
Production release
Added CAS INOP system messages
Added COM 3 function for HF Added TAS Removed automatic Reversionary Mode operation
190-00600-02
Rev A Added Synthetic Vision
Added other GDU 9.01 parameters
190-00600-03 Added GDU 10.01 parameters
Added GSD 41 Added GMA -20 Added new page navigation TCAS II Radar Altimeter Added AOPA Airport Directory Added dual navigation database capability Added database synchronization
Revision Date of Revision Affected Pages Description
A June, 2010 All Production release
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Table of Contents
FLIGHT INSTRUMENTS ................................................................................................................ 1
Selecting the Altimeter Barometric Pressure Setting ...................................................... 1
Selecting Standard Barometric Pressure .............................................................................1
Change Altimeter Barometric Pressure Setting Units ...................................................... 1
Synchronizing the Altimeter Barometric Pressure Settings ........................................... 1
Synchronize CDI......................................................................................................................... 1
Change Navigation Sources ................................................................................................... 2
Enable/Disable OBS Mode While Navigating with GPS .................................................... 2
Generic Timer ............................................................................................................................. 2
Configure Vspeed Bugs Individually ..................................................................................... 2
Turn Vspeed Bugs On or Off by Category ............................................................................ 3
Set Barometric/Radar Altimeter (RA Optional) Minimum Descent Altitude ............... 3
Displaying Wind Data ..............................................................................................................3
ENGINE INDICATION & CREW ALERTING SYSTEM .......................................................5
Crew Alerting System (CAS) ................................................................................................... 6
CAS Messages and Prioritization .......................................................................................... 6
NAV/COM/TRANSPONDER/AUDIO PANEL ......................................................................... 7
Enter or Change Flight ID ....................................................................................................... 7
ADF Tuning (Optional) .............................................................................................................. 7
DME Tuning................................................................................................................................. 7
Enter a Transponder Code....................................................................................................... 8
Select Transponder Mode ....................................................................................................... 8
Selecting a COM Radio ............................................................................................................ 8
Selecting a NAV Radio ............................................................................................................. 9
NAV/COM Tuning ....................................................................................................................... 9
Intercom System (ICS) Isolation .......................................................................................... 10
Passenger Address (PA) System ........................................................................................... 10
Clearance Recorder and Player ...........................................................................................11
AUTOMATIC FLIGHT CONTROL SYSTEM .......................................................................... 13
Flight Director Activation ..................................................................................................... 13
Vertical Modes ......................................................................................................................... 14
Lateral Modes .......................................................................................................................... 15
GPS NAVIGATION ........................................................................................................................ 17
Direct-to Navigation .............................................................................................................. 17
Activate a Stored Flight Plan ............................................................................................... 18
Activate a Flight Plan Leg ..................................................................................................... 18
Stop Navigating a Flight Plan .............................................................................................. 19
Vertical Navigation (VNAV)................................................................................................... 19
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Table of Contents
FLIGHT PLANNING ...................................................................................................................... 21
Weight Planning ...................................................................................................................... 21
Trip Planning ............................................................................................................................ 21
Create a New User Waypoint Defined by Latitude & Longitude ................................. 23
Create a New User Waypoint Defined by Radials from Other Waypoints ................. 24
Create a New User Waypoint Defined by a Radial & Distance from Another
Waypoint ............................................................................................................................. 26
Delete a User Waypoint ......................................................................................................... 27
Create a New Flight Plan ...................................................................................................... 28
Import a Flight Plan from an SD Card ................................................................................ 29
Insert a Waypoint in the Active Flight Plan ...................................................................... 29
Enter an Airway in a Flight Plan .......................................................................................... 30
Invert An Active Flight Plan .................................................................................................. 31
Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 31
Store a Flight Plan .................................................................................................................. 32
Edit a Stored Flight Plan ....................................................................................................... 32
Delete a Waypoint from the Flight Plan ............................................................................ 32
Invert and Activate a Stored Flight Plan ........................................................................... 33
Copy a Flight Plan ................................................................................................................... 33
Delete a Flight Plan ................................................................................................................ 33
Graphical Flight Plan Creation ............................................................................................. 34
Export a Flight Plan to an SD Card ..................................................................................... 34
PROCEDURES ................................................................................................................................. 35
Load and Activate a Departure Procedure ....................................................................... 35
Activate A Departure Leg ..................................................................................................... 35
Load An Arrival Procedure .................................................................................................... 35
Activate An Arrival Leg ......................................................................................................... 36
Load and/or Activate an Approach Procedure ................................................................. 36
Activate An Approach in the Active Flight Plan ............................................................... 37
Activate a Vector to Final Approach Fix ............................................................................ 37
Activate A Missed Approach in the Active Flight Plan ................................................... 38
HAZARD AVOIDANCE ................................................................................................................39
Customizing the Hazard Displays on the Navigation Map ............................................ 39
XM Weather (Subscription Optional) ................................................................................. 39
Traffic Systems ........................................................................................................................ 41
Terrain Awareness & Warning System (TAWS-B).............................................................. 45
Airborne Color Weather Radar ............................................................................................ 47
ADDITIONAL FEATURES ........................................................................................................... 51
Synthetic Vision (Optional) ................................................................................................... 51
Terminal Procedure Charts ...................................................................................................53
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Table of Contents
AOPA Airport Directory ......................................................................................................... 55
XM® Radio Entertainment (Subscription Optional) ........................................................ 55
ABNORMAL OPERATION..........................................................................................................59
Reversionary Mode ................................................................................................................ 59
Abnormal COM Operation .................................................................................................... 59
Audio Panel Fail-safe Operation.......................................................................................... 59
Hazard Displays with Loss of GPS Position ....................................................................... 60
Unusual Attitudes ................................................................................................................... 60
Dead Reckoning ...................................................................................................................... 61
ANNUNCIATIONS & ALERTS ................................................................................................... 63
CAS Messages .......................................................................................................................... 63
Comparator Annunciations ................................................................................................... 65
Reversionary Sensor Annunciations ................................................................................... 66
TAWS-B Alerts .......................................................................................................................... 67
TCAS II Alerts and Annunciations ........................................................................................ 68
Aural Alerts .............................................................................................................................. 70
Flight Plan Import/Export Messages .................................................................................. 70
MFD & PFD Message Advisories .......................................................................................... 72
Database Message Advisories ............................................................................................. 73
GMA 1347D/1347D-20 Message Advisories ....................................................................... 76
GIA 63W Message Advisories ............................................................................................... 77
GSD 41 Message Advisories.................................................................................................. 79
GEA 71 Message Advisories .................................................................................................. 80
GTX 33/33D Message Advisories .......................................................................................... 80
GRS 77 Message Advisories .................................................................................................. 81
GMU 44 Message Advisories ................................................................................................ 82
GDL 69A Message Advisories ............................................................................................... 83
GWX 68 Alert Messages ......................................................................................................... 83
GDC 74B Message Advisories ............................................................................................... 84
GCU 475 Message Advisories ............................................................................................... 84
GMC 710 Message Advisories .............................................................................................. 85
Miscellaneous Message Advisories ..................................................................................... 85
APPENDIX ....................................................................................................................................... 91
PFD Softkey Map .................................................................................................................... 91
MFD Softkey Map ................................................................................................................... 99
Database Updates ................................................................................................................ 101
INDEX .........................................................................................................................................Index-1
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190-00600-03 Rev. A

Flight Instruments

FLIGHT INSTRUMENTS

SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING

Turn the BARO Knob to select the desired setting.

SELECTING STANDARD BAROMETRIC PRESSURE

Press the BARO Knob.

CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS

1)
Press the PFD Softkey to display the second-level softkeys.
2)
Press the ALT UNIT Softkey.
3)
Press the IN Softkey to display the barometric pressure setting in inches of mercury (in Hg).
Or
:
Press the HPA Softkey to display the barometric pressure setting in hectopascals.
4)
Press the BACK Softkey to return to the top-level softkeys.

SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS

Instruments EICAS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
1)
Select the AUX-SYSTEM SETUP Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight BARO in the SYNCHRONIZATION Window.
4)
Turn the
small
FMS Knob clockwise to ON or counterclockwise to OFF.

SYNCHRONIZE CDI

1)
Select the AUX-SYSTEM SETUP Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window.
4)
Turn the
190-00600-03 Rev. A 1
small
FMS Knob clockwise to ON or counterclockwise to OFF.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
Flight Instruments

CHANGE NAVIGATION SOURCES

Flight
InstrumentsEICAS
1)
Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD.
2)
Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This places the light blue tuning box over the NAV2 standby
Nav/Com/
XPDR/AudioAFCSGPS Nav
frequency.
3)
Press the CDI Softkey a third time to return to GPS.

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

1)
Press the OBS Softkey to select OBS Mode.
2)
Turn the CRS Knob to select the desired course to/from the waypoint. Press the CRS Knob to slew the CDI Course Pointer to a course bearing directly to the waypoint.
Flight
PlanningProcedures
3)
Press the OBS Softkey again to disable OBS Mode.

GENERIC TIMER

1)
Press the TMR/REF Softkey, then turn the large FMS Knob to select the time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then
Hazard
Avoidance
Features
Additional
Abnormal
Operation
press the ENT Key. The UP/DOWN field is now highlighted.
2)
Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now highlighted.
3)
Press the ENT Key to START, STOP, or RESET the timer (if the timer is counting DOWN, it will start counting UP after reaching zero). Press the CLR Key or the TMR/REF Softkey to remove the window.

CONFIGURE VSPEED BUGS INDIVIDUALLY

AlertsAppendixIndex
Annun/
1)
Press the TMR/REF Softkey.
2)
Turn the
3)
Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
large
FMS Knob to highlight the desired Vspeed.
speed has been changed from a default value, an asterisk appears next to the speed).
2
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Flight Instruments
4)
Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF field.
5)
Turn the
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
small
FMS Knob clockwise to ON or counterclockwise to OFF.

TURN VSPEED BUGS ON OR OFF BY CATEGORY

1)
Press the TMR/REF Softkey.
2)
Press the MENU Key.
3)
Turn the FMS Knob to highlight the desired option.
4)
Press the ENT Key. Press the TMR/REF Softkey to remove the window.
SET BAROMETRIC/RADAR ALTIMETER (RA OPTIONAL) MINIMUM DESCENT
ALTITUDE
1)
Press the TMR/REF Softkey.
2)
Turn the large FMS Knob to highlight the OFF/BARO/RAD ALT field to the right of ‘MINIMUMS’.
3)
Turn the small FMS Knob clockwise to select BARO or RAD ALT.
4)
Press the ENT Key.
5)
Use the small FMS Knob to enter the desired altitude.
6)
Press the ENT Key.
7)
To remove the window, press the CLR Key or the TMR/REF Softkey.
Instruments EICAS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features

DISPLAYING WIND DATA

1)
Press the PFD Softkey.
2)
Press the WIND Softkey to display wind data below the Selected Heading.
3)
Press one of the OPTN softkeys to change how wind data is displayed.
4)
To remove the Wind Data Window, press the OFF Softkey.
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Operation
Abnormal
Annun/
Alerts Appendix Index
Flight Instruments
Flight
InstrumentsEICAS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
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Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
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EICAS

ENGINE INDICATION & CREW ALERTING SYSTEM

Instruments EICAS
Flight
1
2
5
6
1
XPDR/Audio AFCS GPS Nav
Nav/Com/
5
7
3
Planning Procedures
Flight
8
6
2
Avoidance
4
9
3
7
Hazard
Additional
Features
10
8
10
EICAS Display (Normal Mode)
1
Engine Fan Rotation Speed
2
Oil Pressure & Speed
5
Interstage Turbine Temperature
6
Engine High Pressure
EIS Display (Reversionary Mode)
8
Cabin Pressure Altitude and Change Rate
9
Trim Indicator
Turbine Rotation
3
Fuel Display
4
CAS Display
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Speed
7
Electrical Display
10
Flap Indicator
Operation
Abnormal
Annun/
Alerts Appendix Index
EICAS

CREW ALERTING SYSTEM (CAS)

Flight
InstrumentsEICAS
NOTE: Refer to the Annunciations and Alerts section for specific CAS
messages.
NOTE: Refer to the Airplane Flight Manual (AFM) for emergency procedures.
Nav/Com/
XPDR/AudioAFCSGPS Nav
NOTE: If there is a mismatch between databases or software on the PFDs,
CAS is inoperative.
When CAS messages are present while in reversionary mode, the CAS Window ap-
pears on the display along with the flight instruments and EIS.
Flight
PlanningProcedures
CAS Display
Hazard
Avoidance
Features
Additional

CAS MESSAGES AND PRIORITIZATION

Abnormal
Operation
NOTE: Information on CAS messages in this pilot’s guide is always superseded
AlertsAppendixIndex
Annun/
by the AFM.
• Warning (red) – Immediate crew awareness and action required; Master Warning triggered
• Caution (yellow) – Immediate crew awareness and possible future corrective action required; Master Caution triggered
• Advisory (white) – Crew awareness required and subsequent action may be required
CAS Window
Reversionary ModeNormal Mode
CAS Messages
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NAV/COM/TRANSPONDER/AUDIO PANEL

ENTER OR CHANGE FLIGHT ID

1)
Press the TMR/REF Softkey, then turn the large FMS Knob to highlight the Flight ID field.
2)
Turn the small FMS Knob to enter the first character.
3)
Turn the large FMS Knob to select the next field.
4)
Turn the small FMS Knob to enter the next desired character.
5)
Repeat steps 3 and 4 until the desired Flight ID is entered.
6)
Press the ENT Key to update the Flight ID.

ADF TUNING (OPTIONAL)

Nav/Com/XPDR/Audio Panel
Instruments EICAS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
1)
Press the ADF/DME Softkey.
2)
Turn the small FMS Knob to enter the first digit of the desired ADF frequency.
3)
Turn the large FMS Knob to select the next desired field.
4)
Turn the small FMS Knob to enter the desired number.
5)
Repeat steps 3 and 4 until the desired ADF frequency is entered.
6)
Press the ENT Key to accept the new frequency.
7)
Press the ENT Key again to transfer the frequency to the active field.
8)
Turn the large FMS Knob to select the MODE field.
9)
Turn the small FMS Knob to select ANT, ADF, ADF/BFO, or ANT/BFO.
10)
Press the ENT Key to complete the selection.

DME TUNING

1)
Press the ADF/DME Softkey.
2)
If two DMEs are installed, turn the large FMS to select the DME source field.
3)
Turn the small FMS Knob to select the desired Nav radio.
4)
Press the ENT Key to complete the selection.
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Nav/Com/XPDR/Audio Panel

ENTER A TRANSPONDER CODE

Flight
InstrumentsEICAS
1)
Press the XPDR Softkey (XPDR/TFC if the TCAS II option is available).
2)
Press the CODE Softkey to display the transponder code selection softkeys, for digit entry.
3)
Press the digit softkeys to enter the code in the code field. When entering the code, the next key in sequence must be pressed within 10 seconds, or
Nav/Com/
XPDR/AudioAFCSGPS Nav
the entry is cancelled and restored to the previous code. Five seconds after the fourth digit has been entered, the transponder code becomes active.

SELECT TRANSPONDER MODE

With TCAS II Option
1)
Press the XPDR/TFC Softkey.
2)
Press the MODE Softkey to display the transponder mode selection
Flight
PlanningProcedures
softkeys.
3)
Press the desired transponder mode softkey (STBY, ON, or ALT ).
Without TCAS II Option
1)
Press the XPDR Softkey.
2)
Hazard
Avoidance
If the aircraft is equipped with two transponders, press the XPDR1 or XPDR2 Softkey to select the active transponder.
3)
Press the desired transponder mode softkey (STBY, ON, ALT, or GND).
Features
Additional

SELECTING A COM RADIO

Transmit/Receive
Abnormal
Operation
AlertsAppendixIndex
Annun/
Receive Only
8
Press the COM1 MIC, COM2 MIC
, or
COM3 MIC Key (HF, if installed) on
the audio panel.
Press the COM1, COM2
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
, or
COM3 Key (HF, if installed) on the audio panel.
190-00600-03 Rev. A
Nav/Com/XPDR/Audio Panel

SELECTING A NAV RADIO

1)
To begin navigating using a navigation radio, press the CDI Softkey on the PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).
2)
Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or deselect the navigation radio audio source. All radio keys can be selected individually or together.

NAV/COM TUNING

1)
Turn the respective tuning knobs to enter the desired frequency into the standby frequency field. The large knob enters MHz and the small knob enters kHz.
2)
Press the appropriate Frequency Transfer Key to place the frequency into the active frequency field.
Or
:
1)
Press the COM or NAV Key on the MFD/PFD Control Unit to select the desired COM or NAV frequency box.
2)
Turn the FMS Knob to tune the desired frequency (large knob for MHz; small knob for kHz).
3)
Press the
Frequency Transfer
Key to transfer the frequency to the active field.
Instruments EICAS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
190-00600-03 Rev. A 9
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
Nav/Com/XPDR/Audio Panel

INTERCOM SYSTEM (ICS) ISOLATION

Flight
Pressing the INTR COM Key on either Audio Panel selects and deselects the
InstrumentsEICAS
intercom on both Audio Panels. The annunciator is lit when the intercom is active. The intercom connects the pilot and copilot together. Either the pilot or copilot may select or deselect the intercom.
The MAN SQ Key allows either automatic or manual control of the intercom squelch setting. Pressing the MAN SQ Key enables manual squelch control, indicated by the MAN SQ annunciator.
Nav/Com/
XPDR/AudioAFCSGPS Nav
• WhentheMANSQAnnunciatorisextinguished(AutomaticSquelchison),
the ICS Knob controls only the volume (pressing the ICS Knob has no effect on the VOL/SQ selection).
• Whenthe MANSQAnnunciatorisilluminated (Manual Squelch),theICS Knob controls either volume or squelch (selected by pressing the ICS Knob and indicated by the VOL or SQ annunciation).
Cabin Address (GMA 1347D-20 only)
Flight
PlanningProcedures
The CABIN Key initiates two way communication between the pilot or copilot and the passengers in the cabin. The annunciator is lit when the cabin intercom is active on either Audio Panel.
When the flight crew wants to communicate with the passengers, the pilot or copilot presses the CABIN Key to signal that communication is desired. The cabin signal must be acknowledged to begin intercom conversation.
Hazard
Avoidance
When the passengers want to communicate with the pilot/copilot, they press the “COCKPIT CALL” switch at their seat in the cabin. The CABIN annunciator flashes on both Audio Panels to signal the pilot and copilot that cabin communication is desired.
Features
Additional
The cockpit call signal must be acknowledged by pressing the CABIN Key to begin intercom conversation.
Abnormal
Operation

PASSENGER ADDRESS (PA) SYSTEM

A passenger address system is provided by pressing the PA Key to deliver messages
AlertsAppendixIndex
Annun/
to the passengers. The message is heard by the other pilot on the cockpit speaker (if selected on) or on the headset if the PA Key is enabled on both audio panels. PA messages are one way from the flight deck to the passengers.
10
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
Nav/Com/XPDR/Audio Panel

CLEARANCE RECORDER AND PLAYER

GMA 1347D
NOTE: Only the audio for the selected not recorded for COM3 MIC.
Record
1)
Press the REC Key to begin recording.
2)
Press the REC Key again to stop recording.
Play
1)
Press the PLAY Key once to play the latest recorded memory block.
2)
Press the PLAY Key once while playing to stop.
3)
Press the PLAY Key twice quickly while playing to begin playing the previously recorded block.
Each subsequent two presses will skip back to
the previously recorded block.
GMA 1347D-20
COM MIC
Key is recorded. Audio is
Instruments EICAS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Planning Procedures
Flight
Avoidance
Hazard
NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio
to the Pilot. Pressing the play key on the Copilot’s Audio Panel plays recorded audio to the Copilot.
COM audio is recorded automatically. Recorded audio is stored in separate memory blocks. Once 2.5 minutes of recording time have been reached, the recorder begins recording over the stored memory blocks, starting from the oldest block.
The PLAY Key controls the play function. The PLAY annunciator is illuminated to
indicatewhenplayisinprogress.ThePLAYannunciatorextinguishesafterplayback
is finished.
Pressing the PLAY Key once plays the latest recorded memory block and then returns to normal operation. Pressing the PLAY Key again during play of a memory block stops play. If a COM input signal is detected during play of a recorded memory block, play is halted.
190-00600-03 Rev. A 11
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
Nav/Com/XPDR/Audio Panel
Pressing the PLAY Key twice within one-half second while audio is playing plays
the previous block of recorded audio. Each subsequent two presses of the PLAY Key
Flight
InstrumentsEICAS
within one-half second backtracks through the recorded memory blocks to reach and play any recorded block.
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
12
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A

AUTOMATIC FLIGHT CONTROL SYSTEM

NOTE: If sensor information (other than attitude) required for a flight director mode becomes invalid or unavailable, the flight director automatically reverts to the default mode for that axis.
NOTE: If the attitude information required for the default flight director modes becomes invalid or unavailable, the autopilot automatically disengages.

FLIGHT DIRECTOR ACTIVATION

An initial press of a key listed in the following table (when the flight director is not active) activates the pilot-side flight director in the listed modes.
AFCS
Instruments EICAS
Flight
XPDR/Audio AFCS GPS Nav
Nav/Com/
Control Pressed
Modes Selected
Lateral Vertical FD Key Roll Hold (default) ROL Pitch Hold (default) PIT AP Key Roll Hold (default) ROL Pitch Hold (default) PIT
CWS Button Roll Hold (default) ROL Pitch Hold (default) PIT
GA Switch
Takeoff (on ground)
Go Around
TOGATakeoff (on ground)
Go Around
TO
GA
A LT Key Roll Hold (default) ROL Altitude Hold A LT
VS Key Roll Hold (default) ROL Vertical Speed VS
VNV Key Roll Hold (default) ROL Vertical Path Tracking* VPTH
GPS
NAV Key Navigation**
VOR
Pitch Hold (default) PIT
LOC
BC Key Backcourse*** BC Pitch Hold (default) PIT
APR Key Approach**
GPS VOR LOC
Pitch Hold (default)
Glidepath
Glideslope
PIT GP GS
HDG Key Heading Select HDG Pitch Hold (default) PIT
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
**The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before
NAV
or
APR
Key press activates flight director.
***The selected navigation receiver must have a valid LOC signal before BC Key press activates flight
director.
Planning Procedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
Alerts Appendix Index
190-00600-03 Rev. A 13
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
AFCS

VERTICAL MODES

Flight
InstrumentsEICAS
Vertical Mode Description Control Annunciation
Holds the current aircraft pitch attitude;
Pitch Hold
Nav/Com/
Selected Altitude
XPDR/AudioAFCSGPS Nav
Armed
Altitude Hold Holds the current Altitude Reference A LT Key A LT nnnnn f T
Vertical Speed
Flight Level Change, IAS Hold
Flight
PlanningProcedures
Flight Level Change, Mach Hold
VNAV
Hazard
VNAV Target
Avoidance
Altitude Armed
Features
Additional
Glidepath
Glideslope
Abnormal
Operation
Takeoff
AlertsAppendixIndex
Annun/
Go Around
* ALTS armed automatically when PIT, VS, FLC, or GA active, and under VPTH when Selected Altitude
is to be captured instead of VNAV Target Altitude
** ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of
Selected Altitude
may be used to climb/descend to the Selected Altitude
AFCS armed to capture the altitude displayed in the Selected Altitude window
Maintains the current aircraft vertical speed; may be used to climb/descend to the Selected Altitude
Maintains the current aircraft airspeed (in IAS or Mach) while the aircraft is climbing/descending to the Selected Altitude
Captures and tracks the VNAV flight path
AFCS armed to capture the altitude displayed in the VNAV Target Altitude window
Captures and tracks the WAAS glidepath on approach
Captures and tracks the ILS glideslope on approach
Commands a constant pitch angle and wings level on the ground in preparation for takeoff
Disengages the autopilot and commands a constant pitch angle and wings level in the air
(default) PIT
* ALTS
VS Key VS nnnn f p m
FLC nnn k T
FLC Key
FLC M .nnn
VNV
Key
** ALTV
APR Key
GA
Switch
VPTH
GP
GS
TO
GA
14
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-03 Rev. A
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