Garmin | G1000: Socata TBM 850 | Garmin G1000: Socata TBM 850 G1000 Cockpit Reference Guide for TBM 850/900 - SSV 0719.16

Garmin G1000: Socata TBM 850 G1000 Cockpit Reference Guide for TBM 850/900 - SSV 0719.16
G1000
®
Integrated Flight Deck
Cockpit Reference Guide
TBM 850 & TBM 900
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 © 2007, 2009-2011, 2014-2016 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0719.16 or later for the Socata
TBM 850/900. Some differences in operation may be observed when comparing the information
in this manual to earlier or later software versions.
Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.
Tel: 913/397.8200Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: 503/391.3411Fax 503/364.2138
Garmin (Europe) Ltd, Liberty House, Hounsdown Business Park, Southampton, SO40 9LR, U.K.
Tel: 44/023.8052.4000Fax: 44/23.8052.4004
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: 886/02.2642.9199
Fax: 886/02.2642.9099
For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount
and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836.
Web Site Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied,
transmitted, disseminated, downloaded or stored in any storage medium, for any purpose
without the express written permission of Garmin. Garmin hereby grants permission to
download a single copy of this manual and of any revision to this manual onto a hard drive or
other electronic storage medium to be viewed for personal use, provided that such electronic
or printed copy of this manual or revision must contain the complete text of this copyright
notice and provided further that any unauthorized commercial distribution of this manual or any
revision hereto is strictly prohibited.
Garmin® and G1000®, WATCH®, FliteCharts®, and SafeTaxi® are registered trademarks of
Garmin Ltd. or its subsidiaries. Connext™ is a trademark 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.
SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, Inc.
AC-U-KWIK® is a registered trademark of Penton Business Media Inc.
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively
“AOPA”) expressly disclaim all warranties, with respect to the AOPA information included in this
data, express or implied, including, but not limited to, the implied warranties of merchantability
and fitness for a particular purpose. The information is provided “as is” and AOPA does not
warrant or make any representations regarding its accuracy, reliability, or otherwise. Under
no circumstances including negligence, shall AOPA be liable for any incidental, special or
consequential damages that result from the use or inability to use the software or related
documentation, even if AOPA or an AOPA authorized representative has been advised of the
possibility of such damages. User agrees not to sue AOPA and, to the maximum extent allowed
by law, to release and hold harmless AOPA from any causes of action, claims or losses related
to any actual or alleged inaccuracies in the information. Some jurisdictions do not allow the
limitation or exclusion of implied warranties or liability for incidental or consequential damages
so the above limitations or exclusions may not apply to you.
AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”)
expressly disclaim all warranties with respect to the AC-U-KWIK information included in this
data, express or implied, including, but not limited to, the implied warranties of merchantability
and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK
Organizations do not warrant or make any representations regarding its accuracy, reliability, or
otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the maximum extent
allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of
action, claims or losses related to any actual or alleged inaccuracies in the information arising
out of Garmin’s use of the information in the datasets. Some jurisdictions do not allow the
limitation or exclusion of implied warranties or liability for incidental or consequential damages
so the above limitations or exclusions may not apply to licensee.
April, 2016
190-00708-07 Rev. B
Printed in the U.S.A
Warnings, Cautions & Notes
WARNING: Navigation and terrain separation must NOT be predicated upon
the use of the terrain avoidance feature. The terrain avoidance feature is NOT
intended to be used as a primary reference for terrain avoidance and does
not relieve the pilot from the responsibility of being aware of surroundings
during flight. The terrain avoidance feature is only to be used as an aid for
terrain avoidance. Terrain data is obtained from third party sources. Garmin
is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory
in nature and should not be relied upon as the sole source of obstacle and
terrain avoidance information. Always refer to current aeronautical charts
for appropriate minimum clearance altitudes.
WARNING: Do not use outdated database information. Databases used in
the 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: Do not rely solely upon the display of traffic information for
collision avoidance maneuvering. The traffic display does not provide collision avoidance resolution advisories and does not under any circumstances
or conditions relieve the pilot’s responsibility to see and avoid other aircraft.
WARNING: Do not rely solely upon the display of traffic information to
accurately depict all of the traffic within range of the aircraft. Due to lack
of equipment, poor signal reception, and/or inaccurate information from
aircraft or ground stations, traffic may be present that is not represented on
the display.
WARNING: Do not use data link weather information for maneuvering in,
near or around areas of hazardous weather. Information contained within
data link weather products may not accurately depict current weather conditions.
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Warnings, Cautions & Notes
WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather
product. Due to time delays inherent in gathering and processing weather
data for data link transmission, the weather information shown by the data
link weather product may be significantly older than the indicated weather
product age.
WARNING: Do not rely on information from the lightning detection system
display as the sole basis for hazard weather avoidance. Range limitations
and interference may cause the system to display inaccurate or incomplete
information. Refer to the documentation from the lightning detection system
manufacturer for detailed information about the system.
WARNING: The system, as installed in the TBM 850/900 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 system. It is
thus the responsibility of the pilot to detect such an occurrence by means of
cross-checking with all redundant or correlated information available in the
cockpit.
WARNING: For safety reasons, system operational procedures must be
learned on the ground.
WARNING: The United States government operates the Global Positioning
System and is solely responsible for its accuracy and maintenance. The GPS
system is subject to changes which could affect the accuracy and performance
of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information
presented by the system can be misused or misinterpreted and, therefore,
become unsafe.
WARNING: 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.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Warnings, Cautions & Notes
WARNING: To reduce the risk of unsafe operation, carefully review and
understand all aspects of the Pilot’s Guide documentation and the TBM
850/900 Airplane Flight Manual. Thoroughly practice basic operation prior
to actual use. During flight operations, carefully compare indications from
the system to all available navigation sources, including the information
from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always
resolve any discrepancies before continuing navigation.
WARNING: The illustrations in this guide are only examples. Never use
the system to attempt to penetrate a thunderstorm. Both the FAA Advisory
Circular, Subject: Thunderstorms, and the Aeronautical Information Manual
(AIM) recommend avoiding “by at least 20 miles any thunderstorm identified
as severe or giving an intense radar echo.”
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.
WARNING: Do not use a QFE altimeter setting with this system. System
functions will not operate properly with a QFE altimeter setting. Use only
a QNH altimeter setting for height above mean sea level, or the standard
pressure setting, as applicable.
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Warnings, Cautions & Notes
CAUTION: The PFD and MFD displays use a lens coated with a special antireflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI-REFLECTIVE
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 anti-reflective coatings.
CAUTION: The system does not contain any user-serviceable parts. Repairs
should only be made by an authorized Garmin service center. Unauthorized
repairs or modifications could void both the warranty and the pilot’s authority
to operate this device under FAA/FCC regulations.
NOTE: All visual depictions contained within this document, including screen
images of the panel and displays, are subject to change and may not reflect
the most current system and databases. Depictions of equipment may differ
slightly from the actual equipment.
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.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Warnings, Cautions & Notes
NOTE: Operating the system in the vicinity of metal buildings, metal
structures, or electromagnetic fields can cause sensor differences that may
result in nuisance miscompare annunciations during start up, shut down, or
while taxiing. If one or both of the sensed values are unavailable, it will be
annunciated as a ‘NO COMP’ (no compare).
NOTE: Use of polarized eyewear may cause the flight displays to appear dim
or blank.
NOTE: The FAA has asked Garmin to remind pilots who fly with Garmin
database-dependent avionics of the following:
• It is the pilot’s responsibility to remain familiar with all FAA regulatory
and advisory guidance and information related to the use of databases in
the National Airspace System.
• Garmin equipment will only recognize and use databases that are
obtained from Garmin or Jeppesen. Databases obtained from Garmin
or Jeppesen are assured compliance with all data quality requirements
(DQRs) by virtue of a Type 2 Letter of Authorization (LOA) from the FAA. A
copy of the Type 2 LOA is available for each database and can be viewed
at http://fly.garmin.com by selecting ‘Type 2 LOA Status.’
• Use of a current Garmin or Jeppesen database in your Garmin equipment
is required for compliance with established FAA regulatory guidance, but
does not constitute authorization to fly any and all terminal procedures
that may be presented by the system. It is the pilot’s responsibility to
operate in accordance with established AFM(S) and regulatory guidance or
limitations as applicable to the pilot, the aircraft, and installed equipment.
NOTE: The pilot/operator must review and be familiar with Garmin’s database
exclusion list as discussed in SAIB CE-14-04 to determine what data may be
incomplete. The database exclusion list can be viewed at www.flygarmin.
com by selecting ‘Database Exclusions List.’
NOTE: The pilot/operator must have access to Garmin and Jeppesen database
alerts and consider their impact on the intended aircraft operation. The
database alerts can be viewed at www.flygarmin.com by selecting ‘Aviation
Database Alerts.’
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Warnings, Cautions & Notes
NOTE: If the pilot/operator wants or needs to adjust the database, contact
Garmin Product Support to coordinate the revised DQRs.
NOTE: Garmin requests the flight crew report any observed discrepancies
related to database information. These discrepancies could come in the form
of an incorrect procedure; incorrectly identified terrain, obstacles and fixes;
or any other displayed item used for navigation or communication in the air
or on the ground. Go to FlyGarmin.com and select ‘Report An Aviation Data
Error Report.’
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Record of Revisions
Part Number
190-00708-00
Initial Release
190-00708-01
Rev A
Added SVS and other GDU 9.02 parameters.
Rev B
190-00708-02
190-00708-03
Rev A
190-00708-04
190-00708-05
190-00708-07 Rev. B
Change Summary
Clerical changes
Added temporary user waypoints
Added import/export flight plans
Added CDI availability during Dead Reckoning mode
Added GDU 9.14 parameters.
Added GDU 11.01 parameters.
Added GTS 820
Added AOPA Airport Directory
Added database synchronization
Added Profile View
Added Standby Navigation Database
Added new database update procedures
Added Iridium Satellite Telephone & SMS messaging
Added GFDS Worldwide Weather
Added WX LGND, LEGEND, and METAR softkeys
Updated system messages
Added other GDU 12.01 parameters
Added TBM 900
Added Maintenance Log feature
Added Auxiliary Video
Added CPDLC
Added AC-U-KWIK Airport Directory
Added User Defined Holding Patterns
Added Landing Field Elevation enty
Added temperature compensated altitude
Changed GFDS Weather to Connext™ Weather
Changed XM to SiriusXM
Changed Synthetic Vision System (SVS) to Synthetic Vision
Technology (SVT)
Added other GDU 14.01 parameters
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
RR-1
Record of Revisions
Part Number
190-00708-06
190-00708-07
Change Summary
Added Telephone Contacts
Added Bluetooth Management for Flight Stream 210
Updated CAS and audio messages
Updated softkey maps
Added other GDU 15.00 parameters
Added GDU 15.11 parameters
Updated softkey maps
Updated system software number
Updated CAS messages
Updated NEXRAD references
Added Altitude Compensated Tilt procedures
Updated database procedures
Added datalink receiver messages
Revision Date of Revision Affected Pages
A
April, 2016
All
B
April, 2016
All
RR-2
Description
Production release
Added ESP information
Added AOA indicator information
Updated CAS messages
Updated aural alerts
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
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
Enable/Disable the AOA Indicator Display Mode............................................................... 2
Generic Timer.............................................................................................................................. 2
Configure Vspeed Bugs............................................................................................................. 3
Set Barometric/Radar Altimeter Minimum Descent Altitude.......................................... 3
Manually Testing the Radar Altimeter (KRA 405B only)................................................... 3
Displaying Wind Data............................................................................................................... 4
Changing HSI Format................................................................................................................ 4
ENGINE & AIRFRAME SYSTEMS.............................................................................................. 5
Electrical System........................................................................................................................ 6
Fuel System................................................................................................................................. 8
General Systems...................................................................................................................... 10
Cabin Pressurization............................................................................................................... 11
NAV/COM/TRANSPONDER/AUDIO PANEL........................................................................ 13
Enter or Change Flight ID (Optional)................................................................................... 13
ADF Tuning (Optional)............................................................................................................. 13
DME Tuning (Optional)............................................................................................................ 13
Enter a Transponder Code..................................................................................................... 14
Selecting a COM Radio........................................................................................................... 14
Selecting a NAV Radio............................................................................................................ 14
NAV/COM Tuning...................................................................................................................... 14
Intercom..................................................................................................................................... 15
Controller Pilot Data Link Communications (Optional).................................................. 15
Passenger Address (PA) System............................................................................................ 19
Clearance Recorder and Player............................................................................................ 19
AUTOMATIC FLIGHT CONTROL SYSTEM........................................................................... 21
Flight Director Activation...................................................................................................... 21
Vertical Modes.......................................................................................................................... 22
Lateral Modes........................................................................................................................... 23
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
i
Table of Contents
GPS NAVIGATION......................................................................................................................... 25
Direct-to Navigation............................................................................................................... 25
Activate a Stored Flight Plan................................................................................................ 26
Activate a Flight Plan Leg...................................................................................................... 26
Stop Navigating a Flight Plan............................................................................................... 27
Vertical Navigation (VNAV)................................................................................................... 27
FLIGHT PLANNING....................................................................................................................... 29
Weight Planning....................................................................................................................... 29
Trip Planning............................................................................................................................. 29
Create a User Waypoint Defined by Latitude & Longitude............................................ 31
Create a User Waypoint Defined by Radials from Other Waypoints............................ 32
Create a User Waypoint Defined by a Radial & Distance from Another Waypoint... 34
Delete a User Waypoint.......................................................................................................... 35
Create a Flight Plan................................................................................................................. 36
Import a Flight Plan from an SD Card................................................................................. 37
Insert a Waypoint in the Active Flight Plan....................................................................... 37
Enter an Airway in a Flight Plan........................................................................................... 38
Creating a User-Defined Hold at an Active Flight Plan Waypoint................................. 39
Creating a User-Defined Hold at the Aircraft Present Position..................................... 39
Removing a User-Defined Hold (Created at the Aircraft P.POS)................................... 40
Removing a User-Defined Hold (Created at an Active Waypoint)................................ 40
Invert An Active Flight Plan................................................................................................... 40
Remove a Departure, Arrival, Approach, or Airway from a Flight Plan...................... 41
Store a Flight Plan................................................................................................................... 41
Edit a Stored Flight Plan........................................................................................................ 41
Delete a Waypoint from the Flight Plan............................................................................. 42
Invert and Activate a Stored Flight Plan............................................................................ 42
Copy a Flight Plan.................................................................................................................... 43
Delete a Flight Plan................................................................................................................. 43
Graphical Flight Plan Creation.............................................................................................. 43
Export a Flight Plan to an SD Card...................................................................................... 44
PROCEDURES.................................................................................................................................. 45
Load and Activate a Departure Procedure........................................................................ 45
Activate A Departure Leg...................................................................................................... 45
Load An Arrival Procedure..................................................................................................... 45
Activate An Arrival Leg.......................................................................................................... 46
Load and/or Activate an Approach Procedure.................................................................. 46
Activate An Approach in the Active Flight Plan................................................................ 47
Activate a Vector to Final Approach Fix............................................................................. 47
Activate A Missed Approach in the Active Flight Plan.................................................... 48
Temperature Compensated Altitude................................................................................... 48
ii
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Table of Contents
HAZARD AVOIDANCE................................................................................................................. 51
Customizing the Hazard Displays on the Navigation Map............................................. 51
STORMSCOPE® (Optional)..................................................................................................... 51
SiriusXM Weather (Optional)................................................................................................ 53
Garmin Connext™ Weather.................................................................................................... 55
Traffic Systems......................................................................................................................... 63
Terrain And Obstacle Proximity............................................................................................ 65
Terrain-SVT................................................................................................................................ 65
Terrain Awareness & Warning System (TAWS-B) Display................................................ 67
Airborne Color Weather Radar............................................................................................. 69
Altitude Compensated Tilt..................................................................................................... 74
ADDITIONAL FEATURES............................................................................................................ 75
Synthetic Vision........................................................................................................................ 75
Terminal Procedure Charts.................................................................................................... 76
Airport Directory..................................................................................................................... 78
SiriusXM Satellite Radio Entertainment............................................................................ 79
Satellite Telephone & SMS Messaging Service................................................................. 81
Maintenance Logs.................................................................................................................... 93
Auxiliary Video (Optional)..................................................................................................... 94
Scheduler................................................................................................................................... 95
Pilot Profiles............................................................................................................................. 97
Bluetooth® Management..................................................................................................... 101
Electronic Stability & Protection (ESP™)......................................................................... 102
ABNORMAL OPERATION........................................................................................................ 103
Reversionary Mode............................................................................................................... 103
Abnormal COM Operation................................................................................................... 103
Hazard Displays with Loss of GPS Position...................................................................... 103
Unusual Attitudes.................................................................................................................. 104
Dead Reckoning..................................................................................................................... 104
Suspected Autopilot malfunction...................................................................................... 106
Overpowering Autopilot Servos........................................................................................ 107
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
iii
Table of Contents
ANNUNCIATIONS & ALERTS.................................................................................................. 109
CAS Messages......................................................................................................................... 109
Comparator Annunciations.................................................................................................. 111
Reversionary Sensor Annunciations.................................................................................. 111
AFCS Alerts.............................................................................................................................. 112
Terrain-SVT Alerts.................................................................................................................. 113
Terrain-SVT System Status Annunciations....................................................................... 114
TAWS-B Alerts......................................................................................................................... 115
Voice Alerts............................................................................................................................. 118
Message Advisories............................................................................................................... 119
Flight Plan Import/Export Messages................................................................................. 143
GDL 69/GDL 69A/GDL 69A SXM Data Link Receiver Messages.................................... 144
APPENDIX...................................................................................................................................... 145
PFD Softkey Map................................................................................................................... 145
MFD Softkey Map.................................................................................................................. 151
Updating Databases.............................................................................................................. 154
INDEX..........................................................................................................................................Index-1
iv
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Flight Instruments
Flight
Instruments
FLIGHT INSTRUMENTS
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
EAS
Turn the BARO Knob to select the desired setting.
Nav/Com/
XPDR/Audio
SELECTING STANDARD BAROMETRIC PRESSURE
Press the BARO Knob.
AFCS
CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS
2)
Select the ALT UNIT Softkey.
3)
Select the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Or:
4)
Procedures
Select the HPA Softkey to display the barometric pressure setting in
hectopascals.
Select the BACK Softkey to return to the top-level softkeys.
Hazard
Avoidance
SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS
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.
Abnormal
Operation
Select the AUX-SYSTEM SETUP Page on the MFD.
Additional
Features
1)
Annun/
Alerts
SYNCHRONIZE CDI
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window.
4)
Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Index
Select the AUX-SYSTEM SETUP Page on the MFD.
Appendix
1)
190-00708-07 Rev. B
Flight
Planning
Select the PFD Softkey to display the second-level softkeys.
GPS Nav
1)
1
CHANGE NAVIGATION SOURCES
1)
Select the CDI Softkey to change from GPS to VOR1 or LOC1. This places
the cyan 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 cyan tuning box over the NAV2 standby frequency.
3)
Select the CDI Softkey a third time to return to GPS.
ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS
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.
3)
Select the OBS Softkey again to disable OBS Mode.
1) Press the PFD Softkey.
2) Press AOA/WIND Softkey.
3) Press the AOA Softkey.
4) To turn the function on or off, press the AOA AUTO Softkey.
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
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.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
1)
ENABLE/DISABLE THE AOA INDICATOR DISPLAY MODE
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Flight Instruments
2
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Flight Instruments
Flight
Instruments
CONFIGURE VSPEED BUGS
1) Select the TMR/REF Softkey.
EAS
2) Turn the large FMS Knob to highlight the desired Vspeed.
3) Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field.
5)
Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
AFCS
4)
Nav/Com/
XPDR/Audio
speed has been changed from a default value, an asterisk appears next to
the speed).
GPS Nav
SET BAROMETRIC/RADAR ALTIMETER MINIMUM DESCENT ALTITUDE
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.
Hazard
Avoidance
Turn the large FMS Knob to highlight the OFF/BARO/TEMP COMP/RAD ALT
field to the right of ‘MINIMUMS’.
Additional
Features
MANUALLY TESTING THE RADAR ALTIMETER (KRA 405B ONLY)
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.
Appendix
2)
Annun/
Alerts
Select the AUX-SYSTEM STATUS Page on the MFD.
Abnormal
Operation
1)
Procedures
2)
Flight
Planning
1) Press the TMR/REF Softkey.
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
3
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.
CHANGING HSI FORMAT
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Flight Instruments
1)
Press the PFD Softkey.
2)
Press the HSI FRMT Softkey.
3)
Press the 360 HSI Softkey to display the full size HSI.
Or:
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
Press the ARC HSI Softkey to display the arc style HSI.
4
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Engine & Airframe Systems
1
Flight
Instruments
ENGINE & AIRFRAME SYSTEMS
1
EAS
8
2
2
Nav/Com/
XPDR/Audio
9
10
3
3
AFCS
11
4
GPS Nav
4
12
14
Flight
Planning
13
5
5
6
15
7
17
17
8
9
Hazard
Avoidance
16
Procedures
6
12
13
Additional
Features
15
EIS Display (Normal Mode)
(TBM 850 shown)
Abnormal
Operation
16
EIS Display (Reversionary Mode)
(TBM 850 shown)
Annun/
Alerts
1 Torque
7 CAS Display
13 Fuel Flow
2 Propeller Speed
8 Cabin Pressure Altitude and
14 Fuel Pressure (if installed)
4 Interturbine Temperature
10 Selected Cabin Altitude
6 Oil Temperature
190-00708-07 Rev. B
(TBM850) or
LFE (TBM 900)
11 Oxygen Pressure
12 Fuel Quantity
15 Battery and Generator
Currents
16 Battery and Essential Bus
Voltages
17 Elevator, Aileron, and
Index
5 Oil Pressure
(TBM 850 only)
Appendix
3 Generator Speed
Change Rate
9 Differential Pressure
Rudder Trim and Flap
Position
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
5
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.
EAS
Flight
Instruments
Engine & Airframe Systems
Nav/Com/
XPDR/Audio
1
2
3
GPS Nav
AFCS
4
5
Flight
Planning
6
7
Procedures
8
Abnormal
Operation
Additional
Features
Hazard
Avoidance
9
1
Standby Generator
4
Battery
7
Battery Bus
2
Main Generator
5
Main Bus
8
Essential Bus
3
Ground Power
Unit Door
6
Emergency Switch
9
Power Buses
Index
Appendix
Annun/
Alerts
Electrical Synoptics Page
6
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Engine & Airframe Systems
Flight
Instruments
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
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.
EAS
Switch Open
Switch Closed
Nav/Com/
XPDR/Audio
Standby
AFCS
Main
Generator Switch Status
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Battery Overheat Indication
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
7
FUEL SYSTEM
1) Select the SYSTEM Softkey to display the softkeys for the synoptics system.
2) Select the FUEL Softkey to display the Fuel System Page.
EAS
Flight
Instruments
Engine & Airframe Systems
Nav/Com/
XPDR/Audio
1
2
AFCS
3
4
GPS Nav
5
6
Flight
Planning
7
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
8
1
Left Fuel Tank
4
Auxiliary Boost Pump
7
Right Fuel Line
2
Left Fuel Line
5
Fuel Selector
8
Fuel Flow Data
3
Fuel Pressure (TBM
850 only)
6
Right Fuel Tank
Index
Appendix
Annun/
Alerts
Fuel Synoptics Page
8
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Engine & Airframe Systems
Right
Fuel Tank
Selected
Manual or
Unknown Fuel
Tank Selection
Fuel
Selector
Off
Nav/Com/
XPDR/Audio
Switching
Fuel Tank
Selection
EAS
Left Fuel
Tank
Selected
Flight
Instruments
Status of the fuel selector is indicated between the fuel tank symbols. The mode,
automatic (AUTO), manual (MAN), or off (no indication; CAS message ‘FUEL OFF’
generated) is shown beneath the fuel selector symbol.
AFCS
Flight
Planning
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 cyan (automatic mode) or red (manual
mode).
GPS Nav
Fuel Selector Status
Procedures
Fuel Boost Pump Fuel Boost Pump Fuel Boost Pump
On
Off (Auto)
Off (Manual)
Hazard
Avoidance
Additional
Features
Auxiliary Boost Pump Status
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
9
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 propeller, stall sensor heater, pitot probe, and
windshield heat are also indicated on the diagram:
• White indicates that heat is off (propeller and windshield)
• Cyan indicates heat has been selected (windshield)
• Green indicates heat is on
• Yellow indicates heat has failed (propeller, pitot tube, and stall sensor).
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Engine & Airframe Systems
Index
Appendix
General Synoptics Page
10
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Engine & Airframe Systems
EAS
Nav/Com/
XPDR/Audio
AFCS
Cabin pressurization information (cabin altitude, rate of change, and differential
cabin pressure) is shown at the top of the right EIS column. Only readouts for cabin
altitude and pressure differential are displayed in Reversionary Mode.
Cabin altitude (ALT FT) is shown on a color-coded scale labeled in 5,000-ft
increments with a readout (in feet) below. Cabin altitude change rate (RATE FPM) is
displayed on a scale in terms of 2,000 fpm increments with a readout (in fpm) below.
Cabin pressure differential (DIFF PSI), in pounds per square inch (psi), is indicated
on a color-coded scale with a readout. Selected Cabin Altitude is displayed as a digital
readout (in 100 ft increments) with a range from -1,000 to 11,000 feet.
Flight
Instruments
CABIN PRESSURIZATION
GPS Nav
Pressure
Altitude
Landing Field Elevation
From Active Flight Plan
Additional
Features
Cabin Pressure Display
Hazard
Avoidance
Oxygen
Pressure
Landing Field
Elevation Entered
Manually
11
Index
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Appendix
The Landing Field Elevation can be set based on the destination airport in the active
flight plan, or entered manually. When entered based on the active flight plan, the
elevation will be derived from the navigation database based on the destination airport.
System derived values appear with the destination airport identifier. Manually entered
values appear without the airport identifier. A red “X” is displayed if the LFE is out of
range or the data source is invalid.
Annun/
Alerts
LFE (Landing Field Elevation)(TBM 900 only)
Abnormal
Operation
The pressure (in psi) for the oxygen system is given as a readout below the cabin
pressurization display under normal display conditions.
190-00708-07 Rev. B
Procedures
Selected
Cabin
Altitude
Pressure
Differential
Flight
Planning
Pressure
Change
Rate
Engine & Airframe Systems
Flight
Instruments
Setting the displayed landing field elevation to the value for the
destination airport:
1) Select the SYSTEM Softkey.
EAS
2) Select the FMS LFE Softkey to set the LFE to the value for the destination
airport in the current flight plan.
1)
Select the SYSTEM Softkey.
2)
Select the MAN LFE Softkey.
3)
Use the ±250 and ±25 FT softkeys to set the desired elevation.
4)
To confirm the new LFE value, select the ACCEPT Softkey. If the ACCEPT
Softkey is not selected, the value will flash briefly and return to the previous
setting.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Manually setting the displayed landing field elevation:
12
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Nav/Com/XPDR/Audio Panel
Flight
Instruments
NAV/COM/TRANSPONDER/AUDIO PANEL
ENTER OR CHANGE FLIGHT ID (OPTIONAL)
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.
AFCS
2)
GPS Nav
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.
Abnormal
Operation
3)
Additional
Features
Turn the small FMS Knob to enter the first digit of the desired ADF
frequency.
Hazard
Avoidance
2)
Procedures
Press the ADF/DME Softkey.
Flight
Planning
ADF TUNING (OPTIONAL)
1)
Nav/Com/
XPDR/Audio
Press the TMR/REF Softkey, then turn the large FMS Knob to highlight the
Flight ID field.
EAS
1)
10) Press the ENT Key to complete the selection.
Annun/
Alerts
DME TUNING (OPTIONAL)
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.
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Index
Press the ADF/DME or DME Softkey.
Appendix
1)
13
ENTER A TRANSPONDER CODE
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)
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.
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
SELECTING A COM RADIO
Flight
Planning
Transmit/Receive
Press the COM1 MIC or COM2 MIC on the audio panel.
Press the COM1 or COM2 on the audio panel.
SELECTING A NAV RADIO
1)
To begin navigating using a navigation radio, press the CDI Softkey on the
PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).
2)
Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or
deselect the navigation radio audio source. All radio keys can be selected
individually or together.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Receive Only
1)
Press the small tuning knob to select the desired radio for tuning. A cyan
box highlights the radio frequency to be tuned.
Appendix
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.
Index
Annun/
Alerts
NAV/COM TUNING
3)
Press the Frequency Transfer Key to place the frequency into the active
frequency field.
14
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Nav/Com/XPDR/Audio Panel
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
15
Hazard
Avoidance
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Procedures
190-00708-07 Rev. B
Flight
Planning
A flight plan must be filed prior to logging on to the CPDLC system. After entering
flight plan information in the required fields and successfully logging on to the system,
messages may be sent and received.
The following parameters are used to log on to the system:
• Facility
• Flight ID
• Destination Airport
• Filed Departure Airport
• File Departure Time (Optional)
GPS Nav
Connecting to the CPDLC System
AFCS
The CPDLC (Controller Pilot Data Link Communications) system provides data link
communication between the aircraft and an Air Traffic Control facility. Communication
is normally in the form of text message elements that resemble phraseology used in
voice communications with ATC.
Generally, messages are closed with an acknowledgement or acceptance. When a
message is acknowledged, the connection with the ATC facility is not terminated, but
kept active for future communication.
Communication hand-off to the next ATC facility is usually performed automatically,
but may also be accomplished manually by the pilot.
Nav/Com/
XPDR/Audio
CONTROLLER PILOT DATA LINK COMMUNICATIONS (OPTIONAL)
EAS
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.
Flight
Instruments
INTERCOM
Nav/Com/XPDR/Audio Panel
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Performing the system log-on:
1)
From the MFD, select the CPDLC Softkey. Ensure ‘Link Available’ is
displayed in the Status Box.
2)
Select the LOGON Softkey.
3)
Turn the large FMS Knob to place the selection cursor over the Facility field.
4)
Turn the small FMS Knob to select the desired ATC facility to which the
CPDLC connection will be established.
5)
Press the ENT Key to complete the entry.
6)
Turn the large FMS Knob to place the selection cursor over the Flight ID
field.
7)
Turn the small FMS Knob to enter the Flight ID or aircraft registration
number.
8)
Press the ENT Key to complete the entry.
9)
Turn the large FMS Knob to place the selection cursor over the Destination
Airport field.
Procedures
10) Enter the identifier of the destination airport used in the filed flight plan
and press the ENT Key.
Additional
Features
Hazard
Avoidance
11) The Filed Departure Airport field is prefilled with the airport identifier
corresponding to the current aircraft location. If the flight plan was filed
using a different airport identifier, turn the large FMS Knob to place the
selection cursor over the Filed Departure Airport field, enter the departure
airport, and press the ENT Key.
Abnormal
Operation
12) (Optional) Turn the large FMS Knob to place the selection cursor over the
Filed Departure Time field.
13) (Optional) Enter the departure time used in the filed flight plan and press
the ENT Key.
Index
Appendix
Annun/
Alerts
14) Turn the large FMS Knob to place the selection cursor over SEND and
press the ENT Key. The Status immediately indicates ‘Connecting’. After
successful log-on, the Status indicates ‘Waiting For CPDLC’. Once a CPDLC
session is initiated by ATC, the Status indicates ‘Connected’ and the Current
Facility field is populated with the name of the facility. If a transfer to
another facility is needed, the Next Facility field is populated. Pressing the
LOGOFF Softkey terminates the log-on process.
16
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Nav/Com/XPDR/Audio Panel
Creating a message consists of choosing from a pre-determined list of requests,
entering the required information, and sending the request.
EAS
To create messages:
Flight
Instruments
Creating a Message
From the MFD, select the CPDLC Softkey.
2)
Select the NEW Softkey. The CPDLC Thread Window appears.
3)
With the Response/Request field highlighted, turn the small FMS Knob
to select the desired request from the list and press the ENT Key. For
discussion purposes, ‘Request [level]’ is selected.
4)
Highlight the Level field and enter the desired altitude. To toggle between
multiple units of measure (FT or FL), highlight the first numeric position and
turn the small FMS Knob counterclockwise.
5)
Press the ENT Key to complete the entry.
6)
Highlight the Reason field and enter the desired reason from the list.
7)
Press the ENT Key to complete the entry.
8)
Highlight the SEND Button and press the ENT Key.
Nav/Com/
XPDR/Audio
1)
AFCS
GPS Nav
Flight
Planning
Procedures
Responding to an ATC Message
Additional
Features
To respond to a message:
Hazard
Avoidance
Responding to an ATC message consists of choosing from a pre-determined list
of responses or acknowledgements, then sending the response or acknowledgement.
From the MFD, select the CPDLC Softkey.
2)
Turn the large FMS Knob to place the selection cursor over the desired
message and press the ENT Key.
3)
Turn the small FMS Knob to select the desired Response/Request from the
list and press the ENT Key.
4)
Highlight the SEND Button and press the ENT Key.
Abnormal
Operation
1)
Annun/
Alerts
Appendix
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
17
Viewing CPDLC Message Dialogs
The status of a string of messages, or dialog, may be checked and past message
dialogs viewed. When G1000 power is cycled, the list of message dialogs is deleted.
To view messages:
From the MFD, select the CPDLC Softkey.
2)
Turn the large FMS Knob to place the selection cursor over the desired
message to view and press the ENT Key.
3)
Press the ENT Key to view the CPDLC Thread.
While the G1000 deletes the list of message dialogs when power is turned off,
individual message dialogs may also be deleted manually. Message dialogs considered
closed may also be deleted.
Hazard
Avoidance
Procedures
To delete a single message dialog:
1)
From the MFD, select the CPDLC Softkey.
2)
Turn the large FMS Knob to place the selection cursor over the desired
message to delete.
3)
Select the DELETE Softkey. A confirmation window appears.
4)
Highlight OK and press the ENT Key.
Abnormal
Operation
Additional
Features
To delete all closed message dialogs:
1)
From the MFD, select the CPDLC Softkey.
2)
Select the DEL ALL Softkey. A confirmation window appears.
3)
Highlight OK and press the ENT Key.
Disconnecting from the CPDLC System
After successfully initiating a CPDLC session, the LOGOFF Softkey becomes
available.
Appendix
Annun/
Alerts
1)
Deleting Message Dialogs
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
Index
To Log-off the CPDLC System:
18
1)
From the MFD, select the CPDLC Softkey.
2)
Select the LOGOFF Softkey.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Nav/Com/XPDR/Audio Panel
It may be desirable to disable Data Mode on the GDR 66 VHF Data Link Transceiver,
or conversely, to enable it.
2)
Press the Menu Key to display the page menu.
3)
Turn the small FMS Knob to highlight ‘Disable Data Mode’ and press the
ENT Key.
AFCS
From the MFD, select the CPDLC Softkey.
Nav/Com/
XPDR/Audio
1)
EAS
To disable data mode on the GDR 66:
To enable data mode on the GDR 66:
2)
Press the Menu Key to display the page menu.
3)
Turn the small FMS Knob to highlight ‘Enable Data Mode’ and press the
ENT Key.
Flight
Planning
From the MFD, select the CPDLC Softkey.
GPS Nav
1)
Flight
Instruments
Enabling/Disabling Data Mode
Additional
Features
CLEARANCE RECORDER AND PLAYER
Hazard
Avoidance
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.
Procedures
PASSENGER ADDRESS (PA) SYSTEM
Annun/
Alerts
Appendix
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 flashes to indicate
when play is in progress. The PLAY annunciator turns off after playback is finished.
Abnormal
Operation
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.
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
19
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.
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
within one-half second backtracks through the recorded memory blocks to reach and
play any recorded block.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
20
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
AFCS
Modes Selected
GPS
VOR
LOC
HDG Key
Heading Select
HDG
Appendix
Approach**
PIT
PIT
GP
GS
PIT
Annun/
Alerts
APR Key
Pitch Hold (default)
Pitch Hold (default)
Glidepath
Glideslope
Pitch Hold (default)
Abnormal
Operation
Backcourse***
PIT
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
***The selected navigation receiver must have a valid LOC signal before BC Key press activates flight
director.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
21
Index
**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.
190-00708-07 Rev. B
Additional
Features
BC Key
Pitch Hold (default)
Hazard
Avoidance
Navigation**
GA Switch
ROL
ROL
ROL
TO
GA
ROL
ROL
ROL
GPS
VOR
LOC
BC
Procedures
NAV Key
FD Key
AP Key
CWS Button
Vertical
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Takeoff (on ground)
TO
Go Around (in air)
GA
Altitude Hold
ALT
Vertical Speed
VS
Vertical Path Tracking* VPTH
Flight
Planning
ALT Key
VS Key
VNV Key
Lateral
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
Takeoff (on ground)
Go Around (in air)
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
GPS Nav
Control Pressed
AFCS
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.
Nav/Com/
XPDR/Audio
NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.
EAS
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.
Flight
Instruments
AUTOMATIC FLIGHT CONTROL SYSTEM
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
AFCS
VERTICAL MODES
Vertical Mode
Pitch Hold
Selected Altitude
Armed
Altitude Hold
Vertical Speed
Description
Control Annunciation
Holds the current aircraft pitch attitude;
may be used to climb/descend to the (default)
Selected Altitude
AFCS armed to capture the altitude
displayed in the Selected Altitude
*
window
Holds the current Altitude Reference
ALT Key
Maintains the current aircraft vertical
speed; may be used to climb/descend VS Key
to the Selected Altitude
Flight Level Change, Maintains the current aircraft airspeed
IAS Hold
(in KIAS or Mach Number) while the
FLC Key
Flight Level Change, aircraft is climbing/descending to the
Selected Altitude
Mach Hold
VNAV
VNAV Target
Altitude Armed
Glidepath
Glideslope
Takeoff
Go Around
Captures and tracks the VNAV flight VNV
path
Key
AFCS armed to capture the altitude
displayed in the VNAV Target Altitude
**
window
Captures and tracks the SBAS glidepath
on approach
APR Key
Captures and tracks the ILS glideslope
on approach
Commands a preprogrammed constant
pitch attitude and wings level in
preparation for takeoff
GA
Disengages the autopilot and Switch
commands a constant preprogrammed
pitch attitude and wings level
PIT
ALTS
ALT
nnnnn ft
VS
nnnn fpm
FLC
nnn kt
FLC
M .nnn
VPTH
ALTV
GP
GS
TO
GA
* 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
22
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
AFCS
Roll Hold
Description
Holds current aircraft roll attitude
or rolls wings level, depending on
commanded bank angle
Limits maximum commanded roll angle
Heading Select
Captures and tracks Selected Heading
HDG
GPS
Captures and tracks selected navigation
source (GPS, VOR, LOC)
NAV
Key
VOR
Flight
Planning
LOC
Captures and tracks a localizer signal
for backcourse approaches
BC Key
Procedures
BC
Hazard
Avoidance
GPS
Captures and tracks selected navigation
APR Key
source (GPS, VOR, LOC)
VAPP
Additional
Features
LOC
Annun/
Alerts
TO
GA
Switch
Appendix
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
Abnormal
Operation
Go Around
*
GPS Nav
Takeoff
BANK
Key
HDG
Key
ROL
AFCS
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)
(default)
Nav/Com/
XPDR/Audio
Low Bank
Control Annunciation
EAS
Lateral Mode
Flight
Instruments
LATERAL MODES
GA
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Index
* 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.
23
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
AFCS
Blank Page
24
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
GPS Navigation
Flight
Instruments
GPS NAVIGATION
DIRECT-TO NAVIGATION
2)
3)
6)
9)
12)
1)
2)
5)
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
25
Index
6)
Appendix
4)
) on the PFD or controller.
Turn the large FMS Knob to place the cursor in the desired selection field.
Turn the small FMS Knob to begin selecting the desired identifier, location,
etc.
Press the ENT Key.
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.
Turn the large FMS Knob to place the cursor over the ‘ALT’ altitude field.
Annun/
Alerts
3)
Press the Direct-to Key (
Abnormal
Operation
Direct-to Navigation using the PFD
Additional
Features
11)
Hazard
Avoidance
10)
Procedures
8)
Flight
Planning
7)
GPS Nav
5)
) Key on the MFD Control Unit.
Enter the waypoint identifier.
Press the ENT Key to confirm the identifier. The ‘Activate?’ field is
highlighted.
If no altitude constraint or course is desired, press the ENT Key to activate.
To enter an altitude constraint, proceed to step 5.
Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.
Enter the desired altitude.
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.
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Press the ENT Key. The cursor is now flashing in the VNV offset distance
field.
Enter the desired offset distance before (-) the waypoint.
Press the ENT Key. The ‘Activate?’ field is highlighted.
Press the ENT Key to activate.
AFCS
4)
Press the Direct-to (
Nav/Com/
XPDR/Audio
1)
EAS
Direct-to Navigation using the MFD
EAS
Flight
Instruments
GPS Navigation
7)
Turn the small FMS Knob to enter the desired altitude.
8)
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’.
Nav/Com/
XPDR/Audio
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.
AFCS
12) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to
highlight the ‘CRS’ field.
14) Press the ENT Key to highlight ‘ACTIVATE?’.
15) Press the ENT Key again to activate the Direct-to.
ACTIVATE A STORED FLIGHT PLAN
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
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
13) Turn the small FMS Knob to enter the desired course to the waypoint.
1)
From the Active Flight Plan Page, press the FMS Knob to activate the cursor
and turn the large FMS Knob to highlight the desired waypoint.
2)
Select the ACT LEG Softkey.
Appendix
OR
Index
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)
26
With ‘Activate’ highlighted, press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
GPS Navigation
Flight
Instruments
STOP NAVIGATING A FLIGHT PLAN
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)
AFCS
GPS Nav
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.
Nav/Com/
XPDR/Audio
Press the FPL Key to display the Active Flight Plan Page.
EAS
1)
Flight
Planning
Procedures
Large White
Text
Large Cyan
Text
Hazard
Avoidance
Small Cyan
Text
Additional
Features
Small Cyan
Subdued Text
Abnormal
Operation
Small White Text
with Altitude
Restriction Bar
Annun/
Alerts
Cross AT or ABOVE 5,000 ft
Appendix
Cross AT 2,300 ft
Cross AT or BELOW 3,000 ft
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
27
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
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.
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.
White Text
Cyan Text
Cyan Subdued
Text
Large 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
guidance.
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.
Small Text 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.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
GPS Navigation
28
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Flight Planning
Flight
Instruments
FLIGHT PLANNING
WEIGHT PLANNING
EAS
All procedures apply to the MFD unless otherwise stated.
Entering Weight Parameters
Procedures
3)
Select the FOB SYNC Softkey to enter the fuel on board quantity as read
from the aircraft fuel quantity sensors.
Additional
Features
Turn the large FMS Knob to place the cursor in the ‘FUEL ON BOARD’ field.
Or:
Annun/
Alerts
Press the FMS Knob to remove the cursor.
Abnormal
Operation
Manually enter the desired fuel quantity.
6)
Hazard
Avoidance
2)
Enter the desired reserve fuel quantity.
Flight
Planning
If necessary, press the FMS Knob to activate the cursor.
5)
GPS Nav
1)
Press the ENT Key. The cursor is now in the ‘FUEL RESERVES’ field.
AFCS
Entering Fuel Parameters
4)
Nav/Com/
XPDR/Audio
The Weight Planning Page is displayed after system power-up. If it is necessary to
return to this page, turn the large FMS Knob to select the ‘AUX’ page group. Turn the
small FMS Knob to select the first rectangular page icon.
1) Select the EMPTY WT Softkey to place the cursor in the Basic Empty
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.
TRIP PLANNING
Appendix
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.
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
29
Index
1)
Flight Planning
Flight
Instruments
4)
For Direct-to planning:
a) Select the WPTS Softkey and verify that the starting waypoint field
indicates ‘P.POS’ (present position).
EAS
b) If necessary, press the MENU Key and select ‘Set WPT to Present
Position’ to display ‘P.POS’.
Nav/Com/
XPDR/Audio
c) Press the ENT Key and the flashing cursor moves to the ending
waypoint field.
AFCS
d) Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.
Or:
GPS Nav
For point-to-point planning:
a) Enter the identifier of the starting waypoint.
Flight
Planning
b) Once the waypoint’s identifier is entered, press the ENT Key to accept
the waypoint. The flashing cursor moves to the ending waypoint.
c) Again, enter the identifier of the ending waypoint.
Procedures
d) Press the ENT Key to accept the waypoint.
Or:
Hazard
Avoidance
For flight plan leg planning:
a) Select the FPL Softkey (at the bottom of the display).
Additional
Features
b) Turn the small FMS Knob to select the desired flight plan (already
stored in memory), by number.
c) Turn the large FMS Knob to highlight the ‘LEG’ field.
Annun/
Alerts
Abnormal
Operation
d) Turn the small FMS Knob to select the desired leg of the flight plan, or
select ‘CUM’ to apply trip planning calculations to the entire flight plan.
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.
Appendix
NOTE: The page mode must be set to ‘MANUAL’ to perform the following
steps.
5)
Turn the large FMS Knob to highlight the departure time (DEP TIME) field.
Index
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.
30
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Flight Planning
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.
Abnormal
Operation
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.
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Index
Turn the small FMS Knob to select the User WPT Information Page.
Appendix
2)
Annun/
Alerts
Turn the large FMS Knob on the MFD Control Unit to select the ‘WPT’ page
group.
Additional
Features
CREATE A USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE
1)
Hazard
Avoidance
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.
Procedures
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.
Flight
Planning
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.
GPS Nav
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.
AFCS
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.
Nav/Com/
XPDR/Audio
7)
EAS
Enter the departure time. Press the ENT Key when finished. Departure time
may be entered in local or UTC time, depending upon system settings.
Flight
Instruments
6)
31
Flight Planning
Flight
Instruments
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.
EAS
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Nav/Com/
XPDR/Audio
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 USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS
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.
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
7)
AFCS
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.
Abnormal
Operation
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Appendix
Annun/
Alerts
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.
Index
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:
32
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Flight Planning
b) Turn the large FMS Knob to select the desired waypoint.
EAS
c) Press the ENT Key.
Flight
Instruments
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
Or:
AFCS
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
Nav/Com/
XPDR/Audio
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
c) Turn the large FMS Knob to select the desired waypoint.
GPS Nav
d) Press the ENT Key.
Or:
Procedures
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
Flight
Planning
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
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.
12) Press the ENT Key.
Annun/
Alerts
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
Abnormal
Operation
d) Press the ENT Key.
Additional
Features
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Hazard
Avoidance
Or:
13) Repeat step 10 to enter the next waypoint name.
Index
15) Press the ENT Key.
16) Press the FMS Knob to remove the flashing cursor.
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Appendix
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.
33
CREATE A USER WAYPOINT DEFINED BY A RADIAL & DISTANCE FROM
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.
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Flight Planning
Flight
Planning
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Hazard
Avoidance
Procedures
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.
Additional
Features
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:
Abnormal
Operation
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.
Annun/
Alerts
c) Press the ENT Key.
Or:
Appendix
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Index
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.
34
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Flight Planning
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
EAS
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
Flight
Instruments
Or:
Nav/Com/
XPDR/Audio
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Or:
c) Turn the large FMS Knob to select the desired waypoint.
GPS Nav
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
AFCS
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
d) Press the ENT Key.
Procedures
12) Press the ENT Key.
13) The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.
Hazard
Avoidance
14) Press the ENT Key.
15) Press the FMS Knob to remove the flashing cursor.
Additional
Features
DELETE A USER WAYPOINT
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.
Appendix
Index
35
Annun/
Alerts
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Abnormal
Operation
1)
190-00708-07 Rev. B
Flight
Planning
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
CREATE A FLIGHT PLAN
NOTE: When creating a flight plan in the Active Flight Plan Window, the first
leg is activated automatically after it is created.
EAS
Flight
Instruments
Flight Planning
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
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.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
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.
36
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Flight Planning
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.
EAS
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.
Nav/Com/
XPDR/Audio
1)
Flight
Instruments
IMPORT A FLIGHT PLAN FROM AN SD CARD
8)
Press the ENT Key.
Hazard
Avoidance
Turn the small FMS Knob to highlight the desired flight plan for importing.
Procedures
7)
Flight
Planning
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.
GPS Nav
Or:
AFCS
If an empty flight plan is selected, a list of the available flight plans on
the SD card will be displayed.
Additional
Features
INSERT A WAYPOINT IN 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:
Annun/
Alerts
Press the FPL Key to display the active flight plan.
Abnormal
Operation
1)
Appendix
a) Enter the user waypoint identifier, facility, or city.
b) Press the ENT Key.
Index
Or:
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
37
Flight Planning
Flight
Instruments
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
EAS
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.
Nav/Com/
XPDR/Audio
d) Press the ENT Key.
Or:
AFCS
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
GPS Nav
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.
Flight
Planning
Or:
Procedures
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.
d) Press the ENT Key.
6)
Press the ENT Key again to “accept” the waypoint.
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)
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).
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
c) Turn the large FMS Knob to select the desired user waypoint.
38
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Flight Planning
Turn the FMS Knob to select the desired airway exit point from the list, and
press the ENT Key. ‘LOAD?’ is highlighted.
7)
Press the ENT Key. The system returns to editing the flight plan with the
new airway inserted.
Nav/Com/
XPDR/Audio
6)
CREATING A USER-DEFINED HOLD AT AN ACTIVE FLIGHT PLAN WAYPOINT
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the waypoint for the hold.
3)
Press the MENU Key, highlight ‘Hold At Wpt’, and press the ENT Key. The
HOLD AT window appears with the course field highlighted.
4)
Use the FMS Knobs to edit the entry course, and press the ENT Key.
5)
Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course
direction, and press the ENT Key.
6)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
7)
Use the FMS Knobs to edit the length, and press the ENT Key.
8)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
9)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key.
GPS Nav
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
10) Press the ENT Key while ‘LOAD?’ is highlighted to add the hold into the
flight plan.
Annun/
Alerts
CREATING A USER-DEFINED HOLD AT THE AIRCRAFT PRESENT POSITION
2)
Press the MENU Key, highlight ‘Hold At Present Position’, and press the
ENT Key. The HOLD AT window appears with the Length mode highlighted.
3)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
39
Index
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
Appendix
1)
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
AFCS
1)
190-00708-07 Rev. B
EAS
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.
Flight
Instruments
5)
GPS Nav
Flight
Planning
Procedures
Use the FMS Knobs to edit the length, and press the ENT Key.
5)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
6)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key.
7)
Press the ENT Key while ‘ACTIVATE?’ is highlighted to immediately activate
the hold.
1)
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the PPOS-H waypoint.
3)
Press the CLR Key. A “Remove Holding Pattern?” confirmation window is
displayed.
4)
Select ‘OK’ and press the ENT Key. The holding pattern is removed from
the active flight plan. Select ‘CANCEL’ and press the ENT Key to cancel the
removal of the holding pattern.
REMOVING A USER-DEFINED HOLD (CREATED AT AN ACTIVE WAYPOINT)
1)
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the HOLD waypoint.
3)
Press the CLR Key. A ‘Remove Holding Pattern?’ confirmation window is
displayed.
4)
Select ‘OK’ and press the ENT Key. The holding pattern is removed from
the active flight plan. Select ‘CANCEL’ and press the ENT Key to cancel the
removal of the holding pattern.
INVERT AN ACTIVE FLIGHT PLAN
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
4)
REMOVING A USER-DEFINED HOLD (CREATED AT THE AIRCRAFT P.POS)
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Flight Planning
40
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’.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Flight Planning
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.
Flight
Instruments
4)
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
AFCS
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.
GPS Nav
b) Press the FMS Knob to activate the cursor.
c) Turn the large FMS Knob to highlight the desired flight plan.
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.
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.
Annun/
Alerts
EDIT A STORED FLIGHT PLAN
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.
Index
Press the FPL Key for the MFD and turn the small FMS Knob to display the
Flight Plan Catalog Page.
Appendix
1)
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Abnormal
Operation
1)
Additional
Features
STORE A FLIGHT PLAN
Hazard
Avoidance
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.
Procedures
2)
Flight
Planning
d) Select the EDIT Softkey.
190-00708-07 Rev. B
Nav/Com/
XPDR/Audio
1)
EAS
REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT
PLAN
41
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)
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Flight Planning
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Or, for a stored flight plan:
AFCS
a) Press the FPL Key of the MFD and turn the small FMS Knob to select
the Flight Plan Catalog Page.
GPS Nav
b) Press the FMS Knob to activate the cursor.
c) Turn the large FMS Knob to highlight the desired flight plan.
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
cursor.
INVERT AND ACTIVATE A STORED FLIGHT PLAN
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
d) Select the EDIT Softkey.
42
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 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.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Flight Planning
Flight
Instruments
COPY A FLIGHT PLAN
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.
EAS
1)
Nav/Com/
XPDR/Audio
AFCS
DELETE A FLIGHT PLAN
GPS Nav
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 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.
Flight
Planning
1)
4)
Select the LD WPT Softkey. The selected waypoint is inserted at the selected
point. The default user waypoint naming is USR000, USR001, USR002, and
so on.
5)
To change the user waypoint name, follow the procedure for modifying a user
waypoint.
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
43
Index
The default insertion point is at the end of the flight plan. If the selected
waypoint is to be placed anywhere other than the end of the flight plan,
press the FMS Knob to activate the cursor. Waypoints are inserted ABOVE
the cursor. Turn the large FMS Knob to select the desired insertion point.
Appendix
3)
Annun/
Alerts
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.
Abnormal
Operation
2)
Additional
Features
Press the FPL Key to display the Active Flight Plan Page on the MFD.
Hazard
Avoidance
1)
Procedures
GRAPHICAL FLIGHT PLAN CREATION
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 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 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.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Flight Planning
44
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Procedures
Flight
Instruments
PROCEDURES
LOAD AND ACTIVATE A DEPARTURE PROCEDURE
EAS
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.
Flight
Planning
Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.
Hazard
Avoidance
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.
Additional
Features
1)
Abnormal
Operation
Annun/
Alerts
LOAD AN ARRIVAL PROCEDURE
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.
Appendix
1)
45
Index
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Procedures
ACTIVATE A DEPARTURE LEG
190-00708-07 Rev. B
GPS Nav
2)
AFCS
Press the PROC Key.
Nav/Com/
XPDR/Audio
1)
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Procedures
5)
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)
Press the ENT Key.
10) With ‘LOAD?’ highlighted, press the ENT Key.
AFCS
11) The arrival becomes part of the active flight plan.
ACTIVATE AN ARRIVAL LEG
Procedures
Flight
Planning
GPS Nav
Turn the large FMS Knob to highlight the desired arrival.
1)
Press the FPL Key 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 arrival.
4)
Select the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.
LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE
Additional
Features
Hazard
Avoidance
4)
Press the PROC Key.
2)
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.
Appendix
4)
Turn either FMS Knob to highlight the desired approach.
5)
Press the ENT Key. A list of available transitions for the selected approach
procedure is now displayed.
6)
Turn either FMS Knob to select the desired transition. The “Vectors”
option assumes vectors will be received to the final course segment of
Annun/
Alerts
1)
Index
Abnormal
Operation
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.
46
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Procedures
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,
optional RAD ALT, or TEMP COMP.
9)
Press the ENT Key. The cursor moves to the altitude field. Turn the small
FMS Knob to enter the published DA/MDA for the selected approach
procedure.
AFCS
8)
Nav/Com/
XPDR/Audio
Press the ENT Key. The cursor moves to the MINIMUMS field.
EAS
7)
Flight
Instruments
the approach and will provide navigation guidance relative to the final
approach course.
Procedures
12) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.
Hazard
Avoidance
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.
Additional
Features
13) Press the ENT Key.
ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN
2)
Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.
3)
Press the ENT Key.
Annun/
Alerts
Press the PROC Key.
Abnormal
Operation
1)
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.
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Index
Press the PROC Key.
Appendix
ACTIVATE A VECTOR TO FINAL APPROACH FIX
1)
Flight
Planning
11) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’
highlighted.
GPS Nav
10) Press the ENT Key. If BARO, RAD ALT, or OFF was selected step 8, proceed
to step 11. If TEMP COMP was selected in step 8, the cursor moves to the
‘TEMP AT....” field. Turn the small FMS Knob to enter the temperature at
the destination airport. The temperature compensated altitude minimum is
displayed below the previously enter minimum altitude value.
47
ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN
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.
TEMPERATURE COMPENSATED ALTITUDE
When temperature compensated altitude is enabled for the loaded approach, the
altitudes associated with the approach waypoints are displayed in slanted text.
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Procedures
Additional
Features
Altitudes Displayed Without
Temperature Compensation
Altitudes Displayed With
Temperature Compensation
Annun/
Alerts
Abnormal
Operation
Enabling temperature compensated altitude:
1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is
displayed.
2) Turn the FMS Knob to highlight ‘Temperature Compensation’.
3) Press the ENT Key. The TEMPERATURE COMPENSATION Window is
displayed.
Appendix
4)
Use the small FMS Knob to select the temperature at the <airport>. The
Index
compensated altitude is computed as the temperature is selected.
5)
Press the ENT Key. ‘ACTIVATE COMPENSATION?’ is highlighted.
6)
Press the ENT Key. The compensated altitudes for the approach are
shown in the flight plan.
48
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Procedures
EAS
Press the ENT Key. The temperature compensated altitude at the FAF
AFCS
is cancelled.
Nav/Com/
XPDR/Audio
5)
Flight
Instruments
Disabling temperature compensated altitude:
1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is
displayed.
2) Turn the FMS Knob to highlight ‘Temperature Compensation’.
3) Press the ENT Key. The TEMPERATURE COMPENSATION Window is
displayed.
4) Press the ENT Key. ‘CANCEL COMPENSATION?’ is highlighted.
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
49
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Procedures
Blank Page
50
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Hazard Avoidance
Flight
Instruments
HAZARD AVOIDANCE
CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP
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.
EAS
1)
AFCS
Procedures
Select the STRMSCP Softkey. Select the STRMSCP Softkey again to
remove Stormscope Lightning Data from the Navigation Map Page.
Additional
Features
Lightning Age
Strike is less than 6 seconds old
Hazard
Avoidance
2)
Symbol
Abnormal
Operation
Strike is between 6 and 60 seconds old
Annun/
Alerts
Strike is between 1 and 2 minutes old
Strike is between 2 and 3 minutes old
2)
Turn either FMS Knob to highlight ‘Map Setup’.
3)
Press the ENT Key.
4)
Turn the small FMS Knob to highlight ‘Weather’.
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Index
Press the MENU Key (with the Navigation Map Page displayed).
Appendix
Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode
1)
Flight
Planning
Displaying Stormscope Lightning Data on the Navigation Map Page
Select the MAP Softkey.
GPS Nav
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.
1)
Nav/Com/
XPDR/Audio
STORMSCOPE® (OPTIONAL)
51
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Hazard Avoidance
5)
Press the ENT Key.
6)
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.
AFCS
Clear Stormscope Lightning Data from the Navigation Map Page
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.
GPS Nav
NOTE: If heading input is lost, strikes and/or cells must be cleared manually
Flight
Planning
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.
Procedures
Stormscope Page
1)
Turn the large FMS Knob until the Map Page group is selected.
2)
Turn the small FMS Knob until the Stormscope Page is selected.
1)
Select the Stormscope Page.
2)
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.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’
Annun/
Alerts
NOTE: “Cell mode” uses a clustering program to identify clusters of electrical
activity that indicate cells.
Appendix
Change the Viewing Mode Between 360˚ and 120˚
1)
Select the Stormscope Page.
2)
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.
Index
Select the CLEAR Softkey to remove all Stormscope lightning data from the
display.
52
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Hazard Avoidance
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.
GPS Nav
Select the MAP Softkey.
AFCS
1)
Nav/Com/
XPDR/Audio
Displaying SiriusXM Weather on the Navigation Map Page
Display METAR and TAF information on the Airport Information Page
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).
Procedures
Turn the large FMS Knob to select the WPT Page Group.
Flight
Planning
1)
Displaying Weather on the Weather Data Link Page
Hazard
Avoidance
2)
Turn the small FMS Knob to select the Weather Data Link Page.
3)
Select the available softkeys to select the desired SiriusXM 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.
Map Panning Information – Weather Data Link Page
Annun/
Alerts
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.
Index
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
Appendix
1)
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Abnormal
Operation
Turn the large FMS Knob to select the Map Page Group.
Additional
Features
1)
190-00708-07 Rev. B
EAS
WARNING: Use of SiriusXM Weather for hazardous weather penetration is
not recommended. Weather information provided by SiriusXM is approved
only for weather avoidance, not penetration.
Flight
Instruments
SIRIUSXM WEATHER (OPTIONAL)
53
Hazard Avoidance
Flight
Instruments
information but allows the user to press the ENT Key and select that
Airport’s Information Page to display the text of the report. Pressing the
ENT Key when panning over a TFR displays TFR specific information.
EAS
Weather Products and Symbols
Nav/Com/
XPDR/Audio
Wx Product
Status Icons
Description
AFCS
NEXRAD - Available for the US and Canada. The age of the displayed data
for each is shown at the right.
GPS Nav
ECHO TOP - The age of the displayed data is shown at the right. Not
displayed when CLOUD TOP is displayed.
Flight
Planning
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.
Procedures
CELL MOVEMENT - The age of the displayed data is shown at the right.
Hazard
Avoidance
SIGMET & AIRMET - The age of the displayed data for each is shown at the
right.
Additional
Features
METAR - Available for the US and Canada. The age of the displayed data for
each is shown at the right.
Abnormal
Operation
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.
Annun/
Alerts
FREEZING LEVEL - The age of the displayed data is shown at the right.
Appendix
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.
Index
COUNTY WARNING - The age of the displayed data is shown at the right.
54
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Hazard Avoidance
Flight
Instruments
Wx Product
Status Icons
Description
CYCLONE WARNING - The age of the displayed data is shown at the right.
EAS
AIREP - The age of the displayed data is shown at the right.
Nav/Com/
XPDR/Audio
PIREP - The age of the displayed data is shown at the right. Urgent Pireps
are displayed in yellow.
AFCS
TURBULENCE - The age of the displayed data is shown at the right. The
altitude selection is shown at the bottom.
GPS Nav
ICING POTENTIAL - The age of the displayed data is shown at the right.
The altitude selection is shown at the bottom.
Flight
Planning
GARMIN CONNEXT™ WEATHER
Hazard
Avoidance
Registering the System to Receive Connext™ Weather
Annun/
Alerts
Appendix
Index
55
Abnormal
Operation
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Additional
Features
When an account is established, Garmin Connext provides an Access Code which
must be entered on the G1000 in order to complete the registration process.
1) With the aircraft outside and having a clear view of the sky, turn the large
FMS Knob on the MFD to select the MAP page group.
2) Turn the small FMS Knob to select the MAP-WEATHER DATA LINK (Connext
or XM) Page. If ‘XM’ is displayed in the page title, it will be necessary
to change the datalink source to Connext before continuing. Refer to
‘Viewing the Weather Data Link Page’ procedure to change the datalink
source to Connext prior to registration.
3) If the system displays the ‘Garmin Flight Data Service Registration’ window,
proceed to step 7. Otherwise, press the MENU Key. The Page Menu
window is now displayed.
4) Turn the large FMS Knob to select ‘Register With Connext’ in the menu list.
190-00708-07 Rev. B
Procedures
NOTE: Garmin Connext Weather provides information for avoiding hazardous
weather. Do not utilize Connext Weather information to penetrate hazardous
weather.
Hazard Avoidance
Flight
Instruments
5) Press the ENT Key. The Garmin Flight Data Service Registration window is
now displayed.
EAS
6) Enter the access code provided by Garmin Connext in the ACCESS CODE
field.
7) Press the ENT Key. ‘REGISTER’ will now be highlighted.
Nav/Com/
XPDR/Audio
8) Press the ENT Key. The system will contact Garmin Connext. System
registration is complete when ‘REGISTERED’ is displayed in the STATUS
field.
Weather data is provided when the pilot initiates either a manual or automatic
Connext data request on the Connext Weather Data Link Page on the MFD. No
weather data is displayed until the first Connext Weather Data Request is made.
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Connext Weather Data Link Page.
When a weather product is selected for display on the Connext Weather Data Link
Page, a box containing a symbol for the product and its age (in minutes) are shown
in the upper right. If weather data has not been requested, ‘N/A’ is shown next to the
product symbol instead of age. The age of the weather product is based on the time
difference between when the data was assembled on the ground and the current GPS
time. Weather products are updated continuously or refreshed at specific intervals
(defined in the Refresh Rate column in the following table).
If for any reason, a weather product is not refreshed within the defined Expiration
Time intervals, the data is considered expired and is removed from the display. The
age of the expired product is replaced by dashes. If more than half of the expiration
time has elapsed, the color of the product age readout changes to yellow.
The refresh rate represents the interval at which the Connext servers make available
the most current known weather data. It does not necessarily represent the rate at
which new content is received from weather sources.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Accessing Connext Weather Products
56
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Hazard Avoidance
Refresh Rate
(Minutes)
Radar Precipitation
(PRECIP)
30
U.S./Canada: 3*
Europe: 15
Infrared Satellite
(IR SAT)
60
30
Datalink Lightning
(DL LTNG)
30
Continuous
SIGMETs/AIRMETs
(SIG/AIR)
60
Continuous
Meteorological Aerodrome Report
(METARs)
90
Continuous
Winds Aloft
(WIND)
60
Continuous
Symbol
Flight
Instruments
Expiration
Time
(Minutes)
Weather Product
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Setting Up and Customizing the Connext Weather Data Link Page
Select the Connext Weather Data Link Page.
2)
Press the MENU Key.
3)
With ‘Weather Setup’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select ‘Product Group 1’ or ‘Product Group 2’,
and press the ENT Key.
5)
Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
6)
Turn the small FMS Knob to scroll through options for each product (ON/
OFF, range settings, etc.).
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Annun/
Alerts
1)
190-00708-07 Rev. B
EAS
Pilot Weather Report
90
Continuous
(PIREPs)
Temporary Flight Restrictions
no product image
60
Continuous
(TFRs)
Terminal Aerodrome Reports
no product image
60
Continuous
(TAFs)
* The composite precipitation image is updated every 3 minutes, but individual radar sites
may take between 3 and 10 minutes to provide new data.
57
Flight
Instruments
Hazard Avoidance
7)
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the Connext Weather Data
Link Page with the changed settings.
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Restoring Default Connext Weather Data Link Page Settings
1)
Select the Connext Weather Data Link Page.
2)
Press the MENU Key.
3)
With ‘Weather Setup’ highlighted, press the ENT Key.
4)
Press the MENU Key.
5)
Highlight the desired default(s) to restore (all or for selection) and press
ENT Key.
Hazard
Avoidance
Procedures
Flight
Planning
Switching Between Connext and SiriusXM Weather Sources
1)
Turn the large FMS Knob on the MFD to select the MAP page group.
2)
Turn the small FMS Knob to select the desired Weather Data Link Page.
3)
Press the MENU Key.
4)
Turn the large FMS Knob to select ‘Display Connext Weather’ or ‘Display
XM’ Weather’ (choice dependent on current weather source) and press the
ENT Key.
Additional
Features
Viewing Legends for Displayed Connext Weather Products
1)
Select the Connext Weather Data Link Page.
2)
Select the LEGEND Softkey to display the legends for the displayed
weather products.
Abnormal
Operation
Or:
a) Press the MENU Key.
3)
Turn the FMS Knob to scroll through the legends if more are available than
fit in the window.
4)
To remove the Legend Window, select the LEGEND Softkey, the ENT or the
CLR Key, or press the FMS Knob.
Index
Appendix
Annun/
Alerts
b) Select ‘Weather Legend’ and press the ENT Key.
58
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Hazard Avoidance
Select the Navigation Map Page.
2)
Press the MENU Key.
3)
With ‘Map Setup’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select the ‘Weather’ Group and press the ENT
Key.
5)
Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
AFCS
6)
Turn the small FMS Knob to scroll through options for each product (ON/
OFF, range settings).
7)
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the Navigation Map Page with
the changed settings.
EAS
1)
Nav/Com/
XPDR/Audio
Flight
Instruments
Setting Up and Customizing Weather Data for the Navigation Map
Page
GPS Nav
2)
Press the MENU Key.
3)
With ‘Connext Weather Request’ highlighted, press the ENT Key.
4)
59
Index
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Appendix
190-00708-07 Rev. B
Annun/
Alerts
Turn the large FMS Knob to highlight the desired coverage option(s)
and press the ENT Key to check or uncheck one of more of the following
coverage selections:
• PRESENT POSITION – Requests data based on current location.
• DESTINATION – Requests data based on active flight plan destination (if the flight
plan contains no destination, dashes ‘------” are displayed.)
• FPL – Requests data based on active flight plan. Turn the small FMS Knob to select
the desired flight plan look-ahead distance option (or choose ‘REMAINING FPL’ to
request the remainder of the flight plan).
• WAYPOINT – Requests data based on any valid waypoint.
Abnormal
Operation
Select the Connext Weather Data Link Page.
Additional
Features
1)
Hazard
Avoidance
Requesting Connext Weather Data Manually
Procedures
The Connext Data Request window provides the flight crew with the options to
define the requested weather coverage area(s), choose automatic weather update
intervals (if desired), and the ability to send or cancel weather data requests. The
window also displays the status of the Connext data request process.
Flight
Planning
Connext Weather Data Requests
5)
Turn the large FMS Knob highlight to the ‘DIAMETER / RTE WIDTH’
distance field and turn the small FMS Knob to select the desired diameter
and route width of the request, then press the ENT Key.
6)
Turn the large FMS Knob until the ‘SEND REQ’ button is highlighted. Press
the ENT Key to initiate the request immediately or press the FMS Knob to
return to the Connext Data Link Page without requesting data.
During a Connext Data Request, the Request Status box initially displays “Contacting
Connext...”. Once a connection is established, the Request Status Box displays “Receiving
Wx Data... Time Remaining:” with an estimated data transfer time (either minutes or
seconds). If desired, the Connext Data Request window may be closed while the data
request is processing by pressing the FMS Knob; the data request will continue to process
in the background. Connext Data Requests typically take between 1 to 4 minutes to
complete depending on the size of the selected weather coverage area and Iridium signal
strength.
The system retrieves all available Worldwide Weather products within the selected
coverage area during an initial Connext Data Request, regardless of which products (if
any) are currently enabled for display. On subsequent requests, previously retrieved
textual data (such as METARs and TAFS) is retained if it has not expired, while new
textual weather data matching the current coverage area and all graphical weather data is
downloaded during every data request.
If the system cannot complete a Connext weather data request, one or more messages will appear in the request status window as indicated in the following table.
Description
Abnormal
Operation
Auto requests inhibited
Send manual request to
reset.
The system has disabled automatic weather data requests due to
excessive errors. Automatic weather data requests have stopped. Send
a manual weather data request to resume automatic updates.
Auto update retry: ##
Seconds
The system will attempt another automatic weather data request after
an error occurred during the previous request. Timer counts down until
the next automatic request occurs.
Connext Comm Error [2]
A communications error has occurred with the GDL59 or GIA. The
G1000 should be serviced.
Connext Comm Error [4]
This occurs if multiple automatic weather data requests have recently
failed, or the GDL 59 or a GIA is off-line.
Index
Appendix
Weather Request
Status Message
Annun/
Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Hazard Avoidance
60
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Hazard Avoidance
Connext Comm Error [8]
A server error has occurred or invalid data received.
Connext Login Invalid
There is a problem with the Connext registration. Contact Garmin at
1-866-739-5687 in the United States or 913-397-8200, ext. 1135 for
assistance.
Connext Server
Temporarily Inop
The Connext weather data server is temporarily out of service, but is
expected to return to service in less than 30 minutes.
Connext Server Inop
The Connext weather data server will be out of service for at least 30
minutes.
Invalid Coverage Area
The weather data request coverage area does not contain at least one
of the following: a waypoint, a flight plan, or a flight plan destination.
Verify at least one of the coverage options is enabled (checked) and
contains required criteria, then re-send the data request.
The user has cancelled a Connext weather data request.
Requested area too
large. Reduce coverage
area.
The size of the Connext weather data request has exceeded limits.
Reduce the size of the coverage area and try the weather data request
again.
Request Failed - Try
Again
The weather data request timed-out. Re-send data request.
Transfer Preempted
The GDL 59 is busy. Retry request later.
Appendix
Request Cancelled
Annun/
Alerts
The Connext weather data request area exceeds size limits. Reduce
weather coverage area and re-send data request.
Abnormal
Operation
Reduce Request Area
Additional
Features
NO Connext Subscription The system is not be currently subscribed to Connext, or the access code
is incorrect. Verify the access code. Contact Garmin at 1-866-739-5687
in the United States or 913-397-8200, ext. 1135 for assistance.
Hazard
Avoidance
A weather data transfer has timed out. Check Iridium signal strength
and re-send the data request.
Procedures
Connext Comm Error [7]
Flight
Planning
A communications error has occurred. It this error persists, the G1000
should be serviced.
GPS Nav
Connext Comm Error [6]
AFCS
This can occur if the GDL 59 is off-line or not configured, or the Iridium
or Connext networks are not accessible. Check Iridium signal strength.
If this error persists, the G1000 should be serviced.
Nav/Com/
XPDR/Audio
Connext Comm Error [5]
EAS
Description
Flight
Instruments
Weather Request
Status Message
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
61
Hazard Avoidance
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Cancelling a Connext Weather Data Request in Progress
1)
Select the Connext Weather Data Link Page.
2)
Press the MENU Key.
3)
With ‘Connext Data Request’ highlighted, press the ENT Key.
4)
Turn the large FMS Knob to select ‘CANCEL REQ’ and press the ENT Key.
The request status box indicates ‘Request Cancelled’.
5)
Press the FMS Knob to return to the Connext Weather Datalink Page.
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Enabling Automatic Connext Data Requests
1)
Select the Connext Weather Data Link Page.
2)
Press the MENU Key.
3)
With ‘Connext Weather Request’ highlighted, press the ENT Key.
4)
Choose the desired weather coverage options.
5)
Turn the large FMS Knob to select the ‘UPDATE RATE’ setting. Then turn
the small FMS Knob to highlight the desired automatic update frequency
(OFF, 5 Min, 10 Min, 15 Min, 20 Min, 25 Min, 30 Min, 45 Min, or 60 Min),
then press the ENT Key.
6)
The ‘SEND REQ” button is highlighted and a countdown timer is displayed
in the ‘REQUEST STATUS’ based on the currently selected update rate.
Press the ENT Key to immediately send an immediate Connext Data
Request.
Or:
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Press the FMS Knob to return to the Connext Weather Data Link Page.
62
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Hazard Avoidance
Description
Nav/Com/
XPDR/Audio
Traffic Symbol
EAS
• If Traffic information Service (TIS) is configured, STANDBY, OPERATE, and
TNA MUTE softkeys are displayed.
• If a Traffic Advisory System (TAS) is configured, STANDBY, NORMAL, TEST,
and ALT MODE softkeys are displayed.
Flight
Instruments
TRAFFIC SYSTEMS
Non-Threat Traffic
(intruder is beyond 5 nm and greater than 1200’ vertical separation)
AFCS
Proximity Advisory (PA) (Not available with TIS system)
(intruder is within 5 nm and less than 1200’ vertical separation)
GPS Nav
Traffic Advisory (TA)
(closing rate, distance, and vertical separation meet TA criteria)
Flight
Planning
Traffic Advisory Off Scale
Traffic Symbol Description
Procedures
Traffic Information Service (TIS)
Abnormal
Operation
Displaying Traffic on the Traffic Map Page
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Traffic Map Page.
3)
Select the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
4)
Select the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
5)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
6)
Select the TNA MUTE Softkey to mute the “Traffic Not Available” aural alert.
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Annun/
Alerts
1)
190-00708-07 Rev. B
Additional
Features
NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.
Hazard
Avoidance
NOTE: If the G1000 is configured to use an optional Traffic Advisory System
(TAS), TIS is not available for use.
63
Hazard Avoidance
EAS
Flight
Instruments
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.
Nav/Com/
XPDR/Audio
Traffic Advisory System (TAS) (Optional)
GPS Nav
AFCS
System Self Test
1)
Set the range to 2/6 nm.
2)
Select the STANDBY Softkey.
3)
Select the TEST Softkey.
4)
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.
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
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
Index
Displaying Traffic on the Navigation Map
64
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.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Hazard Avoidance
NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.
Flight
Instruments
TERRAIN AND OBSTACLE PROXIMITY
EAS
Displaying Terrain and Obstacles on the Terrain Proximity Page
Turn the small FMS Knob to select the last rectangular page icon.
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.
Terrain/Obstacle above or within 100’
below current aircraft altitude.
Yellow
Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.
Black
Terrain/Obstacle is more than 1000’
below aircraft altitude.
Hazard
Avoidance
Red
Procedures
Terrain/Obstacle Location
Flight
Planning
Color
GPS Nav
2)
AFCS
Turn the large FMS Knob to select the Map Page Group.
Nav/Com/
XPDR/Audio
1)
With the Navigation Map displayed, select the MAP Softkey.
2)
Select the TERRAIN Softkey. Terrain and obstacle proximity will now be
displayed on the map.
Abnormal
Operation
1)
Additional
Features
Displaying Terrain and Obstacles on the Navigation Map
Annun/
Alerts
TERRAIN-SVT
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
65
Index
NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.
Appendix
NOTE: Terrain-SVT is only available when the Synthetic Vision Technology
(SVT) option is installed and the TAWS option has not been installed.
Hazard Avoidance
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Terrain-SVT 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
Terrain/Obstacle above or within 100’
below current aircraft altitude.
Yellow
Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.
Black
Terrain/Obstacle is more than 1000’
below aircraft altitude.
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Display Terrain on the TERRAIN-SVT Page
Additional
Features
Hazard
Avoidance
Enable/Disable Aviation Data
1)
While the Terrain-SVT Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.
3)
Press the ENT Key.
Terrain-SVT Inhibit
Appendix
Annun/
Alerts
Abnormal
Operation
Inhibit Terrain
While the Terrain-SVT 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.
Index
Enable Terrain
While the Terrain-SVT Page is displayed, select the INHIBIT Softkey.
Or:
66
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Hazard Avoidance
While the Terrain-SVT Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select ‘Enable Terrain’.
3)
Press the ENT Key.
Flight
Instruments
1)
EAS
AFCS
TERRAIN AWARENESS & WARNING SYSTEM (TAWS-B) DISPLAY
Hazard
Avoidance
Manual System Test
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.
Abnormal
Operation
2)
Additional
Features
While the TAWS-B Page is displayed, press the MENU Key.
When all is in working order, “TAWS System Test, OK” is heard.
Turn the small FMS Knob to select the TAWS-B Page.
3)
If desired, select the VIEW Softkey to access the ARC and 360 softkeys.
When the ARC Softkey is selected, a radar-like 120° view is displayed.
Select the 360 Softkey to return to the 360° default display.
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Index
2)
Appendix
Turn the large FMS Knob to select the Map Page Group.
Annun/
Alerts
Display Terrain on the TAWS-B Page
1)
Procedures
NOTE: TAWS operation is only available when the G1000 is configured for a
TAWS-B installation.
Flight
Planning
NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.
GPS Nav
WARNING: The TAWS-B display shows supplemental information only. It
should not be used for navigation.
1)
Nav/Com/
XPDR/Audio
NOTE: If Terrain-SVT 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.
67
Hazard Avoidance
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
4)
Color
Terrain/Obstacle Location
Red
Terrain/Obstacle above or within 100’
below current aircraft altitude.
Yellow
Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.
Black
Terrain/Obstacle is more than 1000’
below aircraft altitude.
Flight
Planning
GPS Nav
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.
Procedures
TAWS Inhibit
Hazard
Avoidance
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.
Annun/
Alerts
Abnormal
Operation
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.
Index
Appendix
Enable TAWS
While the TAWS-B Page is displayed, select the INHIBIT Softkey.
Or:
1) While the TAWS-B Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select ‘Enable TAWS’.
3) Press the ENT Key.
68
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Hazard Avoidance
AFCS
Displaying Weather on the Navigation Map Page
2)
Turn the small FMS Knob to select the Navigation Map Page.
3)
Select the MAP Softkey.
4)
Select the WX RADAR Softkey.
Flight
Planning
Turn the large FMS Knob to select the Map Page Group.
GPS Nav
1)
Procedures
Displaying Weather on the Weather Radar Page
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.
Hazard
Avoidance
1)
If desired, select the VERTICAL Softkey for vertical scanning.
Appendix
6)
Annun/
Alerts
Turn the Joystick to select the desired range.
Abnormal
Operation
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.
Additional
Features
Or:
5)
Nav/Com/
XPDR/Audio
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
aircraft to prevent the antenna from bouncing on the bottom stop and possibly
causing damage to the radar assembly.
EAS
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.
Flight
Instruments
AIRBORNE COLOR WEATHER RADAR
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
69
Adjusting Antenna Tilt
While viewing weather radar on the Weather Radar Page or the Navigation Map
Page, moving the Joystick up or down adjusts the tilt of the antenna up or down.
Monitor the displayed tilt value in the TILT field.
When scanning vertically on the Weather Radar Page, 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
While viewing weather radar on the Weather Radar Page or the Navigation Map
Page, moving the Joystick right or left adjusts the azimuth position of the antenna
right or left. Monitor the displayed bearing value in the BEARING field.
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
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Hazard Avoidance
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.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
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.
70
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Hazard Avoidance
Select the GAIN Softkey to activate the cursor in the ‘GAIN’ field.
2)
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.
3)
Press the FMS Knob to remove the cursor.
4)
Select the GAIN Softkey again to recalibrate the gain. ‘CALIBRATED’ will be
displayed in the ‘GAIN’ field.
Nav/Com/
XPDR/Audio
1)
AFCS
Flight
Planning
Press the MODE Softkey.
2)
Press the GROUND Softkey to place the radar in Ground Map Mode.
3)
Press the BACK Softkey.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to place the cursor in the ‘TILT’ field.
6)
Adjust the antenna tilt angle by turning the small FMS Knob to position the
ground returns as desired.
7)
Press the FMS Knob to remove the cursor.
Procedures
1)
Hazard
Avoidance
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.
Appendix
2)
Annun/
Alerts
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.
Abnormal
Operation
1)
Additional
Features
Sector Scan
71
Index
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
GPS Nav
Ground Mapping
190-00708-07 Rev. B
EAS
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.
Flight
Instruments
Adjusting Gain
Hazard Avoidance
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.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Antenna Stabilization
72
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Hazard Avoidance
Standby (During
Warm-Up),
applicable to GWX
68 only
STANDBY
WARM-UP
XX
(XX indicates number
of seconds remaining in
warm-up)
Weather
WEATHER
None
Ground Mapping
Off
Radar Failed*
GROUND MAPPING
OFF
FAIL
None
OFF
RADAR FAIL
† Annunciations in this column appear in white text in the Weather Radar Mode box on the Navigation
Map Page.
73
Index
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Appendix
190-00708-07 Rev. B
Annun/
Alerts
STAB INOP
Description
Altitude compensated tilt feature is enabled (GWX 70 only)
Altitude compensated tilt feature is disabled (GWX 70 only)
Antenna stabilization is selected on.
Antenna stabilization is selected off.
The radar is not receiving pitch and roll information. The
antenna stabilization feature is inoperative.
Abnormal
Operation
Radar Feature Status
ACT ON
ACT OFF
STAB ON
STAB OFF
Additional
Features
The system displays the status of the radar antenna stabilization feature
in the upper right corner of the Weather Radar Page. For the GWX 70, the
status of the Altitude Compensated Tilt feature also appears in the upper
right corner of the Weather Radar Page.
Hazard
Avoidance
STANDBY
Procedures
STANDBY
Flight
Planning
Standby
GPS Nav
Center Banner
Annunciation
AFCS
Radar Mode Annunciation
Box†
Nav/Com/
XPDR/Audio
Radar Mode
EAS
The radar mode is annunciated in the upper left corner of the Weather
Radar Page. Additional information may be displayed in the center of the
Weather Radar Page as a banner annunciation.
Flight
Instruments
System Status
Hazard Avoidance
Flight
Instruments
If the unit fails, an annunciation as to the cause of the failure is shown as
a banner in the center of the Weather Radar Page.
Nav/Com/
XPDR/Audio
EAS
Weather
Radar Page
Center Banner
Annunciation
BAD CONFIG
AFCS
RDR FAULT
The radar configuration is invalid. The radar should be
serviced.
The radar unit is reporting a fault. The radar should be
serviced.
The system is not receiving valid data from the radar unit.
The system should be serviced.
ALTITUDE COMPENSATED TILT
Enabling/Disabling Altitude Compensated Tilt (ACT) (GWX 70
only):
1)
On the Weather Radar Page, select the MODE Softkey.
2)
Select the ACT ON Softkey. When ACT is enabled, ‘ACT ON’ is annunciated
in upper right corner of the Weather Radar Page. When ACT is disabled,
‘ACT OFF’ is annunciated.
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
RADAR FAIL
Description
1)
On the Weather Radar Page, press the MENU Key.
2)
Turn the FMS Knob to highlight ‘Altitude Compensated Tilt On’ or ‘Altitude
Compensated Tilt Off’, then press the ENT Key.
Abnormal
Operation
Additional
Features
Or:
Adjusting antenna tilt on the Vertical Scan display:
Annun/
Alerts
1)
Select the TILT Softkey to activate the cursor in the TILT field and display the
Tilt Line.
Appendix
If the Tilt Line is not displayed, press the MENU Key and turn the large
FMS Knob to select Show Tilt Line. Press the ENT Key.
Index
2)
Turn the small FMS Knob to adjust the antenna tilt angle. The selected tilt
angle is implemented when Horizontal Scan is again selected.
The Joystick can also be used to adjust tilt.
74
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Additional Features
Flight
Instruments
ADDITIONAL FEATURES
SYNTHETIC VISION
EAS
Nav/Com/
XPDR/Audio
WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. SVT 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.
AFCS
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Displaying Synthetic Terrain
2)
Press the SYN VIS Softkey.
3)
Press the SYN TERR Softkey.
4)
Press the BACK Softkey to return to the previous page.
Appendix
Press the PFD Softkey.
Annun/
Alerts
1)
Procedures
Pathways
Flight Path Marker
Horizon Heading Marks
Terrain and Obstacle Alerting
Three-dimensional Traffic
Airport Signs
Runway Display
Flight
Planning
•
•
•
•
•
•
•
GPS Nav
Synthetic Vision Technology (SVT) functionality is offered as an optional
enhancement to the G1000 Integrated Flight Deck System.
SVT is primarily comprised of a computer-generated forward-looking, attitude
aligned view of the topography immediately in front of the aircraft from the pilot’s
perspective. SVT information is shown on the primary flight display (PFD).
SVT 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 SVT enhancement to the PFD, the following feature enhancements
have been added to the PFD:
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
75
Additional Features
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Displaying Pathways
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.
AFCS
GPS Nav
Flight
Planning
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.
Procedures
Displaying Airport Signs
Hazard
Avoidance
Additional
Features
Press the PFD Softkey.
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 APTSIGNS Softkey.
5)
Press the BACK Softkey to return to the previous page.
TERMINAL PROCEDURE CHARTS
NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may
be necessary to carry another source of charts on-board the aircraft.
Abnormal
Operation
Annun/
Alerts
Appendix
Index
1)
SafeTaxi®
SafeTaxi® is an enhanced feature that gives greater map detail as the map range
is adjusted in on the airport. The airport display on the map reveals runways with
numbers, taxiways identifiers, and airport landmarks including ramps, buildings,
control towers, and other prominent features. Resolution is greater at lower map
ranges. The aircraft symbol provides situational awareness while taxiing.
Pressing the DCLTR Softkey (declutter) once removes the taxiway markings and
airport identification labels. Pressing the DCLTR Softkey twice removes VOR station
76
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Additional Features
AFCS
Additional
Features
Abnormal
Operation
Annun/
Alerts
Or:
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.
77
Index
2)
Appendix
Move the map pointer to point to a desired point on the map and select the
SHW CHRT Softkey.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Hazard
Avoidance
Select the SHW CHRT Softkey when displayed.
Procedures
View Charts from the Navigation Map Page
Flight
Planning
FliteCharts® resemble the paper version of AeroNav Services terminal procedures
charts. The charts are displayed with high-resolution and in color for applicable
charts. The selected Display Pane depiction shows the aircraft position on the moving
map in the plan view of most approach charts and on airport diagrams.
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.
GPS Nav
FliteCharts®
190-00708-07 Rev. B
Nav/Com/
XPDR/Audio
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.
1)
EAS
ChartView
Flight
Instruments
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.
Additional Features
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
View Charts from the Active Flight Plan Page
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.
4)
Select the GO BACK Softkey to return to the previous page.
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)
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.
AIRPORT DIRECTORY
The AOPA or AC-U-KWIK Airport Directory adds enhanced airport information
when viewing airports on the WPT-Airport Information Page.
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.
Index
Appendix
Abnormal
Operation
1)
Annun/
Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Change Day/Night View
78
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Additional Features
The XM Radio Page provides information and control of the audio entertainment
features of the SiriusXM Satellite Radio.
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.
AFCS
Turn the large FMS Knob to select the Auxiliary Page Group.
Nav/Com/
XPDR/Audio
1)
EAS
Selecting the XM Radio Page
Flight
Instruments
SIRIUSXM SATELLITE RADIO ENTERTAINMENT
Active Channel and Channel List
Flight
Planning
Selecting a Category
Additional
Features
Abnormal
Operation
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.
Appendix
Or:
Annun/
Alerts
1)
Press the FMS Knob to highlight the channel list and turn the large FMS
Knob to scroll through the channels.
Index
With the desired channel highlighted, press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Hazard
Avoidance
Select an Available Channel within the Selected Category
190-00708-07 Rev. B
Procedures
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.
3)
GPS Nav
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.
79
Additional Features
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)
Press the ENT Key to activate the selected channel.
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Entering a Channel Directly
AFCS
Assigning Channel Presets
Procedures
Flight
Planning
GPS Nav
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
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.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Adjusting Volume
1)
With the XM Radio Page displayed, select the VOL Softkey.
2)
Select the VOL – Softkey to reduce volume or select the VOL + Softkey to
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.
Index
Appendix
Annun/
Alerts
SiriusXM Radio volume may also be adjusted on each passenger headset.
80
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Additional Features
EAS
Operation of these features in the cockpit is accomplished through the AUXTELEPHONE, AUX-TEXT MESSAGING, AUX-REPORT STATUS, and AUX-WI-FI
SETUP Pages.
Flight
Instruments
SATELLITE TELEPHONE & SMS MESSAGING SERVICE
Registering System With Garmin
Nav/Com/
XPDR/Audio
AFCS
A subscriber account must be established prior to using the Iridium Satellite
System. Before setting up an Iridium account, obtain the serial number of the Iridium
Transceiver (GSR1) and the System ID by viewing the AUX- SYSTEM STATUS Page.
Contact Garmin at 1-866-739-5687 in the United States or 913-397-8200, ext. 1135.
Disable/Enable Iridium Transceiver
GPS Nav
Iridium telephone may be turned on or off by performing the following steps.
Flight
Planning
To enable the Iridium telephone system:
With the AUX-TELEPHONE Page displayed, select the MENU Key on the
MFD to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Enable Iridium Transmission’.
3)
Press the ENT Key.
Hazard
Avoidance
To disable the Iridium telephone system:
2)
Turn either FMS Knob to place the cursor on ‘Disable Iridium Transmission’.
3)
Press the ENT Key.
Abnormal
Operation
With the AUX-TELEPHONE Page displayed, select the MENU Key on the
MFD to display the Page Menu.
Telephone Communication
Turn the small FMS Knob to select the AUX-TELEPHONE Page.
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Index
2)
Appendix
To view the Telephone Page:
Annun/
Alerts
The pilot or copilot can place and answer calls on the Iridium satellite network.
Control and monitoring of telephone functions are accomplished through the AUXTELEPHONE Page.
Turn the large FMS Knob on the MFD to select the AUX page group.
Additional
Features
1)
1)
Procedures
1)
81
Additional Features
Flight
Instruments
Internal
Phone
External
Phone
Description
EAS
Phone is Idle
Nav/Com/
XPDR/Audio
Phone is ringing
AFCS
Phone has a dial tone (off hook) or connected to
another phone
GPS Nav
Phone dialed is busy
Flight
Planning
Phone is dialing another phone
Procedures
Phone has failed
Hazard
Avoidance
Phone status not known
Abnormal
Operation
Additional
Features
Phone is disabled
Annun/
Alerts
Phone is reserved for data transmission
Appendix
Calling other phone or incoming call from other phone
Index
Other phone is on hold
Phones are connected
82
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Additional Features
The names, telephone number, and email addresses can be saved in a list of contacts for easy use when making telephone calls.
7)
Press the ENT Key. The cursor moves to the ‘EMAIL’ field.
8)
Enter the desired email address. Entry can be accomplished through
the alphanumeric keys on the MFD Controller, or the FMS Knobs on the
controller or the MFD.
9)
Press the ENT Key. The SAVE button is highlighted.
9)
Press the ENT Key. The new contact entry is added to the list of saved
contacts.
Annun/
Alerts
Appendix
Delete a contact:
1) With the AUX-TELEPHONE Page displayed, press the FMS Knob to display
the cursor.
2) Turn either FMS Knob to place the cursor on the desired contact name.
3) Select the DELETE Softkey. A confirmation window is displayed.
4) With ‘OK’ highlighted, press the ENT Key to delete the selected contact.
Abnormal
Operation
Enter the desired telephone number. Entry can be accomplished through
the alphanumeric keys on the MFD Controller, or the FMS Knobs on the
controller or the MFD.
Additional
Features
6)
Hazard
Avoidance
Press the ENT Key. The cursor moves to the ‘PHONE NUMBER’ field.
Procedures
5)
Flight
Planning
Enter the desired name of the new contact. Entry can be accomplished
through the alphanumeric keys on the MFD Controller, or the FMS Knobs
on the controller or the MFD.
GPS Nav
4)
AFCS
Press the ENT Key. The cursor moves the ‘NAME’ field of the ‘CONTACT
DETAILS’ window.
Nav/Com/
XPDR/Audio
3)
EAS
Entering a new contact:
1) With the AUX-TELEPHONE Page displayed, press the FMS Knob to display
the cursor.
2) If necessary, turn either FMS Knob to place the cursor on ‘NEW ENTRY’.
Flight
Instruments
Contacts
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
83
Additional Features
4)
Press the ENT Key when each field is conplete. The SAVE Button is now
highlighted.
5)
Press the ENT Key to save the changes.
Incoming Calls
When viewing MFD pages other than the AUX-TELEPHONE Page, a pop-up alert
will be displayed, accompanied by a ringtone heard on the selected cockpit audio. The
pop-up alert may be inhibited at times, such as during takeoff. In addition to the popup alert, a ringing phone symbol will be displayed to the right of the MFD page title.
Answering an incoming call:
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Edit a contact:
1) With the AUX-TELEPHONE Page displayed, press the FMS Knob to display
the cursor.
2) Turn either FMS Knob to place the cursor on the desired contact name.
3) Select the EDIT Softkey. The cursor is placed in the ‘NAME’ field. Enter the
desired changes. Entry can be accomplished through the alphanumeric keys
on the MFD Controller, or the FMS Knobs on the controller or the MFD.
1)
Press the TEL Key on the audio panel.
2)
Select the ANSWER Softkey on the MFD.
Or:
Additional
Features
While viewing the AUX-TELEPHONE Page:
Index
Appendix
Annun/
Alerts
Abnormal
Operation
NOTE: The Push-to-Talk switch is not utilized for telephone communication.
The microphone is active after selecting the ANSWER Softkey, and stays active
until the call is terminated.
1)
Press the TEL Key on the audio panel.
2)
Press the MENU Key to display the Page Menu.
3)
Turn either FMS Knob to place the cursor on ‘Answer Incoming Call’.
4)
Press the ENT Key.
Selecting the IGNORE Softkey will extinguish the pop-up window and leave the
current call unanswered. Selecting the IGNRE ALL Softkey will extinguish the popup window for the current and all future incoming calls and leave the current call
84
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Additional Features
Disabling incoming call alerts:
With the AUX-TELEPHONE Page displayed, press the MENU Key on the
MFD to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Disable Incoming Call Alerts’.
3)
Press the ENT Key. The voice and pop-up alert will not be displayed now
when an incoming call is received.
EAS
1)
AFCS
GPS Nav
To make an external call from the cockpit by dialing the number:
Press the TEL Key on the appropriate audio panel.
2)
Select the DIAL Softkey on the MFD.
3)
Turn the small FMS Knob to select ‘IRIDIUM’.
4)
Press the ENT Key. The cursor has now moved to the phone number entry field.
5)
Enter the desired telephone number by selecting the number softkeys on
the MFD or by pressing the numeric keys on the MFD Control Unit. The
International dialing sequence is necessary to place a call from the cockpit
to an external phone: Country Code + City/Area Code (if any) + Telephone
Number. The following country codes may be used when calling other
satellite telephone systems.
Flight
Planning
1)
Abnormal
Operation
Annun/
Alerts
Appendix
Index
Press the ENT Key. The system will begin calling the number.
To exit the call, select the HANGUP Softkey.
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Additional
Features
7)
Hazard
Avoidance
Press the ENT Key. ‘OK’ is highlighted.
Procedures
Country Code
870
8810 or 8811
8812 or 8813
8816 or 8817
8818 or 8819
6)
Nav/Com/
XPDR/Audio
Outgoing Calls
Voice calls can be made from the cockpit through the Iridium Satellite Network.
Satellite System
Inmarsat
ICO
Ellipso
Iridium
Globalstar
Flight
Instruments
unanswered. Selecting the TEL Softkey will display the AUX-TELEPHONE Page allowing additional call information to be viewed before answering.
85
Additional Features
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Making an external call from the cockpit by using the Contact List:
1) Press the TEL Key on the appropriate audio panel.
2) Press the FMS Knob to activate the cursor.
3) Turn the small FMS Knob to select the desired contact name in the list of
contacts.
4) Select the CALL Softkey. The external call is initiated and the number
associated with the contact name is dialed.
Text Messaging (SMS)
Messages may be sent to an email address or text message capable cellular telephone.
Message length is limited to 160 characters, including the email address.
The text messaging user interface is mainly through the AUX-TEXT MESSAGING
Page.
Viewing the Text Messaging Page
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
To exit the call, select the HANGUP Softkey.
1)
Turn the large FMS Knob on the MFD to select the AUX page group.
2)
Turn the small FMS Knob to select SATELLITE PHONE.
3)
If necessary, press the SMS Softkey to display the AUX-TEXT MESSAGING
Page.
Additional
Features
Message Symbol
Description
Abnormal
Operation
Received text message that has not been opened
Annun/
Alerts
Received text message that has been opened
Appendix
Saved text message, draft not sent
Index
System is sending text message
86
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Additional Features
Description
Flight
Instruments
Message Symbol
Text message has been sent
EAS
System failed to send text message
Nav/Com/
XPDR/Audio
Predefined text message
Press the ENT Key. The pop-up alert will not be displayed when an
incoming text message is received.
Abnormal
Operation
3)
Additional
Features
Turn either FMS Knob to place the cursor on ‘Disable New Message
Popups’ or ‘Enable New Message Popups’.
Hazard
Avoidance
2)
Annun/
Alerts
Reply to a Text Message
While viewing the text message, press the REPLY Softkey.
Appendix
Or:
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Reply To Message’.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Index
c) Press the ENT Key.
190-00708-07 Rev. B
Procedures
With the AUX-TEXT MESSAGING Page displayed, press the MENU Key on
the MFD to display the Page Menu.
Flight
Planning
1)
GPS Nav
Enable/Disable Incoming Text Message Pop-Up Alerts
AFCS
Viewing a Text Message When Received
When viewing MFD pages other than the AUX-TEXT MESSAGING Page, a pop-up
alert will be displayed when a new text message is received.
Press the VIEW Softkey to view the message. Pressing the IGNORE Softkey will
extinguish the pop-up window and leave the text message unopened. Pressing the
IGNR ALL Softkey will extinguish the pop-window and ignore all future incoming
text messages. Pressing the SMS Softkey will display the AUX-TEXT MESSAGING
Page.
The pop-up alerts may be enabled or disabled through the Page Menu.
87
Additional Features
Flight
Instruments
Sending a Text Message
1)
While viewing the AUX-TEXT MESSAGING Page, press the NEW Softkey.
Or:
EAS
a) Press the MENU Key to display the Page Menu.
Nav/Com/
XPDR/Audio
b) Turn either FMS Knob to place the cursor on ‘Draft New Message’.
c) Press the ENT Key.
The TEXT MESSAGE DRAFT Window is now displayed with the cursor in
the ‘TO’ field. Enter the desired telephone number or email address. Entry
can be accomplished through the alphanumeric keys on the controller, or
combination of the FMS Knob on the controller and softkeys on the MFD.
The FMS Knob is used to enter letters and numbers, or numbers can be
entered from the MFD by pressing the NUMBERS Softkey. Press the CAP
LOCK Softkey to create upper and lower case alpha characters. Special
characters can be accessed by pressing the SYMBOLS Softkey.
3)
Press the ENT Key. The cursor is now displayed in the ‘MESSAGE’ field.
4)
Enter the desired message using any combination of entry methods as
described in step 2.
5)
Press the ENT Key.
6)
Press the SEND Softkey to send the message immediately, or press the
SAVE Softkey to save the message in Outbox for sending at a later time.
Press the CANCEL Softkey to delete the message.
Predefined Text Messages
Time and effort can be saved in typing text messages that are used repeatedly by
saving these messages as a predefined message.
Create a Predefined Text Message
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
2)
1)
While viewing the AUX-TEXT MESSAGING Page, press the MENU Key to
display the Page Menu.
2)
Turn either FMS Knob to select ‘Edit Predefined Messages’.
3)
Press the ENT Key. The PREDEFINED MESSSAGES view is now displayed.
4)
Press the NEW Softkey.
Index
Or:
88
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Additional Features
Flight
Instruments
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Draft New Predefined
Message’.
EAS
c) Press the ENT Key. The PREDEFINED SMS TEXT MESSAGE Window is
now displayed.
7)
Enter the desired message using any combination of entry methods as
described in step 5.
8)
Press the ENT Key.
9)
Press the SAVE Softkey. The new predefined message is now shown in
the displayed list. Pressing the CANCEL Softkey will delete the message
without saving.
Flight
Planning
Press the ENT Key. The cursor is now displayed in the ‘MESSAGE’ field.
Procedures
Hazard
Avoidance
10) Press the MENU Key to display the Page Menu.
11) Turn either FMS Knob to place the cursor on ‘Stop Editing Predefined
Message’.
Additional
Features
12) Press the ENT Key.
Send a Predefined Text Message
3)
Press the ENT Key. The cursor is now displayed in the ‘MESSAGE’ field.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
89
Index
The TEXT MESSAGE DRAFT Window is now displayed with the cursor in
the ‘TO’ field. Enter the desired telephone number or email address. Entry
can be accomplished through the alphanumeric keys on the controller, or
combination of the FMS Knob on the controller and softkeys on the MFD.
The FMS Knob is used to enter letters and numbers, or numbers can be
entered from the MFD by pressing the NUMBERS Softkey. Press the CAP
LOCK Softkey to create upper and lower case alpha characters. Special
characters can be accessed by pressing the SYMBOLS Softkey.
Appendix
2)
Annun/
Alerts
While viewing the AUX-TEXT MESSAGING Page, press the NEW Softkey.
Abnormal
Operation
1)
190-00708-07 Rev. B
GPS Nav
6)
AFCS
The cursor is displayed in the ‘TITLE’ field. Enter the desired message title.
Entry can be accomplished through the alphanumeric keys on the controller,
or combination of the FMS Knob on the controller and softkeys on the MFD.
The FMS Knob is used to enter letters and numbers, or numbers can be
entered from the MFD by pressing the NUMBERS Softkey. Press the CAP
LOCK Softkey to create upper and lower case alpha characters. Special
characters can be accessed by pressing the SYMBOLS Softkey.
Nav/Com/
XPDR/Audio
5)
4)
Press the PREDEFD Softkey. The PREDEFINED MESSAGE MENU Window is
displayed.
6)
Press the ENT Key. The predefined message text is inserted into the
message field. If desired, the message can be edited by using the FMS
Knobs.
7)
Press the ENT Key.
8)
Press the SEND Softkey to transmit the message.
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Additional Features
Text Message Boxes
Received text messages reside in the Inbox as ‘Read’ or ‘Unread’ messages. The
Outbox contains ‘Sent” and ‘Unsent’ text messages. Saved messages that are meant to
be sent later are stored as Drafts. Each text message box may be viewed separately, or
together in any combination.
Flight
Planning
Show Inbox Messages
While viewing the AUX-TEXT MESSAGING Page, press the ARRANGE
Softkey, then press the INBOX Softkey.
Procedures
Or:
a) Press the MENU Key to display the Page Menu.
Hazard
Avoidance
b) Turn either FMS Knob to place the cursor on ‘Show Inbox Messages’.
Additional
Features
c) Press the ENT Key. The message box selected for viewing is indicated
at the bottom left of the list window.
Show Outbox Messages
Abnormal
Operation
While viewing the AUX-TEXT MESSAGING Page, press the ARRANGE
Softkey, then press the OUTBOX Softkey.
Or:
Annun/
Alerts
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Show Outbox Messages’.
Appendix
c) Press the ENT Key. The message box selected for viewing is indicated
at the bottom left of the list window.
Show Draft Messages
Index
While viewing the AUX-TEXT MESSAGING Page, press the ARRANGE
Softkey, then press the DRAFTS Softkey.
90
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Additional Features
Flight
Instruments
Or:
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Show Draft Messages’.
EAS
c) Press the ENT Key. The message box selected for viewing is indicated
at the bottom left of the list window.
Nav/Com/
XPDR/Audio
AFCS
Arranging Text Messages
The viewed messages may be listed according to the date/time the message was
sent or received, the type of message (read, unread, sent, unsent, etc.), or by message
address.
View Messages Sorted by Message Date/Time:
GPS Nav
While viewing the AUX-TEXT MESSAGING Page, press the ARRANGE
Softkey, then press the TIME Softkey.
Flight
Planning
Or:
a) Press the MENU Key to display the Page Menu.
Procedures
b) Turn either FMS Knob to place the cursor on ‘Sort By Date/Time’.
c) Press the ENT Key. The sorting selection is indicated at the bottom
center of the list window.
Hazard
Avoidance
View Messages Sorted by Message Type
Additional
Features
While viewing the AUX-TEXT MESSAGING Page, press the ARRANGE
Softkey, then press the TYPE Softkey.
Or:
Abnormal
Operation
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Sort By Type’.
Annun/
Alerts
c) Press the ENT Key. The sorting selection is indicated at the bottom
center of the list window.
View Messages Sorted by Address:
Appendix
While viewing the AUX-TEXT MESSAGING Page, press the ARRANGE
Softkey, then press the ADDRESS Softkey.
190-00708-07 Rev. B
Index
Or:
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
91
Additional Features
Flight
Instruments
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Sort By Address’.
EAS
c) Press the ENT Key. The sorting selection is indicated at the bottom
center of the list window.
AFCS
Nav/Com/
XPDR/Audio
Viewing The Content of a Text Message
1)
While viewing the AUX-TEXT MESSAGING Page, select the desired message box.
2)
Press the FMS Knob to activate the cursor.
3)
Turn either FMS Knob to select the desired message.
4)
Press the VIEW Softkey.
GPS Nav
Or:
Press the ENT Key.
Or:
Flight
Planning
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘View Selected Message’.
Procedures
c) Press the ENT Key.
5)
To close the text message, press the CLOSE Softkey.
Hazard
Avoidance
Or:
a) Press the MENU Key to display the Page Menu.
Additional
Features
b) Turn either FMS Knob to place the cursor on ‘Close Message’.
c) Press the ENT Key.
Annun/
Alerts
Abnormal
Operation
Mark Selected Message As Read
1)
While viewing the Inbox on the AUX-TEXT MESSAGING Page, press the
FMS Knob to activate the cursor.
2)
Turn either FMS Knob to select the desired message.
3)
Press the MRK READ Softkey.
Appendix
Or:
a) Press the MENU Key to display the Page Menu.
Index
b) Turn either FMS Knob to place the cursor on ‘Mark Selected Message
As Read’.
c) Press the ENT Key.
The message symbol now indicates the message has been opened.
92
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Additional Features
2)
Turn either FMS Knob to place the cursor on ‘Mark All New Messages As
Read’.
3)
Press the ENT Key. A confirmation window is displayed.
4)
With cursor highlighting ‘YES’, press the ENT Key. The message symbols
now indicate all the message have been opened.
Nav/Com/
XPDR/Audio
While viewing the Inbox on the AUX-TEXT MESSAGING Page, press the
MENU Key to display the Page Menu.
EAS
1)
Flight
Instruments
Mark All Messages As Read
2)
Turn either FMS Knob to select the desired message.
3)
Press the DELETE Softkey.
Flight
Planning
While viewing the Inbox on the AUX-TEXT MESSAGING Page, press the
FMS Knob to activate the cursor.
GPS Nav
1)
AFCS
Delete a Message
Or:
b) Turn either FMS Knob to place the cursor on ‘Delete Selected Message’.
c) Press the ENT Key.
Hazard
Avoidance
Additional
Features
MAINTENANCE LOGS
The system provides recording of CAS, CMC, exceedances, and other critical
aircraft data that occur while the aircraft is on the ground or in flight.
The Maintenance Logs feature is accessible by entering a password. No pilot action
is required.
Procedures
a) Press the MENU Key to display the Page Menu.
Abnormal
Operation
Annun/
Alerts
Viewing the Maintenance Logs Page:
1) Turn the large FMS Knob on the MFD to select the AUX page group.
2) Turn the small FMS Knob to select ‘MAINTENANCE LOG’. The AUXMAINTENANCE LOGS Page is now displayed.
Appendix
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
93
AUXILIARY VIDEO (OPTIONAL)
There are four modes of operation of the auxiliary video display: Full-Screen,
Full-Screen with Digital Zoom, Split-Screen with Map, and Split-Screen with Map and
Digital Zoom.
EAS
Flight
Instruments
Additional Features
Nav/Com/
XPDR/Audio
Displaying auxiliary video:
1) Turn the large FMS Knob to select the AUX page group.
2) Turn the small FMS Knob to select VIDEO and display the AUX-VIDEO Page.
The video display softkeys shown below appear on the AUX - VIDEO Page.
AFCS
Control of the AUX - VIDEO Page can also be accessed through the Page Menu.
2)
Turn the large FMS Knob to highlight the desired video adjustment option
and press the ENT Key.
Once the ENT key is pressed on any option, the page menu closes and returns to
the AUX - VIDEO Page.
Video Setup
Video brightness, contrast, and saturation may be adjusted be selecting the setup
function. While viewing the setup function softkeys, after 45 seconds of softkey
inactivity, the system reverts to the AUX VIDEO Page softkeys.
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Selecting video menu options:
1) While viewing the AUX - VIDEO Page press the MENU Key to display the
Page Menu OPTIONS.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Adjusting the video settings:
1) With the AUX-VIDEO Page displayed, press the SETUP Softkey.
2) Press the BRIGHT - or BRIGHT +, to adjust display brightness in five
percent increments from 0 to 100%.
3) Press the CNTRST- or CNTRST +, to adjust display contrast in five
percent increments from 0 to 100%.
4) Press the SAT - or SAT +, to adjust display saturationin five percent
increments from 0 to 100%.
5) If desired, return the display to the default settings by pressing the RESET
Softkey.
6) Press the BACK Softkey to return to the previous softkey level.
94
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Abnormal Operation
While on the AUX - VIDEO Page, press the INPUT Softkey to select the video
source.
AFCS
Zoom/Range
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Annun/
Alerts
Press the FMS Knob momentarily to activate the flashing cursor.
Abnormal
Operation
2)
Additional
Features
Select the AUX - Utility Page.
Hazard
Avoidance
1)
Procedures
Entering a Scheduler Message
Flight
Planning
SCHEDULER
The Scheduler feature can be used to enter and display reminder messages (e.g.,
Hot Section Inspection or Phase 1 Maintenance Check) in the Messages Window on
the PFD. Messages can be set to display based on a specific date and time (event), once
the message timer reaches zero (one-time; default setting), or recurrently whenever
the message timer reaches zero (periodic). Message timers set to periodic alerting
automatically reset to the original timer value once the message is displayed. When
power is cycled, all messages are retained until deleted, and message timer countdown
is resumed.
GPS Nav
Pressing the VID ZM + or VID ZM - Softkeys increases or decreases video display
magnification between 1x and 10x.
The Joystick can be used to increase or decrease the range setting on the map
display or zoom in and out on the video display. While in the Split-Screen mode,
pressing the MAP ACTV or VID ACTV Softkey determines which display the Joystick
adjusts. Pressing the softkey to display MAP ACTV allows the Joystick to control the
range setting of the map display. Pressing the softkey to display VID ACTV allows the
Joystick to control the zoom setting of the video display.
When zooming in on the video display, a Zoom Window will appear in the upper
right of the display. A box within this window indicates the portion of the display
currently being viewed. The currently displayed portion of the full display may be
adjusted by using Joystick.
190-00708-07 Rev. B
Nav/Com/
XPDR/Audio
Input Selection
EAS
Pressing the HIDE MAP Softkey removes the map and displays video on the full
screen. The softkey label changes to grey with black characters. Pressing the HIDE
MAP Softkey again restores the map view and the small video image. The softkey label
returns to white characters on a black background.
Flight
Instruments
Display Selection
95
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Abnormal Operation
3)
Turn the large FMS Knob to highlight the first empty scheduler message
naming field.
4)
Use the FMS Knob to enter the message text to be displayed in the
Messages Window and press the ENT Key.
5)
Press the ENT Key again or use the large FMS Knob to move the cursor to
the field next to Type.
6)
Turn the small FMS Knob to select the message type:
• Event—Message issued at the specified date/time
AFCS
• One-time—Message issued when the message timer reaches zero
(default setting)
7)
Press the ENT Key again or use the large FMS Knob to move the cursor to
the next field.
8)
For periodic and one-time message, use the FMS Knob to enter the timer
value (HH:MM:SS) from which to countdown and press the ENT Key.
9)
For event-based messages:
Procedures
Flight
Planning
GPS Nav
• Periodic—Message issued each time the message timer reaches zero
a) Use the FMS Knob to enter the desired date (DD-MM-YY) and press
the ENT Key.
Hazard
Avoidance
b) Press the ENT Key again or use the large FMS Knob to move the cursor
to the next field.
Additional
Features
c) Use the FMS Knob to enter the desired time (HH:MM) and press the
ENT Key.
Abnormal
Operation
10) Press the ENT Key again or use the large FMS Knob to move the cursor to
enter the next message.
Deleting a Scheduler Message
Index
Appendix
Annun/
Alerts
1) Select the AUX - Utility Page.
96
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3)
Turn the large FMS Knob to highlight the name field of the scheduler
message to be deleted.
4)
Press the CLR Key to clear the message text. If the CLR Key is pressed
again, the message is restored.
5)
Press the ENT Key while the message line is cleared to clear the message
text.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Additional Features
GPS Nav
1) Use the FMS Knob to select the AUX - System Setup Page.
Press the FMS Knob momentarily to activate the flashing cursor.
Flight
Planning
2)
3) Turn the large FMS Knob to highlight ‘CREATE’ in the Pilot Profile Box.
Press the ENT Key. A ‘Create Profile’ window is displayed.
Procedures
4)
5) Use the FMS Knob to enter a profile name up to 16 characters long and
Press the ENT Key.
Abnormal
Operation
7)
Additional
Features
In the next field, use the small FMS Knob to select the desired settings
upon which to base the new profile. Profiles can be created based on
Garmin factory defaults, default profile settings (initially based on Garmin
factory defaults unless edited by the pilot), or current system settings.
Hazard
Avoidance
press the ENT Key. Pilot profile names cannot begin with a blank as the
first letter.
6)
8) With ‘CREATE’ highlighted, press the ENT Key to create the profile.
Annun/
Alerts
Or:
Use the large FMS Knob to select ‘CREATE and ACTIVATE’ and press the
ENT Key to activate the new profile.
To cancel the process, select ‘CANCEL’ with the large FMS Knob and press
the ENT Key.
Appendix
9)
AFCS
Creating a Profile
Nav/Com/
XPDR/Audio
When the system is powered on, the last selected pilot profile is shown on the MFD
power-up screen. The system can store up to 25 profiles; the currently active profile,
the amount of memory used, and the amount of memory available are shown at the
top of the AUX - System Setup Page in the box labeled ‘Pilot Profile’.
EAS
PILOT PROFILES
Flight
Instruments
Scheduler messages appear in the Messages Window on the PFD. When a scheduler
message is waiting, the MSG Softkey label flashes. Selecting the MSG Softkey opens
the Messages Window and acknowledges the scheduler message. Selecting the MSG
Softkey again removes the Messages Window from the display, and the scheduler
message is deleted from the message queue.
10) Press the FMS Knob to deactivate the cursor.
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
97
Additional Features
Flight
Instruments
Selecting an Active Profile
1) Use the FMS Knob to select the AUX - System Setup Page.
EAS
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight the active profile field in the Pilot
Nav/Com/
XPDR/Audio
Profile Box.
4) Turn the small FMS Knob to display the pilot profile list and highlight the
desired profile.
AFCS
5) Press the ENT Key. The system loads and displays the system settings for
the selected profile.
GPS Nav
6)
Press the FMS Knob to deactivate the cursor.
Renaming a Profile
Flight
Planning
1) Use the FMS Knob to select the AUX - System Setup Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
Procedures
3) Turn the large FMS Knob to highlight ‘RENAME’ in the Pilot Profile Box.
4)
Press the ENT Key.
5) In the ‘Rename Profile’ window, turn the FMS Knob to select the profile to
Hazard
Avoidance
rename.
6)
Press the ENT Key.
Additional
Features
7) Use the FMS Knob to enter a new profile name up to 16 characters long
and press the ENT Key.
8) With ‘RENAME’ highlighted, press the ENT Key.
Abnormal
Operation
9)
To cancel the process, use the large FMS Knob to select ‘CANCEL’ and
press the ENT Key.
Index
Appendix
Annun/
Alerts
10) Press the FMS Knob to deactivate the cursor.
98
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Additional Features
NOTE: The profile that is currently active cannot be deleted. If this is the
Nav/Com/
XPDR/Audio
1) Use the FMS Knob to select the AUX - System Setup Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
AFCS
3) Turn the large FMS Knob to highlight ‘DELETE’ in the Pilot Profile Box.
4)
Press the ENT Key.
GPS Nav
5) In the ‘Delete Profile’ window, turn the FMS Knob to select the profile to
delete.
6)
EAS
desired profile to delete, select another profile, then delete the desired
profile.
Flight
Instruments
Deleting a Profile
Press the ENT Key.
Flight
Planning
7) With ‘DELETE’ highlighted, press the ENT Key.
To cancel the process, use the large FMS Knob to select ‘CANCEL’ and
press the ENT Key.
9)
Press the FMS Knob to deactivate the cursor.
Procedures
8)
Select the IMPORT Softkey.
4)
The system displays the Pilot Profile Importing Window with ‘IMPORT’
highlighted. To change the selected profile to be imported from the SD card
(shown as ‘SELECT FILE’), turn the large FMS Knob to highlight the profile
file name, then turn the small FMS Knob to highlight a profile from the list,
and press the ENT Key.
5)
If desired, the profile name to be used after profile has been imported can
be changed by turning the FMS Knob to highlight the ‘PROFILE NAME’
field, then use the large and small FMS Knobs to enter the name, and press
the ENT Key. Imported profile names cannot begin with a blank space or
be named ‘DEFAULT’, ‘GARMIN DEFAULTS’ or ‘DEFAULT SETTINGS’.
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
99
Index
3)
Appendix
Turn the FMS Knob to select the AUX - System Setup Page.
Annun/
Alerts
2)
Abnormal
Operation
Insert an SD card containing the pilot profile(s) into the top card slot on the
MFD.
Additional
Features
1)
Hazard
Avoidance
Importing a Profile from an SD Card
6)
With ‘IMPORT’ highlighted, press the ENT Key.
7)
If the imported profile name is the same as an existing profile on the
system, the system displays an ‘Overwrite existing file? OK or CANCEL’
prompt. Press the ENT Key to replace profile on the system with the profile
imported from the SD card, or turn the FMS Knob to highlight ‘CANCEL’
and press the ENT Key to return to the Pilot Profile Importing Window.
8)
If successful, the system displays ‘Pilot profile import succeeded.’ in the
IMPORT RESULTS window below. With ‘OK’ highlighted, press the ENT or
CLR Keys or press the FMS Knob to return to the AUX - System Setup Page.
The imported profile becomes the active profile.
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Additional Features
1)
Insert the SD card for storing the Pilot Profile into the top card slot on the
MFD.
2)
Turn the FMS Knob to select the AUX - System Setup Page.
3)
If necessary, activate the desired pilot profile to export. Only the currently
active Pilot Profile can be exported.
4)
Select the EXPORT Softkey. The system displays the Pilot Profile Exporting
Window.
5)
To export the pilot profile using the current supplied name, press the ENT
Key with ‘EXPORT’ highlighted. To change the profile file name turn the
large FMS Knob to highlight the ‘SELECT FILE’ field, then enter the new
name with the large and small FMS Knobs, then press the ENT Key. Then
press the ENT Key with ‘EXPORT’ highlighted.
6)
If the profile name to be exported is the same as an existing profile file
name on the SD card, the system displays an ‘Overwrite existing file? OK
or CANCEL’ prompt. Press the ENT Key to replace the profile on the SD
card with the profile to be exported, or turn the FMS Knob to highlight
‘CANCEL’ and press the ENT Key to return to the Pilot Profile Exporting
Window without exporting the profile.
7)
If successful, the EXPORT RESULTS window displays ‘Pilot profile export
succeeded.’ With ‘OK’ highlighted, press the ENT or CLR Keys, or press the
FMS Knob to return to the AUX - System Setup Page.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Exporting a Profile to an SD Card
100
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Additional Features
EAS
Nav/Com/
XPDR/Audio
AFCS
The Bluetooth Management Page allows for setting up the installed optional Flight
Stream device for a Bluetooth connection between the G1000 and a mobile device
running the Garmin Pilot™ application.
The mobile device must be ‘paired’ with the G1000 in order to use the various
functions. Pairing is accomplished by first placing the G1000 in pairing mode by
displaying the Bluetooth Management Page. The G1000 is ‘discoverable’ whenever
this page is displayed. The pairing operation is completed from the mobile device and
the Garmin Pilot application. See the device Bluetooth pairing instructions and the
connection instructions in the Garmin Pilot application.
Flight
Instruments
BLUETOOTH® MANAGEMENT
Viewing the Bluetooth Management Page
Turn the large FMS Knob on the MFD to select the AUX page group.
2)
Turn the small FMS Knob to select the BLUETOOTH MANAGEMENT page.
Flight
Planning
Changing the Bluetooth Name
GPS Nav
1)
While viewing the Bluetooth Management Page, press the FMS Knob to
activate the cursor.
2)
Turn the large FMS Knob to place the cursor in the ‘BLUETOOTH NAME’
field.
3)
Enter the desired name by using the large FMS Knob to select the character
field, and the small FMS Knob select the desired alphanumeric character
for that field.
4)
Press the ENT Key. The cursor is removed and the new name is displayed.
Procedures
1)
Hazard
Avoidance
Additional
Features
Enabling/Disabling Flight Plan Importing from Garmin Pilot
Abnormal
Operation
2)
Turn the large FMS Knob to place the cursor in the ‘FLIGHT PLAN IMPORT’
field.
3)
Turn the small FMS Knob to select ‘ENABLED’ or ‘DISABLED’.
4)
Press the FMS Knob to remove the cursor.
Appendix
While viewing the Bluetooth Management Page, press the FMS Knob to
activate the cursor.
Annun/
Alerts
1)
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
101
Enabling/Disabling Automatic Reconnection of a Specific Paired Device
Flight
Planning
Hazard
Avoidance
Procedures
While viewing the Bluetooth Management Page, press the FMS Knob to
activate the cursor.
2)
Turn the large FMS Knob to highlight the desired paired device.
3)
Turn the small FMS Knob to select ‘ENABLED’ or ‘DISABLED’. Selecting
‘ENABLED’ allows the G1000 to automatically connect to a previously
paired device when detected.
4)
Press the FMS Knob to remove the cursor.
1)
While viewing the Bluetooth Management Page, press the FMS Knob to
activate the cursor.
2)
Turn the large FMS Knob to highlight the desired paired device.
3)
Press the REMOVE Softkey. A confirmation screen is displayed as seen in
Figure 8-112.
4)
If necessary, turn the large FMS Knob to select ‘YES’.
5)
Press the ENT Key to remove the device from the list of paired devices.
ELECTRONIC STABILITY & PROTECTION (ESP™)
Electronic Stability and Protection (ESP™) is an optional feature that is intended
to discourage the exceedance of attitude, established airspeed and angle of attack
parameters. This feature will only function when the aircraft is above 200 feet AGL
and the autopilot is not engaged. ESP is automatically enabled on system power up.
Enabling/Disabling ESP:
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
1)
Remove a Specific Paired Device from the List of Paired Devices:
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Additional Features
102
1)
Turn the large FMS Knob to select the AUX Page Group.
2)
Turn the small FMS Knob to select the System Setup Page.
3)
If necessary, select the SETUP 2 Softkey to display the AUX-SYSTEM SETUP 2
Page. If the AUX-SYSTEM SETUP 2 is already displayed, proceed to step 4.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to place the cursor in the STABILITY &
PROTECTION field.
6)
Turn the small FMS Knob to select ‘ENABLE’ or ‘DISABLE’.
7)
Press the FMS Knob to remove the cursor.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Abnormal Operation
Flight
Instruments
ABNORMAL OPERATION
REVERSIONARY MODE
GPS Nav
Flight
Planning
NOTE: The Socata TBM 850/900 Airplane Flight Manual (AFM) always takes
precedence over the information found in this section.
AFCS
• 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.
Nav/Com/
XPDR/Audio
Activation of reversionary display mode is accomplished by pressing the DISPLAY
BACKUP Button on the appropriate audio panel.
EAS
Reversionary mode must be entered manually in the case of PFD1, PFD2,
or MFD failure. In reversionary mode, critical flight instrumentation is combined
with engine instrumentation on the remaining display.
Procedures
ABNORMAL COM OPERATION
Abnormal
Operation
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.
Additional
Features
HAZARD DISPLAYS WITH LOSS OF GPS POSITION
Hazard
Avoidance
When a COM tuning failure is detected by the system, the emergency frequency
(121.500 MHz) is automatically loaded into the active frequency field of the COM
radio for which the tuning failure was detected. In the event of a failure of both PFDs,
the emergency frequency (121.500 MHz) automatically becomes the active frequency
on both COM radios.
Annun/
Alerts
Appendix
Loss of Hazard Functions with Loss of GPS
Position
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
103
UNUSUAL ATTITUDES
The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary
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:
• Traffic Annunciations
• AFCS Annunciations
• Flight Director
Command Bars
• Inset Map
• Temperatures
• DME Information
Window
• Wind Data
• Selected Heading Box
• Selected Course Box
• Transponder Status
Box
• 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
Extreme Pitch Indication
DEAD RECKONING
While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS
solution or is unable to calculate a GPS position, the system automatically reverts to
Dead Reckoning (DR) Mode. In DR Mode, the G1000 uses its last-known position
combined with continuously updated airspeed and heading data (when available) to
calculate and display the aircraft’s current estimated position.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Abnormal Operation
104
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Abnormal Operation
EAS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
DR Mode is indicated on the G1000 by the appearance of the letters ‘DR’
superimposed in yellow over the ‘own aircraft’ symbol as shown in the following
figure. In addition, ‘DR’ is prominently displayed, also in yellow, on the HSI slightly
above and to the right of the aircraft symbol on the CDI as shown in the following
figure. The CDI deviation bar is displayed in yellow, but will be removed from the
display after 20 minutes. Lastly, but at the same time, a ‘GPS NAV LOST’ alert message
appears on the PFD.
Normal navigation using GPS/SBAS source data resumes automatically once a valid
GPS solution is restored.
It is important to note that estimated navigation data supplied by the G1000 in
DR Mode may become increasingly unreliable and must not be used as a sole means
of navigation. If, while in DR Mode, airspeed and/or heading data is also lost or
not available, the DR function may not be capable of estimating your position and,
consequently, the system may display a path that is different than the actual movement
of the aircraft. Estimated position information displayed by the G1000 through
DR while there is no heading and/or airspeed data available should not be used for
navigation.
DR Mode is inherently less accurate than the standard GPS/SBAS Mode due to the
lack of satellite measurements needed to determine a position. Changes in wind speed
and/or wind direction compounds the relative inaccuracy of DR Mode. Because of this
degraded accuracy, the crew must maintain position awareness using other navigation
equipment until GPS-derived position data is restored.
Flight
Instruments
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.
Annun/
Alerts
Appendix
Symbolic Aircraft
(Map pages and Inset Map)
Index
CDI ‘DR’ Indication on PFD
Dead Reckoning Indications
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
105
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
navigation source information. This data includes the following:
•
•
•
•
•
•
Navigation Status Box fields except Active Leg, TAS, and DTK
GPS Bearing Pointer
Wind data and pointers in the Wind Data Box on the PFD
Current Track Indicator
All Bearing Pointer Distances
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-SVT, 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.
SUSPECTED AUTOPILOT MALFUNCTION
NOTE: Consult the aircraft documentation for the location of circuit breakers
as well as specifics that may supplement or amplify this procedure.
If an autopilot failure or trim failure is suspected to have occurred, perform the
following steps:
1)
Firmly grasp the control wheel.
2)
Press and hold the AP DISC Switch. The autopilot will disconnect and
power is removed from the trim motor. Power is also removed from all
primary servo motors and engaged solenoids. Note the visual and aural
alerting indicating autopilot disconnect.
3)
Retrim the aircraft as needed. Substantial trim adjustment may be needed.
4)
Pull the appropriate circuit breaker(s) to electrically isolate the servo and
solenoid components.
5)
Release the AP DISC Switch.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Abnormal Operation
106
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Abnormal Operation
EAS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
In the context of this discussion, “overpowering” refers to any pressure or force
applied to the pitch controls when the autopilot is engaged. A small amount of
pressure or force on the pitch controls can cause the autopilot automatic trim to run
to an out-of-trim condition. Therefore, any application of pressure or force to the
controls should be avoided when the autopilot is engaged.
Overpowering the autopilot during flight will cause the autopilot’s automatic trim
to run, resulting in an out-of-trim condition or cause the trim to hit the stop if the
action is prolonged. In this case, larger than anticipated control forces are required
after the autopilot is disengaged.
The following steps should be added to the preflight check:
1) Check for proper autopilot operation and ensure the autopilot can be
overpowered.
2) Note the forces required to overpower the autopilot servo clutches.
Flight
Instruments
OVERPOWERING AUTOPILOT SERVOS
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
107
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Abnormal Operation
Blank Page
108
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
Flight
Instruments
ANNUNCIATIONS & ALERTS
CAS MESSAGES
Description
AURAL WRN FAIL
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
* TBM 900 Only
Procedures
OIL PRESS
OXYGEN
PARK BRAKE
TORQUE**
USP ACTIVE
Flight
Planning
ITT
GPS Nav
BAT OVERHEAT
BLEED TEMP
CABIN ALTITUDE
CABIN DIFF PRESS
DOOR
EDM
ELEC FEATH FAULT*
FIRE
FLAPS ASYM
FUEL OFF
FUEL PRESS
GEAR UNSAFE*
AFCS
AURAL WRN 1 CHNL
Audio processing in both GIAs is offline, or both audio paths are
invalid
Audio processing in one of the two GIAs is offline, or one of the
2 audio paths is invalid
Battery temperature over 70°C
Bleed temperature high
Cabin altitude over 10,000 ft
Cabin pressure differential over 6.2 psi
Pilot or cabin door open
Autopilot has activated emergency descent mode
Feathering system failure
Engine compartment fire (temperature over 200°C; if installed)
Dissymmetry between left- and right-hand flaps
Fuel tank selectors set to “Off”
Fuel pressure below 10 psi
Gears are in an unsafe configuration
Engine start: ITT over 1000°C, 870°C (5 s), or 840°C (20 s)
Engine running: ITT over 840°C
Oil pressure below 60 psi
Oxygen cylinder closed
Parking brake applied
Torque greater than or equal to 121.4% maximum torque
Underspeed protection is active
Nav/Com/
XPDR/Audio
Message
EAS
Warning Messages
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
109
** TBM 850 Only
Caution Messages
EAS
Flight
Instruments
Annunciations & Alerts
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Message
Description
AP ON YD OFF
AUTO SEL
AUX BOOST PMP ON
BAT AMP
BAT OFF
BLEED OFF
CHIP
The autopilot is ON while the Yaw Damper is OFF
Fuel timer off or out of service
Electric fuel pump running (manual or automatic mode)
Battery current over 50 A while on ground
Battery off
Flow control and shut-off valve/shut-off valve closed
Oil chip detector on (if installed)
Back-up pressurization mode - Cabin altitude target forced to
CPCS BACKUP MODE**
9800 ft
CPDLC DISABLED
CPDLC data mode is disabled
EDM OVERRIDE
Emergency Descent Mode has been overridden by the crew
FRONT CARGO DOOR Forward baggage door open
Fuel tanks imbalanced by more than 15 USGAL for >30
FUEL IMBALANCE
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
INERT SEP FAIL
Inertial separator failure
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
MAX DIFF MODE**
MAX DIFF PRESS MODE activated
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 L-R*
Specified pitot heat (left or right) on while engine off
PITOT NO HT L-R*
Specified pitot heat (left or right) off
PROP DEICE FAIL
Prop deice selected and not on
110
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
Prop deice on while engine off
Stall warning heat on while engine off
Stall warning heat off
Starter generator running
Vacuum pressure less than 3.75 in Hg
Cabin altitude above 10,000 ft
Flight
Instruments
EAS
* Only affected side (L, R, or L-R) displayed in CAS message; applicable messages listed here display
L-R for example
** TBM 900 Only
AFCS
COMPARATOR ANNUNCIATIONS
ROL MISCOMP
IAS NO COMP
PIT NO COMP
ROL NO COMP
Abnormal
Operation
HDG NO COMP
Additional
Features
ALT NO COMP
Hazard
Avoidance
PIT MISCOMP
Procedures
HDG MISCOMP
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 knots.
If either airspeed sensor detects > 80 knots, and the difference in
sensors is > 7 knots.
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.
Flight
Planning
IAS MISCOMP
Condition
GPS Nav
Comparator
Window Text
ALT MISCOMP
Nav/Com/
XPDR/Audio
PROP DEICE ON
STALL HEAT ON
STALL NO HEAT
STARTER
VACUUM LOW
USE OXYGEN MASK
Annun/
Alerts
REVERSIONARY SENSOR ANNUNCIATIONS
Appendix
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
111
Reversionary
Sensor
Window Text
BOTH ON ADC1
BOTH ON ADC2
BOTH ON AHRS1
Condition
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 ON AHRS2
Both PFDs are displaying data from the number two Attitude & Heading Reference
System.
BOTH ON GPS1
BOTH ON GPS2
USING ADC1
USING ADC2
Both PFDs are displaying data from the number one GPS receiver.
USING AHRS1
PFD2 is displaying data from the #1 AHRS.
USING AHRS2
USING GPS1
USING GPS2
PFD1 is displaying data from the #2 AHRS.
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 GPS.
PFD1 is displaying data from the #2 GPS.
AFCS ALERTS
Alert Condition Annunciation
Rudder Mistrim
Right
Rudder Mistrim
Left
Aileron Mistrim
Right
Aileron Mistrim
Left
Elevator Mistrim
Down
Elevator Mistrim
Up
Description
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.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
112
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
Pitch Trim Failure
Description
(or stuck MEPT
Switch)
Yaw Trim Failure
(or stuck MEYT
Switch)
Yaw Damper
Failure
YD control failure; AP also inoperative
Pitch Failure
Pitch axis control failure; AP inoperative
System Failure
GPS Nav
Roll axis control failure; AP inoperative
AFCS
Roll Failure
AP and MEPT are unavailable; FD may still be available
Additional
Features
MFD
Pop-Up Alert
Abnormal
Operation
Aural
Message
“Warning; Terrain,
Terrain”
Reduced Required Obstacle
Clearance Warning (ROC)
“Warning; Obstacle,
Obstacle”
Imminent Obstacle Impact
Warning (IOI)
“Warning; Obstacle,
Obstacle”
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
113
Index
Imminent Terrain Impact
Warning (ITI)
Appendix
“Warning; Terrain,
Terrain”
Annun/
Alerts
PFD/MFD
TERRAIN-SVT
Page
Annunciation
Reduced Required Terrain
Clearance Warning (RTC)
190-00708-07 Rev. B
Hazard
Avoidance
TERRAIN-SVT ALERTS
Alert Type
Procedures
Preflight system test failed; aural alert sounds at failure
Flight
Planning
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
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 Test
Nav/Com/
XPDR/Audio
If AP engaged, take control of the aircraft and disengage AP
If AP disengaged, move the MEYT switch to check if a stuck
switch is causing the annunciation
EAS
If AP engaged, take control of the aircraft and disengage AP
If AP disengaged, move MEPT switches separately to
unstick
Flight
Instruments
Alert Condition Annunciation
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
PFD/MFD
TERRAIN-SVT
Page
Annunciation
Alert Type
MFD
Pop-Up Alert
Aural
Message
Reduced Required Terrain
Clearance Caution (RTC)
“Caution; Terrain,
Terrain”
Imminent Terrain Impact
Caution (ITI)
“Caution; Terrain,
Terrain”
Reduced Required Obstacle
Clearance Caution (ROC)
“Caution; Obstacle,
Obstacle”
Imminent Obstacle Impact
Caution (IOI)
“Caution; Obstacle,
Obstacle”
TERRAIN-SVT SYSTEM STATUS ANNUNCIATIONS
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
TERRAIN-SVT Page
Annunciation
Aural Message
TERRAIN TEST
None
None
“Terrain System
Test OK”
None
None
TERRAIN DATABASE FAILURE
None
Terrain System Test
Fail
TERRAIN FAIL
“Terrain System
Failure”
Terrain or Obstacle
database unavailable
or invalid,
invalid software
configuration, system
audio fault
TERRAIN FAIL
“Terrain System
Failure”
NO GPS POSITION
“Terrain System
Not Available”
Alert Type
PFD/MFD Alert
Annunciation
System Test in
Progress
System Test Pass
None
Terrain Alerting is
disabled
MFD Terrain or
Obstacle database
unavailable or invalid.
Terrain-SVT operating
with PFD Terrain or
Obstacle databases
No GPS position
114
None
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
PFD/MFD Alert
Annunciation
None
“Terrain System
Not Available”
None
“Terrain System
Available”
Excessively degraded
GPS signal, Out of
database coverage
area
Sufficient GPS signal
received after loss
None
Nav/Com/
XPDR/Audio
Aural Message
EAS
TERRAIN-SVT Page
Annunciation
Flight
Instruments
Alert Type
TAWS-B ALERTS
MFD
Pop-Up Alert
Excessive Descent
Rate Warning (EDR)
“Pull Up”
Reduced Required
Terrain Clearance
Caution (RTC)
or
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
or
“Obstacle, Obstacle; Pull Up,
Pull Up”
“Caution, Terrain; Caution,
Terrain”
or
“Terrain Ahead; Terrain Ahead”
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
115
Index
or
Appendix
Imminent Obstacle
Impact Warning
(IOI)
“Obstacle, Obstacle; Pull Up,
Pull Up”
or
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
Annun/
Alerts
or
Abnormal
Operation
Reduced Required
Obstacle Clearance
Warning (ROC)
Terrain Ahead, Pull Up; Terrain
Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up, Pull Up”
Additional
Features
or
Hazard
Avoidance
Imminent Terrain
Impact Warning
(ITI)
“Terrain, Terrain; Pull Up, Pull
Up”
or
“Terrain Ahead, Pull Up; Terrain
Ahead, Pull Up”
Procedures
or
Flight
Planning
Reduced Required
Terrain Clearance
Warning (RTC)
190-00708-07 Rev. B
Aural Message
GPS Nav
PFD/MFD
TAWS-B Page
Annunciation
AFCS
Alert Type
Alert Type
PFD/MFD
TAWS-B Page
Annunciation
Imminent Terrain
Impact Caution (ITI)
Reduced Required
Obstacle Clearance
Caution (ROC)
MFD
Pop-Up Alert
Aural Message
or
“Terrain Ahead; Terrain Ahead”
or
“Caution, Terrain; Caution,
Terrain”
or
Imminent Obstacle
Impact Caution
(IOI)
or
“Caution, Obstacle; Caution,
Obstacle”
or
“Obstacle Ahead; Obstacle
Ahead”
“Obstacle Ahead; Obstacle
Ahead”
or
“Caution, Obstacle; Caution,
Obstacle”
Premature Descent
Alert Caution (PDA)
Altitude Callout
“500”
“Too Low, Terrain”
None
None
Excessive Descent
Rate Caution (EDR)
Negative Climb
Rate Caution
(NCR)
“Five-Hundred”
“Sink Rate”
or
“Don’t Sink”
or
“Too Low, Terrain”
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
116
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
PFD/MFD Alert
Annunciation
Flight
Instruments
TAWS-B System Status Annunciations
Aural
Message
TAWS TEST
None
None
“TAWS System
Test OK”
None
None
TERRAIN DATABASE FAILURE
None
TAWS-B System Test Fail
TAWS FAIL
“TAWS System
Failure”
Terrain or Obstacle
database unavailable or
invalid, invalid software
configuration, system
audio fault
TAWS FAIL
“TAWS System
Failure”
NO GPS POSITION
“TAWS Not
Available”
None
“TAWS Not
Available”
None
“TAWS
Available”
System Test in Progress
None
TAWS Alerting is disabled
None
Hazard
Avoidance
Additional
Features
None
Procedures
Sufficient GPS signal
received after loss
Flight
Planning
Excessively degraded GPS
signal, Out of database
coverage area
GPS Nav
No GPS position
AFCS
MFD Terrain or Obstacle
database unavailable or
invalid. TAWS operating
with PFD Terrain or
Obstacle databases
Nav/Com/
XPDR/Audio
System Test Pass
EAS
TAWS-B Page Annunciation
Alert Type
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
117
VOICE ALERTS
Voice Alert
“Airspeed”
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
“ATC Message”
“Aural Warning OK”
Description
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.
New Data Link message received from ATC.
Played when both audio paths are OK, following a
previous audio path or audio processing issue.
“Engaging Autopilot”
Played when ESP has been engaged for more than 10
seconds cumulative of a 20 second interval, and the
autopilot is automatically engaged.
“Incoming Call”
Satellite telephone is receiving a call.
“Landing Gear, Landing Gear” Gear up in landing condition.
“Minimums, minimums”
The aircraft has descended below the preset
barometric minimum descent altitude.
“Overspeed, Overspeed”
Airspeed has exceeded 265 Kts.
“Stall, Landing Gear”
Combination of airplane in stall condition and gear
up in landing condition.
“Stall, Stall”
Airplane in stall condition.
“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 Failed”
Played when the TAS system fails a pilot-initiated
self test.
“TAS System Test OK”
Played when the TAS system passes a pilotinitiated self test.
“Use Oxygen Mask,
Played in conjuction with associated CAS messages
Use Oxygen Mask”
when cabin altiude exceeds 10,000 ft.
“Vertical track”
The aircraft is one minute from Top of Descent. Issued
only when vertical navigation is enabled.
118
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
Description
Played to indicate bearing of traffic from own aircraft
(GTS 820 only).
Flight
Instruments
EAS
Played to indicate altitude of traffic relative to own
aircraft (GTS 820 only).
Nav/Com/
XPDR/Audio
Played to indicate distance of traffic from own aircraft
(GTS 820 only).
AFCS
GPS Nav
Voice Alert
“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”
MESSAGE ADVISORIES
GDC1 is reporting that the altitude error
correction is unavailable.
GDC1 is reporting that the airspeed error
correction is unavailable.
GDC2 is reporting that the altitude error
correction is unavailable.
GDC2 is reporting that the airspeed error
correction is unavailable.
Hazard
Avoidance
Additional
Features
Abnormal
Operation
The #1 AHRS and #2 AHRS magnetic model
database versions do not match.
Annun/
Alerts
The AHRS1 calibration version error. The system
should be serviced.
AHRS configuration settings do not match those
of backup configuration memory. The system
should be serviced.
Index
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Appendix
190-00708-07 Rev. B
Abort approach due to loss of GPS navigation.
Procedures
ABORT APR – Loss of GPS
navigation. Abort approach.
ADC1 ALT EC – ADC1 altitude
error correction is unavailable.
ADC1 AS EC – ADC1 airspeed
error correction is unavailable.
ADC2 ALT EC – ADC2 altitude
error correction is unavailable.
ADC2 AS EC – ADC2 airspeed
error correction is unavailable.
AHRS MAG DB – AHRS
magnetic model database version
mismatch.
AHRS1 CAL – AHRS1 calibration
version error. Srvc req’d.
AHRS1 CONFIG– AHRS1 config
error. Config service req’d.
Comments
Flight
Planning
Message
119
Message
AHRS1 GPS – AHRS1 not
receiving any GPS information.
AHRS1 GPS – AHRS1 not
receiving backup GPS information.
AHRS1 GPS – AHRS1 operating
exclusively in no-GPS mode.
AHRS1 GPS – AHRS1 using
backup GPS source.
AHRS1 SRVC – AHRS1 Magneticfield model needs update.
AHRS1 TAS – AHRS1 not
receiving airspeed.
AHRS2 GPS – AHRS2 not
receiving any GPS information.
AHRS2 GPS – AHRS2 not
receiving backup GPS information.
AHRS2 GPS – AHRS2 operating
exclusively in no-GPS mode.
Comments
The #1 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
G1000 system should be serviced.
The #1 AHRS is not receiving backup GPS
information. The G1000 system should be
serviced.
The #1 AHRS is operating exclusively in no-GPS
mode. The G1000 system should be serviced.
The #1 AHRS is using the backup GPS path.
Primary GPS path has failed. The G1000 system
should be serviced when possible.
The #1 AHRS earth magnetic field model is out
of date. Update magnetic field model when
practical.
The #1 AHRS is not receiving true airspeed from
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed. The
G1000 system should be serviced.
The AHRS2 calibration version error. The system
should be serviced.
AHRS configuration settings do not match those
of backup configuration memory. The system
should be serviced.
The #2 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
G1000 system should be serviced.
The #2 AHRS is not receiving backup GPS
information. The G1000 system should be
serviced.
The #2 AHRS is operating exclusively in no-GPS
mode. The G1000 system should be serviced.
Index
Appendix
Abnormal
Operation
AHRS2 CAL – AHRS2 calibration
version error. Srvc req’d.
AHRS2 CONFIG– AHRS2 config
error. Config service req’d.
Annun/
Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
120
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
Comments
AHRS2 GPS – AHRS2 using
backup GPS source.
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Selected course for LOC1 differs from published
localizer course by more than 10 degrees.
Selected course for LOC2 differs from published
localizer course by more than 10 degrees.
121
Index
The PFD1 configuration module backup memory
has failed. The G1000 system should be serviced.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
AFCS
190-00708-07 Rev. B
Nav/Com/
XPDR/Audio
CHECK CRS – Database course
for LOC1 / [LOC ID] is [CRS]°.
CHECK CRS – Database course
for LOC2 / [LOC ID] is [CRS]°.
CNFG MODULE – PFD1
configuration module is
inoperative.
EAS
The #2 AHRS is using the backup GPS path.
Primary GPS path has failed. The G1000 system
should be serviced when possible.
AHRS2 SRVC – AHRS2 Magnetic- The #2 AHRS earth magnetic field model is out
field model needs update.
of date. Update magnetic field model when
practical.
AHRS2 TAS – AHRS2 not
The #2 AHRS is not receiving true airspeed from
receiving airspeed.
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed. The
G1000 system should be serviced.
APR DWNGRADE – Approach
Vertical guidance generated by SBAS is
downgraded.
unavailable, use LNAV only minimums.
APR INACTV – Approach is not
The system notifies the pilot that the loaded
active.
approach is not active. Activate approach when
required.
ARSPC AHEAD – Airspace ahead Special use airspace is ahead of aircraft. The
less than 10 minutes.
aircraft will penetrate the airspace within 10
minutes.
ARSPC NEAR – Airspace near – Special use airspace is within 2 nm of the aircraft
less than 2 nm.
position.
ARSPC NEAR – Airspace near
Special use airspace is near and ahead of the
and ahead.
aircraft position.
AUDIO MANIFEST The GDC 74B has incorrect software installed.
Audio software mismatch,
The G1000 system should be serviced.
communication halted.
Flight
Instruments
Message
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
Message
COM1 CONFIG – COM1 config
error. Config service req’d.
COM 1 MANIFEST –
COM1 software mismatch,
communication halted.
COM1 PTT – COM1 push-to-talk
key is stuck.
Comments
The COM1 configuration settings do not match
backup configuration memory. The system should
be serviced.
The COM1 has incorrect software installed. The
system should be serviced.
The COM1 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.
COM1 RMT XFR – COM1 remote The COM1 transfer switch is stuck in the enabled
transfer key is stuck.
(or “pressed”) position. Press the transfer switch
again to cycle its operation. If the problem
persists, the G1000 system should be serviced.
COM1 SERVICE – COM1 needs
The system has detected a failure in COM1.
service. Return unit for repair.
COM1 may still be usable. The G1000 system
should be serviced when possible.
COM1 TEMP – COM1 over temp. The system has detected an over temperature
Reducing transmitter power.
condition in COM1. The transmitter is operating
at reduced power. If the problem persists, the
G1000 system should be serviced.
COM2 CONFIG – COM2 config
The COM2 configuration settings do not match
error. Config service req’d.
backup configuration memory. The system should
be serviced.
COM 2 MANIFEST –
The COM2 has incorrect software installed. The
COM2 software mismatch,
system should be serviced.
communication halted.
COM2 PTT – COM2 push-to-talk The COM2 external push-to-talk switch is stuck in
key is stuck.
the enable (or “pressed”) position. Press the PTT
switch again to cycle its operation.
If the problem persists, the G1000 system should
be serviced.
122
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
Comments
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
123
Flight
Planning
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
GPS Nav
190-00708-07 Rev. B
AFCS
DB CHANGE – Database
changed. Verify user modified
procedures.
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.
This occurs when a stored flight plan contains
procedures that have been manually edited. This
alert is issued only after an navigation database
update. Verify that the user-modified procedures
in stored flight plans are correct and up to date.
Nav/Com/
XPDR/Audio
DATA LOST – Pilot stored data
was lost. Recheck settings.
EAS
COM2 RMT XFR – COM2 remote The COM2 transfer switch is stuck in the enabled
transfer key is stuck.
(or “pressed”) position. Press the transfer switch
again to cycle its operation. If the problem
persists, the G1000 system should be serviced.
COM2 SERVICE – COM2 needs
The system has detected a failure in COM2.
service. Return unit for repair.
COM2 may still be usable. The G1000 system
should be serviced when possible.
COM2 TEMP – COM2 over temp. The system has detected an over temperature
Reducing transmitter power.
condition in COM2. The transmitter is operating
at reduced power. If the problem persists, the
G1000 system should be serviced.
CPDLC – CPDLC connection lost.
Data link connection has been lost.
Establish new connection.
CPDLC – CPDLC facility logon
Logon failed. Check pertinent entries for
failed
accuracy.
CPDLC – CPDLC data link
The data link is ready for use, but logon to the
available. Logon is still required
facility has not yet taken place
CPDLC – CPDLC is available.
Logon successful. Data link is available for use.
CRUISE I – Cruise I conditions
Cruise I engine trend data log has been captured.
met.
CRUISE II – Cruise II conditions
Cruise II engine trend data log has been captured.
met.
Flight
Instruments
Message
Message
DB CHANGE – Database
changed. Verify stored airways.
DB MISMATCH – Navigation
database mismatch. Xtalk is off.
DB MISMATCH – Obstacle
database mismatch.
DB MISMATCH – Standby
Navigation database mismatch.
Comments
This occurs when a stored flight plan contains
an airway that is no longer consistent with the
navigation database. This alert is issued only after
an navigation database update. Verify use of
airways in stored flight plans and reload airways
as needed.
The PFDs and MFD have different navigation
database versions or regions installed. Crossfill
is off. Check the AUX-SYSTEM STATUS Page
to determine versions or regions. Also, check
the AUX-SYSTEM STATUS Page for a database
synchronization function not completed. After
synchronization is complete, power must be
turned off, then on.
The PFDs and MFD have different obstacle
database versions or regions installed. Check the
AUX-SYSTEM STATUS Page to determine versions
or regions. Also, check the AUX-SYSTEM STATUS
Page for a database synchronization function not
completed. After synchronization is complete,
power must be turned off, then on.
The PFDs and MFD have different standby
navigation database versions or regions installed.
Check the AUX-SYSTEM STATUS Page to
determine versions or regions. Also, check the
AUX-SYSTEM STATUS Page for a database
synchronization function not completed. After
synchronization is complete, power must be
turned off, then on.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
124
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
DB MISMATCH – Terrain
database mismatch.
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
A data path connected to the GDU or the GIA
63/W has failed.
Appendix
FAILED PATH – A data path has
failed.
GPS Nav
EXCEEDANCE – Exceedance data
An exceedance log has been captured.
is being logged.
AFCS
ESP OFF– ESP selected off.
The Environmental Control System has failed.
Electrical Power System needs servicing.
Starter Generator speed sensor has failed.
ESP is not configured properly. The system should
be serviced.
AOA mode of ESP is inoperative. The system
should be serviced.
IAS mode of ESP is inoperative. The system should
be serviced.
The ESP function has failed and is inoperative. The
system should be serviced.
Electronic Stability and Protection has been
disabled on the Avionics Settings Screen.
Nav/Com/
XPDR/Audio
ECS – Service required.
EPS – Service required.
EPS – S/G speed sensor failed.
ESP CONFIG– ESP config error.
Config service req’d.
ESP DEGRADE– ESP AOA mode
is inoperative.
ESP DEGRADE– ESP IAS mode
is inoperative.
ESP FAIL– ESP is inoperative.
The PFDs and MFD have different terrain database
versions or regions installed. Check the AUXSYSTEM STATUS Page to determine versions or
regions. Also, check the AUX-SYSTEM STATUS
Page for a database synchronization function not
completed. After synchronization is complete,
power must be turned off, then on.
A failure or disagreement has been detected in a
DME receiver. Check position sensors.
EAS
DME CHECK RANGE – DME
range disagreement. Check
position sensors.
Comments
Flight
Instruments
Message
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
125
Message
FPL WPT LOCK – Flight plan
waypoint is locked.
FPL WPT MOVE – Flight plan
waypoint moved.
FPL TRUNC – Flight plan has
been truncated.
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
G/S1 FAIL – G/S1 is inoperative.
G/S1 SERVICE – G/S1 needs
service. Return unit for repair.
G/S2 SERVICE – G/S2 needs
service. Return unit for repair.
Index
Appendix
G/S2 FAIL – G/S2 is inoperative.
126
Comments
Upon power-up, the G1000 system detects that a
stored flight plan waypoint is locked. This occurs
when an navigation database update eliminates
an obsolete waypoint. The flight plan cannot find
the specified waypoint and flags this message.
This can also occur with user waypoints in a flight
plan that is deleted.
Remove the waypoint from the flight plan if it no
longer exists in any database,
Or
update the waypoint name/identifier to reflect the
new information.
The system has detected that a waypoint
coordinate has changed due to a new navigation
database update. Verify that stored flight plans
contain correct waypoint locations.
This occurs when a newly installed navigation
database eliminates an obsolete approach
or arrival used by a stored flight plan. The
obsolete procedure is removed from the flight
plan. Update flight plan with current arrival or
approach.
A failure has been detected in glideslope receiver
1. The G1000 system should be serviced.
A failure has been detected in glideslope receiver
1. The receiver may still be available. The G1000
system should be serviced when possible.
A failure has been detected in glideslope receiver
2. The G1000 system should be serviced.
A failure has been detected in glideslope receiver
2. The receiver may still be available. The G1000
system should be serviced when possible.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
Comments
GCU CNFG – GCU Config error.
Config service req’d.
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
127
Flight
Planning
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
GPS Nav
190-00708-07 Rev. B
AFCS
GDL 69 configuration settings do not match those
of backup configuration memory. The G1000
system should be serviced.
GDL69 FAIL – GDL 69 has failed. A failure has been detected in the GDL 69. The
receiver is unavailable. The G1000 system should
be serviced
GDR AUX MANIFEST – GDR
The GDR secondary processor has incorrect
AUX software mismatch,
software installed. The system should be serviced.
communication halted.
GDR CONFIG – GDR config error. GDR configuration settings do not match those of
Config service req’d.
backup configuration memory. The system should
be serviced.
Nav/Com/
XPDR/Audio
GDL69 CONFIG – GDL 69 config
error. Config service req’d.
EAS
GCU 475 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.
GCU FAIL – GCU is inoperative.
A failure has been detected in the GCU 475. The
GCU 475 is unavailable.
GCU KEYSTK – GCU [key name] A key is stuck on the GCU 475 bezel. Attempt to
Key is stuck.
free the stuck key by pressing it several times. The
G1000 system should be serviced if the problem
persists.
GCU MANIFEST – GCU software The GCU 475 has incorrect software installed.
mismatch, communication halted. The G1000 system should be serviced.
GDC1 MANIFEST – GDC1
The GDC 74B has incorrect software installed.
software mismatch,
The G1000 system should be serviced.
communication halted.
GDC2 MANIFEST – GDC2
The GDC 74B has incorrect software installed.
software mismatch,
The G1000 system should be serviced.
communication halted.
GDL MANIFEST – GDL software The GDL 69 has incorrect software installed. The
mismatch, communication halted. G1000 system should be serviced.
Flight
Instruments
Message
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
Message
Comments
GDR FAIL – GDR is inoperative.
A failure has been detected in the GDR. The
system should be serviced.
GDR MANIFEST – GDR software The GDR has incorrect software installed. The
mismatch, communication halted. system should be serviced.
GDR SERVICE – GDR needs service.
The GDR should be serviced when possible.
Return unit for repair.
GDR TEMP – GDR over temp.
The system has detected an over temperature
Reducing transmitter power.
condition in the GDR. The transmitter operates
at reduced power. If the problem persists, the
system should be serviced.
GDR TX FAIL – GDR transmitter is
The system should be serviced.
inoperative.
GEA1 CONFIG – GEA1 config
The GEA1 configuration settings do not match
error. Config service req’d.
those of backup configuration memory. The
G1000 system should be serviced.
GEA1 MANIFEST – GEA1
The #1 GEA 71 has incorrect software installed.
software mismatch,
The G1000 system should be serviced.
communication halted.
GEA2 CONFIG – GEA2 config
The GEA2 configuration settings do not match
error. Config service req’d.
those of backup configuration memory. The
G1000 system should be serviced.
GEA2 MANIFEST – GEA2
The #2 GEA 71 has incorrect software installed.
software mismatch,
The G1000 system should be serviced.
communication halted.
GEO LIMITS – AHRS1 too
far North/South, no magnetic
The aircraft is outside geographical limits for
compass.
approved AHRS operation. Heading is flagged as
GEO LIMITS – AHRS2 too
invalid.
far North/South, no magnetic
compass.
GFC MANIFEST – GFC software Incorrect servo software is installed, or gain
mismatch, communication halted. settings are incorrect.
128
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
GIA2 COOLING – GIA2 over
temperature.
GIA2 MANIFEST – GIA2 software
mismatch, communication halted.
GIA2 SERVICE – GIA2 needs
service. Return the unit for repair.
GMA XTALK – GMA crosstalk
error has occurred.
GPS Nav
GIA2 CONFIG – GIA2 audio
config error. Config service req’d.
GIA2 COOLING – GIA2
temperature too low.
AFCS
GIA1 MANIFEST – GIA1 software
mismatch, communication halted.
GIA1 SERVICE – GIA1 needs
service. Return the unit for repair.
GIA2 CONFIG – GIA2 config
error. Config service req’d.
Nav/Com/
XPDR/Audio
GIA1 COOLING – GIA1 over
temperature.
GIA1 COOLING – GIA1
temperature too low.
The GIA1 have an error in the audio configuration.
The G1000 system should be serviced.
The GIA1 configuration settings do not match
backup configuration memory. The G1000 system
should be serviced.
The GIA1 temperature is too high. If problem
persists, the G1000 system should be serviced.
he GIA1 configuration settings do not match
backup configuration memory. The G1000 system
should be serviced.
The GIA1 has incorrect software installed. The
G1000 system should be serviced.
The GIA1 self-test has detected a problem in the
unit. The G1000 system should be serviced.
The GIA2 configuration settings do not match
backup configuration memory. The G1000 system
should be serviced.
The GIA2 have an error in the audio configuration.
The G1000 system should be serviced.
The GIA2 temperature is too low to operate
correctly. Allow units to warm up to operating
temperature.
The GIA2 temperature is too high. If problem
persists, the G1000 system should be serviced.
The GIA 2 has incorrect software installed. The
G1000 system should be serviced.
The GIA2 self-test has detected a problem in the
unit. The G1000 system should be serviced.
An error has occurred in transferring data
between the two GMAs. The G1000 system
should be serviced.
EAS
GIA1 CONFIG – GIA1 audio
config error. Config service req’d.
GIA1 CONFIG – GIA1 config
error. Config service req’d.
Comments
Flight
Instruments
Message
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
129
Message
GMA1 AUX MANIFEST – GMA
1 AUX software mismatch,
communication halted.
GMA1 CONFIG – GMA1 config
error. Config service req’d.
GMA1 FAIL – GMA1 is
inoperative.
GMA1 MANIFEST – GMA1
software mismatch, communication
halted.
GMA1 SERVICE – GMA1 needs
service. Return unit for repair.
GMA2 CONFIG – GMA2 config
error. Config service req’d.
GMA2 FAIL – GMA2 is
inoperative.
GMA2 MANIFEST – GMA2
software mismatch, communication
halted.
GMA2 SERVICE – GMA2 needs
service. Return unit for repair.
GMC CONFIG – GMC Config
error. Config service req’d.
GMC FAIL – GMC is inoperative.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
130
Comments
The digital audio controller has incorrect software
installed. The system should be serviced.
The audio panel configuration settings do not
match backup configuration memory. The G1000
system should be serviced.
The audio panel self-test has detected a failure.
The audio panel is unavailable. The G1000 system
should be serviced.
The audio panel has incorrect software installed. The
G1000 system should be serviced.
The audio panel self-test has detected a problem in
the unit. Certain audio functions may still be available, and the audio panel may still be usable. The
G1000 system should be serviced when possible.
The audio panel configuration settings do not
match backup configuration memory. The G1000
system should be serviced.
The audio panel self-test has detected a failure.
The audio panel is unavailable. The G1000 system
should be serviced.
The audio panel has incorrect software installed. The
G1000 system should be serviced.
The audio panel self-test has detected a problem in
the unit. Certain audio functions may still be available, and the audio panel may still be usable. The
G1000 system should be serviced when possible.
Error in the configuration of the GMC 710.
A failure has been detected in the GMC 710. The
GMC 710 is unavailable.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
Comments
EAS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
GMC KEYSTK – GMC [key name] A key is stuck on the GMC 710 bezel. Attempt to
Key is stuck.
free the stuck key by pressing it several times. The
G1000 system should be serviced if the problem
persists.
GMC MANIFEST – GMC software
The GMC 710 has incorrect software installed.
mismatch. Communication
The G1000 system should be serviced.
halted.
GMU1 MANIFEST –
The GMU 44 has incorrect software installed. The
GMU1 software mismatch,
G1000 system should be serviced.
communication halted.
GMU2 MANIFEST –
he GMU 44 has incorrect software installed. The
GMU2 software mismatch,
G1000 system should be serviced.
communication halted.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to insufficient
navigation. Insufficient satellites. satellites.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to position error.
navigation. Position error.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to GPS failure.
navigation. GPS fail.
GPS1 SERVICE – GPS1 needs
A failure has been detected in the GPS1 and/or
service. Return unit for repair.
GPS2 receiver. The receiver may still be available.
GPS2 SERVICE – GPS2 needs
The G1000 system should be serviced.
service. Return unit for repair.
GRA1 CAL – GRA1 calibration
A calibration error has been detected in the GRA.
error. Service req’d.
The system should be serviced.
GRA1 CONFIG – GRA1 config
The GRA configuration settings do not match
error. Config service req’d.
those of backup configuration memory. The
system should be serviced.
GRS1 CONFIG – GRS1 config
GRS configuration settings do not match those of
error. Config service req’d.
backup configuration memory. The system should
be serviced.
Flight
Instruments
Message
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
131
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
Message
GRS1 MANIFEST – GRS1
software mismatch,
communication halted.
GRS1 SERVICE – GRS1 needs
service. Return unit for repair.
GRS2 CONFIG – GRS2 config
error. Config service req’d.
GRS2 MANIFEST – GRS2
software mismatch,
communication halted.
GRS2 SERVICE – GRS1 needs
service. Return unit for repair.
GSR1 FAIL – GSR1 has failed.
Comments
The #1 AHRS has incorrect software installed. The
G1000 system should be serviced.
The AHRS1 should be serviced when practical.
GRS configuration settings do not match those of
backup configuration memory. The system should
be serviced.
The #2 AHRS has incorrect software installed. The
G1000 system should be serviced.
The AHRS1 should be serviced when practical.
A failure has been detected in the #1 GSR 56.
The system should be serviced.
GTS CONFIG – GTS config error. The GTS and GDU have incompatible
Config service req’d.
configurations. This alert is also set when the GTS
has an invalid mode S address configured or the
mode S address does not match both XPDR mode
S addresses.
GTS MANIFEST – GTS software The GTS has incorrect software installed. The
mismatch, communication halted. G1000 system should be serviced.
GTX1 MANIFEST – GTX1
The transponder has incorrect software installed.
software mismatch,
The G1000 system should be serviced.
communication halted.
GTX2 MANIFEST – GTX2
The transponder has incorrect software installed.
software mismatch,
The G1000 system should be serviced.
communication halted.
GWX CONFIG – GWX config
GWX 68 or GWX 70 configuration settings do
error. Config service req’d.
not match those of the GDU configuration. The
G1000 system should be serviced.
GWX FAIL – GWX is inoperative. The GDU is not receiving status packet from the
GWX 68 or the GWX 70 is reporting a fault. The
GWX 68 radar system should be serviced.
132
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
LOCKED FPL – Cannot navigate
locked flight plan.
This occurs when the pilot attempts to activate a
stored flight plan that contains locked waypoint.
Remove locked waypoint from flight plan. Update
flight plan with current waypoint.
Annun/
Alerts
The aircraft is inside the special use airspace.
Data link avionics were not configured correctly
and therefore will not be able to communicate
with the ground network.
Index
133
Appendix
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
GPS Nav
INSIDE ARSPC – Inside airspace.
INVALID ADM – Invalid ADM:
ATN communication halted.
190-00708-07 Rev. B
AFCS
HDG FAULT – AHRS1
A fault has occurred in the #1 GMU 44. Heading
magnetometer fault has occurred. is flagged as invalid. The AHRS uses GPS for
backup mode operation. The G1000 system
should be serviced.
HDG FAULT – AHRS2
A fault has occurred in the #2 GMU 44. Heading
magnetometer fault has occurred. is flagged as invalid. The AHRS uses GPS for
backup mode operation. The G1000 system
should be serviced.
HOLD EXPIRED – Holding EFC
Expect Further Clearance (EFC) time has expired
time expired.
for the User Defined Hold.
HW MISMATCH – GIA hardware
mismatch. GIA1 communication
halted.
A GIA mismatch has been detected, where only
HW MISMATCH – GIA hardware one is SBAS capable.
mismatch. GIA2 communication
halted.
Nav/Com/
XPDR/Audio
The GWX 68/GWX 70 has incorrect software
installed. The G1000 system should be serviced.
A failure has been detected in the GWX 68 or
GWX 70. The GWX 68 or GWX 70may still be
usable.
EAS
GWX MANIFEST – GWX software
mismatch, communication halted.
GWX SERVICE – GWX needs
service. Return unit for repair.
Comments
Flight
Instruments
Message
Message
GPS integrity is insufficient for the current phase
of flight.
Loss of GPS navigation due to insufficient/poor
satellite coverage.
Low Bank mode is active. Disengage to continue
approach.
Low Bank mode is active. Disengage to continue
RNP 1.0.
The GDU’s internal model cannot determine the
exact magnetic variance for geographic locations
near the magnetic poles. Displayed magnetic
course angles may differ from the actual magnetic
heading by more than 2°.
MFD1 CONFIG – MFD1 config
error. Config service req’d.
The MFD configuration settings do not match
backup configuration memory. The G1000 system
should be serviced.
The MFD is overheating and is reducing power
consumption by dimming the display. If problem
persists, the G1000 system should be serviced.
The MFD detected a failure in the navigation
database. Attempt to reload the navigation
database. If problem persists, the G1000 system
should be serviced.
The MFD detected a failure in the basemap
database.
The MFD detected a that the basemap database is
incompatible.
The MFD detected a failure in the terrain
database. Ensure that the terrain card is properly
inserted in display. Replace terrain card. If
problem persists, The G1000 system should be
serviced.
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
MFD1 COOLING – MFD1 has
poor cooling. Reducing power
usage.
MFD1 DB ERR – MFD1
navigation database error exists.
MFD1 DB ERR – MFD1 basemap
database error exists.
MFD1 DB ERR – MFD1 basemap
database is incompatible.
MFD1 DB ERR – MFD1 terrain
database error exists.
Index
Appendix
Comments
LOI – GPS integrity lost.
Crosscheck with other NAVS.
LOSS OF GPS NAVIGATION –
Poor Satellite Coverage.
LOW BANK ACTIVE – Disengage
for approach.
LOW BANK ACTIVE – Disengage
for RNP less than 1.0.
LRG MAG VAR – Verify all course
angles.
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
134
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
Comments
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
135
GPS Nav
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
AFCS
190-00708-07 Rev. B
Nav/Com/
XPDR/Audio
The terrain database is present on another LRU,
but is missing on the specified LRU.
The MFD detected a failure in the ChartView
database (optional feature). Ensure the data
card is properly inserted. Replace data card. If
problem persists, the system should be serviced.
MFD1 DB ERR – MFD1
The MFD detected a failure in the FliteCharts
FliteCharts database error exists. database (optional feature). Ensure the data
card is properly inserted. Replace data card. If
problem persists, the system should be serviced.
MFD1 DB ERR – MFD1 Airport
The MFD detected a failure in the Airport Directory
Directory database error exists.
database. Ensure the data card is properly inserted.
Replace data card. If problem persists, the system
should be serviced.
MFD1 DB ERR – MFD1 obstacle The MFD detected a failure in the obstacle
database error exists.
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
The G1000 system should be serviced.
MFD1 DB ERR – MFD1 obstacle The obstacle database is present on another LRU,
database missing.
but is missing on the specified LRU.
MFD1 DB ERR – MFD1 Safe Taxi The MFD detected a failure in the Safe Taxi
database error exists.
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
The G1000 system should be serviced.
MFD1 KEYSTK – MFD [key name] A key is stuck on the PFD and/or MFD bezel.
Key is stuck.
Attempt to free the stuck key by pressing it
several times. The G1000 system should be
serviced if the problem persists.
MFD1 MANIFEST – MFD1
The MFD has incorrect software installed. The
software mismatch,
G1000 system should be serviced.
communication halted.
MFD1 SERVICE – MFD1 needs
The MFD self-test has detected a problem. The
service. Return unit for repair.
G1000 system should be serviced.
EAS
MFD1 DB ERR – MFD1 terrain
database missing.
MFD1 DB ERR – MFD1 Chartview
database error exists.
Flight
Instruments
Message
Message
Comments
MFD1 VOLTAGE – MFD1 has low The MFD voltage is low. The G1000 system
voltage. Reducing power usage
should be serviced.
NAV1 MANIFEST – NAV1
software mismatch,
communication halted.
NAV1 RMT XFR – NAV1 remote
transfer key is stuck.
NAV1 SERVICE – NAV1 needs
service. Return unit for repair.
NAV2 MANIFEST – NAV2
software mismatch,
communication halted.
NAV2 RMT XFR – NAV2 remote
transfer key is stuck.
NAV2 SERVICE – NAV2 needs
service. Return unit for repair.
NAV DB UPDATED – Active
navigation database updated.
NON-MAG UNITS– Nonmagnetic NAV ANGLE display
units are active.
NON WGS84 WPT – Do not use
GPS for navigation to [xxxx]
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
136
The NAV1 has incorrect software installed. The
system should be serviced.
The remote NAV1 transfer switch is stuck in the
enabled (or “pressed”) state. Press the transfer
switch again to cycle its operation. If the problem
persists, the G1000 system should be serviced.
A failure has been detected in the NAV1 receiver.
The receiver may still be available. The G1000
system should be serviced.
The NAV2 has incorrect software installed. The
system should be serviced.
The remote NAV2 transfer switch is stuck in the
enabled (or “pressed”) state. Press the transfer
switch again to cycle its operation. If the problem
persists, the G1000 system should be serviced.
A failure has been detected in the NAV2 receiver.
The receiver may still be available. The G1000
system should be serviced.
System has updated the active navigation database
from the standby navigation database.
Navigation angle is not set to MAGNETIC at
power-up.
The position of the selected waypoint [xxxx]
is not calculated based on the WGS84 map
reference datum and may be positioned in error
as displayed. Do not use GPS to navigate to the
selected non-WGS84 waypoint.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
Comments
Flight
Instruments
Message
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
The PFD configuration settings do not match
backup configuration memory. The G1000 system
should be serviced.
PFD1 COOLING – PFD1 has poor The PFD is overheating and is reducing power
cooling. Reducing power usage. consumption by dimming the display. If problem
persists, the G1000 system should be serviced.
PFD1 DB ERR – PFD1 basemap
The PFD detected a failure in the basemap
database error exists.
database.
PFD1 DB ERR – PFD1 basemap
The PFD detected a that the basemap database is
database is incompatible.
incompatible.
PFD1 DB ERR – PFD1 navigation The PFD detected a failure in the navigation
database error exists.
database. Attempt to reload the navigation
database. If problem persists, the G1000 system
should be serviced.
PFD1 DB ERR – PFD1 obstacle
The PFD detected a failure in the obstacle
database error exists.
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
The G1000 system should be serviced.
PFD1 DB ERR – PFD1 obstacle
The obstacle database is present on another LRU,
database missing.
but is missing on the specified LRU.
PFD1 DB ERR – PFD1 Safe Taxi
The PFD detected a failure in the Safe Taxi
database error exists.
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
The G1000 system should be serviced.
PFD1 DB ERR – PFD1 terrain
The PFD detected a failure in the terrain database.
database error exists.
Ensure that the terrain card is properly inserted in
display. Replace terrain card. If problem persists,
The G1000 system should be serviced.
PFD1 DB ERR – PFD1 terrain
The terrain database is present on another LRU,
database missing.
but is missing on the specified LRU.
EAS
PFD1 CONFIG – PFD1 config
error. Config service req’d.
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
137
Message
Comments
PFD1 KEYSTK – PFD1 [key name] A key is stuck on the PFD and/or MFD bezel.
Key is stuck.
Attempt to free the stuck key by pressing it
several times. The G1000 system should be
serviced if the problem persists.
PFD1 MANIFEST – PFD1
The PFD has incorrect software installed. The
software mismatch,
G1000 system should be serviced.
communication halted.
[PFD1, PFD2, or MFD1] CARD 1 The SD card in the top card slot of the PFD or
ERR – Card 1 is invalid.
MFD contains invalid data.
[PFD1, PFD2, or MFD1] CARD
The SD card was removed from the top card slot
1 REM – Card 1 was removed.
of the PFD or MFD. The SD card needs to be
Reinsert card.
reinserted.
[PFD1, PFD2, or MFD1] CARD 2 The SD card in the bottom card slot of the PFD or
ERR – Card 2 is invalid.
MFD contains invalid data.
[PFD1, PFD2, or MFD1] CARD
The SD card was removed from the bottom card
2 REM – Card 2 was removed.
slot of the PFD or MFD. The SD card needs to be
Reinsert card.
reinserted.
PFD1 SERVICE – PFD1 needs
The PFD aself-test has detected a problem. The
service. Return unit for repair.
G1000 system should be serviced.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
138
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
Comments
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
139
GPS Nav
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
AFCS
190-00708-07 Rev. B
Nav/Com/
XPDR/Audio
The PFD1 voltage is low. The G1000 system
should be serviced.
The PFD configuration settings do not match
backup configuration memory. The G1000 system
should be serviced.
PFD2 COOLING – PFD2 has poor The PFD is overheating and is reducing power
cooling. Reducing power usage. consumption by dimming the display. If problem
persists, the G1000 system should be serviced.
PFD2 DB ERR – PFD2 basemap
The PFD detected a failure in the basemap
database error exists.
database.
PFD2 DB ERR – PFD2 basemap
The PFD detected a that the basemap database is
database is incompatible.
incompatible.
PFD2 DB ERR – PFD2 navigation The PFD detected a failure in the navigation
database error exists.
database. Attempt to reload the navigation
database. If problem persists, the G1000 system
should be serviced.
PFD2 DB ERR – PFD2 obstacle
The PFD detected a failure in the obstacle
database error exists.
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
The G1000 system should be serviced.
PFD2 DB ERR – PFD2 obstacle
The obstacle database is present on another LRU,
database missing.
but is missing on the specified LRU.
PFD2 DB ERR – PFD2 Safe Taxi
The PFD detected a failure in the Safe Taxi
database error exists.
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
The G1000 system should be serviced.
PFD2 DB ERR – PFD2 terrain
The PFD detected a failure in the terrain database.
database error exists.
Ensure that the terrain card is properly inserted in
display. Replace terrain card. If problem persists,
The G1000 system should be serviced.
PFD2 DB ERR – PFD2 terrain
The terrain database is present on another LRU,
database missing.
but is missing on the specified LRU.
EAS
PFD1 VOLTAGE – PFD1 has low
voltage. Reducing power usage
PFD2 CONFIG – PFD2 config
error. Config service req’d.
Flight
Instruments
Message
Message
Comments
PFD2 KEYSTK – PFD2 [key name] A key is stuck on the PFD bezel. Attempt to free
Key is stuck.
the stuck key by pressing it several times. The
G1000 system should be serviced if the problem
persists.
PF2 MANIFEST – PFD2 software The PFD has incorrect software installed. The
mismatch, communication halted. G1000 system should be serviced.
PFD2 SERVICE – PFD2 needs
The PFD self-test has detected a problem. The
service. Return unit for repair.
G1000 system should be serviced.
PFD2 VOLTAGE – PFD2 has low The PFD2 voltage is low. The G1000 system
voltage. Reducing power usage
should be serviced.
PTK FAIL – Parallel track
Bad parallel track geometry.
unavailable: bad geometry.
PTK FAIL – Parallel track
Invalid leg type for parallel offset.
unavailable: invalid leg type.
PTK FAIL – Parallel track
IAF waypoint for parallel offset has been passed.
unavailable: past IAF.
RAIM UNAVAIL – RAIM is not
GPS satellite coverage is insufficient to perform
available from FAF to MAP
Receiver Autonomous Integrity Monitoring (RAIM)
waypoints.
from the FAF to the MAP waypoints.
RECORDER SERVICE REQUIRED
The CVDR should be serviced.
- The CVDR needs service.
REGISTER CONNEXT – Data
The system is not registered with Garmin
services are inoperative, register
Connext, or its current registration data has failed
w/ Connext.
authentication.
SCHEDULER [#] – <message>.
SLCT FREQ – Select appropriate
frequency for approach.
SLCT MAG– Select MAGNETIC
NAV ANGLE display units.
Message criteria entered by the user.
The system notifies the pilot to load the approach
frequency for the appropriate NAV receiver. Select
the correct frequency for the approach.
The system notifies the pilot to set the Nav Angle
units on the Avioncs Settings Screen to Magnetic.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
140
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
Comments
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
The current vertical waypoint can not be reached
within the maximum flight path angle and vertical
speed constraints. The system automatically
transitions to the next vertical waypoint.
GPS Nav
UNABLE V WPT – Can’t reach
current vertical waypoint.
AFCS
One of the terrain, or obstacle databases required
for TAWS in the specified PFD or MFD is missing
or invalid.
The system notifies the pilot that the timer has
expired.
The G1000 is no longer receiving data from
the traffic system. The traffic device should be
serviced.
Nav/Com/
XPDR/Audio
TERRAIN DSP – [PFD1, PFD2 or
MFD1] Terrain awareness display
unavailable.
TIMER EXPIRD – Timer has
expired.
TRAFFIC FAIL – Traffic device has
failed.
EAS
SLCT NON-MAG– Select
The system notifies the pilot to set the Nav Angle
alternate NAV ANGLE display
units on the Avioncs Settings Screen to True.
units.
STEEP TURN – Steep turn ahead. A steep turn is 15 seconds ahead. Prepare to
turn.
STRMSCP FAIL – Stormscope has Stormscope has failed. The G1000 system should
failed.
be serviced.
SVT – SVT DISABLED: Out of
Synthetic Vision is disabled because the aircraft is
available terrain region.
not within the boundaries of the installed terrain
database.
SVT – SVT DISABLED: Terrain DB Synthetic Vision is disabled because a terrain
resolution too low.
database of sufficient resolution (9 arc-second or
better) is not currently installed.
SW MISMATCH – GDU software The MFD and PFDs have different software
version mismatch. Xtalk is off.
versions installed. The G1000 system should be
serviced.
Flight
Instruments
Message
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
141
Message
Comments
VNV – Unavailable. Excessive
track angle error.
VNV – Unavailable. Excessive
crosstrack error.
VNV – Unavailable. Parallel
course selected.
VNV – Unavailable. Unsupported
leg type in flight plan.
The current track angle error exceeds the limit,
causing the vertical deviation to go invalid.
The current crosstrack exceeds the limit, causing
vertical deviation to go invalid.
A parallel course has been selected, causing the
vertical deviation to go invalid.
The lateral flight plan contains a procedure turn,
vector, or other unsupported leg type prior to the
active vertical waypoint. This prevents vertical
guidance to the active vertical waypoint.
WPT ARRIVAL – Arriving at
waypoint -[xxxx]
WX ALERT – Possible severe
weather ahead.
Arriving at waypoint [xxxx], where [xxxx] is the
waypoint name.
The GWX 68/GWX 70 indicates severe weather
within ±10º of the aircraft heading at a range of
80 to 320 nm.
XPDR1 ADS-B FAIL – XPDR1
is unable to transmit ADS-B
messages.
ADS-B is inoperative. The transponder may not be
receiving a valid GPS position. Other transponder
functions may be available. Service when
possible.
The transponder configuration settings do not
match those of backup configuration memory.
The G1000 system should be serviced.
There is no communication with the #1
transponder.
The #1 transponder should be serviced when
possible.
ADS-B is inoperative. The transponder may not be
receiving a valid GPS position. Other transponder
functions may be available. Service when
possible.
XPDR1 CONFIG – XPDR1 config
error. Config service req’d.
XPDR1 FAIL – XPDR1 is
inoperative.
XPDR1 SRVC – XPDR1 needs
service. Return unit for repair.
XPDR2 ADS-B FAIL – XPDR2
is unable to transmit ADS-B
messages
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
142
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Annunciations & Alerts
XPDR2 CONFIG – XPDR2 config
error. Config service req’d.
GPS Nav
In some circumstances, some messages may appear in conjunction with others.
Description
Flight
Planning
Flight Plan Import/Export
Results
‘Flight plan partially imported.’
Some flight plan waypoints were successfully imported from
the SD card, however others had errors and were not imported.
A partial stored flight plan now exists in the system.
‘File contained user waypoints only.’
The file stored on the SD card did not contain a flight plan,
only user waypoints. One or more of these waypoints did not
import successfully.
‘Too many points. Flight plan truncated.’
The flight plan on the SD card contains more waypoints than
the system can support. The flight plan was imported with as
many waypoints as possible.
‘Some waypoints not loaded. Waypoints locked.’
The flight plan on the SD card contains one or more waypoints
that the system cannot find in the navigation database. The
flight plan has been imported, but must be edited within the
system before it can be activated for use.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
143
Index
Flight plan data was not successfully imported from the SD card.
Appendix
The SD card contains no flight plan data.
‘Flight plan import failed.’
Annun/
Alerts
‘No flight plan files found to import.’
Abnormal
Operation
The file stored on the SD card did not contain a flight plan,
only user waypoints. These waypoints have been saved to the
system user waypoints. No flight plans stored in the system
have been modified.
Additional
Features
‘File contained user waypoints only.
User waypoints imported successfully. No stored flight plan data was
modified.’
Hazard
Avoidance
A flight plan file stored on the SD card was successfully
imported as a stored flight plan.
Procedures
‘Flight plan successfully imported.’
190-00708-07 Rev. B
AFCS
FLIGHT PLAN IMPORT/EXPORT MESSAGES
Nav/Com/
XPDR/Audio
The transponder configuration settings do not
match those of backup configuration memory.
The G1000 system should be serviced.
There is no communication with the #2
transponder.
The #2 transponder should be serviced when
possible.
The MFD and PFDs are not communicating with
each other. The G1000 system should be serviced.
EAS
XPDR2 FAIL – XPDR2 is
inoperative.
XPDR2 SRVC – XPDR2 needs
service. Return unit for repair.
XTALK ERROR – A flight display
crosstalk error has occurred.
Comments
Flight
Instruments
Message
Flight Plan Import/Export
Results
‘User waypoint database full. Not all
loaded.’
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
The flight plan file on the SD card contains user waypoints.
The quantity of stored user waypoints has exceeded system
capacity, therefore not all the user waypoints on the SD card
have been imported. Any flight plan user waypoints that were
not imported are locked in the flight plan. The flight plan must
be edited within the system before it can be activated for use.
‘Flight plan successfully exported.’
The stored flight plan was successfully exported to the SD card.
‘Flight plan export failed.’
The stored flight plan was not successfully exported to the SD
card. The SD card may not have sufficient available memory or
the card may have been removed prematurely.
GDL 69/GDL 69A/GDL 69A SXM DATA LINK RECEIVER MESSAGES
Message
Message Location
Description
NO SIGNAL
XM Information Page Weather
Datalink Page (MFD)
Loss of signal; signal strength too low
for receiver
LOADING
XM Radio Page (MFD)
Acquiring channel audio or
information
OFF AIR
-------WEATHER DATA
LINK FAILED
ACTIVATION
REQUIRED
DETECTING
ACTIVATION
WAITING FOR
DATA...
XM Radio Page (MFD)
Channel not in service
XM Radio Page (MFD)
Missing channel information
Weather Datalink Page (MFD)
No communication from Data Link
Receiver within last 5 minutes
XM Information Page (MFD)
SiriusXM subscription is not activated
Weather Datalink Page (MFD)
SiriusXM subscription is activating.
Weather Datalink Page (MFD)
SiriusXM subscription confirmed
downloading weather data.
Index
Appendix
Description
‘One or more user waypoints renamed.’ One or more imported user waypoints were renamed when
imported due to naming conflicts with waypoints already
existing in the system.
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
144
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Appendix
Flight
Instruments
APPENDIX
PFD SOFTKEY MAP
EAS
Nav/Com/
XPDR/Audio
AFCS
Top Level PFD Softkeys
GPS Nav
PRECIP
or
STRMSCP NEXRAD
WX LGND
(optional)
DL LTNG
or
METAR
Select the BACK Softkey
to return to the top-level softkeys.
Hazard
Avoidance
TRFC-2
Level 2
Level 3
Additional
Features
Inset Map Softkeys
Level 1
Description
Selects desired amount of map detail; cycles
through declutter levels:
DCLTR (No Declutter): All map features
visible
DCLTR-1: Declutters land data
DCLTR-2: Declutters land and SUA data
DCLTR-3: Removes everything except the
active flight plan
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
145
Index
DCLTR (3)
Appendix
Removes Inset Map
Annun/
Alerts
OFF
Abnormal
Operation
Displays Inset Map in PFD lower left corner
INSET
Procedures
TRFC-1
Flight
Planning
(optional)
Level 1
Level 2
Level 3
TRAFFIC
Nav/Com/
XPDR/Audio
AFCS
TOPO
TERRAIN
Displays Stormscope weather and coverage
information on the Inset Map (optional)
Displays Connext precipitation on Inset Map
(optional with GSR 56)
GPS Nav
STRMSCP
Flight
Planning
PRECIP
or
Displays NEXRAD weather and coverage on
Inset Map (optional GDL 69A)
Displays SiriusXM lightning information on
Inset Map (optional)
Procedures
NEXRAD
XM LTNG
Hazard
Avoidance
or
Displays Connext Worldwide Weather
lightning information on Inset Map (optional)
Displays METAR flags on airport symbols
shown on the Inset Map (optional)
DL LTNG
Additional
Features
Description
Displays icon and age on the Inset Map for
the selected weather products (optional)
Cycles through traffic display options:
TRFC-1: Traffic displayed on inset map
TRFC-2: Traffic Map Page is displayed in
the inset map window
Displays topographical data (e.g.,
coastlines, terrain, rivers, lakes) and
elevation scale on Inset Map
Displays terrain information on Inset Map
WX LGND
EAS
Flight
Instruments
Appendix
Annun/
Alerts
Abnormal
Operation
METAR
ADC1
ADC2
BACK
AHRS2
MSG
Select the BACK Softkey to
return to the top level softkeys.
Appendix
Index
AHRS1
Sensor Softkeys
Level 1
SENSOR
146
Level 2
Level 3
Description
Displays softkeys for selecting the #1 and
#2 AHRS and Air Data Computers
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Appendix
Level 2
Level 3
Description
Selects the #1 Air Data Computer
ADC2
Selects the #2 Air Data Computer
AHRS1
Selects the #1 AHRS
AHRS2
Selects the #2 AHRS
EAS
ADC1
Flight
Instruments
Level 1
Nav/Com/
XPDR/Audio
ADF/DME
AFCS
SYN VIS
ALT UNIT
HSI FMT
GPS Nav
Select the BACK Softkey
to return to the top-level softkeys
Flight
Planning
METERS
BACK
ARC HSI
IN
Procedures
360 HSI
HPA
Hazard
Avoidance
Additional
Features
PATHWAY
SYN TERR HRZN HDG APTSIGNS
Abnormal
Operation
PFD Configuration Softkeys
Level 2
PFD
Level 3
Description
Annun/
Alerts
Level 1
Displays second-level softkeys for
additional PFD configurations
Appendix
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
147
Level 1
Level 2
Level 3
SYN VIS
PATHWAY
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Appendix
Flight
Planning
GPS Nav
AFCS
SYN TERR
DFLTS
Hazard
Avoidance
Procedures
WIND
Additional
Features
Appendix
Wind direction arrow with direction
and speed
Information not displayed
DME
Select to display the DME information
window
BRG1
Cycles the Bearing 1 Information
Window through NAV1 or GPS/
waypoint identifier and GPS-derived
distance information.
Displays the HSI formatting softkeys
Displays the HSI in a 360 degree format
Displays the HSI in an arc format
Annun/
Alerts
Abnormal
Operation
OFF
HSI FRMT
360 HSI
ARC HSI
Index
Displays the softkeys for enabling or
disabling Synthetic Vision features
Displays rectangular boxes representing
the horizontal and vertical flight path of
the active flight plan
Enables synthetic terrain depiction
HRZN HDG Displays compass heading along the
Zero-Pitch line
APTSIGNS Displays position markers for airports
within approximately 15 nm of the
current aircraft position. Airport
identifiers are displayed when the
airport is within approximately 9 nm.
Resets PFD to default settings, including
changing units to standard
Displays softkeys to select wind data
parameters
Wind direction arrows with headwind
OPTN 1
and crosswind components
Wind direction arrow and speed
OPTN 2
OPTN 3
148
Description
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Appendix
Level 2
Level 3
IN
Select to display the BARO setting as
inches of mercury
HPA
Select to display the BARO setting as
hectopacals
GPS Nav
When enabled, displays altimeter in
meters
AFCS
METERS
Nav/Com/
XPDR/Audio
ALT UNIT
EAS
Cycles the Bearing 2 Information
Window through NAV2 or GPS/
waypoint identifier and GPS-derived
distance information.
Displays softkeys for setting the altimeter
and BARO settings to metric units
BRG2
Sets altimeter setting to standard
barometric pressure
Flight
Planning
STD BARO
Description
Flight
Instruments
Level 1
Procedures
Hazard
Avoidance
MSG
Annun/
Alerts
Select the BACK Softkey to return
to the top-level softkeys.
Abnormal
Operation
MSG
Additional
Features
Select the BACK Softkey to return
to the top-level softkeys.
Transponder Softkeys
Appendix
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
149
Level 1
Level 2
Level 3
Description
ADF/DME
Displays the ADF/DME Tuning Window
XPDR
XPDR1
Displays transponder mode selection
softkeys
Selects the #1 transponder as active.
XPDR2
Selects the #2 transponder as active.
STBY
0—7
Selects Standby Mode (transponder does
not reply to any interrogations)
Selects Mode A (transponder replies to
interrogations)
Selects Mode C – Altitude Reporting Mode
(transponder replies to identification and
altitude interrogations)
Automatically enters the VFR code (1200 in
the U.S.A. only)
Displays transponder code selection
softkeys 0-7
Use numbers to enter code
BKSP
Removes numbers entered, one at a time
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Appendix
AFCS
ON
GPS Nav
ALT
Flight
Planning
VFR
Hazard
Avoidance
TMR/REF
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Displays Timer/References Window
NRST
Displays Nearest Airports Window
MSG
Displays Message Window
Index
Appendix
Annun/
Alerts
Abnormal
Operation
IDENT
Additional
Features
Procedures
CODE
150
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Appendix
or
CPDLC
CAS
DCLTR
MAP
(optional)
(optional)
SHW CHRT
CHKLIST
EAS
SYSTEM
Flight
Instruments
MFD SOFTKEY MAP
DCLTR-1
CAS↓
Nav/Com/
XPDR/Audio
CAS↑
DCLTR-2
DCLTR-3
PROFILE
TOPO
TERRAIN
AIRWAYS
(optional)
PRECIP
or
DL LTNG
or
NEXRAD
STRMSCP
XM LTNG
Select the BACK Softkey on this level
to return to the top softkey level.
(optional)
(optional)
(optional)
METAR
LEGEND
WX RADAR
BACK
GPS Nav
AIRWY ON
AFCS
TRAFFIC
(optional)
AIRWY LO
AIRWAY HI
SYSTEM
CPDLC
CPDLC
LOGON
MAP
LOGOFF
NEW
(TBM 900)
FMS LFE
+250 FT
-250 FT
DEL ALL
BACK
CHKLIST
(optional)
ELEC
+25 FT
FUEL
GEN
CHKLIST
-25 FT
ACCEPT
Procedures
(TBM 900)
MAN LFE
DELETE
Flight
Planning
(optional)
SYSTEM
BACK
Hazard
Avoidance
MFD Softkeys
Level 2
Description
Additional
Features
Level 1
Enables the Synoptics Page softkeys
SYSTEM
CAS
FUEL
Selects the Fuel Synoptics Page
GEN
Selects the General Synoptics Page
Appendix
Scroll up or down (Displayed only when a
sufficient number of items are displayed in
the Crew Alerting System Display to warrant
scrolling)
Selects the Electrical Synoptics Page
Annun/
Alerts
CAS ↑
and
CAS ↓
ELEC
Abnormal
Operation
or
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
151
Level 1
Nav/Com/
XPDR/Audio
LOGON
Displays Logon screen for the CPDLC system
LOGOFF
Displays Logoff screen for the CPDLC system
NEW
Accesses New CPDLC message screen
DELETE
Delete selected CPDLC message.
DEL ALL
Delete all CPDLC messages.
BACK
Returns display to previous softkey level
Enables second-level Navigation Map softkeys
TRAFFIC
Displays traffic information on Navigation Map
PROFILE
Displays/removes Profile View on Navigation
Map Page
Displays topographical data (e.g., coastlines,
terrain, rivers, lakes) and elevation scale on
Navigation Map
Displays terrain information on Navigation Map
Procedures
Flight
Planning
TOPO
TERRAIN
Abnormal
Operation
Additional
Features
Hazard
Avoidance
AIRWAYS
STRMSCP
Annun/
Alerts
PRECIP
or
NEXRAD
Displays airways on the map; cycles through the
following:
AIRWAYS: No airways are displayed
AIRWY ON: All airways are displayed
AIRWY LO: Only low altitude airways are
displayed
AIRWY HI: Only high altitude airways are
displayed
Displays Stormscope weather and coverage
information on Navigation Map (optional)
Displays Connext precipitation on Inset Map (optional
with GSR 56)
Displays NEXRAD weather and coverage on Inset Map
(optional GDL 69A)
Index
Appendix
Description
When available, accesses CPDLC softkeys.
MAP
GPS Nav
AFCS
Level 2
CPDLC
EAS
Flight
Instruments
Appendix
152
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Appendix
Level 2
XM LTNG
or
Description
Flight
Instruments
Level 1
Displays SiriusXM lightning information on the
Navigation Map (optional)
EAS
Displays Connext Worldwide Weather lightning
information on the Navigation Map (optional)
Displays METAR flags on airport symbols shown
METAR
on the Navigation Map (optional)
Displays the legend for the selected weather
LEGEND
products. Available only when NEXRAD, XM
LTNG, and/or METAR softkeys are selected.
WX RADAR Displays Color Weather Radar images on the
Navigation Map.
Returns to top-level softkeys
BACK
DL LTNG
GPS Nav
Procedures
Hazard
Avoidance
Additional
Features
Selects desired amount of map detail; cycles
through declutter levels:
DCLTR (No Declutter): All map features visible
DCLTR-1: Declutters land data
DCLTR-2: Declutters land and SUA data
DCLTR-3: Removes everything except the active
flight plan
When available, displays optional airport and
terminal procedure charts
When available, displays optional checklists
Flight
Planning
CHKLIST
AFCS
SHW CHRT
Nav/Com/
XPDR/Audio
DCLTR (3)
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
153
UPDATING DATABASES
CAUTION: Never disconnect power to the system when loading a database.
Power interruption during the database loading process could result in
maintenance being required to reboot the system.
EAS
Flight
Instruments
Appendix
NOTE: DO NOT use the database SD cards for any purpose other than database
storage.
In some cases it may be necessary to obtain an unlock code from Garmin in order
to make the database product functional. It may also be necessary to have the system
configured by a Garmin authorized service facility in order to use some database features.
If an error occurs during synchronization, an error message will be displayed,
followed by the affected display in the Sync Status section of the Database Window. If
synchronization completes on one display, but an error occurs on another, the error
message will be displayed with the affected displays listed after it. When an error message
is displayed, the problem must be corrected before synchronization can be completed.
A power cycle is required to restart synchronization when ‘Card Full’ or ‘Err’ is shown.
Error Message
Description
Canceled
Database synchronization has been canceled by removing the
bottom SD card in display being updated
Card Full
SD card does not contain sufficient memory
Err
Displayed for all other errors that may cause the synchronization
process to be halted
Timeout
System timed-out prior to the database transfer completing
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
NOTE: When loading database updates, the ‘DB Mismatch’ message will
be displayed until database synchronization is complete, followed by turning
system power off, then on. Synchronization can be monitored on the AUXSYSTEM STATUS Page.
154
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Appendix
1)
NOTE: Label the SD cards for each display.
3)
Put the Garmin SD Cards back in the bottom SD card slots of each flight
display unit.
4)
Turn the system ON.
5)
6)
During MFD power-up, check the MFD Power-Up screen and make sure that
the database is initialized and shown on the database information.
Press the ENT Key on MFD display to acknowledge the startup screen.
7)
Turn the large FMS Knob to select the AUX Page group on the MFD.
8)
Turn the small FMS Knob to select the System Status Page.
9)
Press the Display Database Selection Softkey to show database information
for each display. Verify the correct database cycle information is shown for
each display.
GPS Nav
Go to www.flygarmin.com. Download the applicable software and install
the databases on the Garmin SD card for each display. (The FliteChart
database must only be installed on the MFD SD Card).
Hazard
Avoidance
Additional
Features
Abnormal
Operation
10) Remove power from the system.
Annun/
Alerts
Updating ChartView Databases
2)
Go to www.jeppesen.com. Download the applicable software and
install the Chartview database on a blank SD card.
3)
Put the Garmin SD Card back in the bottom SD card slots of the MFD.
Index
With the system OFF, remove the Garmin SD Card from the bottom SD card
slot of the MFD.
Appendix
1)
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Procedures
displayed in the Messages window of the PFD.
Flight
Planning
NOTE: Make sure that no messages related to database errors are
190-00708-07 Rev. B
AFCS
2)
Nav/Com/
XPDR/Audio
With the system OFF, remove the Garmin SD Cards from the bottom SD card
slot of each flight display unit.
EAS
These databases may be copied to one Supplemental Data Card, then automatically
synchronized to other card in the system:
Flight
Instruments
Updating Basemap, FliteCharts, SafeTaxi, Airport Terrain, Obstacle, and
Airport Directory Databases
155
4)
Apply power to the system and press the ENT Key on the MFD display to
acknowledge the startup screen.
5)
Turn the large FMS Knob to select the AUX Page group on the MFD.
6)
Turn the small FMS Knob to select the System Status Page.
7)
Press the Display Database Selection Softkey to show database information
for MFD (MFD1 DB). Use the FMS knob to select the ChartView Database
field and verify the correct database cycle information is shown.
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Appendix
NOTE: Make sure that no messages related to database errors are
AFCS
displayed in the Messages window of the PFD.
Remove power from the system.
Loading the Navigation Database as the Active Navigation Database
The Navigation Database that is loaded to internal memory as the active database
will be used by the system.
NOTE: Loading the Jeppesen Navigation Database as the active database
prior to its effective date will result in the expiration date on the power-up
screen and the effective date on the AUX-System Status Page being displayed
in yellow.
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
8)
1)
With the system OFF, insert the SD card containing the new navigation database
version into the top card slot of the display (PFD1, PFD2 or MFD) to be updated
(label of SD card facing left).
2)
Turn the system ON. A prompt is displayed in the upper left corner of the
display:
3)
Press the NO Softkey to proceed to loading the active database.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
NOTE: After the navigation database is loaded or copied, the top SD card
may be removed.
156
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Appendix
5)
After the update completes, the display starts in normal mode.
6)
Turn the system OFF and remove the SD card from the top card slot.
7)
Repeat steps 1 through 6 for the other displays (PFD1, PFD2 or MFD).
8)
Apply power to the system and press the ENT Key to acknowledge the startup
screen.
9)
Turn the large FMS Knob to select the AUX Page group on the MFD.
EAS
A prompt similar to the following is displayed. Press the YES Softkey to update
the active navigation database.
Flight
Instruments
4)
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Procedures
Hazard
Avoidance
11) Press the Display Database Selection Softkey to show active navigation
database information for each display (MFD1 DB, PFD1 DB, PFD2 DB). Verify
the correct active navigation database cycle information is shown for each
display.
Flight
Planning
10) Turn the small FMS Knob to select the System Status Page.
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
157
Loading the Navigation Database as the Standby Navigation Database
The purpose of the Standby Navigation Database is to allow the loading of the
next cycle of the Navigation Database to the bottom SD card, prior to its effective
date.
NOTE: After the navigation database is loaded or copied, the top SD card
may be removed.
1)
With the system OFF, insert the SD card containing the new navigation
database version into the top card slot of the MFD.
2)
Verify that an SD card is inserted in the bottom slot of each PFD and the
MFD.
3)
Turn the system ON. A prompt similar to the following is displayed.
4)
Press the YES Softkey. The navigation database is copied to the SD card in
the bottom card slot of the MFD.
5)
After the navigation database files are copied to the bottom SD card, the
display will appear as shown in the following figure.
6)
As instructed on the display, press any key to continue. The display will now
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Appendix
158
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Appendix
Flight
Instruments
appear as shown in the following figure.
EAS
8)
Press the NO Softkey. The display now starts in normal mode. Since the
database effective date is not yet valid, it should not be loaded as the
active database. The display now starts in normal mode. Do not remove
power while the display is starting.
9)
Press the ENT Key to acknowledge the startup screen.
AFCS
Press any key to continue. The display will now appear as shown in the
following figure.
Nav/Com/
XPDR/Audio
7)
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
11) Turn the small FMS Knob to select the System Status Page.
Abnormal
Operation
13) Turn system power OFF.
14) Remove the SD card from the top card slot of the MFD.
15) Turn system power ON.
Annun/
Alerts
16) Press the ENT Key to acknowledge the startup screen.
17) Turn the large FMS Knob to select the AUX Page group on the MFD.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
159
Index
19) Press the Display Database Selection Softkey to show standby navigation
database information for each display (MFD1 DB, PFD1 DB, PFD2 DB).
Verify the correct standby navigation database cycle information is shown
for each display.
Appendix
18) Turn the small FMS Knob to select the System Status Page.
190-00708-07 Rev. B
Additional
Features
12) The new database is copied to the SD card in the bottom card slot of each
PFD. Progress can be monitored in the SYNC STATUS field. When copying
is finished, ‘Complete’ is displayed.
Appendix
Standby Nav Database Activation Confirmation Window
Loading the magnetic field variation database update:
A copy of the current magnetic field variation database (MV DB) is included with
the navigation database. At startup, the system compares this version of the MV
DB with that presently being used by each AHRS (GRS1 and GRS2). If the system
determines the MV DB needs to be updated, a prompt is displayed on the Navigation
Map Page, as shown in the following figure.
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
To manually activate the standby navigation database:
1) From the AUX-SYSTEM STATUS Page, select the STANDBY DB Softkey.
2) A prompt similar to the following figure below is displayed, select ‘Yes’
to overwrite the Active Navigation Database with the Standby Navigation
Database. Select ‘No’ to cancel.
Index
Appendix
GRS1 Magnetic Field Variation Database Update Prompt
160
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Appendix
With ‘OK’ highlighted, press the ENT Key on the MFD. A progress monitor
is displayed.
Flight
Instruments
1)
EAS
Nav/Com/
XPDR/Audio
AFCS
Uploading Database to GRS1
GPS Nav
2)
When the upload is complete, the prompt for the next GRS upload is
displayed.
Flight
Planning
Procedures
Hazard
Avoidance
GRS2 Magnetic Field Variation Database Update Prompt
With ‘OK’ highlighted, press the ENT Key on the MFD. A progress monitor
is displayed. When the upload is complete, the system is ready for use.
Additional
Features
3)
Abnormal
Operation
Annun/
Alerts
Appendix
Uploading Database to GRS2
Index
190-00708-07 Rev. B
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
161
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Appendix
Blank Page
162
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Index
Nav/Com/
XPDR/Audio
D
AFCS
Data link communication 15
Data Link Receiver 144
DB Mismatch 154
DCLTR Softkey 76
Dead Reckoning 104
Declutter 104, 145, 153
Designated altitudes 28
Differential cabin pressure 5, 11
Warning 109
Direct-to 25
DME 13, 14
Door status 10
DR mode 104, 105, 106
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
E
B
F
Index-1
Index
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Appendix
Flap position 5
Asymmetrical deflection warning 109
Flight Director 21
Flight ID 13
Flight path marker 75
Flight Stream 101
FliteCharts® 76, 77
Frequency Transfer 14
Annun/
Alerts
Cabin pressure altitude 5, 11
Warning 109
CDI 1, 2, 14
Abnormal
Operation
C
Edit a flight plan 41
Enable Terrain 66, 67
Engine display 5
Essential bus voltage 5
Additional
Features
Barometric Altitude Minimums 3
Battery
Alerts 110
Current 5
Overheat warning 109
Voltage 5
Bearing line 70, 71
Bluetooth 101, 102
190-00708-07 Rev. B
EAS
Activate a flight plan 26
Active Channel 79
Active database 156
Active Navigation Database 156
ADF 13, 14, 104
AHRS 121, 127, 130, 133, 146, 147
Air Data Computer 112
Airport Signs 75, 76
Airways 152
ALT 64
Altimeter setting 1, 104
Altitude mode 64
Altitude volume 64
Antenna stabilization 72
Antenna Tilt 70, 74
AOPA’s Airport Directory 78
ATC 15, 16, 17
Attitude & Heading Reference System
112
Audio panel controls
NAV1, NAV2 14
Cell 51, 52
Cell mode 52
Channel Presets 80
ChartView 76, 77
Code selection softkeys 14
COM 14, 103
CPDLC 15, 16, 17, 18, 152
Flight
Instruments
A
Fuel
Alerts 109–110
Flow 5
Pressure 5
Quantity 5
G
Gain 71
Garmin Pilot 101
Generator
Current 5
Speed 5
Ground mapping 71
H
Horizon heading 75
Horizontal Scan 70, 74
I
Inhibit 66, 68
Inhibit TAWS 68
Inhibit Terrain 66
Inset Map 145, 146, 153
Interturbine Temperature (ITT) 5
Warning 109
IOI 113, 114, 115, 116
Iridium satellite network 81, 85
M
Map panning 53
Message dialogs 18
Messages window 97
METAR 53
Minimums 118
MISCOMP 111
Mode selection softkeys 14
Multi Function Display (MFD)
Softkeys 151
N
NAV 14
NAV1 2, 14
NAV2 2, 14
Navigation database 27, 28
NEXRAD 53, 146, 152
NO COMP 111
O
Jeppesen 77
OBS 2
Obstacles 124, 133
Oil, engine
Alerts 109
Pressure 5
Temperature 5
Overspeed Protection 22
Oxygen
Pressure 5, 11
Warning 109
L
P
Landing Field Elevation 11
LFE 11, 12
Lightning 51, 52
Pairing 101
Pathways 75, 76
Predefined message 88, 89
Propeller speed 5
J
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Index
Index-2
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Index
AFCS
V
GPS Nav
Vertical speed guidance 28
Vertical track 118
Video settings 94
VNV 25, 104, 142
Vspeed 3
Flight
Planning
Procedures
W
Abnormal
Operation
T
Annun/
Alerts
Index
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
Appendix
TA 118
TAF 53
TAS 64, 118, 120, 121
TAWS 67, 68, 115
TAWS-B 67
Telephone 81, 84, 86, 88, 89
Terrain 65, 67, 125, 146, 152
Terrain-SVT 65, 66, 67
190-00708-07 Rev. B
Additional
Features
WATCH® 72
Waypoint Selection Submenu 36
Weather Attenuated Color Highlight 72
Weather data link page 53
Weather radar 69
Wind data 148
Hazard
Avoidance
SafeTaxi® 76
SBAS 22, 46, 67, 68, 105, 121, 133
Scheduler 95
SD Card 37, 44, 99, 100, 143, 144,
154, 156, 157, 158, 159
Sector scan 71
Sensor 111, 112
SiriusXM lightning 146, 153
SiriusXM Weather 53
SMS 81
STAB 72
Standby 69
Standby Navigation Database 158,
159, 160
Store Flight Plan 41
Stormscope lightning data 51, 52
Strike 51
Strike mode 52
Supplemental Data Card 155
SVT 75, 141
Synchronization 154
Nav/Com/
XPDR/Audio
S
EAS
Response/Request 17
Reversionary Mode 103
EICAS 5
ROC 113, 114, 115, 116
Text message 87, 88, 90
Text messaging 86
Tilt line 70
Timer 2
Topographical data 146, 152
Torque 5
Warning 109
Traffic 51, 63, 152
Traffic Advisory 63, 118
Traffic map page 63, 64, 65
Transponder 13, 14, 150
Trim 5
Flight
Instruments
R
Index-3
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Index
Blank Page
Index-4
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-07 Rev. B
Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p: 913.397.8200 f: 913.397.8282
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
p: 503.391.3411 f: 503.364.2138
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
p: 44/023.8052.4000 f: 44/023.8052.4004
Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p: 886/2.2642.9199 f: 886/2.2642.9099
www.garmin.com
© 2007, 2009-2011, 2014-2016 Garmin Ltd. or its subsidiaries
190-00708-07 Rev. B
Was this manual useful for you? yes no
Thank you for your participation!

* Your assessment is very important for improving the work of artificial intelligence, which forms the content of this project

Download PDF

advertising