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