Garmin Corvalis, Corvalis TT Reference Guide

®

G1000

Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Integrated Flight Deck

FLIGHT INSTRUMENTS

ENGINE INDICATION SYSTEM

NAV/COM/TRANSPONDER/AUDIO PANEL

AUTOMATIC FLIGHT CONTROL SYSTEM

GPS NAVIGATION

FLIGHT PLANNING

PROCEDURES

HAZARD AVOIDANCE

ADDITIONAL FEATURES

ABNORMAL OPERATION

ANNUNCIATIONS & ALERTS

APPENDIX

INDEX

Copyright © 2006-2010 Garmin Ltd. or its subsidiaries. All rights reserved.

This manual reflects the operation of System Software version 0534.15 or later for the Cessna
Corvalis/Corvalis TT. Some differences in operation may be observed when comparing the
information in this manual to earlier or later software versions.

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

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

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

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

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

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

August, 2010 190-00567-04 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 G1000 GPS receivers is geometric
height above Mean Sea Level and could vary significantly from the altitude
displayed by pressure altimeters, such as the GDC 74A 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 G1000
PFD or other pressure altimeters in aircraft.

WARNING: Do not use outdated database information.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 Pilots using any outdated database do so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

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

WARNING: Traffic information shown on 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: 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 Corvalis/Corvalis TT

190-00567-04 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 Garmin G1000, as installed in the Cessna Corvalis/Corvalis
TT aircraft, has a very high degree of functional integrity. However, the pilot
must recognize that providing monitoring and/or self-test capability for all
conceivable system failures is not practical. Although unlikely, it may be
possible for erroneous operation to occur without a fault indication shown
by the G1000. It is thus the responsibility of the pilot to detect such an
occurrence by means of cross-checking with all redundant or correlated
information available in the cockpit.

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

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

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

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

190-00567-04 Rev. A

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

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

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

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 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 Pilot’s Guide for this aircraft.

190-00567-04 Rev. A

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Warnings, Cautions & Notes

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Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

Record of Revisions

Part Number Change Summary

190-00567-00

Rev A

Production release

Rev B

Added C350 parameters, TAWS changes, and Stormscope.

190-00567-01

Rev A

Rev B

Added GDU 8.10 parameters, WAAS, VNAV, Airways, and Charts

Changed company references to Cessna

190-00567-02 Reformatted manual

Added GDU 9.03 parameters

190-00567-03 Added GDU 9.05 with Synthethic Vision System (SVS)

Removed Stormscope

190-00567-04 Added Tach Timer

Added Flight Plan Import/Export
Added AOPA Airport Directory
Added Auxiliary Video
Added temporary user waypoints
Added CDI availability during Dead Reckoning mode
Added new MFD page navigation
Added other GDU 10.01 parameters

Revision Date of Revision Affected Pages Description

A August, 2010 All Production release

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Record of Revisions

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190-00567-04 Rev. A

Table of Contents

FLIGHT INSTRUMENTS ................................................................................................................ 1

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

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

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

Change Altimeter and Selected Altitude Display Units ................................................... 1

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

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

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

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

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

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

Changing HSI Format ............................................................................................................... 3

ENGINE INDICATION SYSTEM ................................................................................................. 5

Engine Page................................................................................................................................ 6

Engine Leaning Assist Mode ................................................................................................. 10

NAV/COM/TRANSPONDER/AUDIO PANEL ....................................................................... 13

ADF Tuning (Optional) ............................................................................................................ 13

DME Tuning (Optional) ........................................................................................................... 13

Enter a Transponder Code..................................................................................................... 13

Selecting a COM Radio .......................................................................................................... 14

Selecting a NAV Radio ........................................................................................................... 14

NAV/COM Tuning ..................................................................................................................... 14

Digital Clearance Recorder and Player .............................................................................. 14

Intercom System (ICS) Isolation .......................................................................................... 15

GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM .......................................................17

Flight Director Activation ..................................................................................................... 17

Vertical Modes ......................................................................................................................... 18

Lateral Modes .......................................................................................................................... 19

GPS NAVIGATION ........................................................................................................................ 21

Direct-to Navigation .............................................................................................................. 21

Activate a Stored Flight Plan ............................................................................................... 22

Activate a Flight Plan Leg ..................................................................................................... 22

Stop Navigating a Flight Plan .............................................................................................. 23

Vertical Navigation (VNAV)................................................................................................... 23

FLIGHT PLANNING ...................................................................................................................... 25

Trip Planning ............................................................................................................................ 25

Create a New User Waypoint Defined by Latitude & Longitude ................................. 27

Create a New User Waypoint Defined by Radials from Other Waypoints .................27

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Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Table of Contents

Create a New User Waypoint Defined by a Radial & Distance from Another

Waypoint .............................................................................................................................. 29

Delete a User Waypoint ......................................................................................................... 30

Create a New Flight Plan ...................................................................................................... 31

Import a Flight Plan from an SD Card ................................................................................ 32

Insert a Waypoint in the Active Flight Plan ...................................................................... 32

Enter an Airway in a Flight Plan .......................................................................................... 33

Invert An Active Flight Plan .................................................................................................. 34

Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 34

Store a Flight Plan .................................................................................................................. 35

Edit a Stored Flight Plan ....................................................................................................... 35

Delete a Waypoint from the Flight Plan ............................................................................ 35

Invert and Activate a Stored Flight Plan ........................................................................... 36

Copy a Flight Plan ................................................................................................................... 36

Delete a Flight Plan ................................................................................................................ 36

Graphical Flight Plan Creation ............................................................................................. 37

Export a Flight Plan to an SD Card ..................................................................................... 37

PROCEDURES ................................................................................................................................. 39

Load and Activate a Departure Procedure ....................................................................... 39

Activate A Departure Leg ..................................................................................................... 39

Load An Arrival Procedure .................................................................................................... 39

Activate An Arrival Leg ......................................................................................................... 40

Load and/or Activate an Approach Procedure ................................................................. 40

Activate An Approach in the Active Flight Plan ............................................................... 41

Activate a Vector to Final Approach Fix ............................................................................ 42

Activate A Missed Approach in the Active Flight Plan ................................................... 42

HAZARD AVOIDANCE ................................................................................................................43

Customizing the Hazard Displays on the Navigation Map ............................................ 43

XM Weather (Optional) .......................................................................................................... 43

Traffic Systems ........................................................................................................................ 44

Terrain And Obstacle Proximity ........................................................................................... 46

Terrain-SVS ............................................................................................................................... 47

Terrain Awareness & Warning System (TAWS) Display (Optional) ............................... 49

ADDITIONAL FEATURES ........................................................................................................... 51

Synthetic Vision (Optional) ................................................................................................... 51

Terminal Procedure Charts ................................................................................................... 52

AOPA Airport Directory ......................................................................................................... 54

XM® Radio Entertainment (Optional) ................................................................................. 55

Auxiliary Video (Optional) .................................................................................................... 57

Electronic Checklists .............................................................................................................. 59

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Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

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Table of Contents

ABNORMAL OPERATION..........................................................................................................61

Reversionary Mode ................................................................................................................ 61

Abnormal COM Operation .................................................................................................... 61

Audio Panel Fail-safe Operation.......................................................................................... 61

Hazard Displays with Loss of GPS Position ....................................................................... 61

Unusual Attitudes ................................................................................................................... 62

Dead Reckoning ...................................................................................................................... 62

ANNUNCIATIONS & ALERTS ................................................................................................... 65

WARNING Alerts ...................................................................................................................... 65

CAUTION Alerts ........................................................................................................................ 65

Annunciation Advisory .......................................................................................................... 66

Message Advisory Alerts ....................................................................................................... 66

CO Guardian Messages .......................................................................................................... 66

AFCS Alerts ............................................................................................................................... 67

Terrain-SVS Alerts ................................................................................................................... 68

TAWS-B Alerts .......................................................................................................................... 69

Voice Alerts .............................................................................................................................. 72

MFD & PFD Message Advisories .......................................................................................... 72

Database Message Advisories ............................................................................................. 73

GMA 1347 Message Advisories ............................................................................................ 76

GIA 63 Message Advisories ................................................................................................... 76

GIA 63W Message Advisories ............................................................................................... 79

GEA 71 Message Advisories .................................................................................................. 82

GTX 33 Message Advisories .................................................................................................. 82

GRS 77 Message Advisories .................................................................................................. 83

GMU 44 Message Advisories ................................................................................................ 83

GDL 69A Message Advisories ............................................................................................... 84

GDC 74A Message Advisories ............................................................................................... 84

GCU 476 Message Advisories ............................................................................................... 84

Miscellaneous Message Advisories ..................................................................................... 85

APPENDIX ....................................................................................................................................... 89

PFD Softkey Map .................................................................................................................... 89

MFD Softkey Map ................................................................................................................... 94

Database Updates .................................................................................................................. 96

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

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Table of Contents

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Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 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 (29.92 IN HG)

1)

Select the PFD Softkey.

2)

Select the STD BARO Softkey to set standard barometric pressure.

CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS

1)

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

2)

Select the ALT UNIT Softkey.

3)

Select the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).

Or

:

Select the HPA Softkey to display the barometric pressure setting in
hectopascals.

4)

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

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

CHANGE ALTIMETER AND SELECTED ALTITUDE DISPLAY UNITS

1)

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

2)

Select the ALT UNIT Softkey.

3)

Select the METERS Softkey to add or remove the metric units display for
the altimeter and selected altitude.

4)

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

190-00567-04 Rev. A 1

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Flight Instruments

CHANGE NAVIGATION SOURCES

Flight

1)

InstrumentsEIS

Select 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)

Select 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)

Select the CDI Softkey a third time to return to GPS.

ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS

1)

Select the OBS Softkey to select OBS Mode.

2)

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

waypoint.

Flight

PlanningProcedures

3)

Select the OBS Softkey again to disable OBS Mode.

GENERIC TIMER

1)

Select 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 starts counting UP after reaching zero). Press the CLR
Key or the TMR/REF Softkey to remove the window.

CONFIGURE VSPEED BUGS

AlertsAppendixIndex

Annun/

1)

Select the TMR/REF Softkey.

2)

Turn the

3)

Use the small FMS Knob to change the Vspeed in 1-kt increments (when a

large

speed has been changed from a default value, an asterisk appears next to
the speed).

2

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

FMS Knob to highlight the desired Vspeed.

190-00567-04 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.

SET BAROMETRIC MINIMUM DESCENT ALTITUDE

1)

Select the TMR/REF Softkey.

2)

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

3)

Turn the small FMS Knob clockwise to BARO.

4)

Press the ENT Key.

5)

Use the small FMS Knob to enter the desired altitude.

6)

Press the ENT Key.

7)

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

DISPLAYING WIND DATA

1)

Select the PFD Softkey.

2)

Select the WIND Softkey to display wind data to the left of the HSI.

3)

Select one of the OPTN softkeys to change how wind data is displayed.

4)

To remove the Wind Data Window, select the OFF Softkey.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

CHANGING HSI FORMAT

1)

Select the PFD Softkey.

2)

Select the HSI FRMT Softkey.

3)

Select the 360 HSI Softkey to display the full size HSI.

Or

:

Select the ARC HSI Softkey to display the arc style HSI.

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Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Operation

Abnormal

Annun/

Alerts Appendix Index

Flight Instruments

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

4

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

Engine Indication System

ENGINE INDICATION SYSTEM

1

2

3

4

5

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

6

6

7

8

9

9

10

10

Corvalis Corvalis TT

EIS Display

1

Engine Manifold Pressure Gauge

2

Tachometer

3

Fuel Quantity Indicator

4

Fuel Flow Indicator

5

Oil Pressure Indicator

6

Oil Temperature Indicator

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Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

7

Exhaust Gas Temperature Indicator
(Corvalis only)

8

Turbine Inlet Temperature Indicator
(Corvalis TT only)

9

Cylinder Head Temperature Indicator

10

Trim Group

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Engine Indication System

ENGINE PAGE

Flight

Selecting the SYSTEM Softkey on the MFD accesses the Engine Page, which

InstrumentsEIS

displays all Engine Indication System instruments; selecting the softkey again exits the
Engine Page.

Oxygen quantity and outlet pressure are also shown on the Engine Page. The
OXYGEN Softkey can be used to turn the optional oxygen system on/off. If an oxygen
system is not installed, blank gauges are displayed.

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

1 2 3

PlanningProcedures

11

4

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

10

9

1

Oil Temperature/Pressure Gauge

2

Engine Manifold Pressure Gauge

3

Tachometer

4

Fuel Calculations Group

5

Oxygen Quantity Gauge (Corvalis
TT only)

6

Oxygen Outlet Pressure Gauge (Low
Pressure Gauge shown, High Pressure
Gauge optional)(Corvalis TT only)

6

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Engine Page (Corvalis)

7

Electrical Group

8

Trim Group

9

Engine Temperature Group

10

Fuel Quantity Gauges

11

Fuel Flow Gauge

7

8

Carbon
Monoxide
Warning

190-00567-04 Rev. A

Engine Indication System

1 2 3 5

11

10

9

4

6

7

8

Engine Page (Corvalis TT)

Carbon Monoxide Detection

If carbon monoxide (CO) in the cabin becomes too high (exceeds 50 ppm), a
flashing red annunciation and the current level of CO in parts per million (ppm) are
displayed in the lower right corner of the Engine Page.

When a warning is generated, the CO RST Softkey becomes available to reset the
CO Guardian and acknowledge the alert.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

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Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Alerts Appendix Index

Annun/

Engine Indication System

Fuel Calculations Group

Flight

InstrumentsEIS

NOTE: Fuel calculations do not use the aircraft fuel quantity indicators and

are calculated from the last time the fuel was reset.

Fuel used (GAL USED), endurance (ENDUR), and range (RANGE NM) are all
calculated based on the displayed fuel remaining (GAL REM) and the fuel flow totalizer.
The fuel remaining can be adjusted using the following softkeys:

Nav/Com/

XPDR/AudioAFCSGPS Nav

• DEC FUEL – Decreases totalizer-based fuel remaining in one-gallon incre-
ments

• INC FUEL – Increases totalizer-based fuel remaining in one-gallon
increments

• RST FUEL – Resets totalizer-based fuel remaining to the aircraft’s fuel capacity
(98 gal or 102 gal usable) and sets the GAL USED display to zero

Flight

PlanningProcedures

Fuel

Remaining

Endurance
Calculation

Range
Calculation

Hazard

Fuel Used

Calculation

Avoidance

Fuel Calculations Group

Features

Additional

Engine Temperature Group

Abnormal

The temperature group displays the Cylinder Head Temperature (CHT) and Exhaust

Operation

Gas Temperature (EGT) in degrees Fahrenheit for each cylinder using bar graphs and
digital readouts. For the Corvalis TT, Turbine Inlet Temperature (TIT) is shown on a
sliding bar scale.

AlertsAppendixIndex

Annun/

The following softkeys can be used to modify the display of engine temperature

information:

• DCLTR – Removes/displays the EGT and CHT readouts from the display

• ASSIST – Accesses the Engine Leaning Assist Mode

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Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

Engine Indication System

Exhaust Gas
Temperature

Exhaust Gas
Temperature

Cylinder Head

Temperature

Engine Temperature Group (Corvalis)

Turbine Inlet
Temperature

Cylinder Head

Temperature

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Engine Temperature Group (Corvalis TT)

190-00567-04 Rev. A 9

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Engine Indication System

ENGINE LEANING ASSIST MODE

Flight

InstrumentsEIS

NOTE: Consult the Cessna Corvalis/Corvalis TT Aircraft Flight Manual (AFM)

for leaning procedures.

From the Engine Page, the Engine Leaning Assist Mode may be accessed by selecting
the ASSIST Softkey. Selecting the ASSIST Softkey again returns the MFD to the
Engine Page. Use the SYSTEM Softkey to exit the Engine Page.

Nav/Com/

XPDR/AudioAFCSGPS Nav

While in Assist Mode, the EIS Display is shown along with the Fuel Flow Gauge
and an expanded Engine Temperature Group.

Corvalis

When the ASSIST Softkey is selected, the system initially highlights the

number and EGT readout of the cylinder with the hottest EGT.

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

Fuel Flow Gauge

EGT Deviation
from Peak

Engine Leaning Assist Mode (Corvalis)

10

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

Engine Indication System

When the first peak is detected, the cylinder numbers disappear, “1st” is annunciated
in light blue below that cylinder’s EGT bar, the temperature is marked in light blue on
the graph, and the EGT readout is outlined.

Temperature Deviation from Peak

(First Cylinder)

Light

Blue Bar

Represents

Peak

Indicates

First

Cylinder

to Peak

Assist Mode - First Peaked Cylinder (Corvalis)

The system continues to detect peak EGTs for each cylinder as the fuel flow is
decreased and the peak of each cylinder’s EGT is indicated by a light blue marker. The
last cylinder to peak is denoted by the “Last” annunciation below its bar on the graph
and the EGT readout is outlined in light blue.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Temperature Deviation from Peak

(Last Cylinder)

Indicates

Last

Cylinder to

Peak

Assist Mode - Last Peaked Cylinder (Corvalis)

190-00567-04 Rev. A 11

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Engine Indication System

Corvalis TT

Flight

Once the ASSIST Softkey is selected, the peak of each TIT is indicated by a light

InstrumentsEIS

blue bar which moves and remains at the peak Turbine Inlet Temperature.

Peak TIT

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

Lean or Rich

PlanningProcedures

From Peak

TIT Deviation

from Peak

Engine Leaning Assist Mode (Corvalis TT)

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

12

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

NAV/COM/TRANSPONDER/AUDIO PANEL

ADF TUNING (OPTIONAL)

1)

Select 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 (OPTIONAL)

Nav/Com/XPDR/Audio Panel

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

1)

Select the ADF/DME or DME Softkey.

2)

Turn the large FMS to select the DME source field.

3)

Turn the small FMS Knob to select the desired Nav radio.

4)

Press the ENT Key to complete the selection.

ENTER A TRANSPONDER CODE

1)

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

2)

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

3)

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

190-00567-04 Rev. A 13

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Nav/Com/XPDR/Audio Panel

SELECTING A COM RADIO

Flight

InstrumentsEIS

Transmit/Receive

Press the COM1 MIC, COM2 MIC
installed) on the audio panel.

Receive Only

Nav/Com/

XPDR/AudioAFCSGPS Nav

Press the COM1, COM2
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

Flight

PlanningProcedures

individually or together.

NAV/COM TUNING

, or

COM3 MIC Key (optional COM, if

, or

COM3 Key (optional COM, if installed) on the

1)

Press the small tuning knob to select the desired radio for tuning. A light
blue box highlights the radio frequency to be tuned.

2)

Hazard

Avoidance

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.

Features

3)

Additional

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

DIGITAL CLEARANCE RECORDER AND PLAYER

Abnormal

Operation

AlertsAppendixIndex

Annun/

NOTE: Only the audio for the selected

not recorded for COM3 MIC.

• PressingthePLAY Key once plays the latest recorded memory block, then returns
to normal operation.

• PressingtheMKR/MUTE Key while playing a memory block stops play.

• Pressingthe PLAY Key during play begins playing the previously recorded

memory block. Each subsequent press of the PLAY Key begins playing the next
previously recorded block.

14

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

COM MIC

Key is recorded. Audio is

190-00567-04 Rev. A

Nav/Com/XPDR/Audio Panel

INTERCOM SYSTEM (ICS) ISOLATION

Press the PILOT and/or COPLT Key to select those isolated from hearing the Nav/

Com radios and music.

Mode

PILOT KEY

ANNUNCIATOR

ALL OFF OFF

PILOT ON OFF

COPILOT OFF ON

CREW ON ON

COPLT KEY

ANNUNCIATOR

Pilot Hears

Selected
radios; pilot;
copilot;
passengers;
music

Selected
radios; pilot

Selected
radios; pilot;
passengers;
music

Selected
radios; pilot;
copilot

Copilot

Hears

Selected
radios; pilot;
copilot;
passengers;
music

Copilot;
passengers;
music

Copilot

Selected
radios; pilot;
copilot

Passenger

Hears

Selected
radios; pilot;
copilot;
passengers;
music

Copilot;
passengers;
music

Selected
radios; pilot;
passengers;
music

Passengers;
music

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

190-00567-04 Rev. A 15

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Nav/Com/XPDR/Audio Panel

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

16

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

GFC 700 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 EIS

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 Switch Roll Hold (default) ROL Pitch Hold (default) PIT

GA Switch

Takeoff (on ground)

Go Around (in air)

TO
GA

Takeoff (on ground)

Go Around (in air)

GA

A LT Key Roll Hold (default) ROL Altitude Hold ALT

VS Key Roll Hold (default) ROL Vertical Speed VS

VNV Key Roll Hold (default) ROL Vertical Path Tracking* VPTH

FLC Key Roll Hold (default) ROL Flight Level Change FLC

GPS

NAV Key Navigation**

VOR

Pitch Hold (default) PIT

LOC

BC Key (GDU 1044B) Backcourse*** BC Pitch Hold (default) PIT

APR Key Approach**

GPS

VAPP

LOC

Pitch Hold (default)

Glidepath

Glideslope

PIT
GP
GS

HDG Key Heading Select HDG Pitch Hold (default) PIT

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

*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.

190-00567-04 Rev. A 17

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

AFCS

VERTICAL MODES

Flight

InstrumentsEIS

Vertical Mode Description Control Annunciation

Holds the current aircraft pitch

Pitch Hold

Selected Altitude
Armed

Nav/Com/

XPDR/AudioAFCSGPS Nav

Altitude Hold

Vertical Speed

Flight Level Change

Flight

PlanningProcedures

Vertical Path Tracking

VNAV Target Altitude
Capture

Hazard

Glidepath ***

Avoidance

Glideslope

Features

Additional

Go Around

Abnormal

Operation

* 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

AlertsAppendixIndex

Annun/

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

Selected Altitude

***GP is available in installations with GIA 63W IAUs when SBAS is available.

attitude; may be used to climb/

(default) PIT

descend to the Selected Altitude

Captures the Selected Altitude * ALTS

Holds the current Altitude
Reference

A LT Key A LT nnnnn f T

Holds aircraft vertical speed; may
be used to climb/descend to the

VS Key VS nnnn f p m

Selected Altitude
Holds aircraft airspeed while aircraft

is climbing/descending to the

FLC Key FLC nnn k T

Selected Altitude
Captures and tracks descent legs of

an active vertical profile
Captures the Vertical Navigation

(VNV) Target Altitude

VNV Key VPTH

** ALTV

Captures and tracks the SBAS
glidepath on approach

APR Key

Captures and tracks the ILS
glideslope on approach

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

GA

Switch

GP

GS

GA

18

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

AFCS

LATERAL MODES

Lateral Mode Description Control Annunciation

Holds the current aircraft roll

Roll Hold

Heading Select

Navigation, GPS
Navigation, VOR Enroute

Capture/Track
Navigation, LOC Capture/Track

(No Glideslope)

Navigation, Backcourse
Capture/Track (GDU 1044 only)

Backcourse (GDU 1044B only)

Approach, GPS
Approach, VOR Capture/Track VAPP
Approach, LOC (Glideslope

Mode automatically armed)

Go Around

attitude or rolls the wings
level, depending on the
commanded bank angle

Captures and tracks the
Selected Heading

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

Captures and tracks
a localizer signal for
backcourse approaches

Captures and tracks
a localizer signal for
backcourse approaches

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

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

(default) ROL

HDG

Key

HDG

GPS

VOR

NAV

Key

LOC

BC

BC Key

(GDU

1044B

BC

only)

GPS

APR

Key

LOC

GA

Switch

GA

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00567-04 Rev. A 19

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

AFCS

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

20

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

GPS NAVIGATION

DIRECT-TO NAVIGATION

Direct-to Navigation from the MFD

1)

Press the Direct-to

2)

Enter the waypoint identifier.

3)

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

4)

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

5)

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

6)

Enter the desired altitude.

7)

Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 9.

8)

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

9)

Press the ENT Key. The cursor is now flashing in the VNV offset distance
field.

10)

Enter the desired offset distance before (-) the waypoint.

11)

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

12)

Press the ENT Key to activate.

( )

Key.

GPS Navigation

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Direct-to Navigation from the PFD

1)

Press the Direct-to Key

2)

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

3)

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

4)

Press the ENT Key.

5)

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

6)

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

190-00567-04 Rev. A 21

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

( )

.

Operation

Abnormal

Annun/

Alerts Appendix Index

GPS Navigation

7)

Turn the small FMS Knob to enter the desired altitude.

8)

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

ACTIVATE A STORED FLIGHT PLAN

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 10.

9)

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

10)

Press the ENT Key. The cursor is placed in the ‘OFFSET’ field.

11)

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

the selected Direct-to.

12)

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

highlight the ‘CRS’ field.

13)

Turn the small FMS Knob to enter the desired course to the waypoint.

14)

Press the ENT Key to highlight ‘ACTIVATE?’.

15)

Press the ENT again to activate the Direct-to.

1)

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

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight the desired flight plan.

4)

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

5)

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

ACTIVATE A FLIGHT PLAN LEG

Abnormal

Operation

1)

From the Active Flight Plan Page, press the FMS Knob to activate the cursor

AlertsAppendixIndex

Annun/

and turn the large FMS Knob to highlight the desired waypoint.

2)

On the MFD, select the ACT LEG Softkey.

Or:

Press the MENU Key, select the ‘Activate Leg’ option from the page menu
and press the ENT Key. This step must be used when activating a leg from

the PFD.

3)

With ‘Activate’ highlighted, press the ENT Key.

22

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

GPS Navigation

STOP NAVIGATING A FLIGHT PLAN

1)

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

2)

Press the MENU Key to display the Page Menu Window.

3)

Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT
Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan.
This does not delete the stored flight plan, only the active flight plan.

VERTICAL NAVIGATION (VNAV)

The navigation database only contains altitudes for procedures that call for “Cross
at” altitudes. If the procedure states “Expect to cross at,” the altitude is not in the
database. In this case the altitude may be entered manually.

Large White
Text

Large Light
Blue Text

Small Light
Blue Text

Small Light
Blue Subdued
Text

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Small White Text
with Altitude
Restriction Bar

Cross AT or ABOVE 5,000 ft

Cross AT 2,300 ft

Cross AT or BELOW 3,000 ft

190-00567-04 Rev. A 23

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Operation

Abnormal

Annun/

Alerts Appendix Index

GPS Navigation

Altitudes associated with approach procedures are “auto-designated”. This means

the system automatically uses the altitudes loaded with the approach for giving vertical

Flight

InstrumentsEIS

flight path guidance outside the FAF. Note these altitudes are displayed as small light
blue text.

Altitudes associated with arrival procedures are “manually-designated”. This means
the system does not use the altitudes loaded with the arrival for giving vertical flight
path guidance until designated to do so by the pilot. Note that these altitudes are
initially displayed as white text. These altitudes may be “designated” by placing the

Nav/Com/

XPDR/AudioAFCSGPS Nav

cursor over the desired altitude and pressing the ENT Key. After designation, the text
changes to light blue.

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

Flight

PlanningProcedures

White Text Light Blue Text Light Blue

Subdued Text

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

Large Text

Small Text

24

Altitude calculated by the
system estimating the
altitude of the aircraft as it
passes over the navigation
point. This altitude is
provided as a reference
and is not designated to
be used in determining

vertical flight path

Altitude has been entered
by the pilot. Altitude is
designated for use in

giving vertical flight path
guidance. Altitude does
not match the published
altitude in navigation
database or no published
altitude exists.

The system cannot
use this altitude in
determining vertical

flight path guidance.

guidance.

Altitude is not designated
to be used in determining

vertical flight path
guidance. Altitude has
been retrieved from the
navigation database and
is provided as a reference.

Altitude is designated
for use in giving vertical

flight path guidance.

Altitude has been
retrieved from the
navigation database
or has been entered by

The system cannot
use this altitude in
determining vertical

flight path guidance.

the pilot and matches a
published altitude in the
navigation database.

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

TRIP PLANNING

1)

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

2)

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

3)

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

4)

For Direct-to planning:

a)

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

b)

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

c)

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

d)

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

Or:

For point-to-point planning:

a)

Enter the identifier of the starting waypoint.

b)

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

c)

Again, enter the identifier of the ending waypoint.

d)

Press the ENT Key to accept the waypoint.

Or:

For flight plan leg planning:

a)

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

b)

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

c)

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

d)

Turn the small FMS Knob to select the desired leg of the flight plan, or
select ‘CUM’ to apply trip planning calculations to the entire flight plan.

FLIGHT PLANNING

Flight Planning

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00567-04 Rev. A 25

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Flight Planning

Flight

InstrumentsEIS

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

steps.

5)

Turn the large FMS Knob to highlight the departure time (DEP TIME) field.

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

NOTE: The departure time on the Trip Planning Page is used for preflight

planning. Refer to the Utility Page for the actual flight departure time.

6)

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

7)

The flashing cursor moves to the ground speed (GS) field. Enter the ground
speed. Press the
mode, ground speed is provided by the system.

8)

The flashing cursor moves to the fuel flow field. Enter the fuel flow. Press
the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel flow
is provided by the system.

9)

The flashing cursor moves to the fuel onboard field. Enter the fuel onboard.
Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel
onboard is provided by the fuel totalizer.

10)

The flashing cursor moves to the calibrated airspeed (CALIBRATED AS) field.

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

11)

The flashing cursor moves to the altitude (IND ALTITUDE) field. Enter the

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

12)

The flashing cursor moves to the barometric setting (PRESSURE) field. Enter

the desired baro setting. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, the baro setting is provided by the setting entered
on the PFD.

13)

The flashing cursor moves to the air temperature (TOTAL AIR TEMP) field. Enter

the desired air temperature. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, air temperature is provided by the system outside
air temperature.

Selecting ‘FPL 00’ displays the active flight plan. If an active flight plan
is selected, ‘REM’ is an available option to display planning data for the
remainder of the flight plan.

ENT

Key when finished. Note that in ‘automatic’ page

26

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

Flight Planning

CREATE A NEW USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE

1)

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

2)

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

3)

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

4)

Enter the desired waypoint name.

5)

Press the ENT Key.

6)

The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.

a)

Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.

b)

Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.

7)

With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.

8)

Turn the small FMS Knob to select LAT/LON (latitude and longitude).

9)

Press the ENT Key.

CREATE A NEW USER WAYPOINT DEFINED BY RADIALS FROM OTHER

WAYPOINTS

1)

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

2)

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

3)

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

4)

Enter the desired waypoint name.

5)

Press the ENT Key.

6)

The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.

a)

Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.

b)

Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.

Instruments EIS

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Flight Planning

7)

With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to

Flight

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display a list of waypoint types.

8)

Turn the small FMS Knob to select RAD/RAD (radial/radial).

9)

Press the ENT Key.

10)

The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first

waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:

a)

b)

c)

Or:

a)

b)

c)

d)

Or:

a)

b)

c)

d)

Or:

a)

b)

c)

d)

11)

Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter

the desired radial from the reference waypoint.

When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

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

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

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

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

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

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

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Flight Planning

12)

Press the ENT Key.

13)

Repeat step 10 to enter the next waypoint name.

14)

Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field for the

second waypoint. Enter the desired radial from the reference waypoint.

15)

Press the ENT Key.

16)

Press the FMS Knob to remove the flashing cursor.

CREATE A NEW USER WAYPOINT DEFINED BY A RADIAL & DISTANCE FROM

ANOTHER WAYPOINT

1)

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

2)

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

3)

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

4)

Enter the desired waypoint name.

5)

Press the ENT Key.

6)

The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.

a)

Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.

b)

Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.

7)

With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.

8)

Turn the small FMS Knob to select RAD/DIS (radial/distance).

9)

Press the ENT Key.

10)

The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first

waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:

a)

When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.

b)

Turn the large FMS Knob to select the desired waypoint.

c)

Press the ENT Key.

Instruments EIS

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Flight Planning

Or:

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a)

b)

c)

d)

Or:

a)

b)

c)

d)

Or:

a)

b)

c)

d)

11)

Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter

the desired radial from the reference waypoint.

12)

Press the ENT Key.

13)

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

distance from the reference waypoint.

14)

Press the ENT Key.

15)

Press the FMS Knob to remove the flashing cursor.

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

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

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

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

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

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

Turn the large FMS Knob to select the desired waypoint.

Press the ENT Key.

DELETE A USER WAYPOINT

1)

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

2)

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

3)

Press the FMS Knob to activate the cursor.

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Flight Planning

4)

Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’
field.

5)

Turn the small FMS Knob to highlight the desired waypoint.

6)

Press the DELETE Softkey.

7)

The message ‘Would you like to delete the user waypoint?’ is displayed. With
‘YES’ highlighted, press the ENT Key.

CREATE A NEW FLIGHT PLAN

NOTE: When creating a new flight plan in the Active Flight Plan Window,

the first leg is activated automatically after it is created.

Creating an active flight plan:

1)

Press the FPL Key.

2)

Press the FMS Knob to activate the cursor (only on MFD).

3)

Turn the small FMS Knob to display the Waypoint Information Window.
(Turning it clockwise displays a blank Waypoint Information Window,
turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan,
nearest, recent, user, or airway waypoints).

4)

Enter the identifier, facility, or city name of the departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key. The
active flight plan is modified as each waypoint is entered.

5)

Repeat step numbers 3 and 4 to enter each additional flight plan waypoint.

6)

When all waypoints have been entered, press the FMS Knob to remove the
cursor.

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Abnormal

Creating a stored flight plan:

1)

Press the FPL Key.

2)

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

3)

Select the NEW Softkey; or press the MENU Key, highlight ‘Create New
Flight Plan’, and press the ENT Key to display a blank flight plan for the
first empty storage location.

4)

Turn the small FMS Knob to display the Waypoint Information Window.
(Turning it clockwise displays a blank Waypoint Information Window,
turning it counter-clockwise displays the Waypoint Information Window

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Flight Planning

with a waypoint selection submenu allowing selection of active flight plan,

Flight

InstrumentsEIS

nearest, recent, user, or airway waypoints).

5)

Enter the identifier, facility, or city name of the departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key.

6)

Repeat step numbers 4 and 5 to enter each additional flight plan waypoint.

7)

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

Nav/Com/

XPDR/AudioAFCSGPS Nav

IMPORT A FLIGHT PLAN FROM AN SD CARD

1)

Insert the SD card containing the flight plan in the top card slot on the
MFD.

2)

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

3)

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

4)

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Press the FMS Knob to activate the cursor.

5)

Turn either FMS Knob to highlight an empty or existing flight plan.

6)

Press the IMPORT Softkey.

If an empty flight plan is selected, a list of the available flight plans on the
SD card will be displayed.

Or:

If an existing flight plan is selected, an ‘Overwrite existing flight plan? OK
or CANCEL’ prompt is displayed. Press the ENT Key to choose to overwrite
the selected flight plan and see a list of the available flight plans on the SD
card. If overwriting the existing flight plan is not desired, select ‘CANCEL’
using the FMS Knob, press the ENT Key, select another existing or empty
flight plan, and again press the IMPORT Softkey.

7)

Turn the small FMS Knob to highlight the desired flight plan for importing.

8)

Press the ENT Key.

INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN

1)

Press the FPL Key to display the active flight plan.

2)

If necessary, press the FMS Knob to activate the cursor.

3)

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

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Flight Planning

4)

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

5)

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

a)

Enter the user waypoint identifier, facility, or city.

b)

Press the ENT Key.

Or:

a)

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

b)

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

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

Or:

a)

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

b)

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

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

e)

Press the ENT Key again to “accept” the waypoint.

ENTER AN AIRWAY IN A FLIGHT PLAN

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Features

1)

Press the FPL Key.

2)

Press the FMS Knob to activate the cursor (not required on the PFD).

3)

Turn the large FMS Knob to highlight the waypoint after the desired airway
entry point. If this waypoint is not a valid airway entry point, a valid entry
point should be entered at this time.

4)

Turn the small FMS Knob one click clockwise and select the LD AIRWY
Softkey, or press the MENU Key and select “Load Airway”. The Select
Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway”
menu item is available only when an acceptable airway entry waypoint has
been chosen (the waypoint ahead of the cursor position).

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Alerts Appendix Index

Flight Planning

5)

Turn the FMS Knob to select the desired airway from the list, and press the

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InstrumentsEIS

ENT Key. Low altitude airways are shown first in the list, followed by “all”

altitude airways, and then high altitude airways.

6)

Turn the FMS Knob to select the desired airway exit point from the list, and
press the ENT Key. ‘LOAD?’ is highlighted.

7)

Press the ENT Key. The system returns to editing the flight plan with the
new airway inserted.

Nav/Com/

XPDR/AudioAFCSGPS Nav

INVERT AN ACTIVE FLIGHT PLAN

1)

Press the FPL Key to display the active flight plan.

2)

Press the MENU Key to display the Page Menu.

3)

Turn the large FMS Knob to highlight ‘Invert Flight Plan’.

4)

Press the ENT Key. The original flight plan remains intact in its flight plan
catalog storage location.

Flight

5)

PlanningProcedures

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

REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT

PLAN

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Abnormal

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34

1)

Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.

Or, for a stored flight plan:

a)

Press the FPL Key on the MFD and turn the small FMS Knob to select
the Flight Plan Catalog Page.

b)

Press the FMS Knob to activate the cursor.

c)

Turn the large FMS Knob to highlight the desired flight plan.

d)

Select the EDIT Softkey.

2)

Turn the large FMS Knob to highlight the title for the approach, departure,
arrival, or airway to be deleted. Titles appear in white directly above the
procedure’s waypoints.

3)

Press the CLR Key to display a confirmation window.

4)

With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.

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Flight Planning

STORE A FLIGHT PLAN

1)

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

2)

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

3)

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

EDIT A STORED FLIGHT PLAN

1)

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

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight the desired flight plan.

4)

Select the EDIT Softkey.

5)

Turn the large FMS Knob to place the cursor in the desired location.

6)

Enter the changes, then press the ENT Key.

7)

Press the FMS Knob to return to the Flight Plan Catalog Page.

DELETE A WAYPOINT FROM THE FLIGHT PLAN

1)

Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.

Or, for a stored flight plan:

a)

Press the FPL Key on the MFD and turn the small FMS Knob to select
the Flight Plan Catalog Page.

b)

Press the FMS Knob to activate the cursor.

c)

Turn the large FMS Knob to highlight the desired flight plan.

d)

Select the EDIT Softkey.

2)

Turn the large FMS Knob to highlight the waypoint to be deleted.

3)

Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation
window.

4)

With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel
the delete request, turn the large FMS Knob to highlight ‘CANCEL’ and press
the ENT Key.

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5)

Once all changes have been made, press the FMS Knob to remove the
cursor.

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Flight Planning

INVERT AND ACTIVATE A STORED FLIGHT PLAN

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1)

Press the FPL Key on the MFD.

2)

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

3)

Press the FMS Knob to activate the cursor.

4)

Turn the large FMS Knob to highlight the desired flight plan.

5)

Select the INVERT Softkey. ‘Invert and activate stored flight plan?’ is
displayed.

6)

With ‘OK’ highlighted, press the ENT Key. The selected flight plan is now
inverted and activated. The original flight plan remains intact in its flight plan
catalog storage location.

COPY A FLIGHT PLAN

1)

Press the FPL Key on the MFD.

2)

Flight

Hazard

PlanningProcedures

Avoidance

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

3)

Press the FMS Knob to activate the cursor.

4)

Turn the large FMS Knob to highlight the flight plan to be copied.

5)

Select the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is
displayed.

6)

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

DELETE A FLIGHT PLAN

Features

Additional

1)

Press the FPL Key on the MFD.

2)

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

Abnormal

Operation

3)

Press the FMS Knob to activate the cursor.

4)

Turn the large FMS Knob to highlight the flight plan to be deleted.

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36

5)

Select the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is
displayed.

6)

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

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Flight Planning

GRAPHICAL FLIGHT PLAN CREATION

1)

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

2)

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

3)

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

4)

Select the LD WPT Softkey. The selected waypoint is inserted at the selected
point. The default user waypoint naming is USR000, USR001, USR002, and
so on.

5)

To change the user waypoint name, follow the procedure for modifying a user
waypoint.

EXPORT A FLIGHT PLAN TO AN SD CARD

1)

Insert the SD card into the top card slot on the MFD.

2)

Press the FPL Key on the Contol Unit to display the Active Flight Plan Page
on the MFD.

3)

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

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4)

Press the FMS Knob to activate the cursor.

5)

Turn the large FMS Knob to highlight the flight plan to be exported.

6)

Press the EXPORT Softkey.

7)

Press the ENT Key to confirm the export.

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PROCEDURES

LOAD AND ACTIVATE A DEPARTURE PROCEDURE

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.

3)

Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a
list of available departures.

4)

Turn the large FMS Knob to highlight the desired departure.

5)

Press the ENT Key. A list of runways may be displayed for the departure. If
so, turn either FMS Knob to select the desired runway.

6)

Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a
list of available transitions.

7)

Turn the large FMS Knob to highlight the desired transition.

8)

Press the ENT Key.

9)

With ‘LOAD?’ highlighted, press the ENT Key. The departure is active when
the flight plan is active.

Procedures

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ACTIVATE A DEPARTURE LEG

1)

Press the FPL Key on the MFD to display the active flight plan.

2)

Press the FMS Knob to activate the cursor.

3)

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

4)

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

5)

With ‘ACTIVATE’ highlighted, press the ENT Key.

LOAD AN ARRIVAL PROCEDURE

1)

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’.

3)

Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list
of available arrivals.

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Procedures

4)

Turn the large FMS Knob to highlight the desired arrival.

5)

Flight

InstrumentsEIS

Press the ENT Key. A list of transitions is displayed for the selected arrival.

6)

Turn either FMS Knob to select the desired transition.

7)

Press the ENT Key. A list of runways may be displayed for the selected
arrival.

8)

Turn the large FMS Knob to highlight the desired runway.

9)

Nav/Com/

XPDR/AudioAFCSGPS Nav

Press the ENT Key.

10)

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

11)

The arrival becomes part of the active flight plan.

12)

If an altitude associated with a waypoint in an arrival procedure is to be

used to calculate vertical guidance perform the following steps:

a)

Press the FMS Knob to activate the cursor.

b)

Turn the large FMS Knob to highlight the desired waypoint altitude.

c)

Flight

PlanningProcedures

Press the ENT Key to designate the altitude for use in giving vertical
guidance.

ACTIVATE AN ARRIVAL LEG

1)

Press the FPL Key to display the active flight plan.

2)

Hazard

Avoidance

Press the FMS Knob to activate the cursor.

3)

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

Features

4)

Additional

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

5)

Abnormal

Operation

With ‘ACTIVATE’ highlighted, press the ENT Key.

LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE

AlertsAppendixIndex

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NOTE: If certain GPS parameters (SBAS, RAIM, etc.) are not available, some

published approach procedures for the desired airport may not be displayed
in the list of available approaches.

1)

Press the PROC Key.

2)

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

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Procedures

3)

Press the ENT Key. A list of available approaches for the destination airport
is displayed.

4)

Turn either FMS Knob to highlight the desired approach.

5)

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

6)

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

7)

Press the ENT Key. The cursor moves to the MINIMUMS field.

8)

If desired, the DA/MDA for the selected approach procedure may be
entered and displayed on the PFD. Turn the small

FMS

Knob in the

direction of the green arrow to change the display from OFF to BARO.

9)

Press the

FMS

ENT

Key. The cursor moves to the altitude field. Turn the small

Knob to enter the published DA/MDA for the selected approach

procedure.

10)

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

highlighted.

11)

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

Selecting ‘LOAD?’ enters the selected approach procedure into the active
flight plan, but is not currently active. Selecting ‘ACTIVATE?’ enters the
selected approach procedure into the active flight plan and activates the
first leg of the approach.

12)

Press the ENT Key.

ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

1)

Press the PROC Key.

2)

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

3)

Press the ENT Key.

190-00567-04 Rev. A 41

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Alerts Appendix Index

Annun/

Procedures

ACTIVATE A VECTOR TO FINAL APPROACH FIX

Flight

Nav/Com/

Flight

Hazard

1)

InstrumentsEIS

ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN

XPDR/AudioAFCSGPS Nav

PlanningProcedures

Avoidance

Press the PROC Key.

2)

Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’.

3)

Press the ENT Key.

4)

The final approach course becomes the active leg.

1)

Press the PROC Key.

2)

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

3)

Press the ENT Key. A confirmation window is displayed.

4)

With ‘ACTIVATE’ highlighted, press the ENT Key.

Or:

Press the Go-around Switch.

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

42

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

Hazard Avoidance

HAZARD AVOIDANCE

CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP

1)

With the Navigation Map Page displayed, press the MENU Key to display
the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’
option.

2)

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

3)

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

XM WEATHER (OPTIONAL)

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

WARNING: Use of XM weather for hazardous weather penetration is not

recommended. Weather information provided by XM Radio Service is
approved only for weather avoidance, not penetration.

Displaying XM Weather on the Navigation Map Page

1)

Select the MAP Softkey.

2)

Select the NEXRAD or XM LTNG Softkey to display the desired weather.
Select the applicable softkey again to remove weather data from the
Navigation Map Page.

Display METAR and TAF information on the Airport Information Page

1)

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

2)

Turn the small FMS Knob to select the Airport Information Page.

3)

Select the WX Softkey to display METAR and TAF text (METAR and TAF
information is updated every 12 minutes).

Displaying Weather on the Weather Data Link Page

1)

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

2)

Turn the small FMS Knob to select the Weather Data Link Page.

3)

Select the available softkeys to select the desired XM weather product.

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00567-04 Rev. A 43

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Hazard Avoidance

4)

Select the LEGEND Softkey to view the legends for the selected products.

Flight

InstrumentsEIS

If necessary, turn either FMS Knob to scroll through the list. Press the small
FMS Knob or the ENT Key to return to the map.

Map Panning Information – Weather Data Link Page

1)

Push in the Joystick to display the panning arrow.

2)

Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs,

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

SIGMETs, PIREPs or AIREPs.

3)

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

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

Weather Products and Symbols

Echo Top (Cloud Top and Echo Top Mutually Exclusive)

Icing Potential

Hazard

Avoidance

Turbulence PIREPs

Features

Additional

TRAFFIC SYSTEMS

Abnormal

Operation

• IfTrafcinformationService(TIS)iscongured,STANDBY, OPERATE, and
TNA MUTE softkeys are displayed.

AlertsAppendixIndex

Annun/

• IfaTrafcAdvisorySystem(TAS)iscongured,STANDBY, NORMAL, TEST,
and ALT MODE softkeys are displayed.

44

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

AIREPs

NEXRAD

XM Lightning

Cloud Top

Cell Movement

SIGMETs/AIRMETs

City Forecast

METARs

Cyclone Warnings

Freezing Levels

Surface Analysis

Winds Aloft

County Warnings

190-00567-04 Rev. A

Hazard Avoidance

Traffic Symbol Description

Non-Threat Traffic

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

Proximity Advisory (PA) (Not available with TIS system)

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

Traffic Advisory (TA)

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

Traffic Advisory Off Scale

Traffic Symbol Description

Traffic Information Service (TIS)

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

NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Displaying Traffic on the Traffic Map Page

1)

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

2)

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

3)

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

4)

Select the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.

5)

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

6)

Select the TNA MUTE Softkey to mute the “Traffic Not Available” aural
alert.

190-00567-04 Rev. A 45

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Hazard Avoidance

Displaying Traffic on the Navigation Map

Flight

1)

InstrumentsEIS

Ensure TIS is operating. With the Navigation Map displayed, select the
MAP Softkey.

2)

Select the TRAFFIC Softkey. Traffic is now displayed on the map.

Traffic Advisory System (TAS) (Optional)

Nav/Com/

Flight

Hazard

Additional

Displaying Traffic on the Traffic Map Page

XPDR/AudioAFCSGPS Nav

1)

Turn the large

2)

Turn the small

FMS

Knob to select the Map Page Group.

FMS

Knob to select the Traffic Map Page. ‘OPERATING’ is

displayed in the Traffic Mode field.

3)

Select the

ALT MODE

Softkey to change the altitude volume. Select the

desired altitude volume by selecting the

UNREST

4)

Mode field.

Rotate the

PlanningProcedures

(unrestricted) Softkey. The selection is displayed in the Altitude

Joystick

clockwise to display a larger area or rotate counter-

clockwise to display a smaller area.

5)

Select the MUTE Softkey to mute TAS voice alerts.

Displaying Traffic on the Navigation Map

Avoidance

1)

Ensure TAS is operating.

2)

With the Navigation Map displayed, select the MAP Softkey.

3)

Features

Select the TRAFFIC Softkey. Traffic is now displayed on the map.

BELOW, NORMAL, ABOVE

, or

TERRAIN AND OBSTACLE PROXIMITY

Abnormal

Operation

AlertsAppendixIndex

Annun/

NOTE: Terrain data is not displayed when the aircraft latitude is greater than

75 degrees north or 60 degrees south.

Displaying Terrain and Obstacles on the Terrain Proximity Page

1)

46

Turn the large

2)

Turn the small

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

FMS

Knob to select the Map Page Group.

FMS

Knob to select the Terrain Proximity Page.

190-00567-04 Rev. A

Hazard Avoidance

3)

If desired, select the
When the
Select the

4)

Rotate the

ARC
360

Joystick

VIEW

Softkey to access the

ARC

Softkey is selected, a radar-like 120° view is displayed.

Softkey to return to the 360° default display.

clockwise to display a larger area or rotate counter-

clockwise to display a smaller area.

Color Terrain/Obstacle Location

Red

Yellow

Black

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

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

Terrain/Obstacle is more than 1000’

below aircraft altitude.

Displaying Terrain and Obstacles on the Navigation Map

1)

With the Navigation Map displayed, select the

2)

Select the

TERRAIN

Softkey. Terrain and obstacle proximity will now be

MAP

Softkey.

displayed on the map.

TERRAIN-SVS

and

360

Softkeys.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

NOTE: Terrain-SVS is only available when the Synthetic Vision System (SVS)

option is installed and the TAWS option has not been installed.

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

Display Terrain on the TERRAIN-SVS Page

1)

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

2)

Turn the small FMS Knob to select the Terrain-SVS Page.

3)

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

4)

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

190-00567-04 Rev. A 47

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Hazard Avoidance

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Enable/Disable Aviation Data

1)

While the Terrain-SVS Page is displayed, press the MENU Key.

2)

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

3)

Press the ENT Key.

Terrain-SVS Inhibit

Flight

PlanningProcedures

Inhibit Terrain Alerting

While the Terrain-SVS Page is displayed, select the INHIBIT Softkey.

Or

:

1)

Press the MENU Key.

2)

Hazard

Avoidance

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

3)

Press the ENT Key.

Color Terrain/Obstacle Location

Red

Yellow

Black

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

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

Terrain/Obstacle is more than 1000’

below aircraft altitude.

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

Enable Terrain Alerting

While the Terrain-SVS Page is displayed, select the INHIBIT Softkey.

Or

:

1)

While the Terrain-SVS Page is displayed, press the MENU Key.

2)

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

3)

Press the ENT Key.

NOTE: If Terrain-SVS alerts are inhibited when the Final Approach Fix is the

active waypoint in a GPS SBAS approach, a LOW ALT annunciation may appear
on the PFD next to the altimeter if the current aircraft altitude is at least 164
feet below the prescribed altitude at the Final Approach Fix.

48

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

Hazard Avoidance

TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY (OPTIONAL)

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

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

Manual System Test

1)

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

2)

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

3)

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

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

Display Terrain on the TAWS-B Page

1)

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

2)

Turn the small FMS Knob to select the TAWS-B Page.

3)

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

4)

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

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Color Terrain/Obstacle Location

Red

Yellow

Black

190-00567-04 Rev. A 49

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

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

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

Terrain/Obstacle is more than 1000’

below aircraft altitude.

Operation

Abnormal

Annun/

Alerts Appendix Index

Hazard Avoidance

Enable/Disable Aviation Data

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

1)

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

2)

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

3)

Press the ENT Key.

TAWS Inhibit

NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active
waypoint in a GPS SBAS approach, a LOW ALT annunciation may appear on
the PFD next to the altimeter if the current aircraft altitude is at least 164
feet below the prescribed altitude at the Final Approach Fix.

Inhibit TAWS

While the TAWS-B Page is displayed, select the INHIBIT Softkey.

Or

:

1)

Press the MENU Key.

2)

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

3)

Press the ENT Key.

Enable TAWS

While the TAWS-B Page is displayed, select the INHIBIT Softkey.

Or

:

1)

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

2)

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

Abnormal

Operation

AlertsAppendixIndex

Annun/

50

3)

Press the ENT Key.

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

Additional Features

ADDITIONAL FEATURES

SYNTHETIC VISION (OPTIONAL)

WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. SVS is intended as an aid to situational aware­ness only and may not provide either the accuracy or reliability upon which
to solely base decisions and/or plan maneuvers to avoid terrain, obstacles,
or traffic.

WARNING: Do not use SVS 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.

Synthetic Vision System (SVS) functionality is offered as an optional enhancement

to the G1000 system.

SVS is primarily comprised of a computer-generated forward-looking, attitude
aligned view of the topography immediately in front of the aircraft from the pilot’s
perspective. SVS information is shown on the primary flight display (PFD).

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

• Pathways

• Flight Path Marker

• Horizon Heading Marks

• Terrain and Obstacle Alerting

• Three-dimensional Traffic

• Airport Signs

• Runway Display

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Displaying SVS Terrain

1)

Select the PFD Softkey.

2)

Select the SYN VIS Softkey.

3)

Select the SYN TERR Softkey.

4)

Select the BACK Softkey to return to the previous page.

190-00567-04 Rev. A 51

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Alerts Appendix Index

Annun/

Additional Features

Displaying Pathways

Flight

Nav/Com/

Flight

Hazard

1)

InstrumentsEIS

XPDR/AudioAFCSGPS Nav

PlanningProcedures

Avoidance

Select the PFD Softkey.

2)

Select the SYN VIS Softkey.

3)

If not already enabled, select the SYN TERR Softkey.

4)

Select the PATHWAY Softkey.

5)

Select the BACK Softkey to return to the previous page.

Displaying Heading on the Horizon

1)

Select the PFD Softkey.

2)

Select the SYN VIS Softkey.

3)

If not already enabled, select the SYN TERR Softkey.

4)

Select the HRZN HDG Softkey.

5)

Select the BACK Softkey to return to the previous page.

Displaying Airport Signs

1)

Select the PFD Softkey.

2)

Select the SYN VIS Softkey.

3)

If not already enabled, select the SYN TERR Softkey.

4)

Select the APTSIGNS Softkey.

5)

Select the BACK Softkey to return to the previous page.

TERMINAL PROCEDURE CHARTS

Features

Additional

NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may

be necessary to carry another source of charts on-board the aircraft.

Abnormal

Operation

AlertsAppendixIndex

Annun/

SafeTaxi

SafeTaxi® is an enhanced feature that gives greater map detail as the map range

®

is adjusted in on the airport. The airport display on the map reveals runways with
numbers, taxiways identifiers, and airport landmarks including ramps, buildings,
control towers, and other prominent features. Resolution is greater at lower map
ranges. The aircraft symbol provides situational awareness while taxiing.

Selecting the DCLTR Softkey (declutter) once removes the taxiway markings and
airport identification labels. Selecting the DCLTR Softkey twice removes VOR station
ID, the VOR symbol, and intersection names if within the airport plan view. Selecting

52

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

Additional Features

the DCLTR Softkey a third time removes the airport runway layout, unless the airport
in view is part of an active route structure. Selecting the DCLTR Softkey again cycles
back to the original map detail.

The SafeTaxi database contains detailed airport diagrams for selected airports.
These diagrams provide the pilot with situational awareness by displaying the aircraft
position in relation to taxiways, ramps, runways, terminals, and services. This
information should not be used by the pilot as the basis for maneuvering the aircraft
on the ground. This database is updated on a 56-day cycle.

ChartView (Optional)

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

The ChartView database is updated on a 14-day cycle. If the ChartView database
is not updated within 70 days of the expiration date, ChartView will no longer
function.

FliteCharts

®

FliteCharts® resemble the paper version of AeroNav Services terminal procedures
charts. The charts are displayed with high-resolution and in color for applicable
charts. Current aircraft position is not displayed on FliteCharts.

The FliteCharts database contains procedure charts for the United States only.
This database is updated on a 28-day cycle. If not updated within 180 days of the
expiration date, FliteCharts will no longer function.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

View Charts from the Navigation Map Page

1)

Select the SHW CHRT Softkey when displayed.

Or

:

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

2)

Select the DP, STAR, APR, WX, and NOTAM softkeys to access charts for
departures, arrivals, approaches, weather and NOTAMs Note that NOTAMS
are only available with ChartView.

3)

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

190-00567-04 Rev. A 53

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Operation

Abnormal

Annun/

Alerts Appendix Index

Additional Features

View Charts from the Active Flight Plan Page

Flight

1)

InstrumentsEIS

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

2)

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

3)

Select the SHW CHRT Softkey. The appropriate chart is displayed, if

Nav/Com/

XPDR/AudioAFCSGPS Nav

available for the item selected.

4)

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

Change Day/Night View

1)

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

2)

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

Flight

Hazard

Additional

PlanningProcedures

Avoidance

Features

3)

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

4)

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

5)

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

6)

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

7)

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

AOPA AIRPORT DIRECTORY

Abnormal

Operation

AOPA Airport Directory adds enhanced airport information when viewing airports

on the WPT-Airport Information Page.

AlertsAppendixIndex

Annun/

This database is updated four times per year. Check fly.garmin.com for the current

database.

View Airport Directory Information

While viewing the WPT-Airport Information Page, if necessary, select the
INFO-1 Softkey to change the softkey label to display INFO-2. AOPA
airport information is displayed on the right half of the display.

54

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

Additional Features

XM® RADIO ENTERTAINMENT (OPTIONAL)

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

Selecting the XM Radio Page

1)

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

2)

Turn the small FMS Knob to select XM Radio.

3)

Select the RADIO Softkey to show the XM Radio Page where audio
entertainment is controlled.

Active Channel and Channel List

The Active Channel Box on the XM Radio Page displays the currently selected
channel. The Channels List Box of the XM Radio Page shows a list of the available
channels for the selected category.

Selecting a Category

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

1)

Select the CATGRY Softkey on the XM Radio Page.

2)

Select the CAT + and CAT - softkeys to cycle through the categories.

Or

:

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

3)

Press the ENT Key.

Select an Available Channel within the Selected Category

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

1)

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

2)

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

Or

:

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

3)

With the desired channel highlighted, press the ENT Key.

190-00567-04 Rev. A 55

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Alerts Appendix Index

Annun/

Additional Features

Entering a Channel Directly

Flight

1)

InstrumentsEIS

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

2)

Select the DIR CH Softkey. The channel number in the Active Channel Box
is highlighted.

3)

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

4)

Nav/Com/

XPDR/AudioAFCSGPS Nav

Press the ENT Key to activate the selected channel.

Assigning Channel Presets

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

1)

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

2)

Select the MORE Softkey to access the next five channels (PS6 – PS10),
and again to access the last five channels (PS11 – PS15). Selecting the

Flight

PlanningProcedures

MORE Softkey repeatedly cycles through the preset channels.

3)

Select the SET Softkey.

4)

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

Adjusting Volume

Hazard

Avoidance

1)

With the XM Radio Page displayed, select the VOL Softkey.

2)

Select the VOL – Softkey to reduce volume or select the VOL + Softkey to

Features

Additional

Abnormal

Operation

increase volume. (Once the VOL Softkey is selected, the volume can also be
adjusted using the small FMS Knob.)

3)

Select the MUTE Softkey to mute the audio. Select the MUTE Softkey
again to unmute the audio.

AlertsAppendixIndex

Annun/

56

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

Additional Features

AUXILIARY VIDEO (OPTIONAL)

There are four modes of operation of the optional auxiliary video display: Full­Screen, Full-Screen with Digital Zoom, Split-Screen with Map, and Split-Screen with
Map and Digital Zoom.

Displaying auxiliary video:

1)

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

2)

Turn the small

FMS

Knob to select VIDEO and display the AUX-VIDEO Page.

The video display softkeys shown below appear on the AUX - VIDEO Page.

Control of the AUX - VIDEO Page can also be accessed through the Page Menu.

Selecting video menu options:

1)

While viewing the AUX - VIDEO Page press the MENU Key to display the
Page Menu OPTIONS.

2)

Turn the large
and press the

FMS

Knob to highlight the desired video adjustment option

ENT

Key.

Once the ENT key is pressed on any option, the page menu closes and returns to
the AUX - VIDEO Page.

Video Setup

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Video brightness, contrast, and saturation may be adjusted be selecting the setup
function. While viewing the setup function softkeys, after 45 seconds of softkey
inactivity, the system reverts to the AUX - VIDEO Page softkeys.

Adjusting the video settings:

1)

With the AUX-VIDEO Page displayed, press the SETUP Softkey.

2)

Press the BRIGHT - or BRIGHT +, to adjust display brightness in five
percent increments from 0 to 100%.

3)

Press the CNTRST- or CNTRST +, to adjust display contrast in five
percent increments from 0 to 100%.

4)

Press the SAT - or SAT +, to adjust display saturationin five percent
increments from 0 to 100%.

5)

If desired, return the display to the default settings by pressing the RESET
Softkey.

6)

Press the BACK Softkey to return to the previous softkey level.

190-00567-04 Rev. A 57

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Additional Features

Display Selection

Flight

Pressing the HIDE MAP Softkey removes the map and displays video on the full

InstrumentsEIS

screen. The softkey label changes to grey with black characters. Pressing the HIDE
MAP Softkey again restores the map view and the small video image. The softkey label

returns to white characters on a black background.

Input Selection

Nav/Com/

While on the AUX - VIDEO Page, press the INPUT Softkey to select the EVS or

XPDR/AudioAFCSGPS Nav

AUX video source.

Zoom/Range

Pressing the VID ZM + or VID ZM - Softkeys increases or decreases video display

magnification between 1x and 10x.

The RANGE Knob can be used to increase or decrease the range setting on the
map display or zoom in and out on the video display. While in the Split-Screen
mode, pressing the MAP ACTV or VID ACTV Softkey determines which display the

Flight

PlanningProcedures

RANGE Knob adjusts. Pressing the softkey to display MAP ACTV allows the RANGE
Knob to control the range setting of the map display. Pressing the softkey to display
VID ACTV allows the RANGE Knob to control the zoom setting of the video display.

When zooming in on the video display, a Zoom Window will appear in the upper
right of the display. A box within this window indicates the portion of the display

Hazard

currently being viewed. The currently displayed portion of the full display may be

Avoidance

adjusted by using the Joystick.

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

58

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

Additional Features

ELECTRONIC CHECKLISTS

The system accesses the checklists from an SD card inserted into the bezel slot.
If the SD card contains an invalid checklist file or no checklist, the Power-up Page
messages display ‘Checklist File: Invalid’ or ‘Checklist File: N/A’ (not available) and the
CHKLIST Softkey is not available.

Accessing and Navigating Checklists

1)

From any page on the MFD, press the CHKLIST Softkey.

2)

Turn the large FMS Knob to select the ‘GROUP’ field.

3)

Turn the small FMS Knob to select the desired procedure and press the
ENT Key.

4)

Turn the large FMS Knob to select the ‘CHECKLIST’ field.

5)

Turn the FMS Knob to select the desired checklist and press the ENT Key.
The selected checklist item is indicated with white text surrounded by a
white box.

6)

Press the ENT Key or CHECK Softkey to check the selected checklist item.
The line item turns green and a checkmark is placed in the associated box.
The next line item is automatically selected for checking.

Either FMS Knob can be used to scroll through the checklist and select the
desired checklist item.

Press the CLR Key or UNCHECK Softkey to remove a check mark from an
item.

7)

When all checklist items have been checked, ‘*Checklist Finished*’ is
displayed in green text at the bottom left of the checklist window. If all
items in the checklist have not been checked, ‘*CHECKLIST NOT FINISHED*’
will be displayed in yellow text.\

8)

Press the ENT Key. ‘GO TO NEXT CHECKLIST?’ will be highlighted by the
cursor.

9)

Press the ENT Key to advance to the next checklist.

10)

Press the EXIT Softkey to exit the Checklist Page and return to the page

last viewed.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00567-04 Rev. A 59

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Additional Features

Immediately Accessing Emergency Procedures

Flight

InstrumentsEIS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

1)

From any page on the MFD, press the CHKLIST Softkey.

2)

Press the EMERGCY Softkey.

3)

Turn the FMS Knob to select the desired emergency checklist and press the
ENT Key.

4)

Press the ENT Key or CHECK Softkey to check the selected emergency
checklist item. The line item turns green and a checkmark is placed in the
box next to it. The next line item is automatically highlighted for checking.

Either FMS Knob can be used to scroll through the checklist and select the
desired checklist item.

Press the CLR Key or UNCHECK Softkey to remove a check mark from an
item.

5)

When all checklist items have been checked, ‘*Checklist Finished*’ is
displayed in green text at the bottom left of the checklist window. If all
items in the checklist have not been checked, ‘*CHECKLIST NOT FINISHED*’
will be displayed in yellow text.\

6)

Press the ENT Key. ‘GO TO NEXT CHECKLIST?’ will be highlighted by the
cursor.

7)

Press the ENT Key to advance to the next checklist.

8)

Press the RETURN Softkey to return to the previous checklist.

9)

Press the EXIT Softkey to exit the Checklist Page and return to the page
last viewed.

Abnormal

Operation

AlertsAppendixIndex

Annun/

60

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

Abnormal Operation

ABNORMAL OPERATION

REVERSIONARY MODE

Should a system detected failure occur in either display, the G1000 automatically
enters reversionary mode. In reversionary mode, critical flight instrumentation is
combined with engine instrumentation on the remaining display.

Reversionary display mode can be manually activated by pressing the DISPLAY

BACKUP Button on the audio panel.

NOTE: The Cessna Corvalis/Corvalis TT Airplane Flight Manual (AFM) always
takes precedence over the information found in this section.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

ABNORMAL COM OPERATION

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

AUDIO PANEL FAIL-SAFE OPERATION

If there is a failure of the Audio Panel, a fail-safe circuit connects the pilot’s headset
and microphone directly to the COM1 transceiver. Audio is not available on the
speaker during Fail-safe operation.

HAZARD DISPLAYS WITH LOSS OF GPS POSITION

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

Loss of Hazard Functions with Loss of GPS

Position

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00567-04 Rev. A 61

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Abnormal Operation

UNUSUAL ATTITUDES

Flight

The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary

InstrumentsEIS

functions are displayed in these situations.

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

are disabled) when the aircraft experiences unusual attitudes:

• TrafcAnnunciations

• AFCSAnnunciations

Nav/Com/

XPDR/AudioAFCSGPS Nav

• FlightdirectorCom­mand Bars

• InsetMap

• Temperatures

• DMEInformation

Window

• WindData

• SelectedHeadingBox

Flight

PlanningProcedures

• SelectedCourseBox

• TransponderStatus

Box

Hazard

Avoidance

• SystemTime

• PFDSetupMenu

• Windowsdisplayedin

the lower right corner

of the PFD:
– Timer/References
– Nearest Airports
– Flight Plan
– Messages
– Procedures
– ADF/DME Tuning

• BarometricMinimum

Descent Altitude Box

• Glideslope,Glide­path, and Vertical
Deviation Indicators

• AltimeterBarometric

Setting

• SelectedAltitude

• VNV Target Altitude

Features

Additional

Extreme Pitch Indication

Abnormal

Operation

DEAD RECKONING

AlertsAppendixIndex

Annun/

While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS
solution or is unable to calculate a GPS position, the system automatically reverts to
Dead Reckoning (DR) Mode. In DR Mode, the G1000 uses its last-known position
combined with continuously updated airspeed and heading data (when available) to
calculate and display the aircraft’s current estimated position.

62

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

Abnormal Operation

NOTE: Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic
(OCN) phase of flight. In all other phases, an invalid GPS solution produces
a “NO GPS POSITION” annunciation on the map and the G1000 stops
navigating in GPS Mode.

DR Mode is indicated on the G1000 by the appearance of the letters ‘DR’
superimposed in yellow over the ‘own aircraft’ symbol as shown in the following
figure. In addition, ‘DR’ is prominently displayed, also in yellow, on the HSI slightly
above and to the right of the aircraft symbol on the CDI as shown in the following
figure. The CDI deviation bar is displayed in yellow, but will be removed from the
display after 20 minutes. Lastly, but at the same time, a ‘GPS NAV LOST’ alert message
appears on the PFD.

Normal navigation using GPS/SBAS source data resumes automatically once a valid
GPS solution is restored.

It is important to note that estimated navigation data supplied by the G1000 in
DR Mode may become increasingly unreliable and must not be used as a sole means
of navigation. If, while in DR Mode, airspeed and/or heading data is also lost or
not available, the DR function may not be capable of estimating your position and,
consequently, the system may display a path that is different than the actual movement
of the aircraft. Estimated position information displayed by the G1000 through
DR while there is no heading and/or airspeed data available should not be used for
navigation.

DR Mode is inherently less accurate than the standard GPS/SBAS Mode due to the
lack of satellite measurements needed to determine a position. Changes in wind speed
and/or wind direction compounds the relative inaccuracy of DR Mode. Because of this
degraded accuracy, the crew must maintain position awareness using other navigation
equipment until GPS-derived position data is restored.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

CDI ‘DR’ Indication on PFD

Symbolic Aircraft

(Map pages and Inset Map)

Dead Reckoning Indications

190-00567-04 Rev. A 63

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Alerts Appendix Index

Annun/

Abnormal Operation

As a result of operating in DR Mode, all GPS-derived data is computed based upon

an estimated position and is displayed as yellow text on the display to denote degraded

Flight

InstrumentsEIS

navigation source information. This data includes the following:

• NavigationStatusBoxeldsexceptActiveLeg,TAS,andDTK

• GPSBearingPointer

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

• CurrentTrackIndicator

Nav/Com/

• AllBearingPointerDistances

XPDR/AudioAFCSGPS Nav

• ActiveFlightPlandistances,bearings,andETEvalues

Also, while the G1000 is in DR Mode, the autopilot will couple to GPS for up to 20
minutes. Terrain Proximity, TERRAIN-SVS, and TAWS are also disabled. Additionally,
the accuracy of all nearest information (airports, airspaces, and waypoints) is
questionable. Finally, airspace alerts continue to function, but with degraded
accuracy.

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

64

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

ANNUNCIATIONS & ALERTS

WARNING ALERTS

Annunciations & Alerts

Instruments EIS

Flight

Annunciation Window

Text

Alerts Window Message Audio Alert/Voice

Message

(Repeating)

DOOR OPEN Door not secured Chime/”Door Open”

FUEL VALVE Fuel tank is not correctly selected

Chime/”Fuel Valve”

or in OFF position

L BUS OFF No power on the left bus Chime
R BUS OFF No power on the right bus Chime

CO LVL HIGH Carbon Monoxide level is too high Chime/”Carbon Monoxide”

OIL PRES LOW Low oil pressure Chime/”Oil Pressure Low”

CAUTION ALERTS

Annunciation Window

Text

L ALT OFF Left Alternator offline Single Chime/”Left

R ALT OFF Right Alternator offline Single Chime/”Right

FUEL PUMP Fuel pump is operating Single Chime/”Fuel Pump”

L-LOW FUEL Low fuel in the left tank Single Chime/None

Alerts Window Message Audio Alert/Voice

Message

Alternator Out”

Alternator Out”

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

R LOW FUEL Low fuel in the right tank Single Chime/None

OXYGEN

Pressure above 12,000 ft and

Single Chime/None

oxygen off

OXYGEN PRES



Oxygen outlet pressure below 60

Single Chime/None

psi

OXYGEN PRES

†

Oxygen outlet pressure below

Single Chime/None

16.5 psi

OXYGEN QTY Oxygen quantity below 250 psi. Single Chime/None

RUDR LMTR * Rudder limter is engaged Single Chime/None

STARTER ENGD Starter relay has power applied Single Chime/None

*Corvalis only / High pressure oxygen outlet only / †Low pressure oxygen outlet only

190-00567-04 Rev. A 65

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Operation

Abnormal

Annun/

Alerts Appendix Index

Annunciations & Alerts

ANNUNCIATION ADVISORY

Flight

Annunciation Window

InstrumentsEIS

Alerts Window Message Audio Alert

Text

AP/TRIM OFF

AP/TRIM master switch is in the OFF position None

OXYGEN ON Reminder: Turn off oxygen None

RUDR HOLD * Rudder hold is engaged None

Nav/Com/

XPDR/AudioAFCSGPS Nav

SPEED BRAKES Speed brakes are active None

* Corvalis TT only

MESSAGE ADVISORY ALERTS

Alerts Window Message Audio Alert

PFD FAN FAIL – The cooling fan for the PFD is inoperative. None
MFD FAN FAIL – The cooling fan for the MFD is inoperative. None

Flight

AVIONICS FAN – The cooling fan for remote avionics is inoperative. None

PlanningProcedures

TIMER ZERO – Timer has counted down to zero. “Timer Expired”
FUEL IMBAL – Fuel imbalance is greater than 10 gallons. None
LOW MAN PRES – Manifold pressure is below 15 in. None
VAPOR SUPPR – Turn on Vapor Suppression.* None

Hazard

* Corvalis TT only

Avoidance

CO GUARDIAN MESSAGES

Features

Additional

Alerts Window Message Comments

CO DET SRVC – The carbon

Abnormal

Operation

monoxide detector needs
service.

AlertsAppendixIndex

Annun/

CO DET FAIL – The carbon

monoxide detector is inopera­tive.

66

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

There is a problem within
the CO Guardian that
requires services.

Loss of communication
between the G1000 and
the CO Guardian.

190-00567-04 Rev. A

Annunciations & Alerts

AFCS ALERTS

Condition Annunciation Description

Pitch Failure Pitch axis control failure. AP is inoperative.

Roll Failure Roll axis control failure. AP is inoperative.

MET Switch Stuck, or

Pitch Trim Axis Control

Failure

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

Elevator Mistrim Up A condition has developed causing the pitch

Elevator Mistrim Down A condition has developed causing the pitch

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

Aileron Mistrim Right A condition has developed causing the roll servo

Preflight Test Performing preflight system test. Upon

If annunciated when AP is engaged, take control
of the aircraft and disengage the autopilot. If
annunciated when AP is not engaged, move each
half of the MET switch separately to check if a
stuck switch is causing the annunciation.

available.

servo to provide a sustained force. Be prepared
to apply nose up control wheel force upon
autopilot disconnect.

servo to provide a sustained force. Be prepared
to apply nose down control wheel force upon
autopilot disconnect.

provide a sustained left force. Ensure the slip/skid
indicator is centered and observe any maximum
fuel imbalance limits.

to provide a sustained right force. Ensure the
slip/skid indicator is centered and observe any
maximum fuel imbalance limits.

completion, the aural alert will be heard.
Preflight system test has failed.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00567-04 Rev. A 67

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Annunciations & Alerts

TERRAIN-SVS ALERTS

Flight

InstrumentsEIS

Alert Type

PFD/MFD

TERRAIN-SVS

Page

Annunciation

Reduced Required Terrain
Clearance Warning (RTC)

Nav/Com/

Imminent Terrain Impact

XPDR/AudioAFCSGPS Nav

Warning (ITI)

Reduced Required Obstacle
Clearance Warning (ROC)

Imminent Obstacle Impact
Warning (IOI)

Reduced Required Terrain
Clearance Caution (RTC)

Flight

Imminent Terrain Impact

PlanningProcedures

Caution (ITI)

Reduced Required Obstacle
Clearance Caution (ROC)

Imminent Obstacle Impact
Caution (IOI)

Hazard

Avoidance

Terrain-SVS System Status Annunciations

MFD

Pop-Up Alert

Aural

Message

“Warning; Terrain,

Terrain”

“Warning; Terrain,

Terrain”

“Warning; Obstacle,

Obstacle”

“Warning; Obstacle,

Obstacle”

“Caution; Terrain,

Terrain”

“Caution; Terrain,

Terrain”

“Caution; Obstacle,

Obstacle”

“Caution; Obstacle,

Obstacle”

Features

Additional

Abnormal

Operation

Alert Type

System Test in Progress TERRAIN TEST None

PFD/MFD Alert

Annunciation

TERRAIN-SVS Page

Annunciation

System Test Pass None None

AlertsAppendixIndex

Annun/

Terrain System Test Fail TERRAIN FAIL

Terrain or Obstacle
database unavailable or
invalid, invalid software

TERRAIN FAIL

configuration, system
audio fault

68

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Aural

Message

“Terrain System

Test OK”

“Terrain System

Failure”

“Terrain System

Failure”

190-00567-04 Rev. A

Annunciations & Alerts

Alert Type

PFD/MFD Alert

Annunciation

TERRAIN-SVS Page

Annunciation

MFD Terrain or Obstacle
database unavailable
or invalid. System
operating with PFD

None TERRAIN DATABASE FAILURE None

Terrain or Obstacle
databases

No GPS position NO GPS POSITION

Excessively degraded
GPS signal or out of

None

database coverage area

Sufficient GPS signal
received after loss or
database coverage area

None None

entered

TAWS-B ALERTS

Alert Type

Excessive Descent
Rate Warning (EDR)

Reduced Required
Terrain Clearance
Warning (RTC)

Imminent Terrain
Impact Warning (ITI)

Reduced Required
Obstacle Clearance
Warning (ROC)

PFD/MFD
TAWS-B Page
Annunciation

MFD

Pop-Up Alert

or

or

or

Aural

Message

“Terrain System

Not Available”

“Terrain System

Not Available”

“Terrain System

Available”

Aural Message

“Pull Up”

“Terrain, Terrain; Pull Up,

Pull Up”

or

“Terrain Ahead, Pull Up;

Terrain Ahead, Pull Up”

Terrain Ahead, Pull Up;

Terrain Ahead, Pull Up”

or

“Terrain, Terrain; Pull Up,

Pull Up”

“Obstacle, Obstacle; Pull

Up, Pull Up”

or

“Obstacle Ahead, Pull Up;

Obstacle Ahead, Pull Up”

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00567-04 Rev. A 69

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Annunciations & Alerts

Flight

Alert Type

InstrumentsEIS

Imminent Obstacle
Impact Warning
(IOI)

Nav/Com/

XPDR/AudioAFCSGPS Nav

Reduced Required
Terrain Clearance
Caution (RTC)

Imminent Terrain
Impact Caution (ITI)

Flight

PlanningProcedures

Reduced Required
Obstacle Clearance
Caution (ROC)

Hazard

Avoidance

Imminent Obstacle
Impact Caution (IOI)

Features

Additional

Premature Descent
Alert Caution (PDA)

Abnormal

Operation

Altitude Callout
“500”

AlertsAppendixIndex

Annun/

Excessive Descent
Rate Caution (EDR)

Negative Climb
Rate Caution (NCR)

PFD/MFD

TAWS-B Page

Annunciation

MFD

Pop-Up Alert

Aural Message

“Obstacle Ahead, Pull Up;

or

Obstacle Ahead, Pull Up”

“Obstacle, Obstacle; Pull

“Caution, Terrain; Caution,

or

“Terrain Ahead; Terrain

“Terrain Ahead; Terrain

or

“Caution, Terrain; Caution,

“Caution, Obstacle; Cau-

or

tion, Obstacle”

“Obstacle Ahead; Obstacle

“Obstacle Ahead; Obstacle

or

“Caution, Obstacle; Cau-

tion, Obstacle”

“Too Low, Terrain”

None None “Five-Hundred”

or

“Too Low, Terrain”

or

Up, Pull Up”

Terrain”

or

Ahead”

Ahead”

or

Terrain”

or

Ahead”

Ahead”

or

“Sink Rate”

“Don’t Sink”

or

70

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

190-00567-04 Rev. A

Annunciations & Alerts

TAWS-B System Status Annunciations

Alert Type

PFD/MFD Alert

Annunciation

System Test in
Progress

System Test Pass None None

TAWS-B System Test
Fail

Terrain or Obstacle
database unavailable
or invalid,
invalid software
configuration, system
audio fault

MFD Terrain or
Obstacle database
unavailable or invalid.
System operating

None TERRAIN DATABASE FAILURE None

with PFD Terrain or
Obstacle databases

No GPS position NO GPS POSITION

Excessively degraded
GPS signal or out of
database coverage
area

Sufficient GPS signal
received after loss or
database coverage

None None “TAWS Available”

area entered

TAWS-B Page

Annunciation

TAWS TEST None

TAWS FAIL

TAWS FAIL

None

Aural

Message

“TAWS System

Test OK”

“TAWS System

Failure”

“TAWS System

Failure”

“TAWS Not

Available”

“TAWS Not

Available”

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00567-04 Rev. A 71

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Annunciations & Alerts

VOICE ALERTS

Flight

InstrumentsEIS

Voice Alert Description

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

descent altitude.

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

vertical navigation is enabled.

Nav/Com/

XPDR/AudioAFCSGPS Nav

“Traffic” Played when a Traffic Advisory (TA) is issued.

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

“Traffic, Traffic” Played when a Traffic Advisory (TA) is issued (TAS system).

“Traffic Advisory System

Played when the TAS system passes a pilot-initiated self test.

Test Passed”

“Traffic Advisory System

Played when the TAS system fails a pilot-initiated self test.

Test Failed”

MFD & PFD MESSAGE ADVISORIES

Flight

PlanningProcedures

Message Comments

DATA LOST

was lost. Recheck settings.

– Pilot stored data

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

Hazard

Avoidance

XTALK ERROR

– A flight display

crosstalk error has occurred.

Features

Additional

PFD1 SERVICE

– PFD1 needs

service. Return unit for repair.

Abnormal

Operation

MFD1 SERVICE

– MFD1 needs

settings, if desired.
The MFD and PFDs are not communicating

with each other. The G1000 system should be
serviced.

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

service. Return unit for repair.

AlertsAppendixIndex

Annun/

MANIFEST

mismatch, communication halted.

MANIFEST

– PFD1 software

– MFD1 software

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

mismatch, communication halted.

PFD1 CONFIG

Config service req’d.

– PFD1 config error.

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

72

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190-00567-04 Rev. A

Annunciations & Alerts

MFD & PFD MESSAGE ADVISORIES (CONT.)

Message Comments

MFD1 CONFIG

error. Config service req’d.

– MFD1 config

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

SW MISMATCH

version mismatch. Xtalk is off.

PFD1 COOLING

cooling. Reducing power usage.

MFD1 COOLING

cooling. Reducing power usage.

PFD1 KEYSTK

Key is stuck.

MFD1 KEYSTK

Key is stuck.

CNFG MODULE

configuration module is
inoperative.

PFD1 VOLTAGE

voltage. Reducing power usage

MFD1 VOLTAGE

voltage. Reducing power usage

– GDU software

– PFD1 has poor

– MFD1 has poor

– PFD1 [key name]

– MFD [key name]

– PFD1

– PFD1 has low

– MFD1 has low

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

The PFD and/or MFD is overheating and is
reducing power consumption by dimming the
display. If problem persists, the G1000 system
should be serviced.

A key is stuck on the PFD and/or MFD bezel.
Attempt to free the stuck key by pressing it
several times. The G1000 system should be
serviced if the problem persists.

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

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

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

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

DATABASE MESSAGE ADVISORIES

Message Comments

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

MFD1 DB ERR

database error exists.

PFD1 DB ERR

– MFD1 aviation

– PFD1 aviation

– MFD1 basemap

– PFD1 basemap

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

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

database error exists.

190-00567-04 Rev. A 73

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Operation

Abnormal

Annun/

Alerts Appendix Index

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEIS

Message Comments

MFD1 DB ERR

database error exists.

PFD1 DB ERR

– PFD1 terrain

database error exists.

Nav/Com/

XPDR/AudioAFCSGPS Nav

MFD1 DB ERR

database missing.

PFD1 DB ERR

– PFD1 terrain

database missing.

MFD1 DB ERR

database error exists.

PFD1 DB ERR

Flight

database error exists.

PlanningProcedures

– PFD1 obstacle

MFD1 DB ERR

database missing.

PFD1 DB ERR

– PFD1 obstacle

database missing.

Hazard

MFD1 DB ERR

Avoidance

terrain database error exists.

PFD1 DB ERR

Features

Additional

terrain database error exists.

– PFD1 airport

MFD1 DB ERR

Abnormal

Operation

terrain database missing.

PFD1 DB ERR

AlertsAppendixIndex

terrain database missing.

Annun/

– PFD1 airport

MFD1 DB ERR

database error exists.

PFD1 DB ERR

– PFD1 Safe Taxi

database error exists.

– MFD1 terrain

– MFD1 terrain

– MFD1 obstacle

– MFD1 obstacle

– MFD1 airport

– MFD1 airport

– MFD1 Safe Taxi

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

The terrain database is present on another LRU,
but is missing on the specified LRU.

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

The obstacle database is present on another LRU,
but is missing on the specified LRU.

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

The airport terrain database is present on
another LRU, but is missing on the specified LRU.

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

74

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Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Message Comments

MFD1 DB ERR

database error exists.

– MFD1 Chartview

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

MFD1 DB ERR

database error exists.

– MFD1 FliteCharts

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

DB MISMATCH

database version mismatch. Xtalk
is off.

– Aviation

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

DB MISMATCH

database type mismatch. Xtalk is
off.

– Aviation

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

DB MISMATCH

version mismatch.

– Terrain database

The PFDs and MFD have different terrain
database versions installed. Install correct terrain
database version in all displays.

DB MISMATCH

type mismatch.

– Terrain database

The PFDs and MFD have different terrain
database types installed. Install correct terrain
database type in all displays.

DB MISMATCH

database version mismatch.

– Obstacle

The PFDs and MFD have different obstacle
database versions installed. Install correct
obstacle database version in all displays.

DB MISMATCH

database mismatch.

– Airport Terrain

The PFDs and MFD have different airport terrrain
databases installed. Install correct airport terrain
database in all displays.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00567-04 Rev. A 75

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Annunciations & Alerts

GMA 1347 MESSAGE ADVISORIES

Flight

InstrumentsEIS

GMA1 FAIL

GMA1 CONFIG

error. Config service req’d.

Nav/Com/

XPDR/AudioAFCSGPS Nav

Message Comments

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

– GMA1 config

MANIFEST – GMA1 software
mismatch, communication halted.

GMA1 SERVICE – GMA1 needs
service. Return unit for repair.

Flight

PlanningProcedures

GIA 63 MESSAGE ADVISORIES

Message Comments

GIA1 CONFIG – GIA1 config error.
Config service req’d.

Hazard

Avoidance

GIA2 CONFIG – GIA2 config error.

Config service req’d.

Features

Additional

GIA1 CONFIG – GIA1 audio config

error. Config service req’d.

GIA2 CONFIG – GIA2 audio config

Abnormal

Operation

error. Config service req’d.

GIA1 COOLING – GIA1 temperature

AlertsAppendixIndex

Annun/

too low.
GIA2 COOLING – GIA2 temperature

too low.
GIA1 COOLING – GIA1 over

temperature.
GIA2 COOLING – GIA2 over

temperature.

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

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

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

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

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

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

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

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

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Annunciations & Alerts

GIA 63 MESSAGE ADVISORIES (CONT.)

Message

Comments

GIA1 SERVICE – GIA1 needs service.
Return the unit for repair.

GIA2 SERVICE – GIA2 needs service.
Return the unit for repair.

MANIFEST – GIA1 software mismatch,
communication halted.

MANIFEST – GIA2 software mismatch,
communication halted.

COM1 TEMP – COM1 over temp.
Reducing transmitter power.

COM2 TEMP – COM2 over temp.
Reducing transmitter power.

COM1 SERVICE – COM1 needs ser­vice. Return unit for repair.

COM2 SERVICE – COM2 needs ser­vice. Return unit for repair.

COM1 PTT – COM1 push-to-talk key
is stuck.

COM2 PTT – COM2 push-to-talk key
is stuck.

COM1 RMT XFR – COM1 remote
transfer key is stuck.

COM2 RMT XFR – COM2 remote
transfer key is stuck.

RAIM UNAVAIL – RAIM is not
available from FAF to MAP waypoints.

Instruments EIS

The GIA1 and/or GIA2 self-test has detected a
problem in the unit. The G1000 system should
be serviced.

XPDR/Audio AFCS GPS Nav

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

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

Planning Procedures

be serviced.

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

Avoidance

The COM1 and/or COM2 external push-to-talk
switch is stuck in the enable (or “pressed”)
position. Press the PTT switch again to cycle its

Features

operation.
If the problem persists, the G1000 system

Operation

should be serviced.
The COM1 and/or COM2 transfer switch is

stuck in the enabled (or “pressed”) position.

Alerts Appendix Index

Press the transfer switch again to cycle its
operation. If the problem persists, the G1000
system should be serviced.

GPS satellite coverage is insufficient to perform
Receiver Autonomous Integrity Monitoring
(RAIM) from the FAF to the MAP waypoints.

Flight

Nav/Com/

Flight

Hazard

Additional

Abnormal

Annun/

190-00567-04 Rev. A 77

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Annunciations & Alerts

GIA 63 MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEIS

Message Comments

LOI – GPS integrity lost. Crosscheck

with other NAVS.
GPS NAV LOST – Loss of GPS naviga-

tion. Insufficient satellites.

GPS NAV LOST – Loss of GPS

Nav/Com/

XPDR/AudioAFCSGPS Nav

navigation. Position error.
GPS NAV LOST – Loss of GPS

navigation. GPS fail.
ABORT APR – Loss of GPS navigation.

Abort approach.
TRUE APR – True north approach.

Change hdg reference to TRUE.

Flight

PlanningProcedures

GPS1 FAIL – GPS1 is inoperative.

GPS2 FAIL – GPS2 is inoperative.

GPS1 SERVICE

Return unit for repair.

Hazard

Avoidance

GPS2 SERVICE

– GPS1 needs service.

– GPS2 needs service.

Return unit for repair.

Features

Additional

NAV1 SERVICE

– NAV1 needs service.

Return unit for repair.

NAV2 SERVICE

Abnormal

Operation

– NAV2 needs service.

Return unit for repair.

NAV1 RMT XFR

AlertsAppendixIndex

Annun/

transfer key is stuck.

NAV2 RMT XFR

– NAV1 remote

– NAV2 remote

transfer key is stuck.

G/S1 FAIL – G/S1 is inoperative.

G/S2 FAIL – G/S2 is inoperative.

Loss of GPS integrity monitoring.

Loss of GPS navigation due to insufficient
satellites.

Loss of GPS navigation due to position error.

Loss of GPS navigation due to GPS failure.

Abort approach due to loss of GPS navigation.

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

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

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

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

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

A failure has been detected in glideslope
receiver 1 and/or receiver 2. The G1000 system
should be serviced.

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Annunciations & Alerts

GIA 63 MESSAGE ADVISORIES (CONT.)

Message Comments

G/S1 SERVICE – G/S1 needs service.

Return unit for repair.
G/S2 SERVICE – G/S2 needs service.

Return unit for repair.

GIA 63W MESSAGE ADVISORIES

Message Comments

GIA1 CONFIG

Config service req’d.

– GIA1 config error.

The GIA1 and/or GIA2 configuration settings do
not match backup configuration memory. The

GIA2 CONFIG

– GIA2 config error.

G1000 system should be serviced.

Config service req’d.

GIA1 CONFIG

error. Config service req’d.

– GIA1 audio config

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

GIA2 CONFIG

– GIA2 audio config

be serviced.

error. Config service req’d.

GIA1 COOLING

temperature too low.

– GIA1

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

GIA2 COOLING

– GIA2

operating temperature.

temperature too low.

GIA1 COOLING

temperature.

– GIA1 over

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

GIA2 COOLING

– GIA2 over

serviced.

temperature.

GIA1 SERVICE

service. Return the unit for repair.

– GIA1 needs

The GIA1 and/or GIA2 self-test has detected a
problem in the unit. The G1000 system should

GIA2 SERVICE

– GIA2 needs

be serviced.

service. Return the unit for repair.

A failure has been detected in glideslope
receiver 1 and/or receiver 2. The receiver may
still be available. The G1000 system should be
serviced when possible.

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00567-04 Rev. A 79

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEIS

HW MISMATCH

Message Comments

– GIA hardware
mismatch. GIA1 communication
halted.

HW MISMATCH

mismatch. GIA2 communication

Nav/Com/

XPDR/AudioAFCSGPS Nav

– GIA hardware

halted.

MANIFEST

– GIA1 software

mismatch, communication halted.

MANIFEST

– GIA2 software

mismatch, communication halted.

MANIFEST

– GFC software

mismatch, communication halted.

Flight

PlanningProcedures

COM1 TEMP

– COM1 over temp.

Reducing transmitter power.

COM2 TEMP

– COM2 over temp.

Reducing transmitter power.

COM1 SERVICE

Hazard

service. Return unit for repair.

Avoidance

COM2 SERVICE

– COM1 needs

– COM2 needs

service. Return unit for repair.

Features

Additional

COM1 PTT

– COM1 push-to-talk

key is stuck.

COM2 PTT

Abnormal

Operation

– COM2 push-to-talk

key is stuck.

AlertsAppendixIndex

Annun/

COM1 RMT XFR

– COM1 remote

transfer key is stuck.

COM2 RMT XFR

– COM2 remote

transfer key is stuck.

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

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

Incorrect servo software is installed, or gain
settings are incorrect.

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

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

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

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

80

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190-00567-04 Rev. A

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Message Comments

LOI

– GPS integrity lost. Crosscheck

with other NAVS.

GPS NAV LOST

– Loss of GPS

navigation. Insufficient satellites.

GPS NAV LOST

– Loss of GPS

navigation. Position error.

GPS NAV LOST

– Loss of GPS

navigation. GPS fail.

ABORT APR

– Loss of GPS

navigation. Abort approach.

APR DWNGRADE

– Approach

downgraded.

TRUE APR

– True north approach.

Change HDG reference to TRUE.

GPS integrity is insufficient for the current phase
of flight.

Loss of GPS navigation due to insufficient
satellites.

Loss of GPS navigation due to position error.

Loss of GPS navigation due to GPS failure.

Abort approach due to loss of GPS navigation.

Vertical guidance generated by SBAS is
unavailable, use LNAV only minimums.

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

GPS1 SERVICE

service. Return unit for repair.

– GPS1 needs

A failure has been detected in the GPS1 and/
or GPS2 receiver. The receiver may still be

GPS2 SERVICE

– GPS2 needs

available. The G1000 system should be serviced.

service. Return unit for repair.

NAV1 SERVICE

service. Return unit for repair.

– NAV1 needs

A failure has been detected in the NAV1 and/
or NAV2 receiver. The receiver may still be

NAV2 SERVICE

– NAV2 needs

available. The G1000 system should be serviced.

service. Return unit for repair.

NAV1 RMT XFR

transfer key is stuck.

NAV2 RMT XFR

transfer key is stuck.

– NAV1 remote

– NAV2 remote

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

G/S1 FAIL

G/S2 FAIL

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

– G/S2 is inoperative.

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

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-00567-04 Rev. A 81

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEIS

G/S1 SERVICE

Message Comments

– G/S1 needs

service. Return unit for repair.

G/S2 SERVICE

– G/S2 needs

service. Return unit for repair.

Nav/Com/

XPDR/AudioAFCSGPS Nav

GEA 71 MESSAGE ADVISORIES

Message Comments

GEA1 CONFIG

– GEA1 config error.

Config service req’d.

MANIFEST

mismatch, communication halted.

Flight

PlanningProcedures

– GEA1 software

GTX 33 MESSAGE ADVISORIES

Message Comments

XPDR1 CONFIG

error. Config service req’d.

Hazard

Avoidance

MANIFEST

mismatch, communication halted.

Features

Additional

XPDR1 SRVC

– XPDR1 config

– GTX1 software

– XPDR1 needs

service. Return unit for repair.

Abnormal

Operation

XPDR1 FAIL

– XPDR1 is

inoperative.

AlertsAppendixIndex

Annun/

A failure has been detected in glideslope
receiver 1 and/or receiver 2. The receiver may
still be available. The G1000 system should be
serviced when possible.

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

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

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

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

The #1 transponder should be serviced when
possible.

There is no communication with the #1
transponder.

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Annunciations & Alerts

GRS 77 MESSAGE ADVISORIES

Message Comments

AHRS1 TAS

– AHRS1 not receiving

valid airspeed.

AHRS1 GPS

– AHRS1 using backup

GPS source.

AHRS1 GPS

– AHRS1 not receiving

any GPS information.

AHRS1 GPS

– AHRS1 not receiving

backup GPS information.

AHRS1 GPS

– AHRS1 operating

exclusively in no-GPS mode.

AHRS1 SRVC

– AHRS1 Magnetic-

field model needs update.

GEO LIMITS

– AHRS1 too far

North/South, no magnetic compass.

MANIFEST

– GRS1 software

mismatch, communication halted.

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

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

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

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

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

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

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

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

Instruments EIS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

GMU 44 MESSAGE ADVISORIES

Message Comments

HDG FAULT

magnetometer fault has occurred.

– AHRS1

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

MANIFEST

mismatch, communication halted.

190-00567-04 Rev. A 83

– GMU1 software

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

Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT

Alerts Appendix Index

Annun/

Annunciations & Alerts

GDL 69A MESSAGE ADVISORIES

Flight

InstrumentsEIS

GDL69 CONFIG

Message Comments

– GDL 69 config

error. Config service req’d.

Nav/Com/

XPDR/AudioAFCSGPS Nav

GDL69 FAIL

MANIFEST

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

– GDL software

mismatch, communication halted.

GDC 74A MESSAGE ADVISORIES

Flight

PlanningProcedures

MANIFEST

Message Comments

– GDC1 software

mismatch, communication halted.

GCU 476 MESSAGE ADVISORIES

Hazard

Avoidance

GCU CNFG

Message Comments

– GCU Config error.

Config service req’d.

Features

Additional

Abnormal

Operation

GCU FAIL

MANIFEST

– GCU is inoperative. A failure has been detected in the GCU 476.

– GCU software

mismatch, communication halted.

GCU KEYSTK

AlertsAppendixIndex

Annun/

– GCU [key name] Key

is stuck.

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

The receiver is unavailable. The G1000 system
should be serviced

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

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

GCU 476 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.

The GCU 476 is unavailable.
The GCU 476 has incorrect software installed.

The G1000 system should be serviced.
A key is stuck on the GCU 476 bezel. Attempt

to free the stuck key by pressing it several
times. The G1000 system should be serviced if
the problem persists.

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