Garmin T240 Reference Guide

™

G2000

Cockpit Reference Guide for the Model T240

Integrated Flight Deck

FLIGHT INSTRUMENTS

ENGINE INDICATION SYSTEM

NAV/COM/TRANSPONDER/AUDIO PANEL

AUTOMATIC FLIGHT CONTROL SYSTEM

FMS NAVIGATION

FLIGHT PLANNING

PROCEDURES

HAZARD AVOIDANCE

ADDITIONAL FEATURES

ABNORMAL OPERATION

ANNUNCIATIONS & ALERTS

APPENDIX

INDEX

Copyright © 2012-2013 Garmin Ltd. or its subsidiaries. All rights reserved.

This manual reflects the operation of System Software version 1308.07 or later for the Cessna
Corvalis T240. Some differences in operation may be observed when comparing the information
in this manual to earlier or later software versions.

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Tel: [phone] Fax: [phone]

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Tel: [phone] Fax: [phone]

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Tel: [phone] Fax: [phone]

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

Web Site Address: www.garmin.com

Except as expressly provided herein, no part of this manual may be reproduced, copied,
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without the express written permission of Garmin. Garmin hereby grants permission to
download a single copy of this manual and of any revision to this manual onto a hard drive or
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or printed copy of this manual or revision must contain the complete text of this copyright
notice and provided further that any unauthorized commercial distribution of this manual or any
revision hereto is strictly prohibited.

Garmin® , FliteCharts®, and SafeTaxi® are registered trademarks of Garmin Ltd. or its subsidiaries.
These trademarks may not be used without the express permission of Garmin. G2000™, Garmin
SVT™, and Garmin ESP™ are trademarks of Garmin Ltd. or its subsidiaries.

NavData® is a registered trademark of Jeppesen, Inc.; Stormscope® is a registered trademark
of L-3 Communications.

SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, 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
data, express or implied, including, but not limited to, the implied warranties of merchantability
and fitness for a particular purpose. The information is provided “as is” and AOPA does not
warrant or make any representations regarding its accuracy, reliability, or otherwise. Under
no circumstances including negligence, shall AOPA be liable for any incidental, special or
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
possibility of such damages. User agrees not to sue AOPA and, to the maximum extent allowed
by law, to release and hold harmless AOPA from any causes of action, claims or losses related
to any actual or alleged inaccuracies in the information. 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 you.

AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”)
expressly disclaim all warranties with respect to the AC-U-KWIK information included in this
data, express or implied, including, but not limited to, the implied warranties of merchantability
and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK
Organizations do not warrant or make any representations regarding its accuracy, reliability, or
otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the maximum extent
allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of
action, claims or losses related to any actual or alleged inaccuracies in the information arising
out of Garmin’s use of the information 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.

May, 2013 190-01264-01 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: Do not use outdated database information. Databases used in
the G2000 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 only
upon ATC guidance or positive visual acquisition of conflicting traffic.

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 significantly older than the indicated weather
product age.

190-01264-01 Rev. A

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

Warnings, Cautions & Notes

WARNING: Do not rely on information from the lightning detection system
display as the sole basis for hazardous weather avoidance. Range limitations
and interference may cause the system to display inaccurate or incomplete
information. Refer to documentation from the lightning detection system
manufacturer for detailed information about the system.

WARNING: The Garmin G2000, as installed in the Cessna Corvalis T240
aircraft, has a very high degree of functional integrity. However, the pilot
must recognize that providing monitoring and/or self-test capability for all
conceivable system failures is not practical. Although unlikely, it may be
possible for erroneous operation to occur without a fault indication shown
by the G2000. 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, G2000 operational procedures must be learned
on the ground.

WARNING: The United States government operates the Global Positioning
System and is solely responsible for its accuracy and maintenance. The GPS
system is subject to changes which could affect the accuracy and performance
of all GPS equipment. Portions of the Garmin G2000 utilize GPS as a
precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs,
information presented by the G2000 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 G2000 Pilot’s Guide documentation and the
Cessna Corvalis T240 Pilot’s Operating Handbook (POH). Thoroughly practice
basic operation prior to actual use. During flight operations, carefully compare
indications from the G2000 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 G2000 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.”

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

190-01264-01 Rev. A

Warnings, Cautions & Notes

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, MFD, and Touchscreen displays use a lens coated with a
special anti-reflective coating. DO NOT use chemical cleaning agents. Clean
the lens using a microfiber or soft cotton cloth dampened with clean water.

CAUTION: The Garmin G2000 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 G2000 panel and displays, are subject to change and may not
reflect the most current G2000 system and aviation 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: 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.

190-01264-01 Rev. A

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

Warnings, Cautions & Notes

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 G2000 system more easily. It is not intended to be a comprehensive
operating guide. Complete operating procedures for the system are found
in the G2000 Pilot’s Guide for this aircraft.

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

190-01264-01 Rev. A

Record of Revisions

Part Number Change Summary

190-01264-00 Initial release
190-01264-01 Updated Flight Instruments section

Renamed GPS Navigation section to FMS Navigation
Updated VNAV discussion in the FMS Navigation section
Added Lightning Detections System to Hazard Avoidance section
Added GFDS Connext Weather to Hazard Avoidance section
Added Electronic Documents to Additional Features section
Added Electronic Checklists to Additional Features section
Added ECS to Additional Features section
Added SMA to Additional Features section
Added Crew Profiles to Additional Features section
Updated PFD softkeys in the Appendix
Added GTC Screen navigation to the Appendix

Revision Date of Revision Affected Pages Description

A May, 2013 All Production release

190-01264-01 Rev. A RR-1

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

Record of Revisions

Blank Page

RR-2

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

190-01264-01 Rev. A

Table of Contents

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

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

Selecting Standard Barometric Pressure .............................................................................1

Changing Altimeter Barometric Pressure Setting Units .................................................. 1

Setting the Selected Altitude ................................................................................................ 1

Displaying Selected Altitude in Meters ............................................................................... 2

Setting the Baro Transition Alert .......................................................................................... 2

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

Changing the Selected GPS CDI Setting .............................................................................. 2

Changing Navigation Angle Setting ..................................................................................... 3

Enable/Disable OBS Mode While Navigating with FMS ................................................... 3

Adjusting Selected Heading ................................................................................................... 3

Adjusting Selected Course ...................................................................................................... 3

Selecting Bearing Display and Changing Sources ............................................................. 3

Set Barometric Minimum Descent Altitude ........................................................................ 4

Displaying Wind Data .............................................................................................................. 4

Changing Vspeeds and Turning Vspeed Flags On/Off ....................................................... 4

Turning All Vspeed Flags On/Off ............................................................................................ 4

Restoring All Vspeed Defaults ............................................................................................... 5

Enable Split Screen PFD .......................................................................................................... 5

Disable Split Screen PFD ......................................................................................................... 5

Synthetic Vision System .......................................................................................................... 5

Engine Indication System ........................................................................................................ 7

Engine/System Display ............................................................................................................ 8

Fuel Calculations ..................................................................................................................... 10

Engine Lean Assist Mode ...................................................................................................... 11

Nav/Com/Transponder/Audio Panel ................................................................................. 13

Selecting a COM Radio .......................................................................................................... 13

Com Frequency Tuning ........................................................................................................... 14

Changing Com Frequency Channel Spacing ...................................................................... 15

Simultaneous COM Operation ............................................................................................. 16

Selecting a NAV Radio ........................................................................................................... 16

NAV Radio Tuning ................................................................................................................... 16

ADF Tuning (Optional) ............................................................................................................ 17

DME Tuning (Optional) ........................................................................................................... 19

Transponder Operation ......................................................................................................... 19

Intercom .................................................................................................................................... 21

Digital Clearance Player ........................................................................................................ 25

Entertainment Inputs ............................................................................................................. 26

3D Audio ................................................................................................................................... 27

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Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

Table of Contents

Automatic Flight Control System ..................................................................................... 29

Flight Director Activation ..................................................................................................... 29

Vertical Modes .........................................................................................................................30

Lateral Modes .......................................................................................................................... 31

FMS Navigation ........................................................................................................................... 33

Direct-to Navigation .............................................................................................................. 33

Activate a Stored Flight Plan ............................................................................................... 34

Activate a Flight Plan Leg ..................................................................................................... 34

Stop Navigating a Flight Plan .............................................................................................. 35

Vertical Navigation (VNAV)................................................................................................... 35

Flight Planning............................................................................................................................. 41

Weight And Fuel Planning .....................................................................................................41

Trip Planning ............................................................................................................................ 42

Create a User Waypoint ......................................................................................................... 45

Create a Flight Plan ................................................................................................................ 46

Import a Flight Plan from an SD Card ................................................................................ 48

Insert a Waypoint in the Active Flight Plan ...................................................................... 49

Enter an Airway in an Active Flight Plan ........................................................................... 49

Activating Parallel Track ....................................................................................................... 50

User-Defined Holding Patterns ............................................................................................ 50

Invert An Active Flight Plan .................................................................................................. 52

Store a Flight Plan .................................................................................................................. 52

Insert a Waypoint in a Stored Flight Plan ......................................................................... 53

Enter an Airway in a Stored Flight Plan ............................................................................53

Removing Flight Plan Items ................................................................................................. 54

Invert and Activate a Stored Flight Plan ........................................................................... 57

Copy a Stored Flight Plan ..................................................................................................... 57

Delete a Stored Flight Plan .................................................................................................. 57

Export a Flight Plan to an SD Card ..................................................................................... 58

Procedures ..................................................................................................................................... 59

Load and Activate a Departure Procedure ....................................................................... 59

Load An Arrival Procedure .................................................................................................... 60

Load and/or Activate an Approach Procedure ................................................................. 61

Activate An Approach in the Active Flight Plan ............................................................... 63

Activate a Vector to Final Approach Fix ............................................................................ 64

Activate A Missed Approach in the Active Flight Plan ................................................... 64

Temperature Compensated Altitude .................................................................................. 65

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Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

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Table of Contents

Hazard Avoidance ...................................................................................................................... 67

Customizing the Hazard Displays on the Navigation Map ............................................ 67

Lightning Detection System (Optional) ............................................................................. 70

SiriusXM Weather (Optional) ............................................................................................... 72

Garmin Connext™ Weather (Optional) ............................................................................... 74

Traffic Advisory System ......................................................................................................... 80

Terrain-SVT ............................................................................................................................... 82

Terrain Awareness & Warning System (TAWS) Display (Optional) ............................... 83

Additional Features .................................................................................................................. 87

Terminal Procedure Charts ................................................................................................... 87

Airport Directory .................................................................................................................... 90

SiriusXM Radio Entertainment (Optional) ........................................................................ 90

Text Messaging (SMS) (Optional) ........................................................................................ 93

Scheduled Messages .............................................................................................................. 96

Electronic Stability and Protection ..................................................................................... 98

Electronic Documents (Optional) ........................................................................................ 99

Environmental Control Settings ........................................................................................ 102

Crew Profiles .......................................................................................................................... 103

Electronic Checklists (Optional) ......................................................................................... 105

Abnormal Operation .............................................................................................................. 107

Reversionary Mode .............................................................................................................. 107

Stuck Microphone ................................................................................................................. 107

COM Tuning Failure ...............................................................................................................107

Audio Controller Fail-Safe Operation ..............................................................................108

Hazard Displays with Loss of FMS Position .................................................................... 108

Unusual Attitudes ................................................................................................................. 108

Dead Reckoning .................................................................................................................... 109

Annunciations & Alerts ......................................................................................................... 111

CAS Alerts ............................................................................................................................... 111

Comparator Alerts ................................................................................................................ 113

Reversionary Sensor Alerts ................................................................................................ 114

Message Advisory ................................................................................................................. 114

AFCS Alerts ............................................................................................................................. 115

Terrain-SVT Alerts ................................................................................................................. 116

TAWS Alerts ............................................................................................................................ 117

GDL 69/69A Data Link Receiver Messages ...................................................................... 120

Voice Alerts ............................................................................................................................ 120

GDU 1400W Primary Flight Display & Multi Function Display .................................... 121

Database System Messages ............................................................................................... 123

GIA 63W Integrated Avionics Unit System Messages ................................................... 124

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Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

Table of Contents

GDC 74A Air Data Computer System Messages ............................................................. 128

GEA 71 Engine/Airframe Unit System Messages ........................................................... 128

GTX 33 Transponder System Messages ............................................................................ 128

GTS 800 Traffic Advisory System Messages .................................................................... 129

GSR 56 Message Advisories ................................................................................................ 129

GMU 44 Magnetometer System Messages ..................................................................... 129

GRS 77 Attitude and Heading Reference System Messages ....................................... 130

GTC 570 Touchscreen Controller System Messages ...................................................... 132

GCU 275 PFD Controller System Messages ..................................................................... 132

GDL 69/69A Satellite Datalink Receiver System Messages ......................................... 133

GMA 36 Remote Audio Controller System Messages ................................................... 133

GMC 720 AFCS Controller System Messages .................................................................. 134

Miscellaneous System Messages ...................................................................................... 134

Flight Plan Import/Export Messages ................................................................................ 139

Crew Profile Import/Export Messages ............................................................................. 140

Appendix ....................................................................................................................................... 143

PFD Softkeys .......................................................................................................................... 143

GTC Screens ............................................................................................................................ 149

Database Management ....................................................................................................... 161

Automatic Database Synchronization Feature .............................................................. 165

Garmin Databases ................................................................................................................ 168

Magnetic Field Variation Database Update .................................................................... 170

Cleaning the Touchscreen ................................................................................................... 172

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

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Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

190-01264-01 Rev. A

Flight Instruments

FLIGHT INSTRUMENTS

SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING

Turn the BARO Knob on the PFD Controller to select the desired setting.

SELECTING STANDARD BAROMETRIC PRESSURE

Press the BARO Knob on the GDU Controller to select standard pressure;
STD BARO is displayed in the Barometric Setting box.

CHANGING ALTIMETER BAROMETRIC PRESSURE SETTING UNITS

1)

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

2)

Press the Other PFD Settings Softkey.

3)

Press the Altitude Units Softkey.

4)

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 (hPa).

5)

Press the Back Softkey to return to the previous level of softkeys.

Instruments EIS

Flight

XPDR/Audio AFCS FMS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

SETTING THE SELECTED ALTITUDE

Turn the ALT Knob on the AFCS Controller to set the Selected Altitude in
100-ft increments. When meters are displayed, Selected Altitude is adjusted
in 50 meter increments..

If set, the Minimum Descent Altitude/Decision Height (MDA/DH) value is
also available for the Selected Altitude.

190-01264-01 Rev. A 1

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Flight Instruments

DISPLAYING SELECTED ALTITUDE IN METERS

Flight

1)

InstrumentsEIS

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

2)

Press the Other PFD Settings Softkey.

3)

Press the Altitude Units Softkey.

4)

Press the Meters Softkey to turn on metric altitude readouts.

Nav/Com/

XPDR/AudioAFCSFMS Nav

5)

Press the Back Softkey to return to the previous level of softkeys.

SETTING THE BARO TRANSITION ALERT

1)

From the Home Screen on the Touchscreen Controller, touch Utilities >
Setup > Avionics Settings.

2)

Touch the Alerts Tab.

•

To turn the alert on or off, touch the Baro Transition Alert Enable

Flight

PlanningProcedures

Hazard

CHANGE NAVIGATION SOURCES

Avoidance

Button. An illuminated green line below “Enable” indicates that the alert is
on.

•

To set or change the Baro Transition Alert Altitude, touch the Baro
Transition Alert Data Field. Enter the desired altitude on the keypad, and
touch Enter.

1)

Press the Active Nav Softkey on the PFD to change from FMS to VOR1 or

Features

Additional

LOC1.

2)

Press the Active Nav Softkey again to change from VOR1 or LOC1 to
VOR2 or LOC2.

Abnormal

Operation

3)

Press the Active Nav Softkey a third time to return to FMS.

CHANGING THE SELECTED GPS CDI SETTING

AlertsAppendixIndex

Annun/

1)

From the Home Screen on the Touchscreen Controller, touch Utilities >
Setup > Avionics Settings.

2)

Touch the System Tab.

3)

Touch the GPS CDI Data Field.

4)

Touch desired setting (2.00 NM, 1.00 NM, 0.30 NM, or AUTO).

2

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

190-01264-01 Rev. A

Flight Instruments

CHANGING NAVIGATION ANGLE SETTING

1)

From the Home Screen on the Touchscreen Controller, touch Utilities >
Setup > Avionics Settings.

2)

Touch the Units Tab.

3)

Touch the Nav Angle Data Field.

4)

Touch the desired setting (Magnetic or True).

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH FMS

1)

Press the OBS Softkey on the PFD to select OBS Mode.

2)

Turn the CRS Knob on the AFCS Controller 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 return to automatic waypoint sequencing.

ADJUSTING SELECTED HEADING

Turn the HDG Knob on the AFCS Controller to set the selected heading.

Press the HDG Knob to synchronize the bug to the current heading.

ADJUSTING SELECTED COURSE

Instruments EIS

Flight

XPDR/Audio AFCS FMS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Turn the CRS Knob on the AFCS Controller to set the Selected Course.

Press the CRS Knob to re-center the CDI and return the course pointer to
the bearing of the active waypoint or navigation station (see OBS Mode for
adjusting an FMS course).

SELECTING BEARING DISPLAY AND CHANGING SOURCES

1)

Press the PFD Settings Softkey on the PFD.

2)

Press a bearing softkey (Bearing 1 or Bearing 2) to display the desired
bearing pointer and information window with a NAV source.

3)

Press the bearing softkey again to change the bearing source to FMS.

4)

To remove the bearing pointer and information window, press the bearing
softkey again.

190-01264-01 Rev. A 3

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Flight Instruments

SET BAROMETRIC MINIMUM DESCENT ALTITUDE

Flight

1)

InstrumentsEIS

From the Home Screen on the Touchscreen Controller, touch Utilities >
Minimums.

2)

Touch Baro, or Temp Comp (use the keypad to enter the desired
temperature for temperature compensated VNAV) (OFF is selected by
default). To remove the window from the PFD display, touch OFF.

3)

Nav/Com/

XPDR/AudioAFCSFMS Nav

Use the keypad to enter the desired altitude (from zero to 16,000 feet for
Baro), and touch Enter.

DISPLAYING WIND DATA

1)

Press the PFD Settings Softkey on the PFD.

2)

Press the Other PFD Settings Softkey.

3)

Press the Wind Softkey to display wind data display options.

4)

Flight

PlanningProcedures

Press one of the option softkeys (Option 1, Option 2, or Option 3) to
change how wind data is displayed.

5)

To remove the window, press the Off Softkey.

CHANGING VSPEEDS AND TURNING VSPEED FLAGS ON/OFF

1)

Hazard

Avoidance

From the Home Screen on the Touchscreen Controller, touch Speed Bugs

2)

To turn the Vspeed on or off, touch the On Button . The illuminated green
line below “On” indicates that the Vspeed flag is on.

Features

Additional

3)

To set or change a Vspeed value, touch the Data Field for the Vspeed, enter
a value in the keypad, and touch

Enter.

The pencil icon next to the Vspeed

value indicates that the Vspeed is a pilot-entered value.

Abnormal

Operation

TURNING ALL VSPEED FLAGS ON/OFF

AlertsAppendixIndex

Annun/

1)

From the Home Screen on the Touchscreen Controller, touch Utilities >
Speed Bugs.

2)

To activate all Vspeed flags, touch the All Bugs On Button.

3)

To remove all Vspeed flags, touch the All Bugs Off Button.

4

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

190-01264-01 Rev. A

Flight Instruments

RESTORING ALL VSPEED DEFAULTS

1)

From the Home Screen on the Touchscreen Controller, touch Utilities >
Speed Bugs.

2)

Touch the Restore All Defaults Button.

ENABLE SPLIT SCREEN PFD

1)

Press the PFD Settings Softkey on the PFD.

2)

Press the PFD Mode Softkey. Split is now annunciated on the softkey
label and the multi-function pane is displayed to the right of the Primary
Flight Display.

DISABLE SPLIT SCREEN PFD

1)

Press the PFD Settings Softkey on the PFD.

2)

Press the PFD Mode Softkey. FULL is now annunciated on the softkey
label and the multi-function pane is no longer displayed.

SYNTHETIC VISION SYSTEM

WARNING: Use appropriate primary systems for navigation, and for terrain
and obstacle 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.

Instruments EIS

Flight

XPDR/Audio AFCS FMS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

WARNING: Do not use SVT runway depiction as the sole means for determining
the proximity of the aircraft to the runway or for maintaining the proper approach
path angle during landing.

Garmin SVT™ (Synthetic Vision Technology) functionality is offered as an

enhancement to the G2000 system.

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).

In addition to SVT enhancement to the PFD, the following features have been
added to the PFD:

190-01264-01 Rev. A 5

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

Operation

Abnormal

Annun/

Alerts Appendix Index

Flight Instruments

• Flight Path Marker

Flight

• Horizon Heading Marks

InstrumentsEIS

• Terrain and Obstacle Alerting

• Three-dimensional Traffic

• Airport Signs

• Runway Display

Activating and deactivating SVT:

Nav/Com/

XPDR/AudioAFCSFMS Nav

Press the PFD Settings Softkey > Attitude Overlays Softkey >
Synthetic Terrain Softkey. The SVT display will cycle on or off with each
press of the Synthetic Terrain Softkey.

NOTE: Pathways, Horizon Headings and Airport Signs are only available if

Synthetic Terrain is active.

Activating and deactivating Pathways:

Flight

PlanningProcedures

Press the PFD Settings Softkey > Attitude Overlays Softkey >
Pathways Softkey. Pathways will cycle on or off with each press of the
Pathways Softkey.

Activating and deactivating Horizon Headings:

Press the PFD Settings Softkey > Attitude Overlays Softkey > Horizon

Hazard

Avoidance

Heading Softkey. The Horizon Heading display will cycle on or off with
each press of the Horizon Heading Softkey.

Features

Additional

Abnormal

Operation

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Activating and deactivating Airport Signs:

Press the PFD Settings Softkey > Attitude Overlays Softkey > Airport
Signs Softkey. Airport Signs will cycle on or off with each press of the
Airport Signs Softkey.

6

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

190-01264-01 Rev. A

Engine Indication System

ENGINE INDICATION SYSTEM

Instruments EIS

Flight

1

2

3

4

5

6

Selected Tank

7

8

10

11

12

13

14

15

16

9

XPDR/Audio AFCS FMS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

EIS Display (Normal Mode)

Manifold Pressure

1

Cruise Power

2

Display

Cylinder Head

3

Temperature

Fuel Flow

4

190-01264-01 Rev. A 7

Oil Temperature

5

Oil Pressure

6

Fuel Quantity

7

Engine Hours

8

Display

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

Tachometer

9

Turbo Inlet

10

Temperature

Dual Voltmeter

11

Dual Ammeter

12

Elevator Trim

13

Aileron Trim

14

Anti-Ice Fluid

15

Quantity (Optional)

Flaps Position

16

Indicator

Alerts Appendix Index

Annun/

Engine Indication System

ENGINE/SYSTEM DISPLAY

Flight

The Engine/Systems Display shows engine, electrical, oxygen, and fuel calculation

InstrumentsEIS

information using bar graphs, digital readouts, and slide bars on the selected Display
Pane.

Accessing the Engine/Systems Display:

Nav/Com/

XPDR/AudioAFCSFMS Nav

From the Home Screen on the Touchscreen Controller, touch Aircraft
Systems > Engine/Sys.

NOTE: The Engine/Systems display is shown in Half Mode, and is not available

in Full Mode or Reversionary Mode.

Flight

PlanningProcedures

1

5

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

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6

2

3

7

4

Engine and Systems Display

8

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

190-01264-01 Rev. A

Engine Indication System

1

Exhaust Gas Temperature

(EGT °F)

For each cylinder, the exhaust gas temperatures
are shown in degrees Fahrenheit (°F). Each bar
segment on the graph represents 25 degrees.

2

Alternator Amps

(ALT AMPS)

Currents for the right and left alternators are
displayed using vertical bar indicators and
readouts

3

Oxygen Outlet Pressure Gauge

(OXY OUTLET PSI)

Oxygen outlet pressure in psi. Gauge ranges
are dependent on the oxygen outlet pressure
system.

4

Anti-ice Time Remaining

(A-ICE TIME REM)

5

Oxygen Quantity Gauge

(OXY QTY PSI)

6

Cylinder Head Temperature

(CHT °F)

Anti-ice time remaining based on the remaining
fluid quantity. (Optional).

Oxygen amount in psi; note that gauge
increment is 100 psi.

For each cylinder, the head temperatures are
shown in degrees Fahrenheit (°F). Each bar
segment on the graph represents 100 degrees.

7

Fuel Calculations Group

(GAL REM, GAL USED,
ENDUR, RANGE NM)

The fuel totalizer fuel remaining and used
and the totalizer-based endurance and range
calculations are displayed

Enabling/Disabling the Oxygen System:

1)

From the Home Screen on the Touchscreen Controller, touch Aircraft
Systems.

2)

Touch the Oxygen Button. When the button annunciator is green, oxygen
is enabled, annunciator is gray when disabled.

Instruments EIS

Flight

XPDR/Audio AFCS FMS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

190-01264-01 Rev. A 9

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

Alerts Appendix Index

Annun/

Engine Indication System

FUEL CALCULATIONS

Flight

InstrumentsEIS

NOTE: Fuel calculations do not use the aircraft fuel quantity indicators and
are calculated from the last time the fuel totalizer quantity was reset.

The system calculates Fuel used (GAL USED), endurance (ENDUR), and range
(RANGE NM) based on the displayed fuel remaining (GAL REM), fuel flow, and
groundspeed.

Nav/Com/

XPDR/AudioAFCSFMS Nav

Adjusting the Totalizer-Based Fuel Remaining:

1)

From the Home Screen on the Touchscreen Controller, touch Aircraft
Systems > Fuel Calc.

2)

Touch the Gal Rem Button.

3)

Enter the fuel quantity using the numeric keypad or large and small right
knobs, then touch the Enter Button. The totalizer-based fuel remaining is

Flight

PlanningProcedures

set to the entered fuel quantity and the GAL USED is set to zero.

Setting the Totalizer-Based Fuel Remaining to Full Fuel:

1)

From the Home Screen on the Touchscreen Controller, touch Aircraft
Systems > Fuel Calc.

2)

Touch the Set To Full Fuel Button. The totalizer-based fuel remaining is

Hazard

Avoidance

set to the aircraft’s usable fuel capacity and the GAL USED is set to zero.

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

10

Fuel

Remaining

Fuel Used

Calculation

Edit Remaining Fuel

Quantity

Set Fuel Quantity

to Full

Fuel Calculations Screen

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

Range
Calculation

Endurance
Calculation

190-01264-01 Rev. A

Engine Indication System

ENGINE LEAN ASSIST MODE

Instruments EIS

Flight

NOTE: Consult the Cessna Corvalis T240 Aircraft Flight Manual (AFM) for
leaning procedures.

While the Lean Assist Mode is active, the system indicates the peak of each TIT on

XPDR/Audio AFCS FMS Nav

Nav/Com/

the EIS display with a light blue bar which remains at the peak Turbo Inlet Temperature.
Readouts below each TIT gauge indicate the difference between each peak TIT and
the current temperature. An indicator below the readout shows whether each TIT is
operating ‘LEAN’ or ‘RICH’ of peak TIT.

Enabling/Disabling Lean Assist Mode:

1)

From the Home Screen on the Touchscreen Controller, touch Aircraft
Systems.

2)

Touch the Lean Assist Button. The button annunciator is green when Lean

Planning Procedures

Flight

Assist Mode is enabled, annunciator is gray when disabled.

Avoidance

Hazard

Peak TIT

TIT Deviation

Lean or Rich

from Peak

from Peak

Engine Lean Assist Mode (EIS Display)

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Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

Additional

Features

Operation

Abnormal

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Alerts Appendix Index

Engine Indication System

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSFMS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

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12

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

190-01264-01 Rev. A

Nav/Com/XPDR/Audio Panel

NAV/COM/TRANSPONDER/AUDIO PANEL

CNS Bar MIC Button (COM1 selected for transmission)

Instruments EIS

Flight

COM1 Active Frequency

(selected for transmission)

COM1 Standby

Frequency

MIC Button

(COM1 selected for

transmission)

MIC Button(COM2)

Audio & Radios Screen

Selecting a COM Radio for Transmission

SELECTING A COM RADIO

Selecting a COM Radio for transmission:

Touch the MIC Button in the CNS Bar on the Touchscreen Controller to
switch between COM radios until the desired COM is selected.

Or:

1)

Touch the Audio & Radios Button to display the Audio & Radios Screen.

2)

If necessary, touch the Copilot Tab.

3)

If necessary, touch the Sync to Pilot Button to disable synchronizing
selections to the pilot.

4)

Touch the desired MIC Button on the Audio & Radios Screen to select the
COM radio for transmission.

Or:

COM2 Primary
Frequency

COM2 Standby
Frequency

COM1 Active
Frequency

COM1 Standby
Frequency

COM2 Primary
Frequency

COM2 Standby
Frequency

XPDR/Audio AFCS FMS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-01264-01 Rev. A 13

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

Nav/Com/XPDR/Audio Panel

1)

On the PFD Controller, press the COM/NAV Button to display the COM/

Flight

InstrumentsEIS

NAV Window on the PFD.

2)

Turn the large PFD Knob to move the cursor to the MIC field.

3)

Turn the small PFD Knob to select the desired COM.

4)

Press the COM/NAV Button to hide the COM/NAV Window.

Selecting a COM Radio for monitoring:

Nav/Com/

XPDR/AudioAFCSFMS Nav

Touch the MON Button in the CNS Bar on the Touchscreen Controller to
monitor the COM not selected for transmission.

Or:

1)

Touch the Audio & Radios Button to display the Audio & Radios Screen.

2)

If necessary, touch the Copilot Tab.

3)

If necessary, touch the Sync to Pilot Button to disable synchronizing
selections to the pilot.

4)

Flight

PlanningProcedures

Touch the COM1 Button or COM2 Button to select the COM1/COM2 radio
for monitoring.

COM FREQUENCY TUNING

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

Selecting a COM frequency using the Touchscreen Controller:

1)

Touch the COM1 STBY Button or COM2 STBY Button in the CNS Bar on
the Touchscreen Controller to display the COM1/COM2 Standby Screen.

2)

Use the keypad to select the frequency.

3)

Touch the Enter Button to accept the new frequency as the COM1/COM2
standby frequency; or touch the XFER Button to accept the new frequency
as the COM1/COM2 active frequency and transfer the previously active
frequency to the standby frequency.

Or:

1)

Touch the Audio & Radios Button to display the Audio & Radios Screen.

2)

Touch the COM1/COM2 frequency button to display the COM1/COM2
Standby Screen.

3)

Use the keypad to select the desired frequency.

4)

Touch the Enter Button to accept the new frequency as the COM1/COM2
standby frequency; or touch the XFER Button to accept the new frequency
as the COM1/COM2 active frequency and transfer the previously active
frequency to the standby frequency.

14

Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240

190-01264-01 Rev. A