Garmin TBM700 Reference Guide

G1000

®

Integrated Flight Deck

Cockpit Reference Guide

FLIGHT INSTRUMENTS

ENGINE & AIRFRAME SYSTEMS

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 © 2010 Garmin Ltd. or its subsidiaries. All rights reserved.

This manual reflects the operation of System Software version 0829.00 or later for the Socata
TBM 700 A, B, C, and N. 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]

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

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

AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively
“AOPA”) expressly disclaim all warranties, with respect to the AOPA information included in this
data, express or implied, including, but not limited to, the implied warranties of merchantability
and fitness for a particular purpose. The information is provided “as is” and AOPA does not
warrant or make any representations regarding its accuracy, reliability, or otherwise. Under

no circumstances including negligence, shall AOPA be liable for any incidental, special or
consequential damages that result from the use or inability to use the software or related
documentation, even if AOPA or an AOPA authorized representative has been advised of the
possibility of such damages. User agrees not to sue AOPA and, to the maximum extent allowed
by law, to release and hold harmless AOPA from any causes of action, claims or losses related
to any actual or alleged inaccuracies in the information. Some jurisdictions do not allow the
limitation or exclusion of implied warranties or liability for incidental or consequential damages
so the above limitations or exclusions may not apply to you.

December, 2010 190-01247-00 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 74B Air Data Computer,
or other altimeters in the aircraft. GPS altitude should never be used for
vertical navigation. Always use pressure altitude displayed by the 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: Use of the Stormscope is not intended for hazardous weather
penetration (thunderstorm penetration). Stormscope information, as
displayed on the G1000 MFD, is to be used only for weather avoidance, not
penetration.

190-01247-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Warnings, Cautions & Notes

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.

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 Socata TBM 700 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
Socata TBM 700 Airplane Flight Manual. 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.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Warnings, Cautions & Notes

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.”

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.

190-01247-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Warnings, Cautions & Notes

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.

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.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Record of Revisions

Part Number Change Summary

190-01247-00 Initial Release

Revision Date of Revision Affected Pages Description

A December, 2010 All Production release

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Record of Revisions

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Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

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Table of Contents

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

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

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

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

Synchronizing the Altimeter Barometric Pressure Settings ........................................... 1

Synchronize CDI......................................................................................................................... 1

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

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

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

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

Set Barometric/Radar Altimeter Minimum Descent Altitude ......................................... 3

Manually Testing the Radar Altimeter (KRA 405B only) .................................................. 3

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

Changing HSI Format ............................................................................................................... 4

ENGINE & AIRFRAME SYSTEMS ............................................................................................. 5

Electrical System ....................................................................................................................... 6

Fuel System .............................................................................................................................. 10

General Systems ..................................................................................................................... 11

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

Enter or Change Flight ID ..................................................................................................... 13

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

DME Tuning............................................................................................................................... 13

Enter a Transponder Code..................................................................................................... 14

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

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

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

Intercom .................................................................................................................................... 15

Passenger Address (PA) System ........................................................................................... 15

Clearance Recorder and Player ...........................................................................................15

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

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Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Table of Contents

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

Weight 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 ................. 28

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

Waypoint ............................................................................................................................. 30

Delete a User Waypoint ......................................................................................................... 31

Create a New Flight Plan ...................................................................................................... 32

Import a Flight Plan from an SD Card ................................................................................ 33

Insert a Waypoint in the Active Flight Plan ...................................................................... 33

Enter an Airway in a Flight Plan .......................................................................................... 34

Invert An Active Flight Plan .................................................................................................. 35

Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 35

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

Edit a Stored Flight Plan ....................................................................................................... 36

Delete a Waypoint from the Flight Plan ............................................................................ 36

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

Copy a Flight Plan ................................................................................................................... 37

Delete a Flight Plan ................................................................................................................ 37

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

Export a Flight Plan to an SD Card ..................................................................................... 38

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 ............................................................................ 41

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

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

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

STORMSCOPE® (Optional) .................................................................................................... 43

XM Weather (Optional) .......................................................................................................... 45

Traffic Systems ........................................................................................................................ 47

Terrain And Obstacle Proximity ........................................................................................... 50

Terrain-SVS ............................................................................................................................... 50

Terrain Awareness & Warning System (TAWS) Display ................................................... 52

Airborne Color Weather Radar ............................................................................................ 54

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Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

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Table of Contents

ADDITIONAL FEATURES ........................................................................................................... 59

Synthetic Vision ....................................................................................................................... 59

Terminal Procedure Charts ...................................................................................................60

AOPA Airport Directory ......................................................................................................... 62

XM® Radio Entertainment..................................................................................................... 63

ABNORMAL OPERATION..........................................................................................................65

Reversionary Mode ................................................................................................................ 65

Abnormal COM Operation .................................................................................................... 65

Hazard Displays with Loss of GPS Position ....................................................................... 65

Unusual Attitudes ................................................................................................................... 66

Dead Reckoning ...................................................................................................................... 66

ANNUNCIATIONS & ALERTS ................................................................................................... 69

CAS Messages .......................................................................................................................... 69

Comparator Annunciations ................................................................................................... 71

Reversionary Sensor Annunciations ................................................................................... 71

AFCS Alerts ............................................................................................................................... 72

Terrain-SVS Alerts ................................................................................................................... 73

Terrain-SVS System Status Annunciations ........................................................................ 74

TAWS Alerts .............................................................................................................................. 75

Voice Alerts .............................................................................................................................. 77

MFD & PFD Message Advisories .......................................................................................... 78

Database Message Advisories ............................................................................................. 79

GMA 1347D Message Advisories ......................................................................................... 82

GIA 63W Message Advisories ............................................................................................... 83

GEA 71 Message Advisories .................................................................................................. 86

GTX 33/33D Message Advisories .......................................................................................... 87

GRS 77 Message Advisories .................................................................................................. 87

GMU 44 Message Advisories ................................................................................................ 89

GDL 69A Message Advisories ............................................................................................... 90

GWX 68 Alert Messages ......................................................................................................... 90

GDC 74B Message Advisories ............................................................................................... 91

GCU 475 Message Advisories ............................................................................................... 91

GMC 710 Message Advisories .............................................................................................. 92

GTS 820 Message Advisories ................................................................................................ 92

Miscellaneous Message Advisories ..................................................................................... 93

Flight Plan Import/Export Messages .................................................................................. 97

APPENDIX ....................................................................................................................................... 99

PFD Softkey Map .................................................................................................................... 99

MFD Softkey Map ................................................................................................................. 105

Loading Updated Databases .............................................................................................. 107

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

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Table of Contents

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Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Flight Instruments

FLIGHT INSTRUMENTS

SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING

Turn the BARO Knob to select the desired setting.

SELECTING STANDARD BAROMETRIC PRESSURE

Press the BARO Knob.

CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS

1)

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.

SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

1)

Select the AUX-SYSTEM SETUP Page on the MFD.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight BARO in the SYNCHRONIZATION
Window.

4)

Turn the

small

FMS Knob clockwise to ON or counterclockwise to OFF.

SYNCHRONIZE CDI

1)

Select the AUX-SYSTEM SETUP Page on the MFD.

2)

Press the FMS Knob to activate the cursor.

3)

Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window.

4)

Turn the

190-01247-00 Rev. A 1

small

FMS Knob clockwise to ON or counterclockwise to OFF.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Flight Instruments

CHANGE NAVIGATION SOURCES

Flight

InstrumentsEAS

1)

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
the 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 will start 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 Socata TBM 700

FMS Knob to highlight the desired Vspeed.

190-01247-00 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/RADAR ALTIMETER MINIMUM DESCENT ALTITUDE

1)

Press the TMR/REF Softkey.

2)

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

3)

Turn the small FMS Knob clockwise to select BARO or RAD ALT.

4)

Press the ENT Key.

5)

Use the small FMS Knob to enter the desired altitude.

6)

Press the ENT Key.

7)

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

MANUALLY TESTING THE RADAR ALTIMETER (KRA 405B ONLY)

1)

Select the AUX-SYSTEM STATUS Page on the MFD.

2)

Select the RA TEST Softkey. The Radar Altitude window displays 50
feet, and ‘RA TEST’ is displayed to the left of the Radar Altitude window,
indicating a properly functioning system.

3)

Selecting the RA TEST Softkey again, or exiting the System Status Page
cancels the test.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

DISPLAYING WIND DATA

1)

Select the PFD Softkey.

2)

Select the WIND Softkey to display wind data below the Selected Heading.

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.

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Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Operation

Abnormal

Annun/

Alerts Appendix Index

Flight Instruments

CHANGING HSI FORMAT

Flight

InstrumentsEAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

1)

Press the PFD Softkey.

2)

Press the HSI FRMT Softkey.

3)

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

Or

:

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

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

4

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Engine & Airframe Systems

ENGINE & AIRFRAME SYSTEMS

Instruments EAS

Flight

1

1

8

XPDR/Audio AFCS GPS Nav

Nav/Com/

2

2

9

10

3

4

Planning Procedures

Flight

3

4

11

5

6

7

12

13

14

15

10

5

6

15

Avoidance

8

Hazard

9

Additional

Features

11

13

14

EIS Display, Normal Mode

(Models A, B, and C shown)\

(Model N similar)

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Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

EIS Display (Reversionary Mode)

(Models A, B, and C)

(Model N similar)

Operation

Abnormal

Annun/

Alerts Appendix Index

Engine & Airframe Systems

1

Torque

Flight

2

InstrumentsEAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Propeller Speed

3

Generator Speed

4

Interturbine Temperature

5

Oil Pressure

6

Oil Temperature

7

CAS Display

8

Cabin Pressure Altitude and Change
Rate

ELECTRICAL SYSTEM

1)

Select the SYSTEM Softkey to display the softkeys for the synoptics system.

2)

Select the ELEC Softkey to display the Electrical System Page.

Flight

PlanningProcedures

9

Differential Pressure

10

Fuel Quantity

11

Fuel Flow

12

Fuel Pressure

13

Battery and Generator Currents

14

Battery and Essential Bus Voltages

15

Elevator, Aileron, and Rudder Trim
and Flap Position

1

2

3

4

5

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

11

6

7

10

9 8

Electrical Synoptics Page

6

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Engine & Airframe Systems

1

Standby Generator

2

Main Generator

3

Ground Power Unit Door

4

Battery

5

Amperage

6

Battery Bus

7

Essential Bus

8

Battery Bus Voltage

9

Essential Bus Voltage

10

DC Buses 1through 4

11

Main Bus

Active generator currents are displayed below the generator icons. A disconnected
generator is indicated in gray; the current is removed from the display and the switch
symbol is closed.

Connected

Disconnected

Generator Status

Connected Disconnected

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

GPU status information is removed from the electrical diagram when the GPU door
is closed. If the GPU door is open and selected, the GPU status is shown in green;
when the door is open, but not selected, the status is shown in gray with the switch
closed. A CAS message, ‘GPU DOOR’ is generated if the GPU door is open.

GPU Door Open

Selected Not Selected

GPU Door Status

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Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

GPU Door Closed

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Engine & Airframe Systems

Battery connection status to the main bus is indicated in green; direction of

current flow is indicated with an arrow next to the current readout. If the battery is

Flight

InstrumentsEAS

disconnected from the main bus, the switch is closed. Battery overheating is indicated
in red with a ‘BAT OVHT’ annunciation; a CAS message is also generated.

Connected Disconnected Battery Overheat

Nav/Com/

XPDR/AudioAFCSGPS Nav

Battery Status

Flight

PlanningProcedures

in green when energized. When not energized, the connection line to the main bus is
removed and the bus label is displayed in red.

Hazard

Avoidance

Features

Additional

Battery and Essential Bus Low Voltage

Abnormal

Operation

AlertsAppendixIndex

Annun/

Bus Not Energized

Battery and essential bus voltages are displayed using gauges. DC buses are shown

DC Bus Status

8

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Engine & Airframe Systems

The Emergency Buses switch has two positions, UP (open) and DN (ground). If the
switch is in the UP position, the essential bus is connected to the battery bus. If the
switch is in the DN position, the essential bus is connected to the main bus.

Essential Bus Connected to

the Battery Bus

Essential Bus Connections

Essential Bus Connected to

the Main Bus

A red “X” over a component indicates invalid data or a failed unit.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

190-01247-00 Rev. A 9

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Engine & Airframe Systems

FUEL SYSTEM

Flight

InstrumentsEAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

1)

Select the SYSTEM Softkey to display the softkeys for the synoptics system.

2)

Select the FUEL Softkey to display the Fuel System Page.

3

2

1

4

5

6

7

8

9

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

Left Fuel Tank

1

Left Fuel Line

2

3

Fuel Pressure

4

Engine Driven Boost Pump

Auxiliary Boost Pump

5

6

Fuel Selector

7

Right Fuel Tank

Right Fuel Line

8

Fuel Flow Data

9

Fuel Synoptics Page

Status of the fuel selector is indicated between the fuel tank symbols. The mode,

automatic (AUTO) or manual (MAN) is shown beneath the fuel selector symbol.

10

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Engine & Airframe Systems

Left Fuel

Tank

Selected

Switching

Fuel Tank
Selection

Right

Fuel Tank

Selected

Unknown
Fuel Tank
Selection

Fuel

Selector

Off

Fuel Selector Status

If the auxiliary fuel boost pump is on, the symbol is displayed in green. The mode,
automatic (AUTO) or manual (MAN) is displayed next to the pump symbol. If the
boost pump is off, the symbol is shown in light blue (automatic mode) or red (manual
mode).

Fuel Boost Pump OnFuel Boost Pump

Off (Auto)

Auxiliary Boost Pump Status

Fuel Boost Pump

Off (Manual)

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

GENERAL SYSTEMS

1)

Select the SYSTEM Softkey to display the softkeys for the synoptics system.

2)

Select the GEN Softkey to display the Fuel System Page.

The General Synoptics Page aircraft diagram displays open doors in red (CAS mes­sages also generated). Statuses of stall sensor, propeller, and pitot probes heat are also
indicated on the diagram:

• Whiteindicatesthatheatisoff(propeller)

• Greenindicatesheatison

• Yellowindicatesheathasfailed(stallsensor,propellerandpitottube).

Invalid sensor information is indicated with a red ‘X’.

190-01247-00 Rev. A 11

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Engine & Airframe Systems

Flight

InstrumentsEAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

5

4

3

2

1

Rear Cargo Door Open

1

Cabin Door Open

2

6

7

8

Pitot Probe 2

5

6

Forward Cargo Door Open

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

12

3

Pilot Door Open

4

Pitot Probe 1

7

Propeller Heaters

Stall Warning Sensor

8

General Synoptics Page

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

NAV/COM/TRANSPONDER/AUDIO PANEL

ENTER OR CHANGE FLIGHT ID

1)

Press the TMR/REF Softkey, then turn the large FMS Knob to highlight the
Flight ID field.

2)

Turn the small FMS Knob to enter the first character.

3)

Turn the large FMS Knob to select the next field.

4)

Turn the small FMS Knob to enter the next desired character.

5)

Repeat steps 3 and 4 until the desired Flight ID is entered.

6)

Press the ENT Key to update the Flight ID. Do not perform any other
G1000 functions until ‘updating’ is no longer displayed.

ADF TUNING (OPTIONAL)

1)

Press the ADF/DME Softkey.

2)

Turn the small FMS Knob to enter the first digit of the desired ADF
frequency.

3)

Turn the large FMS Knob to select the next desired field.

4)

Turn the small FMS Knob to enter the desired number.

5)

Repeat steps 3 and 4 until the desired ADF frequency is entered.

6)

Press the ENT Key to accept the new frequency.

7)

Press the ENT Key again to transfer the frequency to the active field.

8)

Turn the large FMS Knob to select the MODE field.

9)

Turn the small FMS Knob to select ANT, ADF, ADF/BFO, or ANT/BFO.

10)

Press the ENT Key to complete the selection.

Nav/Com/XPDR/Audio Panel

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

DME TUNING

1)

Press 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.

190-01247-00 Rev. A 13

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Nav/Com/XPDR/Audio Panel

ENTER A TRANSPONDER CODE

Flight

InstrumentsEAS

1)

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

2)

If two transponders are available, press XPDR1 or XPDR2 to set the active
transponder. Otherwise, proceed to step 3.

3)

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

4)

Nav/Com/

XPDR/AudioAFCSGPS Nav

Use the digit keys 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.

SELECTING A COM RADIO

Transmit/Receive

Flight

PlanningProcedures

Press the COM1 MIC, COM2 MIC
the audio panel.

Receive Only

Press the COM1, COM2

SELECTING A NAV RADIO

Hazard

Avoidance

1)

To begin navigating using a navigation radio, press the CDI Softkey on the
PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).

Features

Additional

2)

Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or
deselect the navigation radio audio source. All radio keys can be selected
individually or together.

Abnormal

Operation

NAV/COM TUNING

, or

COM3 MIC Key (HF, if installed) on

, or

COM3 Key (HF, if installed) on the audio panel.

AlertsAppendixIndex

Annun/

14

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)

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.

3)

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

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Nav/Com/XPDR/Audio Panel

INTERCOM

Pressing the INTR COM Key on either Audio Panel selects and deselects the
intercom on both Audio Panels. The annunciator is lit when the intercom is active.
The intercom connects the pilot and copilot together. Either the pilot or copilot may
select or deselect the intercom.

The CABIN Key initiates two way communication between the pilot or copilot and
the passengers in the cabin. The annunciator is lit when the cabin intercom is active
on either Audio Panel.

The MAN SQ Key allows either automatic or manual control of the intercom
squelch setting. Pressing the MAN SQ Key enables manual squelch control, indicated
by the MAN SQ annunciator.

During manual squelch operation, pressing the ICS Knob switches between volume
and squelch adjustment, lighting the associated annunciator beneath the knob. When
the MAN SQ annunciator is lit, the ICS Knob controls both volume and squelch. When
the MAN SQ annunciator is extinguished, the ICS Knob controls only volume.

PASSENGER ADDRESS (PA) SYSTEM

A passenger address system is provided by pressing the PA Key to deliver messages
to the passengers. The message is heard by the other pilot on the headset only if the
INTR COM Key is enabled. PA messages are one way from the flight deck to the
passengers.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

CLEARANCE RECORDER AND PLAYER

NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio
to the Pilot. Pressing the play key on the Copilot’s Audio Panel plays recorded
audio to the Copilot.

Recorded COM audio is stored in separate memory blocks. Once 2.5 minutes
of recording time have been reached, the recorder begins recording over the stored
memory blocks, starting from the oldest block.

The PLAYKeycontrolstheplayfunction.ThePLAYannunciatorashestoindicate

whenplayisinprogress.ThePLAYannunciatorturnsoffafterplaybackisnished.

Pressing the PLAY Key once plays the latest recorded memory block and then
returns to normal operation. Pressing the PLAY Key again during play of a memory
block stops play. If a COM input signal is detected during play of a recorded memory
block, play is halted.

190-01247-00 Rev. A 15

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Nav/Com/XPDR/Audio Panel

Pressing the PLAY Key twice within one-half second while audio is playing plays

the previous block of recorded audio. Each subsequent two presses of the PLAY Key

Flight

InstrumentsEAS

within one-half second backtracks through the recorded memory blocks to reach and
play any recorded block.

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

16

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

AUTOMATIC FLIGHT CONTROL SYSTEM

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

NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.

FLIGHT DIRECTOR ACTIVATION

An initial press of a key listed in the following table (when the flight director is not
active) activates the pilot-side flight director in the listed modes.

AFCS

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Control Pressed

Modes Selected

Lateral Vertical

FD Key Roll Hold (default) ROL Pitch Hold (default) PIT

AP Key Roll Hold (default) ROL Pitch Hold (default) PIT

CWS Button Roll Hold (default) ROL Pitch Hold (default) PIT

GA Switch

Takeoff (on ground)

Go Around (in air)TOGA

Takeoff (on ground)

Go Around (in air)TOGA

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

VS Key Roll Hold (default) ROL Vertical Speed VS

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

GPS

NAV Key Navigation**

VOR

Pitch Hold (default) PIT

LOC

BC Key Backcourse*** BC Pitch Hold (default) PIT

APR Key Approach**

GPS
VOR
LOC

Pitch Hold (default)

Glidepath

Glideslope

PIT
GP
GS

HDG Key Heading Select HDG Pitch Hold (default) PIT

*Valid VNV flight plan must be entered before VNV Key press activates flight director.

**The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before

NAV

or

APR

Key press activates flight director.

***The selected navigation receiver must have a valid LOC signal before BC Key press activates flight

director.

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-01247-00 Rev. A 17

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

AFCS

VERTICAL MODES

Flight

InstrumentsEAS

Vertical Mode Description Control Annunciation

Holds the current aircraft pitch attitude;

Pitch Hold

Selected Altitude

Nav/Com/

XPDR/AudioAFCSGPS Nav

Armed

Altitude Hold Holds the current Altitude Reference A LT Key A LT nnnnn f T

Vertical Speed

Flight Level Change,
IAS Hold

Flight

PlanningProcedures

Flight Level Change,
Mach Hold

VNAV

VNAV Target

Hazard

Avoidance

Altitude Armed

Glidepath

Features

Additional

Glideslope

Abnormal

Operation

Takeoff

AlertsAppendixIndex

Annun/

Go Around

* ALTS armed automatically when PIT, VS, FLC, or GA active, and under VPTH when Selected Altitude

is to be captured instead of VNAV Target Altitude

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

Selected Altitude

may be used to climb/descend to the
Selected Altitude

AFCS armed to capture the altitude
displayed in the Selected Altitude
window

Maintains the current aircraft vertical
speed; may be used to climb/descend
to the Selected Altitude

Maintains the current aircraft airspeed
(in KIAS or Mach Number) while the
aircraft is climbing/descending to the
Selected Altitude

Captures and tracks the VNAV flight
path

AFCS armed to capture the altitude
displayed in the VNAV Target Altitude
window

Captures and tracks the SBAS glidepath
on approach

Captures and tracks the ILS glideslope
on approach

Commands a preprogrammed constant
pitch attitude and wings level in
preparation for takeoff

Disengages the autopilot and
commands a constant preprogrammed
pitch attitude and wings level

(default) PIT

* ALTS

VS Key VS nnnn f p m

FLC nnn k T

FLC Key

FLC M .nnn

VNV

Key

** ALTV

APR Key

GA

Switch

VPTH

GP

GS

TO

GA

18

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

AFCS

LATERAL MODES

Lateral Mode Description Control Annunciation

Holds current aircraft roll attitude

Roll Hold

Low Bank Limits maximum commanded roll angle

Heading Select Captures and tracks Selected Heading

Navigation, GPS
Arm/Capture/Track

Navigation, VOR
Enroute Arm/
Capture/Track

Navigation, LOC
Arm/Capture/Track
(No Glideslope)

Backcourse Arm/
Capture/Track

Approach, GPS
Arm/Capture/Track

Approach, VOR
Arm/Capture/Track

Approach, ILS Arm/
Capture/Track
(Glideslope Mode
automatically armed)

Takeoff

Go Around

* No annunciation appears in the AFCS Status Box. The low bank angle range is indicated in green

along the Roll Scale of the Attitude Indicator.

or rolls wings level, depending on
commanded bank angle

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

Captures and tracks a localizer signal
for backcourse approaches

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

Commands a constant preprogrammed
constant pitch attitude and wings level
in preparation for takeoff

Disengages autopilot and commands
a preprogrammed constant pitch
attitude and wings level

(default) ROL

BANK

Key

HDG

Key

*

HDG

GPS

NAV

VOR

Key

LOC

BC Key BC

GPS

VAPP

APR Key

LOC

TO

GA

Switch

GA

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-01247-00 Rev. A 19

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Flight

InstrumentsEAS

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 Socata TBM 700

190-01247-00 Rev. A

GPS NAVIGATION

DIRECT-TO NAVIGATION

Direct-to Navigation using 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 on the MFD Control Unit.

GPS Navigation

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Direct-to Navigation using 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.

190-01247-00 Rev. A 21

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

( )

on the PFD or controller.

Operation

Abnormal

Annun/

Alerts Appendix Index

GPS Navigation

7)

Turn the small FMS Knob to enter the desired altitude.

8)

Flight

InstrumentsEAS

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 Key again to activate the Direct-to.

1)

Press the FPL Key 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)

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 Socata TBM 700

190-01247-00 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 will 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

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Small Light

Blue Subdued

Text

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

190-01247-00 Rev. A 23

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

GPS Navigation

Since altitudes loaded with an arrival procedure are published only for turbojet

aircraft, the altitudes are displayed as white text indicating that the altitudes are

Flight

InstrumentsEAS

displayed for reference only. An arrival waypoint altitude may be used (or “designated”)
as is, or changed to a different altitude. An altitude is designated by pressing the FMS
Knob and turning the large FMS Knob to place the cursor on the desired altitude and
pressing the ENT Key or entering a different value and pressing the ENT Key. The
altitude is now displayed as blue text, indicating that the altitude is now designated to
give vertical speed and deviation guidance.

Nav/Com/

XPDR/AudioAFCSGPS Nav

Approach waypoint altitude constraints are designated in the same way as
previously described for arrivals. These altitudes are also displayed as blue text after
being designated for use. Waypoint altitude constraints may be designated up to, but
not including the FAF. The FAF is always a “reference only” altitude and cannot be
designated, unless the selected approach does not provide vertical guidance. In this
case, the FAF altitude can be designated.

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

Large Text

Small Text

White Text Light Blue Text Light Blue

Subdued Text

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

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 pilot and matches a
published altitude in the
navigation database.

The system cannot
use this altitude in
determining vertical
flight path guidance.

24

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

FLIGHT PLANNING

WEIGHT PLANNING

All procedures apply to the MFD unless otherwise stated.

Flight Planning

Instruments EAS

Flight

Entering Weight Parameters

The Weight Planning Page is displayed after system power-up. If it is necessary to
return to this page, turn the large
small

FMS

Knobtoselecttherstrectangularpageicon.

1)

Select the EMPTY WT Softkey to place the cursor in the Basic Empty

FMS

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

Weight field.

2)

Enter the desired aircraft empty weight.

3)

Press the ENT Key. The cursor is now over the ‘PILOT & STORES’ field.

4)

Enter the desired weight of Pilot & Stores.

5)

Press the ENT Key.

6)

Continue repeating these steps until all desired weights have been entered.

Entering Fuel Parameters

1)

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

2)

Turn the large FMS Knob to place the cursor in the ‘FUEL ON BOARD’ field.

3)

Select the FOB SYNC Softkey to enter the fuel on board quantity as read
from the aircraft fuel quantity sensors.

Or:

Manually enter the desired fuel quantity.

4)

Press the ENT Key. The cursor is now in the ‘FUEL RESERVES’ field.

5)

Enter the desired reserve fuel quantity.

6)

Press the FMS Knob to remove the cursor.

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

TRIP PLANNING

1)

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

2)

Turn the small FMS Knob to select the second 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.

190-01247-00 Rev. A 25

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Flight Planning

4)

For Direct-to planning:

Flight

InstrumentsEAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

a)

b)

c)

d)

Or:

For point-to-point planning:

a)

b)

c)

d)

Or:

For flight plan leg planning:

a)

b)

c)

d)

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

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

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

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

Enter the identifier of the starting waypoint.

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

Again, enter the identifier of the ending waypoint.

Press the ENT Key to accept the waypoint.

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

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

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

Turn the small FMS Knob to select the desired leg of the flight plan, or
select ‘CUM’ to apply trip planning calculations to the entire flight plan.
Selecting ‘FPL 00’ displays the active flight plan. If an active flight plan
is selected, ‘REM’ will be an available option to display planning data
for the remainder of the flight plan.

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

26

5)

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

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.

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190-01247-00 Rev. A

Flight Planning

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

ENT

Key when finished. Note that in ‘automatic’ page

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. Modify the fuel onboard.
Press the ENT Key when finished. In ‘AUTOMATIC’ mode, fuel onboard is
provided by the entry made on the Weight Planning Page.

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.

CREATE A NEW USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE

Instruments EAS

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Abnormal

1)

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

2)

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

3)

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

4)

Enter the desired waypoint name.

5)

Press the ENT Key.

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Flight Planning

6)

The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint

Flight

InstrumentsEAS

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.

Nav/Com/

XPDR/AudioAFCSGPS Nav

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)

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28

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

2)

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

3)

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

4)

Enter the desired waypoint name.

5)

Press the ENT Key.

6)

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

a)

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

b)

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

7)

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

8)

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

9)

Press the ENT Key.

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:

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Flight Planning

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.

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.

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 ‘USER’ waypoints.

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

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)

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.

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Alerts Appendix Index

16)

Press the FMS Knob to remove the flashing cursor.

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Flight Planning

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

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ANOTHER WAYPOINT

1)

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

2)

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

3)

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

4)

Enter the desired waypoint name.

5)

Press the ENT Key.

6)

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

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.

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.

30

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Flight Planning

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.

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 ‘USER’ waypoints.

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

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.

Instruments EAS

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Avoidance

Hazard

15)

Press the FMS Knob to remove the flashing cursor.

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.

4)

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

5)

Turn the small FMS Knob to highlight the desired waypoint.

6)

Select the DELETE Softkey.

7)

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

190-01247-00 Rev. A 31

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Flight Planning

CREATE A NEW FLIGHT PLAN

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Hazard

Avoidance

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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.

Creating a stored flight plan:

1)

Press the FPL Key.

2)

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

3)

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

4)

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

5)

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

6)

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

7)

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

32

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Flight Planning

IMPORT A FLIGHT PLAN FROM AN SD CARD

1)

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

2)

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

3)

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

4)

Press the FMS Knob to activate the cursor.

5)

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

6)

Select the IMPORT Softkey.

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 select the IMPORT
Softkey.

7)

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

8)

Press the ENT Key.

Instruments EAS

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Planning Procedures

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Avoidance

Hazard

Additional

Features

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.

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:

190-01247-00 Rev. A 33

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Flight Planning

a)

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

Flight

InstrumentsEAS

is displayed.

b)

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

c)

Turn the large FMS Knob to select the desired waypoint.

d)

Press the ENT Key.

Nav/Com/

XPDR/AudioAFCSGPS Nav

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.

Flight

PlanningProcedures

ENTER AN AIRWAY IN A FLIGHT PLAN

1)

Press the FPL Key.

2)

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

3)

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Turn the large FMS Knob to highlight the waypoint field after the desired
airway entry point. If this previous 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).

5)

Turn the FMS Knob to select the desired airway from the list, and press the
ENT Key. Low altitude airways are shown first in the list, followed by “all”

altitude airways, and then high altitude airways.

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.

34

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Flight Planning

INVERT AN ACTIVE FLIGHT PLAN

1)

Press the FPL Key to display the active flight plan.

2)

Press the MENU Key to display the Page Menu.

3)

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

4)

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

5)

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

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

PLAN

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 MFD FPL Key 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.

Instruments EAS

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Planning Procedures

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Avoidance

Hazard

Additional

Features

Operation

Abnormal

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.

190-01247-00 Rev. A 35

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Flight Planning

EDIT A STORED FLIGHT PLAN

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InstrumentsEAS

1)

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

2)

Press the FMS Knob to activate the cursor.

3)

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

4)

Select the EDIT Softkey.

Nav/Com/

XPDR/AudioAFCSGPS Nav

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.

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

Or, for a stored flight plan:

a)

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

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.

5)

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

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cursor.

INVERT AND ACTIVATE A STORED FLIGHT PLAN

1)

Press the FPL Key for the MFD.

2)

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

3)

Press the FMS Knob to activate the cursor.

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Flight Planning

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 for 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 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

1)

Press the FPL Key for the MFD.

2)

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

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3)

Press the FMS Knob to activate the cursor.

4)

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

5)

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

6)

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

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.

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Flight Planning

3)

The default insertion point is at the end of the flight plan. If the selected

Flight

InstrumentsEAS

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)

Nav/Com/

XPDR/AudioAFCSGPS Nav

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 MFD 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.

Flight

PlanningProcedures

4)

Press the FMS Knob to activate the cursor.

5)

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

6)

Select the EXPORT Softkey.

7)

Press the ENT Key to confirm the export.

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38

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

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

Instruments EAS

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XPDR/Audio AFCS GPS Nav

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Planning Procedures

Flight

ACTIVATE A DEPARTURE LEG

1)

Press the FPL Key for 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 TO waypoint of the desired leg
within the departure.

4)

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

5)

With ‘ACTIVATE’ highlighted, press the ENT Key.

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.

190-01247-00 Rev. A 39

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Procedures

4)

Turn the large FMS Knob to highlight the desired arrival.

5)

Flight

InstrumentsEAS

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.

ACTIVATE AN ARRIVAL LEG

1)

Press the FPL Key to display the active flight plan.

2)

Press the FMS Knob to activate the cursor.

3)

Flight

PlanningProcedures

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

4)

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

5)

With ‘ACTIVATE’ highlighted, press the ENT Key.

Hazard

Avoidance

LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE

Features

Additional

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.

Abnormal

Operation

1)

Press the PROC Key.

2)

AlertsAppendixIndex

Annun/

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

3)

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

4)

Turn either FMS Knob to highlight the desired approach.

5)

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

40

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Procedures

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 EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

1)

Press the PROC Key.

2)

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

3)

Press the ENT Key.

ACTIVATE A VECTOR TO FINAL APPROACH FIX

1)

Press the PROC Key.

2)

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

3)

Press the ENT Key.

4)

The final approach course becomes the active leg.

190-01247-00 Rev. A 41

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Procedures

ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN

Flight

InstrumentsEAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

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 button.

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

42

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 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.

STORMSCOPE® (OPTIONAL)

WARNING: The Stormscope system is not intended to be used for hazardous
thunderstorm penetration. Weather information on the G1000 MFD is
approved for weather avoidance only. Refer to the WX-500 Pilot’s Guide for
detailed operation.

Displaying Stormscope Lightning Data on the Navigation Map Page

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

1)

Select the MAP Softkey.

2)

Select the STRMSCP Softkey. Select the STRMSCP Softkey again to
remove Stormscope Lightning Data from the Navigation Map Page.

Lightning Age Symbol

Strike is less than 6 seconds old

Strike is between 6 and 60 seconds old

Strike is between 1 and 2 minutes old
Strike is between 2 and 3 minutes old

Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode

1)

Press the MENU Key (with the Navigation Map Page displayed).

2)

Turn either FMS Knob to highlight ‘Map Setup’.

3)

Press the ENT Key.

4)

Turn the small FMS Knob to highlight ‘Weather’.

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Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Hazard Avoidance

5)

Press the ENT Key.

6)

Flight

InstrumentsEAS

Turn the large FMS Knob to place the cursor in the ‘STRMSCP MODE’ field.

7)

Turn the small FMS Knob to display the ‘Cell/Strike’ window.

8)

Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key.

9)

Push the FMS Knob to return to the Navigation Map Page.

Clear Stormscope Lightning Data from the Navigation Map Page

Nav/Com/

XPDR/AudioAFCSGPS Nav

1)

Press the MENU Key (with the Navigation Map Page displayed).

2)

Turn either FMS Knob to highlight the ‘Clear Stormscope® Lightning’ field
and press the ENT Key.

Flight

Stormscope Page

PlanningProcedures

1)

2)

Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’

Hazard

Additional

Abnormal

Annun/

1)

Avoidance

2)

Features

Operation

AlertsAppendixIndex

Change the Viewing Mode Between 360˚ and 120˚

1)

2)

NOTE:

If heading input is lost, strikes and/or cells must be cleared manually
after the execution of each turn. This is to ensure that the strike and/or cell
positions are depicted accurately in relation to the nose of the aircraft.

Turn the large FMS Knob until the Map Page group is selected.

Turn the small FMS Knob until the Stormscope Page is selected.

Select the Stormscope Page.

Select the MODE Softkey. The CELL and STRIKE Softkeys are displayed.
Select the CELL Softkey to display ‘CELL’ data or select the STRIKE Softkey
to display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’ is displayed in the mode box
located in the upper left corner of the Stormscope Page.

NOTE: “Cell mode” uses a clustering program to identify clusters of electrical
activity that indicate cells.

Select the Stormscope Page.

Select the VIEW Softkey. The 360 and ARC Softkeys are displayed. Select
the 360 Softkey to display a 360˚ viewing area or select the ARC Softkey to
display a 120˚ viewing area.

Select the CLEAR Softkey to remove all Stormscope lightning data from the
display.

44

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

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Hazard Avoidance

XM WEATHER (OPTIONAL)

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.

4)

Select the LEGEND Softkey to view the legends for the selected products.
If necessary, turn either FMS Knob to scroll through the list. Press the small

FMS Knob or the ENT Key to return to the map.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Map Panning Information – Weather Data Link Page

1)

Push in the Joystick to display the panning arrow.

2)

Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs,
SIGMETs, PIREPs or AIREPs.

3)

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

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

190-01247-00 Rev. A 45

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Alerts Appendix Index

Annun/

Hazard Avoidance

information but allows the user to press the ENT Key and select that

Flight

InstrumentsEAS

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

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

Wx Product

Status Icons

Description

NEXRAD - Available for the US and Canada. The age of the displayed data

for each is shown at the right.

ECHO TOP - The age of the displayed data is shown at the right. Not
displayed when CLOUD TOP is displayed.

CLOUD TOP - The age of the displayed data is shown at the right. Not
displayed when ECHO TOP is displayed.

XM LIGHTNING - The age of the displayed data is shown at the right.

CELL MOVEMENT - The age of the displayed data is shown at the right.

SIGMET & AIRMET - The age of the displayed data for each is shown at the

right.

METAR - Available for the US and Canada. The age of the displayed data for
each is shown at the right.

SURFACE ANALYSIS with CITY FORECAST - The upper symbol depicts
Surface Analysis. The lower symbol depicts City Forecast. The age of the
displayed data for each is shown at the right. The selected forecast period is
shown at the bottom.

AlertsAppendixIndex

Annun/

46

FREEZING LEVEL - The age of the displayed data is shown at the right.

WINDS ALOFT - Available for the US and Canada. The age of the displayed

data for each is shown at the right. The altitude selection is shown at the
bottom.

COUNTY WARNING - The age of the displayed data is shown at the right.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Hazard Avoidance

Wx Product

Status Icons

Description

CYCLONE WARNING - The age of the displayed data is shown at the right.

AIREP - The age of the displayed data is shown at the right.

PIREP - The age of the displayed data is shown at the right. Urgent Pireps

are displayed in yellow.

TURBULENCE - The age of the displayed data is shown at the right. The
altitude selection is shown at the bottom.

ICING POTENTIAL - The age of the displayed data is shown at the right.
The altitude selection is shown at the bottom.

TRAFFIC SYSTEMS

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

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

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

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 Advisory (TA) arrow with ADS-B directional information. Points in
the direction of the intruder aircraft track (GTS 820 only).

Proximity Advisory (PA) arrow with ADS-B directional information. Points
in the direction of the aircraft track (GTS 820 only).

190-01247-00 Rev. A 47

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Hazard Avoidance

Traffic Symbol Description

Flight

InstrumentsEAS

Non-threat traffic arrow with ADS-B directional information. Points in the
direction of the intruder aircraft track (GTS 820 only).

PA or Non-threat traffic arrow with ADS-B directional information, but
positional accuracy is degraded. Points in the direction of the aircraft
track (GTS 820 only).

Nav/Com/

XPDR/AudioAFCSGPS Nav

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

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

within the service volume of a TIS capable terminal radar site.

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 “TIS Not Available” aural alert.

Traffic Symbol Description

AlertsAppendixIndex

Annun/

Displaying Traffic on the Navigation Map

1)

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

2)

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

48

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Hazard Avoidance

Traffic Advisory System (TAS) (Optional)

System Self Test

1)

Set the range to 2/6 nm.

2)

Select the STANDBY Softkey.

3)

Select the TEST Softkey.

4)

Self test takes approximately eight seconds to complete. When completed
successfully, traffic symbols are displayed and a voice alert “TAS System Test
OK” is heard. If the self test fails, the system reverts to Standby Mode and
a voice alert “TAS System Test Fail” is heard.

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 second rectangular page icon.

3)

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

4)

Select the ALT MODE Softkey to change the altitude volume. Select the
desired altitude volume by selecting the BELOW, NORMAL, ABOVE, or
UNREST (unrestricted) Softkey. The selection is displayed in the Altitude
Mode field.

5)

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

6)

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

7)

Select the FLT ID Softkey (GTS 820 only) to enable or disable Flight ID
displayed with the intruder information.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Displaying Traffic on the Navigation Map

1)

Ensure TAS is operating.

2)

With the Navigation Map displayed, select the MAP Softkey.

3)

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

190-01247-00 Rev. A 49

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Alerts Appendix Index

Annun/

Hazard Avoidance

TERRAIN AND OBSTACLE PROXIMITY

Flight

InstrumentsEAS

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)

Nav/Com/

XPDR/AudioAFCSGPS Nav

Turn the large

2)

Turn the small

3)

If desired, select the
When the
Select the

4)

Rotate the
clockwise to display a smaller area.

FMS

Knob to select the Map Page Group.

FMS

Knob to select the last rectangular page icon.

VIEW

Softkey to access the

ARC

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

360

Softkey to return to the 360° default display.

Joystick

clockwise to display a larger area or rotate counter-

ARC

and

360

Softkeys.

Flight

Hazard

PlanningProcedures

Avoidance

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

Features

Additional

Abnormal

Operation

1)

With the Navigation Map displayed, select the

2)

Select the

TERRAIN

Softkey. Terrain and obstacle proximity will now be

displayed on the map.

TERRAIN-SVS

AlertsAppendixIndex

Annun/

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.

MAP

Softkey.

50

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Hazard Avoidance

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.

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.

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.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Terrain-SVS Inhibit

Inhibit Terrain

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

Or

:

1)

Press the MENU Key.

2)

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

3)

Press the ENT Key.

190-01247-00 Rev. A 51

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Operation

Abnormal

Annun/

Alerts Appendix Index

Hazard Avoidance

Enable Terrain

Flight

InstrumentsEAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

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.

TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY

Flight

PlanningProcedures

WARNING: The TAWS display shows supplemental information only. It should

not be used for navigation.

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

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

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.

52

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Hazard Avoidance

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.

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.

Enable/Disable Aviation Data

1)

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

2)

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

3)

Press the ENT Key.

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.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

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.

190-01247-00 Rev. A 53

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Operation

Abnormal

Annun/

Alerts Appendix Index

Hazard Avoidance

Enable TAWS

Flight

InstrumentsEAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

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’.

3)

Press the ENT Key.

AIRBORNE COLOR WEATHER RADAR

WARNING: Begin transmitting only when it is safe to do so. If it is desired to
transmit while the aircraft is on the ground, no personnel or objects should
be within 11 feet of the antenna.

CAUTION: In Standby Mode, the antenna is parked at the center line. It
is always a good idea to put the radar in Standby Mode before taxiing the

Flight

PlanningProcedures

aircraft to prevent the antenna from bouncing on the bottom stop and possibly
causing damage to the radar assembly.

Displaying Weather on the Weather Radar Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

54

1)

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

2)

Turn the small FMS Knob to select the Weather Radar Page.

3)

Select the MODE Softkey.

4)

If the aircraft is on the ground, select the STANDBY Softkey to initiate the
one minute warm-up period. After the warm-up is complete, the radar will
enter the Standby Mode. After the aircraft is airborne, select the WEATHER
Softkey.

Or

:

If the aircraft is already airborne, select the WEATHER or GROUND
Softkey. The one-minute warm-up period will be initiated, after which the
radar will begin transmitting. The horizontal scan is initially displayed.

5)

Turn the Joystick to select the desired range.

6)

If desired, select the VERTICAL Softkey for vertical scanning.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Hazard Avoidance

Adjusting Antenna Tilt

Move the

Joystick

up or down to adjust the tilt of the antenna up or down.

MonitorthedisplayedtiltvalueintheTILTeld.

When scanning vertically, a Tilt Line may be displayed to aid in positioning the tilt

of the antenna. If the Tilt Line is not displayed, perform the following steps:

1)

Press the MENU Key

2)

Turn the large FMS Knob to select ‘Show Tilt Line’.

3)

Press the ENT Key.

Adjusting Antenna Bearing

Move the

Joystick

right or left to adjust the azimuth position of the antenna right

orleft.MonitorthedisplayedbearingvalueintheBEARINGeld.

When scanning horizontally, a Bearing Line may be displayed to aid in positioning
the antenna for the vertical scan. If the Bearing Line is not displayed, perform the
following steps:

1)

Press the MENU Key

2)

Turn the large FMS Knob to select ‘Show Bearing Line’.

3)

Press the ENT Key.

Vertically Scan a Storm Cell

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

1) While in the Horizontal Scan view, move the Joystick to place the Bearing

Line on the desired storm cell, or other area, to be vertically scanned.

2)

Select the VERTICAL Softkey. A vertical ‘slice’ of the selected area will now
be displayed.

3)

Move the Joystick right or left to move the scanned “slice” a few degrees
right or left.

4)

Turn the Joystick to adjust the range.

5)

To select a new area to be vertically scanned, select the HORIZON Softkey
to return to the Horizontal Scan view and repeat the previous steps.

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Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Hazard Avoidance

Adjusting Gain

Flight

InstrumentsEAS

1)

XPDR/AudioAFCSGPS Nav

2)

Nav/Com/

3)

4)

Ground Mapping

Flight

PlanningProcedures

1)

2)

3)

4)

Hazard

Avoidance

5)

6)

Features

Additional

7)

WARNING: Changing the gain in Weather Mode will cause precipitation
intensity to be displayed as a color not representative of the true intensity.
Remember to return the gain setting to ‘Calibrated’ for viewing the actual
intensity of precipitation.

Select the GAIN Softkey to activate the cursor in the ‘GAIN’ field.

Turn the small FMS Knob to adjust the gain for the desirable level. The
gain setting is visible in the gain field as a movable horizontal bar in
a flashing box. The line pointer is a reference depicting the calibrated
position.

Press the FMS Knob to remove the cursor.

Select the GAIN Softkey again to recalibrate the gain. ‘CALIBRATED’ will be
displayed in the ‘GAIN’ field.

Press the MODE Softkey.

Press the GROUND Softkey to place the radar in Ground Map Mode.

Press the BACK Softkey.

Press the FMS Knob to activate the cursor.

Turn the large FMS Knob to place the cursor in the ‘TILT’ field.

Adjust the antenna tilt angle by turning the small FMS Knob to position the
ground returns as desired.

Press the FMS Knob to remove the cursor.

Abnormal

Operation

AlertsAppendixIndex

Annun/

Sector Scan

1)

While in the Horizontal Scan Mode, move the Joystick right or left to place
the Bearing Line in the desired position. The location of the Bearing Line
will become the center point of the Sector Scan.

2)

Press the FMS Knob to display the cursor.

3)

Turn the large FMS Knob to place the cursor in the SECTOR SCAN field.

4)

Turn the small FMS Knob to select FULL, 60˚, 40˚, or 20˚ scan.

5)

If desired, readjust the Bearing Line with the Joystick to change the center
of the Sector Scan.

6)

Press the FMS Knob to remove the cursor.

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Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

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Hazard Avoidance

Antenna Stabilization

1)

To activate or deactivate the antenna stabilization, select the MODE
Softkey.

2)

Select the STAB ON Softkey to activate antenna stabilization or select
the STAB OFF Softkey to deactivate. The current stabilization condition is
shown in the upper right of the weather radar display.

Weather Attenuated Color Highlight (WATCH®)

To activate or deactivate the WATCH® feature, select the WATCH Softkey. This
feature is only available in the Horizontal Scan Mode.

Weather Alert

To activate or deactivate Weather Alert, select the WX ALRT Softkey. Activating
and deactivating will also enable or inhibit the alert on the PFD.

Automatic Standby

When the weather radar system is in the Weather or Ground Map Mode, upon
landing the system will automatically switch to Standby Mode.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

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Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Hazard Avoidance

Flight

InstrumentsEAS

Nav/Com/

XPDR/AudioAFCSGPS Nav

Flight

PlanningProcedures

Blank Page

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

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Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

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Additional Features

ADDITIONAL FEATURES

SYNTHETIC VISION

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 the accuracy and/or fidelity upon which
to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or
traffic.

Synthetic Vision System (SVS) functionality is offered as an optional enhancement
to the G1000 Integrated Flight Deck 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).

SVS offers a three-dimensional view of terrain and obstacles. Terrain and
obstacles that pose a threat to the aircraft in flight are shaded yellow or red.

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

• Pathways

• Flight Path Marker

• Horizon Heading Marks

• Terrain and Obstacle Alerting

• Three-dimensionalTrafc

• Airport Signs

• Runway Display

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Displaying Synthetic Terrain

1)

Press the PFD Softkey.

2)

Press the SYN VIS Softkey.

3)

Press the SYN TERR Softkey.

4)

Press the BACK Softkey to return to the previous page.

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Alerts Appendix Index

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Additional Features

Displaying Pathways

Flight

Nav/Com/

Flight

Hazard

1)

InstrumentsEAS

XPDR/AudioAFCSGPS Nav

PlanningProcedures

Avoidance

Press the PFD Softkey.

2)

Press the SYN VIS Softkey.

3)

If not already enabled, press the SYN TERR Softkey.

4)

Press the PATHWAY Softkey.

5)

Press the BACK Softkey to return to the previous page.

Displaying Heading on the Horizon

1)

Press the PFD Softkey.

2)

Press the SYN VIS Softkey.

3)

If not already enabled, press the SYN TERR Softkey.

4)

Press the HRZN HDG Softkey.

5)

Press the BACK Softkey to return to the previous page.

Displaying Airport Signs

1)

Press the PFD Softkey.

2)

Press the SYN VIS Softkey.

3)

If not already enabled, press the SYN TERR Softkey.

4)

Press the APTSIGNS Softkey.

5)

Press the BACK Softkey to return to the previous page.

TERMINAL PROCEDURE CHARTS

Features

Additional

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

Abnormal

Operation

AlertsAppendixIndex

Annun/

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

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 identiers, 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.

Pressing the DCLTR Softkey (declutter) once removes the taxiway markings and

airportidenticationlabels.PressingtheDCLTRSoftkeytwiceremovesVORstation

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Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

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Additional Features

ID, the VOR symbol, and intersection names if within the airport plan view. Pressing
the DCLTR Softkey a third time removes the airport runway layout, unless the airport
in view is part of an active route structure. Pressing 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

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.

View Charts from the Navigation Map Page

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

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.

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Alerts Appendix Index

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Additional Features

View Charts from the Active Flight Plan Page

Flight

InstrumentsEAS

1)

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

2)

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

3)

Select the SHW CHRT Softkey. The appropriate chart is displayed, if
available for the item selected.

Nav/Com/

XPDR/AudioAFCSGPS Nav

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.

3)

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

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.

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Additional Features

XM® RADIO ENTERTAINMENT

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 EAS

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.

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Alerts Appendix Index

Annun/

Additional Features

Entering a Channel Directly

Flight

InstrumentsEAS

1)

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

2)

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

3)

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

4)

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)

Features

Additional

Abnormal

Operation

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

XM Radio volume may also be adjusted on each passenger headset.

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Abnormal Operation

ABNORMAL OPERATION

REVERSIONARY MODE

Reversionary mode must be entered manually in the case of PFD1, PFD2,
or MFD failure

with engine instrumentation on the remaining display.

Activation of reversionary display mode is accomplished by pressing the DISPLAY

BACKUP Button on the appropriate audio panel.

• PFD1 – By pressing the DISPLAY BACKUP Button on the left audio panel.

• MFD – By pressing the DISPLAY BACKUP Button on the left or the right

audio panel.

• PFD2 – By pressing the DISPLAY BACKUP Button on the right audio

panel.

NOTE: The Socata TBM 700 Airplane Flight Manual (AFM) always takes
precedence over the information found in this section.

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eldof the COM
radio for which the tuning failure was detected. In the event of a failure of both PFDs,
the emergency frequency (121.500 MHz) automatically becomes the active frequency
on both COM radios.

. In reversionary mode, critical flight instrumentation is combined

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

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

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Operation

Abnormal

Annun/

Alerts Appendix Index

Abnormal Operation

UNUSUAL ATTITUDES

Flight

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

InstrumentsEAS

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

• Radar Altimeter

• SelectedAltitude

• VNV Target Altitude

Features

Additional

Extreme Pitch Indication

Abnormal

Operation

DEAD RECKONING

While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS

AlertsAppendixIndex

Annun/

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.

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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

gure.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

gure.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 EAS

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

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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

InstrumentsEAS

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/

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Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

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CAS MESSAGES

Annunciations & Alerts

ANNUNCIATIONS & ALERTS

Instruments EAS

Flight

Warning Messages

Messages Comments

BAT OVERHEAT Battery temperature over 70°C

BLEED TEMP Bleed temperature high

CABIN ALTITUDE Cabin altitude over 10,000 ft

CABIN DIFF PRESS Cabin pressure differential over 6.2 psi

DOOR Pilot or cabin door open

FIRE Engine compartment fire (temperature over 200°C; if installed)

FLAPS ASYM Dissymmetry between left- and right-hand flaps

FUEL OFF Fuel tank selectors set to “Off”

FUEL PRESS Fuel pressure below 10 psi

Engine start (models A, B, & C): ITT over 1000°C, 870°C (5 seconds),
or 800°C (20 seconds)

ITT

Engine start (model N only): ITT over 1000°C, 870°C (5 seconds), or
840°C (20 seconds)
Engine running: ITT over 840°C

OIL PRESS Oil pressure below 60 psi

OXYGEN

Oxygen cylinder closed (gaseous oxygen systems). Oxygen system
has been activated (chemical oxygen systems).

PARK BRAKE Parking brake applied

TORQUE

Torque greater than or equal to 121.4% maximum torque (N only)

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 Socata TBM 700

Alerts Appendix Index

Annun/

Annunciations & Alerts

Caution Messages

Flight

InstrumentsEAS

Messages Comments

AUTO SEL Fuel timer off or out of service

AUX BOOST PMP ON Electric fuel pump running (manual or automatic mode)

BAT AMP Battery current over 50 A while on ground

BAT OFF Battery off

Nav/Com/

XPDR/AudioAFCSGPS Nav

BLEED OFF Flow control and shut-off valve/shut-off valve closed

CHIP Oil chip detector on (if installed)

FRONT CARGO DOOR Forward baggage door open

FUEL IMBALANCE

Fuel tanks imbalanced by more than 25 USGAL (A, B, and C) or
15 USGAL (N) for >30 seconds

FUEL LOW L-R* Fuel quantity less than or equal to 9.1 USGAL in specified tank

GPU DOOR GPU receptacle door not closed

IGNITION Ignition exciter running

Flight

INERT SEP FAIL Inertial separator failure

PlanningProcedures

INERT SEP ON Inertial separator extended

LOW LVL FAIL L-R* Low fuel level sensor failure for specified tank

LOW VOLTAGE Battery voltage below 26 V

MAIN GEN Starter generator unconnected

Hazard

Avoidance

NG HI Generator speed is more than 103%
OIL PRESS Oil pressure between 60 and 100 psi
OIL TEMP Oil temperature below 0°C or above 104°C

PITOT HT ON 1-2* Specified pitot heat (#1 or #2) on while engine off

Features

Additional

PITOT NO HT 1-2* Specified pitot heat (#1 or #2) off

PROP DEICE FAIL Prop deice selected and not on

Abnormal

Operation

PROP DEICE ON Prop deice on while engine off

REAR CARGO DOOR Rear cargo door open

STALL HEAT ON Stall warning heat on while engine off

AlertsAppendixIndex

Annun/

STALL NO HEAT Stall warning heat off

STARTER Starter generator running

VACUUM LOW Vacuum pressure less than 3.75 in Hg

* Only affected side (L, R, L-R or 1, 2, 1-2) displayed in CAS message; applicable messages listed here
display L-R or 1-2 for example

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Annunciations & Alerts

COMPARATOR ANNUNCIATIONS

Comparator

Window Text

ALT MISCOMP

IAS MISCOMP

HDG MISCOMP

PIT MISCOMP

ROL MISCOMP

ALT NO COMP
IAS NO COMP

HDG NO COMP

PIT NO COMP

ROL NO COMP

Difference in altitude sensors is > 200 ft.

If both airspeed sensors detect < 35 knots, this is inhibited.

If either airspeed sensor detects > 35 knots, and the difference in sensors is > 10
kts.

If either airspeed sensor detects > 80 knots, and the difference in sensors is > 7
kts.

Difference in heading sensors is > 6 degrees.

Difference in pitch sensors is > 5 degrees.

Difference in roll sensors is > 6 degrees.

No data from one or both altitude sensors.

No data from one or both airspeed sensors.

No data from one or both heading sensors.

No data from one or both pitch sensors.

No data from one or both roll sensors.

Condition

REVERSIONARY SENSOR ANNUNCIATIONS

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Reversionary

Condition

Sensor

Window Text

BOTH ON ADC1
BOTH ON ADC2

BOTH ON AHRS1

BOTH ON AHRS2

BOTH ON GPS1
BOTH ON GPS2

USING ADC1
USING ADC2

USING AHRS1

190-01247-00 Rev. A 71

Both PFDs are displaying data from the number one Air Data Computer.

Both PFDs are displaying data from the number two Air Data Computer.

Both PFDs are displaying data from the number one Attitude & Heading Reference
System.

Both PFDs are displaying data from the number two Attitude & Heading Reference
System.

Both PFDs are displaying data from the number one GPS receiver.

Both PFDs are displaying data from the number two GPS receiver.

PFD2 is displaying data from the #1 Air Data Computer.

PFD1 is displaying data from the #2 Air Data Computer.

PFD2 is displaying data from the #1 AHRS.

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

Annunciations & Alerts

Reversionary

Flight

InstrumentsEAS

Window Text

USING AHRS2

Nav/Com/

XPDR/AudioAFCSGPS Nav

Sensor

USING GPS1
USING GPS2

PFD1 is displaying data from the #2 AHRS.

PFD2 is displaying data from the #1 GPS.

PFD1 is displaying data from the #2 GPS.

Condition

AFCS ALERTS

Alert Condition Annunciation Description

Flight

PlanningProcedures

Hazard

Avoidance

Features

Additional

Abnormal

Operation

AlertsAppendixIndex

Annun/

Rudder Mistrim

Right

Rudder Mistrim

Left

Aileron Mistrim

Right

Aileron Mistrim

Left

Elevator Mistrim

Down

Elevator Mistrim

Up

Pitch Trim Failure

(or stuck MEPT

Switch)

Yaw Trim Failure

(or stuck MEYT

Switch)

Yaw Damper

Failure

Roll Failure Roll axis control failure; AP inoperative

Yaw servo providing sustained force in the indicated
direction. Aircraft rudder retrim after substantial pitch and
power changes required.

Roll servo providing sustained force in the indicated
direction

Pitch servo providing sustained force in the indicated
direction. May indicate a failure of the pitch trim servo or
trim system.

If AP engaged, take control of the aircraft and disengage AP
If AP disengaged, move MEPT switches separately to

unstick

If AP engaged, take control of the aircraft and disengage AP
If AP disengaged, move the MEYT switch to

switch is causing the annunciation

YD control failure; AP also inoperative

check if a stuck

Pitch Failure Pitch axis control failure; AP inoperative

System Failure AP and MEPT are unavailable; FD may still be available

72

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Annunciations & Alerts

Alert Condition Annunciation Description

Performing preflight system test; aural alert sounds at
completion

Do not press the AP DISC Switch during servo power-up
and preflight system tests as this may cause the preflight

Preflight Test

system test to fail or never to start (if servos fail their power­up tests). Power must be cycled to the servos to remedy
the situation.

Preflight system test failed; aural alert sounds at failure

TERRAIN-SVS ALERTS

PFD/MFD

Alert Type

Reduced Required Terrain
Clearance Warning (RTC)

Imminent Terrain Impact
Warning (ITI)

Reduced Required Obstacle
Clearance Warning (ROC)

Imminent Obstacle Impact
Warning (IOI)

Reduced Required Terrain
Clearance Caution (RTC)

Imminent Terrain Impact
Caution (ITI)

Reduced Required Obstacle
Clearance Caution (ROC)

Imminent Obstacle Impact
Caution (IOI)

TERRAIN-SVS

Page

Annunciation

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”

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-01247-00 Rev. A 73

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Annunciations & Alerts

TERRAIN-SVS SYSTEM STATUS ANNUNCIATIONS

Flight

InstrumentsEAS

Alert Type

System Test in
Progress

PFD/MFD Alert

Annunciation

TERRAIN-SVS Page

Annunciation

TERRAIN TEST None

System Test Pass None None

Nav/Com/

XPDR/AudioAFCSGPS Nav

Terrain Alerting is
disabled

MFD Terrain or
Obstacle database
unavailable or invalid.
Terrain-SVS operating

None TERRAIN DATABASE FAILURE None

with PFD Terrain or
Obstacle databases

Terrain System Test

Flight

PlanningProcedures

Fail

TERRAIN FAIL

Terrain or Obstacle
database unavailable
or invalid,
invalid software

TERRAIN FAIL

configuration, system

Hazard

audio fault

Avoidance

No GPS position NO GPS POSITION

Features

Additional

Excessively degraded
GPS signal, Out of
database coverage

Abnormal

Operation

area

Sufficient GPS signal
received after loss

AlertsAppendixIndex

Annun/

None None

None

None

Aural Message

“Terrain System

Test OK”

None

“Terrain System

Failure”

“Terrain System

Failure”

“Terrain System

Not Available”

“Terrain System

Not Available”

“Terrain System

Available”

74

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Annunciations & Alerts

TAWS 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)

Imminent Obstacle
Impact Warning
(IOI)

Reduced Required
Terrain Clearance
Caution (RTC)

Imminent Terrain
Impact Caution (ITI)

Reduced Required
Obstacle Clearance
Caution (ROC)

PFD/MFD
TAWS-B Page
Annunciation

MFD

Pop-Up Alert

or

or

or

or

or

or

or

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”

“Obstacle Ahead, Pull Up;

Obstacle Ahead, Pull Up”

or

“Obstacle, Obstacle; Pull Up,

Pull Up”

“Caution, Terrain; Caution,

Terrain”

or

“Terrain Ahead; Terrain Ahead”

“Terrain Ahead; Terrain Ahead”

or

“Caution, Terrain; Caution,

Terrain”

“Caution, Obstacle; Caution,

Obstacle”

or

“Obstacle Ahead; Obstacle

Ahead”

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-01247-00 Rev. A 75

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Annunciations & Alerts

Flight

InstrumentsEAS

Imminent Obstacle
Impact Caution

Alert Type

PFD/MFD

TAWS-B Page

Annunciation

MFD

Pop-Up Alert

or

Aural Message

“Obstacle Ahead; Obstacle

(IOI)

“Caution, Obstacle; Caution,

Nav/Com/

XPDR/AudioAFCSGPS Nav

Premature Descent

“Too Low, Terrain”

Alert Caution (PDA)

Altitude Callout

None None “Five-Hundred”

“500”

Excessive Descent
Rate Caution (EDR)

Negative Climb
Rate Caution

Flight

(NCR)

PlanningProcedures

or

“Don’t Sink”

“Too Low, Terrain”

TAWS System Status Annunciations

Alert Type

Hazard

Avoidance

System Test in Progress TAWS TEST None

PFD/MFD Alert

Annunciation

TAWS-B Page Annunciation

Ahead”

or

Obstacle”

“Sink Rate”

or

Aural

Message

System Test Pass None None

Features

Additional

TAWS Alerting is disabled

MFD Terrain or Obstacle
database unavailable or

Abnormal

Operation

invalid. TAWS operating

None TERRAIN DATABASE FAILURE None

with PFD Terrain or

AlertsAppendixIndex

Obstacle databases

Annun/

TAWS-B System Test Fail TAWS FAIL

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

76

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

None

TAWS FAIL

“TAWS System

Test OK”

None

“TAWS System

Failure”

“TAWS System

Failure”

190-01247-00 Rev. A

Annunciations & Alerts

Alert Type

PFD/MFD Alert

Annunciation

TAWS-B Page Annunciation

No GPS position NO GPS POSITION

Excessively degraded GPS
signal, Out of database

None

coverage area

Sufficient GPS signal
received after loss

None None

Aural

Message

“TAWS Not

Available”

“TAWS Not

Available”

“TAWS

Available”

VOICE ALERTS

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.

“Airspeed, Airspeed” Played when the indicated airspeed is below a given threshold for a

given aircraft configuration. Note this alert may be heard under normal
conditions during the landing flare.

“Traffic” Played when a Traffic Advisory (TA) is issued with the TIS system.

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

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

“TAS System Test OK” Played when the TAS system passes a pilot-initiated self test.

“TAS System Test Failed” Played when the TAS system fails a pilot-initiated self test.

“One o’clock” through

“Twelve o’clock”

or “No Bearing”

“High”, “Low”, “Same

Altitude” (if within 200
feet of own altitude), or
“Altitude not available”

“Less than one mile”,

“One Mile” through “Ten
Miles”, or “More than ten

miles”

Played to indicate bearing of traffic from own aircraft (GTS 820 only).

Played to indicate altitude of traffic relative to own aircraft (GTS 820 only).

Played to indicate distance of traffic from own aircraft (GTS 820 only).

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-01247-00 Rev. A 77

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Annunciations & Alerts

MFD & PFD MESSAGE ADVISORIES

Flight

InstrumentsEAS

DATA LOST

Message Comments

– Pilot stored data was

lost. Recheck settings.

XTALK ERROR

Nav/Com/

XPDR/AudioAFCSGPS Nav

– A flight display

crosstalk error has occurred.

PFD1 SERVICE

– PFD1 needs

service. Return unit for repair.

PFD2 SERVICE

– PFD2 needs

service. Return unit for repair.

MFD1 SERVICE

Flight

service. Return unit for repair.

PlanningProcedures

MANIFEST

– MFD1 needs

– PFD1 software

mismatch, communication halted.

MANIFEST

– PFD2 software

mismatch, communication halted.

Hazard

MANIFEST

Avoidance

– MFD1 software

mismatch, communication halted.

PFD1 CONFIG

Features

Additional

Config service req’d.

PFD2 CONFIG

Config service req’d.

Abnormal

Operation

MFD1 CONFIG

– PFD1 config error.

– PFD2 config error.

– MFD1 config

error. Config service req’d.

AlertsAppendixIndex

Annun/

SW MISMATCH

– GDU software

version mismatch. Xtalk is off.

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

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.

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

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

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

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

78

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Annunciations & Alerts

MFD & PFD MESSAGE ADVISORIES (CONT.)

Message Comments

PFD1 COOLING

cooling. Reducing power usage.

PFD2 COOLING

cooling. Reducing power usage.

MFD1 COOLING

– PFD1 has poor

– PFD2 has poor

– MFD1 has poor

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.

cooling. Reducing power usage.

PFD1 KEYSTK

Key is stuck.

PFD2 KEYSTK

Key is stuck.

MFD1 KEYSTK

– PFD1 [key name]

– PFD2 [key name]

– MFD [key name]

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.

Key is stuck.

CNFG MODULE

configuration module is
inoperative.

PFD1 VOLTAGE

voltage. Reducing power usage

PFD2 VOLTAGE

voltage. Reducing power usage

MFD1 VOLTAGE

voltage. Reducing power usage

– PFD1

– PFD1 has low

– PFD2 has low

– MFD1 has low

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 PFD2 voltage is low. The G1000 system
should be serviced.

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

DATABASE MESSAGE ADVISORIES

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Message Comments

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 navigation

– PFD1 navigation

– PFD2 navigation

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

database error exists.

190-01247-00 Rev. A 79

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Alerts Appendix Index

Annun/

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEAS

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

Nav/Com/

PFD2 DB ERR

XPDR/AudioAFCSGPS Nav

database error exists.

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

database error exists.

Flight

PlanningProcedures

MFD1 DB ERR

database missing.

PFD1 DB ERR

database missing.

PFD2 DB ERR

Hazard

database missing.

Avoidance

MFD1 DB ERR

database error exists.

Features

Additional

PFD1 DB ERR

database error exists.

PFD2 DB ERR

Abnormal

Operation

database error exists.

MFD1 DB ERR

AlertsAppendixIndex

Annun/

database missing.

PFD1 DB ERR

database missing.

PFD2 DB ERR

database missing.

Message Comments

– MFD1 basemap

– PFD1 basemap

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

– PFD2 basemap

– MFD1 terrain

The MFD and/or PFD detected a failure in the

– PFD1 terrain

terrain database. Ensure that the terrain card is
properly inserted in display. Replace terrain card.
If problem persists, The G1000 system should be

– PFD2 terrain

serviced.

– MFD1 terrain

– PFD1 terrain

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

– PFD2 terrain

– MFD1 obstacle

The MFD and/or PFD detected a failure in the

– PFD1 obstacle

obstacle database. Ensure that the data card is
properly inserted. Replace data card. If problem

– PFD2 obstacle

persists, The G1000 system should be serviced.

– MFD1 obstacle

– PFD1 obstacle

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

– PFD2 obstacle

80

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Message Comments

MFD1 DB ERR

terrain database error exists.

PFD1 DB ERR

terrain database error exists.

PFD2 DB ERR

– MFD1 airport

– PFD1 airport

– PFD2 airport

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.

terrain database error exists.

MFD1 DB ERR

– MFD1 airport

terrain database missing.

PFD1 DB ERR

– PFD1 airport

terrain database missing.

PFD2 DB ERR

– PFD2 airport

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

terrain database missing.

MFD1 DB ERR

database error exists.

PFD1 DB ERR

database error exists.

PFD2 DB ERR

– MFD1 Safe Taxi

– PFD1 Safe Taxi

– PFD2 Safe Taxi

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.

database error exists.

MFD1 DB ERR

database error exists.

– MFD1 Chartview

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

MFD1 DB ERR

database error exists.

– MFD1 FliteCharts

The MFD 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.

– Navigation

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

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-01247-00 Rev. A 81

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Annunciations & Alerts

DATABASE MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEAS

DB MISMATCH

Message Comments

– Navigation
database type mismatch. Xtalk is
off.

DB MISMATCH

Nav/Com/

XPDR/AudioAFCSGPS Nav

– Terrain database
version mismatch.

DB MISMATCH

– Terrain database
type mismatch.

DB MISMATCH

– Obstacle
database version mismatch.

Flight

PlanningProcedures

DB MISMATCH

– Airport Terrain
database mismatch.

NAV DB UPDATED

navigation database updated.

Hazard

Avoidance

TERRAIN DSP

– Active

– [PFD1, PFD2 or
MFD1] Terrain awareness display
unavailable.

Features

Additional

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

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

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

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

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

System has updated the active navigation
database from the standby navigation database.

One of the terrain, airport terrain, or obstacle
databases required for TAWS in the specified PFD
or MFD is missing or invalid.

GMA 1347D MESSAGE ADVISORIES

Abnormal

Operation

AlertsAppendixIndex

Annun/

GMA1 FAIL
GMA2 FAIL

GMA XTALK

Message Comments

– GMA1 is inoperative. The audio panel self-test has detected a failure.
– GMA2 is inoperative.

– GMA crosstalk error

has occurred.

82

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

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

An error has occurred in transferring data
between the two GMAs. The G1000 system
should be serviced.

190-01247-00 Rev. A

Annunciations & Alerts

GMA 1347D MESSAGE ADVISORIES (CONT.)

Message Comments

GMA1 CONFIG

error. Config service req’d.

– GMA1 config

The audio panel configuration settings do not
match backup configuration memory. The

GMA2 CONFIG

– GMA2 config

G1000 system should be serviced.

error. Config service req’d.

MANIFEST – GMA1 software

mismatch, communication halted.

MANIFEST – GMA2 software

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

mismatch, communication halted.

GMA1 SERVICE – GMA1 needs

service. Return unit for repair.

GMA2 SERVICE – GMA2 needs

service. Return unit for repair.

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.

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 be

GIA2 CONFIG

– GIA2 audio config

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.

Instruments EAS

Flight

XPDR/Audio AFCS GPS Nav

Nav/Com/

Planning Procedures

Flight

Avoidance

Hazard

Additional

Features

Operation

Abnormal

Annun/

Alerts Appendix Index

190-01247-00 Rev. A 83

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

Annunciations & Alerts

GIA 63W MESSAGE ADVISORIES (CONT.)

Flight

InstrumentsEAS

GIA1 SERVICE

Message Comments

– GIA1 needs

service. Return the unit for repair.

GIA2 SERVICE

– GIA2 needs

service. Return the unit for repair.

Nav/Com/

HW MISMATCH

XPDR/AudioAFCSGPS Nav

– GIA hardware
mismatch. GIA1 communication
halted.

HW MISMATCH

– GIA hardware
mismatch. GIA2 communication
halted.

MANIFEST

– GIA1 software

mismatch, communication halted.

Flight

PlanningProcedures

MANIFEST

– GIA2 software

mismatch, communication halted.

MANIFEST

– GFC software

mismatch, communication halted.

COM1 TEMP

Hazard

Reducing transmitter power.

Avoidance

COM2 TEMP

– COM1 over temp.

– COM2 over temp.

Reducing transmitter power.

Features

Additional

COM1 SERVICE

– COM1 needs

service. Return unit for repair.

Abnormal

Operation

COM2 SERVICE

– COM2 needs

service. Return unit for repair.

AlertsAppendixIndex

Annun/

COM1 PTT

– COM1 push-to-talk

key is stuck.

COM2 PTT

– COM2 push-to-talk

key is stuck.

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

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.

84

Garmin G1000 Cockpit Reference Guide for the Socata TBM 700

190-01247-00 Rev. A