Garmin TBM850 GPS Receiver User Manual

G1000
®
Integrated Flight Deck
Cockpit Reference Guide
System Software 0719.06 or later
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 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0719.06 or later for the Socata TBM
850. 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: 913/397.8200
Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: 503/391.3411
Fax 503/364.2138
Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park,
Southampton, SO40 9RB, U.K.
Tel: 44/0870.8501241
Fax: 44/0870.8501251
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: 886/02.2642.9199
Fax: 886/02.2642.9099
Web Site Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted,
disseminated, downloaded or stored in any storage medium, for any purpose without the express
written permission of Garmin. Garmin hereby grants permission to download a single copy of this
manual and of any revision to this manual onto a hard drive or other electronic storage medium to
be viewed for personal use, provided that such electronic or printed copy of this manual or revision
must contain the complete text of this copyright notice and provided further that any unauthorized
commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin® and G1000® are registered trademarks of Garmin Ltd. or its subsidiaries. WATCH®,
FliteCharts®, and SafeTaxi® are trademarks of Garmin Ltd. or its subsidiaries. These trademarks may
not be used without the express permission of Garmin.
NavData® is a registered trademark of Jeppesen, Inc.; Stormscope® and SkyWatch® are registered
trademarks of L-3 Communications; and XM® is a registered trademark of XM Satellite Radio, Inc.
May, 2009
190-00708-02 Rev. A
Printed in the U.S.A.
Warnings, Cautions & Notes
WARNING: Navigation and terrain separation must NOT be predicated upon
the use of the terrain avoidance feature. The terrain avoidance feature is NOT
intended to be used as a primary reference for terrain avoidance and does
not relieve the pilot from the responsibility of being aware of surroundings
during flight. The terrain avoidance feature is only to be used as an aid for
terrain avoidance. Terrain data is obtained from third party sources. Garmin
is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory
in nature and should not be relied upon as the sole source of obstacle and
terrain avoidance information. Always refer to current aeronautical charts
for appropriate minimum clearance altitudes.
WARNING: The altitude calculated by G1000 GPS receivers is geometric
height above Mean Sea Level and could vary significantly from the altitude
displayed by pressure altimeters, such as the GDC 74B Air Data Computer,
or other altimeters in the aircraft. GPS altitude should never be used for
vertical navigation. Always use pressure altitude displayed by the G1000
PFD or other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in
the G1000 system must be updated regularly in order to ensure that the
information remains current. Pilots using any outdated database do so
entirely at their own risk.
WARNING: Do not use basemap (land and water data) information for
primary navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING: Traffic information shown on system displays is provided as an
aid in visually acquiring traffic. Pilots must maneuver the aircraft based only
upon ATC guidance or positive visual acquisition of conflicting traffic.
WARNING: Use of the Stormscope is not intended for hazardous weather
penetration (thunderstorm penetration). Stormscope information, as
displayed on the G1000 MFD, is to be used only for weather avoidance, not
penetration.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Warnings, Cautions & Notes
WARNING: XM Weather should not be used for hazardous weather
penetration. Weather information provided by the GDL 69A is approved only
for weather avoidance, not penetration.
Warning: NEXRAD weather data is to be used for long-range planning
purposes only. Due to inherent delays in data transmission and the relative
age of the data, NEXRAD weather data should not be used for short-range
weather avoidance.
WARNING: The Garmin G1000, as installed in the Socata TBM 850 aircraft, has
a very high degree of functional integrity. However, the pilot must recognize
that providing monitoring and/or self-test capability for all conceivable system
failures is not practical. Although unlikely, it may be possible for erroneous
operation to occur without a fault indication shown by the G1000. It is
thus the responsibility of the pilot to detect such an occurrence by means of
cross-checking with all redundant or correlated information available in the
cockpit.
WARNING: For safety reasons, G1000 operational procedures must be learned
on the ground.
WARNING: The United States government operates the Global Positioning
System and is solely responsible for its accuracy and maintenance. The GPS
system is subject to changes which could affect the accuracy and performance
of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a
precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs,
information presented by the G1000 can be misused or misinterpreted and,
therefore, become unsafe.
WARNING: To reduce the risk of unsafe operation, carefully review and
understand all aspects of the G1000 Pilot’s Guide documentation and the
Socata TBM 850 Airplane Flight Manual. Thoroughly practice basic operation
prior to actual use. During flight operations, carefully compare indications
from the G1000 to all available navigation sources, including the information
from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always
resolve any discrepancies before continuing navigation.
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Warnings, Cautions & Notes
WARNING: The illustrations in this guide are only examples. Never use
the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory
Circular, Subject: Thunderstorms, and the Aeronautical Information Manual
(AIM) recommend avoiding “by at least 20 miles any thunderstorm identified
as severe or giving an intense radar echo.”
WARNING: Lamp(s) inside this product may contain mercury (HG) and must
be recycled or disposed of according to local, state, or federal laws. For
more information, refer to our website at www.garmin.com/aboutGarmin/
environment/disposal.jsp.
WARNING: Because of anomalies in the earth’s magnetic field, operating
the G1000 within the following areas could result in loss of reliable attitude
and heading indications. North of 70° North latitude and south of 70° South
latitude. An area north of 65° North latitude between longitude 75º West
and 120º West. An area south of 55° South latitude between longitude 120º
East and 165º East.
CAUTION: The PFD and MFD displays use a lens coated with a special
anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive
cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTIREFLECTIVE COATING. It is very important to clean the lens using a clean,
lint-free cloth and an eyeglass lens cleaner that is specified as safe for antireflective coatings.
CAUTION: The Garmin G1000 does not contain any user-serviceable parts.
Repairs should only be made by an authorized Garmin service center.
Unauthorized repairs or modifications could void both the warranty and the
pilot’s authority to operate this device under FAA/FCC regulations.
nOTE: All visual depictions contained within this document, including screen
images of the G1000 panel and displays, are subject to change and may not
reflect the most current G1000 system and aviation databases. Depictions
of equipment may differ slightly from the actual equipment.
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.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Warnings, Cautions & Notes
NOTE: The data contained in the terrain and obstacle databases comes from
government agencies. Garmin accurately processes and cross-validates the
data, but cannot guarantee the accuracy and completeness of the data.
NOTE: This product, its packaging, and its components contain chemicals
known to the State of California to cause cancer, birth defects, or reproductive
harm. This notice is being provided in accordance with California’s Proposition
65. If you have any questions or would like additional information, please
refer to our web site at www.garmin.com/prop65.
NOTE: Interference from GPS repeaters operating inside nearby hangars can
cause an intermittent loss of attitude and heading displays while the aircraft
is on the ground. Moving the aircraft more than 100 yards away from the
source of the interference should alleviate the condition.
NOTE: Use of polarized eyewear may cause the flight displays to appear dim
or blank.
NOTE: The purpose of this Cockpit Reference Guide is to provide the pilot
a resource with which to find operating instructions on the major features
of the G1000 system more easily. It is not intended to be a comprehensive
operating guide. Complete operating procedures for the system are found
in the G1000 Pilot’s Guide for this aircraft.
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Warnings, Cautions & Notes
Blank Page
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Record of Revisions
Part Number
190-00708-00
Change Summary
Initial Release
190-00708-01
Rev A
Added SVS and other GDU 9.02 parameters.
Rev B
190-00708-02
Clerical changes
Added temporary user waypoints
Added import/export flight plans
Added CDI availability during Dead Reckoning mode
Added GDU 9.14 parameters.
Revision Date of Revision Affected Pages
A
May, 2009
All
190-00708-02 Rev. A
Description
Production release
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
RR-1
Record of Revisions
Blank Page
RR-2
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Table of Contents
Flight Instruments. ............................................................................................................... 1
Selecting the Altimeter Barometric Pressure Setting....................................................... 1
Selecting Standard Barometric Pressure.............................................................................. 1
Change Altimeter Barometric Pressure Setting Units....................................................... 1
Synchronizing the Altimeter Barometric Pressure Settings............................................ 1
Synchronize CDI......................................................................................................................... 1
Change Navigation Sources.................................................................................................... 2
Enable/Disable OBS Mode While Navigating with GPS..................................................... 2
Generic Timer.............................................................................................................................. 2
Configure Vspeed Bugs............................................................................................................. 2
Set Barometric/Radar Altimeter Minimum Descent Altitude.......................................... 3
Testing the Radar Altimeter.................................................................................................... 3
Displaying Wind Data............................................................................................................... 3
Changing HSI Format................................................................................................................ 4
Engine & Airframe Systems............................................................................................. 5
Electrical System........................................................................................................................ 6
Fuel System................................................................................................................................. 8
General Systems........................................................................................................................ 9
Nav/Com/Transponder/Audio Panel....................................................................... 11
Enter or Change Flight ID...................................................................................................... 11
ADF Tuning (Optional)............................................................................................................. 11
DME Tuning............................................................................................................................... 11
Enter a Transponder Code..................................................................................................... 12
Selecting a COM Radio........................................................................................................... 12
Selecting a NAV Radio............................................................................................................ 12
NAV/COM Tuning...................................................................................................................... 12
Intercom..................................................................................................................................... 13
Passenger Address (PA) System............................................................................................ 13
Clearance Recorder and Player............................................................................................ 13
Automatic Flight Control System........................................................................... 15
Flight Director Activation...................................................................................................... 15
Vertical Modes.......................................................................................................................... 16
Lateral Modes........................................................................................................................... 17
GPS Navigation......................................................................................................................... 19
Direct-to Navigation............................................................................................................... 19
Activate a Stored Flight Plan................................................................................................ 20
Activate a Flight Plan Leg...................................................................................................... 20
Stop Navigating a Flight Plan............................................................................................... 21
Vertical Navigation (VNAV)................................................................................................... 21
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
i
Table of Contents
Flight Planning....................................................................................................................... 23
Weight Planning....................................................................................................................... 23
Trip Planning............................................................................................................................. 23
Create a New User Waypoint Defined by Latitude & Longitude.................................. 25
Create a New User Waypoint Defined by Radials from Other Waypoints.................. 26
Create a New User Waypoint Defined by a Radial & Distance from Another
Waypoint................................................................................................................................ 28
Delete a User Waypoint.......................................................................................................... 29
Create a New Flight Plan....................................................................................................... 30
Import a Flight Plan from an SD Card................................................................................. 31
Insert a Waypoint in the Active Flight Plan....................................................................... 31
Enter an Airway in a Flight Plan........................................................................................... 32
Invert An Active Flight Plan................................................................................................... 33
Remove a Departure, Arrival, Approach, or Airway from a Flight Plan...................... 33
Store a Flight Plan................................................................................................................... 34
Edit a Stored Flight Plan........................................................................................................ 34
Delete a Waypoint from the Flight Plan............................................................................. 34
Invert and Activate a Stored Flight Plan............................................................................ 35
Copy a Flight Plan.................................................................................................................... 35
Delete a Flight Plan................................................................................................................. 35
Graphical Flight Plan Creation.............................................................................................. 36
Export a Flight Plan to an SD Card...................................................................................... 36
Procedures................................................................................................................................. 37
Load and Activate a Departure Procedure........................................................................ 37
Activate A Departure Leg...................................................................................................... 37
Load An Arrival Procedure..................................................................................................... 37
Activate An Arrival Leg.......................................................................................................... 38
Load and/or Activate an Approach Procedure.................................................................. 38
Activate An Approach in the Active Flight Plan................................................................ 39
Activate a Vector to Final Approach Fix............................................................................. 39
Activate A Missed Approach in the Active Flight Plan.................................................... 40
Hazard Avoidance................................................................................................................. 41
Customizing the Hazard Displays on the Navigation Map............................................. 41
STORMSCOPE® (Optional)..................................................................................................... 41
XM Weather (Optional)........................................................................................................... 43
Traffic Systems......................................................................................................................... 44
Terrain And Obstacle Proximity............................................................................................ 46
Terrain-SVS................................................................................................................................ 47
Terrain Awareness & Warning System (TAWS) Display.................................................... 49
Airborne Color Weather Radar............................................................................................. 50
ii
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Table of Contents
Additional Features............................................................................................................ 55
Synthetic Vision........................................................................................................................ 55
Terminal Procedure Charts.................................................................................................... 56
XM® Radio Entertainment..................................................................................................... 58
Abnormal Operation.......................................................................................................... 61
Reversionary Mode................................................................................................................. 61
Abnormal COM Operation..................................................................................................... 61
Hazard Displays with Loss of GPS Position........................................................................ 61
Unusual Attitudes.................................................................................................................... 62
Dead Reckoning....................................................................................................................... 63
Annunciations & Alerts................................................................................................... 65
CAS Messages........................................................................................................................... 65
Comparator Annunciations.................................................................................................... 68
Reversionary Sensor Annunciations.................................................................................... 68
AFCS Alerts................................................................................................................................ 69
Terrain-SVS Alerts.................................................................................................................... 70
Terrain-SVS System Status Annunciations......................................................................... 71
TAWS Alerts............................................................................................................................... 71
Voice Alerts............................................................................................................................... 73
MFD & PFD Message Advisories........................................................................................... 74
Database Message Advisories.............................................................................................. 75
GMA 1347D Message Advisories.......................................................................................... 78
GIA 63W Message Advisories................................................................................................ 79
GEA 71 Message Advisories................................................................................................... 82
GTX 33/33D Message Advisories........................................................................................... 82
GRS 77 Message Advisories................................................................................................... 83
GMU 44 Message Advisories................................................................................................. 85
GDL 69A Message Advisories................................................................................................ 85
GWX 68 Alert Messages.......................................................................................................... 86
GDC 74B Message Advisories................................................................................................ 86
GCU 475 Message Advisories................................................................................................ 87
GMC 710 Message Advisories............................................................................................... 87
Miscellaneous Message Advisories...................................................................................... 88
Flight Plan Import/Export Messages................................................................................... 92
Appendix........................................................................................................................................ 93
PFD Softkey Map..................................................................................................................... 93
MFD Softkey Map.................................................................................................................... 98
Index..........................................................................................................................................Index-1
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
iii
Table of Contents
Blank Page
iv
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
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
1) Select the PFD Softkey to display the second-level softkeys.
Or:
Select the HPA Softkey to display the barometric pressure setting in
hectopascals.
Procedures
Flight
Planning
3) Select the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
GPS Nav
2) Select the ALT UNIT Softkey.
4) Select the BACK Softkey to return to the top-level softkeys.
Hazard
Avoidance
Synchronizing the Altimeter Barometric Pressure Settings
Additional
Features
1) Select the AUX-SYSTEM SETUP Page on the MFD.
2) Press the FMS Knob to activate the cursor.
Abnormal
Operation
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.
Annun/
Alerts
Synchronize CDI
1) Select the AUX-SYSTEM SETUP Page on the MFD.
Appendix
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window.
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Index
4) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
1
Change Navigation Sources
1) Select the CDI Softkey to change from GPS to VOR1 or LOC1. This places
the light blue tuning box over the NAV1 standby frequency in the upper left
corner of the PFD.
EAS
Flight
Instruments
Flight Instruments
3) Select the CDI Softkey a third time to return to GPS.
Enable/Disable OBS Mode While Navigating with GPS
1) Select the OBS Softkey to select OBS Mode.
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
2) Select the CDI Softkey again to change from VOR1 or LOC1 to VOR2
or LOC2. This places the light blue tuning box over the NAV2 standby
frequency.
3) Select the OBS Softkey again to disable OBS Mode.
Generic Timer
1) Select the TMR/REF Softkey, then turn the large FMS Knob to select the
time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then
press the ENT Key. The UP/DOWN field is now highlighted.
Hazard
Avoidance
Procedures
Flight
Planning
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.
Additional
Features
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.
Configure Vspeed Bugs
1) Select the TMR/REF Softkey.
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
Appendix
Annun/
Alerts
Abnormal
Operation
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
speed has been changed from a default value, an asterisk appears next to
the speed).
2
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Flight Instruments
Flight
Instruments
4) 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.
EAS
6) To remove the window, press the CLR Key or the TMR/REF Softkey.
Set Barometric/Radar Altimeter Minimum Descent Altitude
Nav/Com/
XPDR/Audio
1) Press the TMR/REF Softkey.
AFCS
2) Turn the large FMS Knob to highlight the OFF/BARO/RAD ALT field to the
right of ‘Minimums’.
3) Turn the small FMS Knob clockwise to select BARO or RAD ALT.
GPS Nav
4) Press the ENT Key.
5) Use the small FMS Knob to enter the desired altitude.
Flight
Planning
6) Press the ENT Key.
7) To remove the window, press the CLR Key or the TMR/REF Softkey.
Procedures
Testing the Radar Altimeter
1) Select the AUX-SYSTEM STATUS Page on the MFD.
Hazard
Avoidance
2) Select the RA TEST Softkey. The Radar Altitude window displays 50 feet,
indicating a properly functioning system.
Additional
Features
3) Selecting the RA TEST Softkey again, or exiting the System Status Page
cancels the test.
Displaying Wind Data
2) Select the WIND Softkey to display wind data below the Selected Heading.
Annun/
Alerts
3) Select one of the OPTN softkeys to change how wind data is displayed.
Abnormal
Operation
1) Select the PFD Softkey.
4) To remove the Wind Data Window, select the OFF Softkey.
Appendix
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
3
Flight
Instruments
Flight Instruments
Changing HSI Format
1) Press the PFD Softkey.
EAS
2) Press the HSI FRMT Softkey.
3) Press the 360 HSI Softkey to display the full size HSI.
Nav/Com/
XPDR/Audio
Or:
Press the ARC HSI Softkey to display the arc style HSI.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
4
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Engine & Airframe Systems
1
Flight
Instruments
Engine & Airframe Systems
1
EAS
8
Nav/Com/
XPDR/Audio
2
2
9
10
11
3
AFCS
3
GPS Nav
4
4
12
14
Flight
Planning
13
5
5
15
7
17
17
8
9
Hazard
Avoidance
16
Procedures
6
6
12
Additional
Features
13
15
Abnormal
Operation
16
EIS Display (Normal Mode)
EIS Display (Reversionary Mode)
13 Fuel Flow
2 Propeller Speed
8 Cabin Pressure Altitude and
14 Fuel Pressure
Appendix
7 CAS Display
Annun/
Alerts
1 Torque
3 Generator Speed
Change Rate
9 Differential Pressure
4 Interturbine Temperature
10 Selected Cabin Altitude
16 Battery and Essential Bus
5 Oil Pressure
11 Oxygen Pressure
17 Elevator, Aileron, and
6 Oil Temperature
12 Fuel Quantity
Currents
Voltages
Index
190-00708-02 Rev. A
15 Battery and Generator
Rudder Trim and Flap
Position
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
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
190-00708-02 Rev. A
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
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
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
6
Right Fuel Tank
Index
Appendix
Annun/
Alerts
Fuel Synoptics Page
8
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Engine & Airframe Systems
Right
Fuel Tank
Selected
Unknown
Fuel Tank
Selection
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
Fuel Selector Status
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
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)
• Light blue indicates heat has been selected (windshield)
• Green indicates heat is on
• Yellow indicates heat has failed (propeller, pitot tube, and stall sensor).
Procedures
1) Select the SYSTEM Softkey to display the softkeys for the synoptics system.
2) Select the GEN Softkey to display the Fuel System Page.
Flight
Planning
General Systems
GPS Nav
If the auxiliary fuel boost pump is on, the symbol is displayed in green. The mode,
automatic (AUTO) or manual (MAN) is displayed next to the pump symbol. If the
boost pump is off, the symbol is shown in light blue (automatic mode) or red (manual
mode).
Appendix
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
9
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Engine & Airframe Systems
General Synoptics Page
10
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Nav/Com/XPDR/Audio Panel
Flight
Instruments
Nav/Com/Transponder/Audio Panel
Enter or Change Flight ID
3) Turn the large FMS Knob to select the next field.
AFCS
4) Turn the small FMS Knob to enter the next desired character.
Nav/Com/
XPDR/Audio
2) Turn the small FMS Knob to enter the first character.
EAS
1) Press the TMR/REF Softkey, then turn the large FMS Knob to highlight the
Flight ID field.
5) Repeat steps 3 and 4 until the desired Flight ID is entered.
GPS Nav
6) Press the ENT Key to update the Flight ID. Do not perform any other
G1000 functions until ‘updating’ is no longer displayed.
Flight
Planning
ADF Tuning (Optional)
1) Press the ADF/DME Softkey.
Procedures
2) Turn the small FMS Knob to enter the first digit of the desired ADF
frequency.
Hazard
Avoidance
3) Turn the large FMS Knob to select the next desired field.
4) Turn the small FMS Knob to enter the desired number.
5) Repeat steps 3 and 4 until the desired ADF frequency is entered.
Additional
Features
6) Press the ENT Key to accept the new frequency.
7) Press the ENT Key again to transfer the frequency to the active field.
Abnormal
Operation
8) Turn the large FMS Knob to select the MODE field.
9) Turn the small FMS Knob to select ANT, ADF, ADF/BFO, or ANT/BFO.
10) Press the ENT Key to complete the selection.
Annun/
Alerts
DME Tuning
Appendix
1) Press the ADF/DME or DME Softkey.
2) Turn the large FMS to select the DME source field.
3) Turn the small FMS Knob to select the desired Nav radio.
Index
4) Press the ENT Key to complete the selection.
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
11
Flight
Instruments
Nav/Com/XPDR/Audio Panel
Enter a Transponder Code
1) Press the XPDR Softkey to display the transponder mode selection softkeys.
EAS
4) Press the digit softkeys to enter the code in the code field. When entering
the code, the next key in sequence must be pressed within 10 seconds, or
the entry is cancelled and restored to the previous code. Five seconds after
the fourth digit has been entered, the transponder code becomes active.
AFCS
3) Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
Nav/Com/
XPDR/Audio
2) Press the XPDR1 or XPDR2 Softkey to select the active transponder.
GPS Nav
Selecting a COM Radio
Transmit/Receive
Press the COM1 or COM2 on the audio panel.
Selecting a NAV Radio
Additional
Features
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.
NAV/COM Tuning
1) Press the small tuning knob to select the desired radio for tuning. A light
blue box highlights the radio frequency to be tuned.
Annun/
Alerts
Abnormal
Operation
Press the COM1 MIC or COM2 MIC on the audio panel.
Receive Only
Hazard
Avoidance
Procedures
Flight
Planning
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
3) Press the Frequency Transfer Key to place the frequency into the active
frequency field.
12
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Nav/Com/XPDR/Audio Panel
Annun/
Alerts
Appendix
Index
13
Abnormal
Operation
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Additional
Features
190-00708-02 Rev. A
Hazard
Avoidance
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.
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.
Procedures
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.
Flight
Planning
GPS Nav
Clearance Recorder and Player
AFCS
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.
Nav/Com/
XPDR/Audio
Passenger Address (PA) System
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
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
14
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
AFCS
Note: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.
AFCS
Flight Director Activation
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
15
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.
190-00708-02 Rev. A
Additional
Features
BC Key
Pitch Hold (default)
Hazard
Avoidance
Navigation**
Procedures
NAV Key
ROL
ROL
ROL
GA
ROL
ROL
ROL
GPS
VOR
LOC
BC
Vertical
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Go Around
GA
Altitude Hold
ALT
Vertical Speed
VS
Vertical Path Tracking* VPTH
Flight
Planning
FD Key
AP Key
CWS Button
GA Switch
ALT Key
VS Key
VNV Key
Lateral
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
Go Around
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
GPS Nav
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.
Control Pressed
Nav/Com/
XPDR/Audio
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.
EAS
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 WAAS
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
16
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
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
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Index
* No annunciation appears in the AFCS Status Box. The acceptable bank angle range is indicated in
green along the Roll Scale of the Attitude Indicator.
17
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
18
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
GPS Navigation
Flight
Instruments
GPS Navigation
Direct-to Navigation
EAS
Direct-to Navigation using the MFD
2)
3)
6)
9)
12)
1) Press the Direct-to Key (
2)
5)
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
19
Index
6)
Appendix
4)
Annun/
Alerts
3)
) 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.
Abnormal
Operation
Direct-to Navigation using the PFD
Additional
Features
11)
Hazard
Avoidance
10)
Procedures
8)
Flight
Planning
7)
GPS Nav
5)
AFCS
4)
) 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.
Nav/Com/
XPDR/Audio
1) Press the Direct-to (
GPS Navigation
Flight
Instruments
7) Turn the small FMS Knob to enter the desired altitude.
EAS
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.
Procedures
Flight
Planning
GPS Nav
13) Turn the small FMS Knob to enter the desired course to the waypoint.
2) Press the FMS Knob to activate the cursor.
Hazard
Avoidance
3) Turn the large FMS Knob to highlight the desired flight plan
4) Select the ACTIVE Softkey. The confirmation window is now displayed.
Activate a Flight Plan Leg
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.
Annun/
Alerts
Abnormal
Operation
Additional
Features
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.
Index
Appendix
2) Select the ACT LEG Softkey.
or
Press the MENU Key, select the ‘Activate Leg’ option from the page menu
and press the ENT Key. This step must be used when activating a leg from
the PFD.
3) With ‘Activate’ highlighted, press the ENT Key.
20
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
GPS Navigation
Flight
Instruments
Stop Navigating a Flight Plan
1) Press the FPL Key to display the Active Flight Plan Page.
2) Press the MENU Key to display the Page Menu Window.
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
Vertical Navigation (VNAV)
EAS
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.
Flight
Planning
Procedures
Large White
Text
Large Light
Blue Text
Hazard
Avoidance
Small Light
Blue Text
Abnormal
Operation
Small White Text
with Altitude
Restriction Bar
Additional
Features
Small Light
Blue Subdued
Text
Annun/
Alerts
Cross AT or ABOVE 5,000 ft
Appendix
Cross AT 2,300 ft
Cross AT or BELOW 3,000 ft
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
21
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
Light Blue Text
Light Blue
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
22
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Flight Planning
Flight
Instruments
Flight Planning
Weight Planning
EAS
All procedures apply to the MFD unless otherwise stated.
Entering Weight Parameters
Procedures
Hazard
Avoidance
Additional
Features
3) Select the FOB SYNC Softkey to enter the fuel on board quantity as read
from the aircraft fuel quantity sensors.
Abnormal
Operation
Manually enter the desired fuel quantity.
Flight
Planning
2) Turn the large FMS Knob to place the cursor in the ‘Fuel On Board’ field.
GPS Nav
1) If necessary, press the FMS Knob to activate the cursor.
Or:
AFCS
Entering Fuel Parameters
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.
4) Press the ENT Key. The cursor is now in the ‘Fuel Reserves’ field.
5) Enter the desired reserve fuel quantity.
Annun/
Alerts
6) Press the FMS Knob to remove the cursor.
Trip Planning
Appendix
1) Turn the large FMS Knob to select the ‘AUX’ page group.
2) Turn the small FMS Knob to select the second rectangular page icon.
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
23
Index
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.
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.
Or:
For point-to-point planning:
GPS Nav
AFCS
d) Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.
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.
Or:
For flight plan leg planning:
Hazard
Avoidance
Procedures
d) Press the ENT Key to accept the waypoint.
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
24
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.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Flight Planning
Hazard
Avoidance
Additional
Features
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
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.
Nav/Com/
XPDR/Audio
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.
EAS
7) The flashing cursor moves to the ground speed (GS) field. Enter the ground
speed. Press the ENT Key when finished. Note that in ‘automatic’ page
mode, ground speed is provided by the system.
Flight
Instruments
6) Enter the departure time. Press the ENT Key when finished. Departure time
may be entered in local or UTC time, depending upon system settings.
Abnormal
Operation
Create a New User Waypoint Defined by Latitude & Longitude
Annun/
Alerts
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.
Appendix
3) Press the NEW Softkey. A waypoint is created at the current aircraft
position.
4) Enter the desired waypoint name.
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Index
5) Press the ENT Key.
25
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.
Nav/Com/
XPDR/Audio
EAS
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’. This list is populated only when there is an active flight
plan.
b) Press the ENT Key to place a check-mark in the box.
7) The cursor is now in the ‘WAYPOINT TYPE’ field. Turn the small FMS Knob
to display a list of waypoint types.
AFCS
8) Turn the small FMS Knob to select LAT/LON (latitude and longitude).
Create a New User Waypoint Defined by Radials from Other
Waypoints
Flight
Planning
GPS Nav
9) Press the ENT Key.
1) Turn the large FMS Knob on the MFD Control Unit to select the ‘WPT’ page
group.
Procedures
2) Turn the small FMS Knob to select the User WPT Information Page.
Hazard
Avoidance
3) Press the NEW Softkey. A waypoint is created at the current aircraft
position.
4) Enter the desired waypoint name.
Additional
Features
5) Press the ENT Key.
Abnormal
Operation
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.
Annun/
Alerts
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’. This list is populated only when there is an active flight
plan.
b) Press the ENT Key to place a check-mark in the box.
Appendix
7) The cursor is now 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).
Index
9) Press the ENT Key.
26
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Flight Planning
Flight
Instruments
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:
Nav/Com/
XPDR/Audio
b) Turn the large FMS Knob to select the desired waypoint.
c) Press the ENT Key.
Or:
GPS Nav
b) Turn the small FMS Knob to the right to display the ‘NRST’ waypoints
to the aircraft’s current position.
c) Turn the large FMS Knob to select the desired waypoint.
Flight
Planning
d) Press the ENT Key.
Or:
Hazard
Avoidance
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
Procedures
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.
Or:
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
Abnormal
Operation
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Additional
Features
d) Press the ENT Key.
AFCS
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
EAS
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
Annun/
Alerts
d) Press the ENT Key.
12) Press the ENT Key.
Appendix
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
13) Repeat step 10 to enter the next waypoint name.
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
27
Index
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.
Flight Planning
16) Press the FMS Knob to remove the flashing cursor.
Create a New User Waypoint Defined by a Radial & Distance from
Another Waypoint
1) Turn the large FMS Knob on the MFD Control Unit to select the ‘WPT’ page
group.
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
15) Press the ENT Key.
2) Turn the small FMS Knob to select the User WPT Information Page.
AFCS
3) Press the NEW Softkey. A waypoint is created at the current aircraft
position.
GPS Nav
4) Enter the desired waypoint name.
5) Press the ENT Key.
Flight
Planning
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.
Procedures
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’. This list is populated only when there is an active flight
plan.
Hazard
Avoidance
b) Press the ENT Key to place a check-mark in the box.
Additional
Features
7) The cursor is now 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.
Abnormal
Operation
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:
Annun/
Alerts
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
Appendix
b) Turn the large FMS Knob to select the desired waypoint.
c) Press the ENT Key.
Or:
Index
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
28
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
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Flight Planning
Flight
Instruments
b) Turn the small FMS Knob to the right to display the ‘NRST’ waypoints
to the aircraft’s current position.
c) Turn the large FMS Knob to select the desired waypoint.
EAS
d) Press the ENT Key.
Or:
AFCS
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.
GPS Nav
d) Press the ENT Key.
Nav/Com/
XPDR/Audio
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Or:
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
Procedures
c) Turn the large FMS Knob to select the desired waypoint.
Flight
Planning
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
d) Press the ENT Key.
12) Press the ENT Key.
Additional
Features
13) The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.
Hazard
Avoidance
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
14) Press the ENT Key.
Abnormal
Operation
15) Press the FMS Knob to remove the flashing cursor.
Delete a User Waypoint
Annun/
Alerts
1) Turn the large FMS Knob to select the ‘WPT’ page group.
3) Press the FMS Knob to activate the cursor.
5) Turn the small FMS Knob to highlight the desired waypoint.
190-00708-02 Rev. A
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29
Index
4) Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’
field.
Appendix
2) Turn the small FMS Knob to select the User WPT Information Page.
Flight Planning
7) The message ‘Would you like to delete the user waypoint?’ is displayed. With
‘YES’ highlighted, press the ENT Key.
Create a New Flight Plan
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
6) Select the DELETE Softkey.
NOTE: When creating a new flight plan in the Active Flight Plan Window,
the first leg is activated automatically after it is created.
AFCS
Using the MFD
1) Press the FPL Key on the MFD Control Unit.
GPS Nav
2) Turn the small FMS Knob to display the Flight Plan Catalog Page.
Flight
Planning
3) Select the NEW Softkey to display a blank flight plan for the first empty storage
location.
4) Turn the small FMS Knob to display the Waypoint Information Window.
5) Enter the identifier of the departure waypoint.
Procedures
6) Press the ENT Key.
Hazard
Avoidance
7) Repeat step number 4, 5, and 6 to enter the identifier for each additional
flight plan waypoint.
8) 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.
Additional
Features
Using the PFD
Abnormal
Operation
NOTE: If a flight plan is active, an additional flight plan cannot be entered
using the PFD.
1) Press the FPL Key on the PFD.
Annun/
Alerts
2) Turn the small FMS Knob to display the Waypoint Information Page.
Appendix
3) Turn the small FMS Knob to enter the first letter of the destination waypoint
identifier.
4) Turn the large FMS Knob to the right to move the cursor to the next character
position.
Index
5) Repeat step 3 and 4 to spell out the rest of the waypoint identifier.
6) Press the ENT Key and the cursor is now ready for entering of the next flight
plan waypoint.
30
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Flight Planning
EAS
8) Once all waypoints have been entered, press the FMS Knob to remove the
cursor. The new flight plan is now active.
Flight
Instruments
7) Repeat steps 3 through 6 to enter the identifier for each additional flight plan
waypoint.
Import a Flight Plan from an SD Card
1) Insert the SD card containing the flight plan in the top card slot on the
MFD.
Nav/Com/
XPDR/Audio
2) Press the FPL Key on the MFD Control Unit to display the Active Flight Plan
Page on the MFD.
AFCS
3) Turn the small FMS Knob to select the Flight Plan Catalog Page.
GPS Nav
4) Press the FMS Knob to activate the cursor.
5) Turn either FMS Knob to highlight an empty or existing flight plan.
Or:
Annun/
Alerts
Insert a Waypoint in the Active Flight Plan
Abnormal
Operation
8) Press the ENT Key.
Additional
Features
7) Turn the small FMS Knob to highlight the desired flight plan for importing.
Hazard
Avoidance
If an existing flight plan is selected, an ‘Overwrite existing flight plan?
OK or CANCEL’ prompt is displayed. Press the ENT Key to choose to
overwrite the selected flight plan and see a list of the available flight
plans on the SD card. If overwriting the existing flight plan is not
desired, select ‘CANCEL’ using the FMS Knob, press the ENT Key, select
another existing or empty flight plan, and again press the IMPORT
Softkey.
Procedures
If an empty flight plan is selected, a list of the available flight plans on
the SD card will be displayed.
Flight
Planning
6) Press the IMPORT Softkey.
1) Press the FPL Key to display the active flight plan.
3) Turn the large FMS Knob to highlight the desired flight plan waypoint. The
new waypoint is inserted before the highlighted waypoint.
Index
4) Turn the small FMS Knob. The Waypoint Information Window is now
displayed.
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Appendix
2) If necessary, press the FMS Knob to activate the cursor.
31
Flight Planning
Flight
Instruments
5) Enter the new flight plan waypoint by one of the following:
a) Enter the user waypoint identifier, facility, or city.
b) Press the ENT Key.
EAS
Or:
Nav/Com/
XPDR/Audio
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
b) Turn the small FMS Knob to the right to display the ‘NRST’ airport
waypoints to the aircraft’s current position.
AFCS
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
GPS Nav
Or:
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Flight
Planning
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
d) Press the ENT Key.
e) Press the ENT Key again to “accept” the waypoint.
Enter an Airway in a Flight Plan
1) Press the FPL Key.
Additional
Features
Hazard
Avoidance
Procedures
c) Turn the large FMS Knob to select the desired waypoint.
2) Press the FMS Knob to activate the cursor (not required on the PFD).
Abnormal
Operation
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.
Appendix
Annun/
Alerts
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
5) Turn the FMS Knob to select the desired airway from the list, and press the
ENT Key. Low altitude airways are shown first in the list, followed by “all”
altitude airways, and then high altitude airways.
32
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Flight Planning
7) Press the ENT Key. The system returns to editing the flight plan with the
new airway inserted.
Flight
Instruments
6) Turn the FMS Knob to select the desired airway exit point from the list, and
press the ENT Key. ‘LOAD?’ is highlighted.
EAS
Invert An Active Flight Plan
Nav/Com/
XPDR/Audio
1) Press the FPL Key to display the active flight plan.
2) Press the MENU Key to display the Page Menu.
AFCS
3) Turn the large FMS Knob to highlight ‘Invert Flight Plan’.
GPS Nav
4) Press the ENT Key. The original flight plan remains intact in its flight plan
catalog storage location.
5) With ‘OK’ highlighted, press the ENT Key to invert the flight plan.
Or, for a stored flight plan:
Hazard
Avoidance
a) Press the MFD FPL Key and turn the small FMS Knob to select the
Flight Plan Catalog Page.
Procedures
1) Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Flight
Planning
Remove a Departure, Arrival, Approach, or Airway from a Flight
Plan
Additional
Features
b) Press the FMS Knob to activate the cursor.
c) Turn the large FMS Knob to highlight the desired flight plan.
d) Select the EDIT Softkey.
2) Turn the large FMS Knob to highlight the title for the approach, departure,
arrival, or airway to be deleted. Titles appear in white directly above the
procedure’s waypoints.
Abnormal
Operation
3) Press the CLR Key to display a confirmation window.
Annun/
Alerts
Appendix
4) With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.
Index
190-00708-02 Rev. A
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33
Store a Flight Plan
1) After creating a flight plan on either the PFD or MFD, it may be saved by
pressing the MENU Key.
2) Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key.
EAS
Flight
Instruments
Flight Planning
Edit a Stored Flight Plan
1) Press the FPL Key for the MFD and turn the small FMS Knob to display the
Flight Plan Catalog Page.
AFCS
Nav/Com/
XPDR/Audio
3) With ‘OK’ highlighted, press the ENT Key to store the flight plan.
2) Press the FMS Knob to activate the cursor.
GPS Nav
3) Turn the large FMS Knob to highlight the desired flight plan.
4) Select the EDIT Softkey.
6) Enter the changes, then press the ENT Key.
7) Press the FMS Knob to return to the Flight Plan Catalog Page.
Delete a Waypoint from the Flight Plan
1) Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Hazard
Avoidance
Procedures
Flight
Planning
5) Turn the large FMS Knob to place the cursor in the desired location.
Or, for a stored flight plan:
Additional
Features
a) Press the FPL Key of the MFD and turn the small FMS Knob to select
the Flight Plan Catalog Page.
Abnormal
Operation
b) Press the FMS Knob to activate the cursor.
c) Turn the large FMS Knob to highlight the desired flight plan.
d) Select the EDIT Softkey.
Annun/
Alerts
2) Turn the large FMS Knob to highlight the waypoint to be deleted.
Appendix
3) Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation
window.
Index
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.
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Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
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Flight Planning
Flight
Instruments
Invert and Activate a Stored Flight Plan
1) Press the FPL Key for the MFD.
2) Turn the small FMS Knob to select the Flight Plan Catalog Page.
EAS
3) Press the FMS Knob to activate the cursor.
5) Select the INVERT Softkey. ‘Invert and activate stored flight plan?’ is
displayed.
AFCS
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.
Nav/Com/
XPDR/Audio
4) Turn the large FMS Knob to highlight the desired flight plan.
GPS Nav
Copy a Flight Plan
Flight
Planning
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.
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.
Hazard
Avoidance
5) Select the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is
displayed.
Procedures
4) Turn the large FMS Knob to highlight the flight plan to be copied.
Additional
Features
Delete a Flight Plan
Abnormal
Operation
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.
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.
Appendix
5) Select the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is
displayed.
Annun/
Alerts
4) Turn the large FMS Knob to highlight the flight plan to be deleted.
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
35
Graphical Flight Plan Creation
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Press the Joystick to activate the map pointer. Use the Joystick to move
the pointer to the desired point on the map to be inserted as a waypoint in
the flight plan.
EAS
Flight
Instruments
Flight Planning
AFCS
Nav/Com/
XPDR/Audio
3) The default insertion point is at the end of the flight plan. If the selected
waypoint is to be placed anywhere other than the end of the flight plan,
press the FMS Knob to activate the cursor. Waypoints are inserted ABOVE
the cursor. Turn the large FMS Knob to select the desired insertion point.
5) To change the user waypoint name, follow the procedure for modifying a user
waypoint.
Export a Flight Plan to an SD Card
1) Insert the SD card into the top card slot on the MFD.
Procedures
Flight
Planning
GPS Nav
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.
Hazard
Avoidance
3) Turn the small FMS Knob to select the Flight Plan Catalog Page.
Additional
Features
2) Press the FPL Key on the MFD Contol Unit to display the Active Flight Plan
Page on the MFD.
5) Turn the large FMS Knob to highlight the flight plan to be exported.
4) Press the FMS Knob to activate the cursor.
6) Press the EXPORT Softkey.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
7) Press the ENT Key to confirm the export.
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Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Procedures
Flight
Instruments
Procedures
Load and Activate a Departure Procedure
EAS
1) Press the PROC Key.
3) Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a
list of available departures.
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.
Flight
Planning
7) Turn the large FMS Knob to highlight the desired transition.
GPS Nav
6) Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a
list of available transitions.
AFCS
4) Turn the large FMS Knob to highlight the desired departure.
Nav/Com/
XPDR/Audio
2) Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.
8) Press the ENT Key.
Hazard
Avoidance
Activate A Departure Leg
Procedures
9) With ‘LOAD?’ highlighted, press the ENT Key. The departure is active when
the flight plan is active.
1) Press the FPL Key for the MFD to display the active flight plan.
Additional
Features
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.
Abnormal
Operation
4) Select the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5) With ‘ACTIVATE’ highlighted, press the ENT Key.
Annun/
Alerts
Load An Arrival Procedure
Appendix
1) Press the PROC Key.
2) Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’.
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
37
Index
3) Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list
of available arrivals.
Procedures
Flight
Instruments
4) Turn the large FMS Knob to highlight the desired arrival.
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.
EAS
7) Press the ENT Key. A list of runways may be displayed for the selected
arrival.
Nav/Com/
XPDR/Audio
8) Turn the large FMS Knob to highlight the desired runway.
9) Press the ENT Key.
10) With ‘LOAD?’ highlighted, press the ENT Key.
Activate An Arrival Leg
1) Press the FPL Key to display the active flight plan.
2) Press the FMS Knob to activate the cursor.
Flight
Planning
GPS Nav
AFCS
11) The arrival becomes part of the active flight plan.
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
Procedures
3) Turn the large FMS Knob to highlight the TO waypoint of the desired leg
within the arrival.
Abnormal
Operation
NOTE: If certain GPS parameters (WAAS, RAIM, etc.) are not available, some
published approach procedures for the desired airport may not be displayed
in the list of available approaches.
Annun/
Alerts
1) Press the PROC Key.
2) Turn the large FMS Knob to highlight ‘SELECT APPROACH’.
Appendix
3) Press the ENT Key. A list of available approaches for the destination airport
is displayed.
4) Turn either FMS Knob to highlight the desired approach.
Index
5) Press the ENT Key. A list of available transitions for the selected approach
procedure is now displayed.
38
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Procedures
Flight
Instruments
6) Turn either FMS Knob to select the desired transition. The “Vectors”
option assumes vectors will be received to the final course segment of
the approach and will provide navigation guidance relative to the final
approach course.
EAS
7) Press the ENT Key. The cursor moves to the MINIMUMS field.
Nav/Com/
XPDR/Audio
8) If desired, the DA/MDA for the selected approach procedure may be
entered and displayed on the PFD. Turn the small FMS Knob in the
direction of the green arrow to change the display from OFF to BARO.
AFCS
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.
GPS Nav
10) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’
highlighted.
11) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.
Flight
Planning
Procedures
Selecting ‘LOAD?’ enters the selected approach procedure into the active
flight plan, but is not currently active. Selecting ‘ACTIVATE?’ enters the
selected approach procedure into the active flight plan and activates the
first leg of the approach.
12) Press the ENT Key.
Hazard
Avoidance
Activate An Approach in the Active Flight Plan
Additional
Features
1) Press the PROC Key.
2) Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.
3) Press the ENT Key.
Abnormal
Operation
Activate a Vector to Final Approach Fix
Annun/
Alerts
1) Press the PROC Key.
2) Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’.
Appendix
3) Press the ENT Key.
4) The final approach course becomes the active leg.
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
39
Flight
Instruments
Procedures
Activate A Missed Approach in the Active Flight Plan
1) Press the PROC Key.
EAS
2) Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’.
3) Press the ENT Key. A confirmation window is displayed.
Or:
Press the go-around button.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
4) With ‘ACTIVATE’ highlighted, press the ENT Key.
40
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Hazard Avoidance
Flight
Instruments
Hazard Avoidance
Customizing the Hazard Displays on the Navigation Map
EAS
1) With the Navigation Map Page displayed, press the MENU Key to display
the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’
option.
GPS Nav
STORMSCOPE® (Optional)
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 the large FMS Knob to select ‘STRMSCP MODE’.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
41
Index
1) With the Weather Group selected, press the ENT Key. The cursor flashes on
‘STRMSCP LTNG’.
Appendix
Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode
190-00708-02 Rev. A
Additional
Features
2) Press the STRMSCP Softkey. Press the STRMSCP Softkey again to remove
Stormscope Lightning Data from the Navigation Map Page.
Hazard
Avoidance
1) Press the MAP Softkey.
Procedures
Displaying Stormscope Lightning Data on the Navigation Map Page
Flight
Planning
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.
Lightning Age
Strike is less than 6 seconds old
AFCS
3) Press the small FMS Knob to return to the Navigation Map Page.
Nav/Com/
XPDR/Audio
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.
Hazard Avoidance
Flight
Instruments
3) Turn the small FMS Knob to display the ‘Cell/Strike’ window.
4) Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key.
5) Push the FMS Knob to return to the Navigation Map Page.
EAS
Clear Stormscope Lightning Data from the Navigation Map Page
Nav/Com/
XPDR/Audio
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.
AFCS
NOTE: If heading input is lost, strikes and/or cells must be cleared manually
after the execution of each turn. This is to ensure that the strike and/or cell
GPS Nav
positions are depicted accurately in relation to the nose of the aircraft.
Stormscope Page
Flight
Planning
1) Turn the large FMS Knob until the Map Page group is selected.
Procedures
2) Turn the small FMS Knob until the Stormscope Page is selected.
Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’
Hazard
Avoidance
1) Select the Stormscope Page.
Additional
Features
2) Press the MODE Softkey. The CELL and STRIKE Softkeys are displayed.
Press the CELL Softkey to display ‘CELL’ data or press 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
NOTE: “Cell mode” uses a clustering program to identify clusters of electrical
activity that indicate cells.
Annun/
Alerts
Change the Viewing Mode Between 360˚ and 120˚
1) Select the Stormscope Page.
Appendix
2) Press the VIEW Softkey. The 360 and ARC Softkeys are displayed. Press
the 360 Softkey to display a 360˚ viewing area or press the ARC Softkey to
display a 120˚ viewing area.
Index
42
Press the CLEAR Softkey to remove all Stormscope lightning data from the
display.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Hazard Avoidance
Nav/Com/
XPDR/Audio
Displaying XM Weather on the Navigation Map Page
EAS
WARNING: Use of XM weather for hazardous weather penetration is not
recommended. Weather information provided by XM Radio Service is
approved only for weather avoidance, not penetration.
Flight
Instruments
XM Weather (Optional)
1) Select the MAP Softkey.
AFCS
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
Display METAR and TAF information on the Airport Information Page
1) Turn the large FMS Knob to select the WPT Page Group.
Flight
Planning
2) Turn the small FMS Knob to select the Airport Information Page.
Procedures
3) Select the WX Softkey to display METAR and TAF text (METAR and TAF
information is updated every 12 minutes).
Displaying Weather on the Weather Data Link Page
Hazard
Avoidance
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Weather Data Link Page.
Map Panning Information – Weather Data Link Page
3) Press the ENT Key to display pertinent information for the selected product.
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
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
2) Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs,
or SIGMETs.
Annun/
Alerts
1) Push in the Joystick to display the panning arrow.
Abnormal
Operation
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.
Additional
Features
3) Select the available softkeys to select the desired XM weather product.
43
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
Turbulence
PIREPs
NEXRAD XM Lightning
Cloud Top
METARs Surface Analysis
SIGMETs/AIRMETs
County Warnings
Winds Aloft
Traffic Systems
• 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.
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Echo Top (Cloud Top and Echo Top Mutually Exclusive)
Cyclone Warnings
City Forecast
AIREPs
Cell Movement
Icing Potential
Freezing Levels
Hazard
Avoidance
Traffic Symbol
Description
Additional
Features
Non-Threat Traffic
(intruder is beyond 5 nm and greater than 1200’ vertical separation)
Proximity Advisory (PA) (Not available with TIS system)
(intruder is within 5 nm and less than 1200’ vertical separation)
Abnormal
Operation
Traffic Advisory (TA)
(closing rate, distance, and vertical separation meet TA criteria)
Annun/
Alerts
Traffic Advisory Off Scale
Index
Appendix
Traffic Symbol Description
44
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Hazard Avoidance
NOTE: If the G1000 is configured to use an optional Traffic Advisory System
(TAS), TIS is not available for use.
NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.
EAS
Flight
Instruments
Traffic Information Service (TIS)
Nav/Com/
XPDR/Audio
Displaying Traffic on the Traffic Map Page
AFCS
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Traffic Map Page.
GPS Nav
3) Press the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
Flight
Planning
4) Press the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
Procedures
5) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Hazard
Avoidance
6) Press the TNA MUTE Softkey to mute the “Traffic Not Available” aural
alert.
Displaying Traffic on the Navigation Map
Additional
Features
1) Ensure TIS is operating. With the Navigation Map displayed, press the
MAP Softkey.
2) Press the TRAFFIC Softkey. Traffic is now displayed on the map.
Abnormal
Operation
Traffic Advisory System (TAS) (Optional)
Annun/
Alerts
System Self Test
1) Set the range to 2/6 nm.
3) Select the TEST Softkey.
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
45
Index
4) Self test takes approximately eight seconds to complete. When completed
successfully, traffic symbols are displayed and a voice alert “TAS System Test
OK” is heard. If the self test fails, the system reverts to Standby Mode and
a voice alert “TAS System Test Fail” is heard.
Appendix
2) Select the STANDBY Softkey.
Hazard Avoidance
Flight
Instruments
Displaying Traffic on the Traffic Map Page
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the second rectangular page icon.
EAS
3) Select the NORMAL Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
AFCS
Nav/Com/
XPDR/Audio
4) Select the ALT MODE Softkey to change the altitude volume. Select the
desired altitude volume by pressing 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.
GPS Nav
6) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Flight
Planning
Displaying Traffic on the Navigation Map
1) Ensure TAS is operating.
3) Select the TRAFFIC Softkey. Traffic is now displayed on the map.
Terrain And Obstacle Proximity
Additional
Features
Hazard
Avoidance
Procedures
2) With the Navigation Map displayed, select the MAP Softkey.
NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.
Abnormal
Operation
Displaying Terrain and Obstacles on the Terrain Proximity Page
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the last rectangular page icon.
Appendix
Annun/
Alerts
3) If desired, press the VIEW Softkey to access the ARC and 360 Softkeys.
When the ARC Softkey is pressed, a radar-like 120° view is displayed. Press
the 360 Softkey to return to the 360° default display.
Index
4) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
46
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Hazard Avoidance
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.
Nav/Com/
XPDR/Audio
Red
EAS
Terrain/Obstacle Location
Flight
Instruments
Color
Displaying Terrain and Obstacles on the Navigation Map
AFCS
1) With the Navigation Map displayed, press the MAP Softkey.
GPS Nav
2) Press the TERRAIN Softkey. Terrain and obstacle proximity will now be
displayed on the map.
Terrain-SVS
NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.
Display Terrain on the TERRAIN-SVS Page
Hazard
Avoidance
Procedures
NOTE: Terrain-SVS is only available when the Synthetic Vision System (SVS)
option is installed and the TAWS option has not been installed.
Flight
Planning
Additional
Features
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Terrain-SVS Page.
Abnormal
Operation
3) If desired, press the VIEW Softkey to access the ARC and 360 softkeys.
When the ARC Softkey is selected, a radar-like 120° view is displayed.
Press the 360 Softkey to return to the 360° default display.
Annun/
Alerts
4) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Appendix
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
47
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Hazard Avoidance
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.
AFCS
Enable/Disable Aviation Data
1) While the Terrain-SVS Page is displayed, press the MENU Key.
GPS Nav
2) Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.
3) Press the ENT Key.
Flight
Planning
Terrain-SVS Inhibit
Additional
Features
Hazard
Avoidance
Procedures
Inhibit Terrain
While the Terrain-SVS Page is displayed, press the INHIBIT Softkey.
Or:
1) Press the MENU Key.
2) Turn the small FMS Knob to select ‘Inhibit Terrain’.
3) Press the ENT Key.
Appendix
Annun/
Alerts
Abnormal
Operation
Enable Terrain
While the Terrain-SVS Page is displayed, press the INHIBIT Softkey.
Or:
1) While the Terrain-SVS Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select ‘Enable Terrain’.
3) Press the ENT Key.
Index
48
NOTE: If Terrain-SVS alerts are inhibited when the Final Approach Fix is the
active waypoint in a GPS WAAS 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.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Hazard Avoidance
NOTE: TAWS operation is only available when the G1000 is configured for a
TAWS-B installation.
AFCS
NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.
Nav/Com/
XPDR/Audio
EAS
WARNING: The TAWS display shows supplemental information only. It should
not be used for navigation.
Flight
Instruments
Terrain Awareness & Warning System (TAWS) Display
Manual System Test
GPS Nav
1) While the TAWS-B Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select ‘Test TAWS’.
When all is in working order, “TAWS System Test, OK” is heard.
Procedures
Flight
Planning
3) Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center
of the TAWS-B Page.
Display Terrain on the TAWS-B Page
Hazard
Avoidance
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the TAWS-B Page.
Additional
Features
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.
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.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Index
Red
Appendix
Terrain/Obstacle Location
Annun/
Alerts
190-00708-02 Rev. A
Color
Abnormal
Operation
4) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
49
Hazard Avoidance
Flight
Instruments
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”.
EAS
3) Press the ENT Key.
Nav/Com/
XPDR/Audio
TAWS Inhibit
GPS Nav
AFCS
Procedures
Flight
Planning
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.
Additional
Features
Hazard
Avoidance
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.
Airborne Color Weather Radar
Annun/
Alerts
Abnormal
Operation
NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active
waypoint in a GPS WAAS 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.
Appendix
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.
Index
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.
50
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Hazard Avoidance
Flight
Instruments
Displaying Weather on the Weather Radar Page
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Weather Radar Page.
EAS
3) Select the MODE Softkey.
AFCS
Or:
Nav/Com/
XPDR/Audio
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.
GPS Nav
If the aircraft is already airborne, select the WEATHER or GROUND
Softkey. The one-minute warm-up period will be initiated, after which the
radar will begin transmitting. The horizontal scan is initially displayed.
5) Turn the Joystick to select the desired range.
Flight
Planning
6) If desired, select the VERTICAL Softkey for vertical scanning.
Adjusting Antenna Tilt
Appendix
Index
51
Annun/
Alerts
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Abnormal
Operation
190-00708-02 Rev. A
Additional
Features
Move the Joystick right or left to adjust the azimuth position of the antenna right
or left. Monitor the displayed bearing value in the BEARING 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.
Hazard
Avoidance
Adjusting Antenna Bearing
Procedures
Move the Joystick up or down to adjust the tilt of the antenna up or down.
Monitor the displayed tilt value in the TILT field.
When scanning vertically, a Tilt Line may be displayed to aid in positioning the tilt
of the antenna. If the Tilt Line is not displayed, perform the following steps:
1) Press the MENU Key
2) Turn the large FMS Knob to select ‘Show Tilt Line’.
3) Press the ENT Key.
Hazard Avoidance
Flight
Instruments
Vertically Scan a Storm Cell
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.
EAS
2) Select the VERTICAL Softkey. A vertical ‘slice’ of the selected area will now
be displayed.
Nav/Com/
XPDR/Audio
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.
AFCS
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.
GPS Nav
Adjusting Gain
Procedures
Flight
Planning
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.
1) Select the GAIN Softkey to activate the cursor in the ‘GAIN’ field.
Hazard
Avoidance
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.
Additional
Features
3) Press the FMS Knob to remove the cursor.
Abnormal
Operation
4) Select the GAIN Softkey again to recalibrate the gain. ‘CALIBRATED’ will be
displayed in the ‘GAIN’ field.
Ground Mapping
1) Select the MODE Softkey.
Annun/
Alerts
2) Select the GROUND Softkey to place the radar in Ground Map Mode.
Index
Appendix
3) Select the BACK Softkey.
52
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Hazard Avoidance
2) Press the FMS Knob to display the cursor.
4) Turn the small FMS Knob to select FULL, 60˚, 40˚, or 20˚ scan.
6) Press the FMS Knob to remove the cursor.
GPS Nav
Antenna Stabilization
AFCS
5) If desired, readjust the Bearing Line with the Joystick to change the center
of the Sector Scan.
Nav/Com/
XPDR/Audio
3) Turn the large FMS Knob to place the cursor in the SECTOR SCAN field.
EAS
1) While in the Horizontal Scan Mode, move the Joystick right or left to place
the Bearing Line in the desired position. The location of the Bearing Line
will become the center point of the Sector Scan.
Flight
Instruments
Sector Scan
Flight
Planning
1) To activate or deactivate the antenna stabilization, select the MODE
Softkey.
Abnormal
Operation
Annun/
Alerts
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.
Additional
Features
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.
Hazard
Avoidance
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.
Procedures
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.
Appendix
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
53
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Hazard Avoidance
Blank Page
54
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
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. SVS is intended as an aid to situational
awareness only and may not provide the accuracy and/or fidelity upon which
to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or
traffic.
AFCS
Procedures
Hazard
Avoidance
Pathways
Flight Path Marker
Horizon Heading Marks
Terrain and Obstacle Alerting
Three-dimensional Traffic
Airport Signs
Runway Display
Flight
Planning
Additional
Features
Abnormal
Operation
•
•
•
•
•
•
•
GPS Nav
Synthetic Vision System (SVS) functionality is offered as an optional enhancement
to the G1000 Integrated Flight Deck System.
SVS is primarily comprised of a computer-generated forward-looking, attitude
aligned view of the topography immediately in front of the aircraft from the pilot’s
perspective. SVS information is shown on the primary flight display (PFD).
SVS offers a three-dimensional view of terrain and obstacles. Terrain and
obstacles that pose a threat to the aircraft in flight are shaded yellow or red.
In addition to SVS enhancement to the PFD, the following feature enhancements
have been added to the PFD:
Displaying Synthetic Terrain
Annun/
Alerts
1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
Appendix
3) Press the SYN TERR Softkey.
4) Press the BACK Softkey to return to the previous page.
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
55
Additional Features
Flight
Instruments
Displaying Pathways
1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
EAS
3) If not already enabled, press the SYN TERR Softkey.
Nav/Com/
XPDR/Audio
4) Press the PATHWAY Softkey.
5) Press the BACK Softkey to return to the previous page.
Displaying Heading on the Horizon
AFCS
1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
GPS Nav
3) If not already enabled, press the SYN TERR Softkey.
4) Press the HRZN HDG Softkey.
Flight
Planning
5) Press the BACK Softkey to return to the previous page.
Displaying Airport Signs
Procedures
1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
3) If not already enabled, press the SYN TERR Softkey.
5) Press the BACK Softkey to return to the previous page.
Terminal Procedure Charts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
4) Press the APTSIGNS Softkey.
Index
Appendix
Annun/
Alerts
NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts® in
electronic form, it is still advisable to carry another source of charts on-board
the aircraft.
SafeTaxi®
SafeTaxi® is an enhanced feature that gives greater map detail as the map range
is adjusted in on the airport. The airport display on the map reveals runways with
numbers, taxiways 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
56
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Additional Features
Flight
Instruments
EAS
Nav/Com/
XPDR/Audio
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 aid in following ground control instructions by accurately displaying
the aircraft position on the map in relation to taxiways, ramps, runways, terminals, and
services. This database is updated on a 56-day cycle.
ChartView
Additional
Features
Abnormal
Operation
3) Select the GO BACK Softkey to return to the previous page.
57
Index
2) Select the DP, STAR, APR, WX, and NOTAM softkeys to access charts for
departures, arrivals, approaches, weather and NOTAMs Note that NOTAMS
are only available with ChartView.
Appendix
Move the map pointer to point to a desired point on the map and select the
SHW CHRT Softkey.
Annun/
Alerts
Or:
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Hazard
Avoidance
1) Select the SHW CHRT Softkey when displayed.
190-00708-02 Rev. A
Procedures
View Charts from the Navigation Map Page
Flight
Planning
FliteCharts® resemble the paper version of National Aeronautical Charting Office
(NACO) terminal procedures charts. The charts are displayed with high-resolution
and in color for applicable charts. Current aircraft position is not displayed on
FliteCharts.
The FliteCharts database contains procedure charts for the United States only.
This database is updated on a 28-day cycle. If not updated within 180 days of the
expiration date, FliteCharts will no longer function.
GPS Nav
FliteCharts®
AFCS
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.
Additional Features
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.
EAS
2) Turn the large FMS Knob to select the departure airport, destination
airport, departure, arrival, or approach.
Nav/Com/
XPDR/Audio
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.
AFCS
Change Day/Night View
GPS Nav
1) While viewing a chart press the MENU Key to display the Page Menu
OPTIONS.
Flight
Planning
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.
Procedures
4) Turn the small FMS Knob to choose between the ‘On’ and ‘Off’ Full Screen
Options.
Hazard
Avoidance
5) Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’
Options.
7) Press the FMS Knob when finished to remove the Chart Setup Menu.
XM® Radio Entertainment
The XM® Radio Page provides information and control of the audio entertainment
features of the XM Satellite Radio.
Selecting the XM Radio Page
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
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.
1) Turn the large FMS Knob to select the Auxiliary Page Group.
Index
2) Turn the small FMS Knob to select the displayed AUX - XM Information
Page.
3) Select the RADIO Softkey to show the XM Radio Page where audio
entertainment is controlled.
58
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Additional Features
EAS
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.
Flight
Instruments
Active Channel and Channel List
Selecting a Category
Flight
Planning
Procedures
Hazard
Avoidance
2) Select the CH + Softkey to go up through the list in the Channel Box, or
move down the list with the CH – Softkey.
Or:
GPS Nav
1) While on the XM Radio Page, select the CHNL Softkey.
AFCS
Select an Available Channel within the Selected Category
Nav/Com/
XPDR/Audio
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.
Additional
Features
Press the FMS Knob to highlight the channel list and turn the large FMS
Knob to scroll through the channels.
3) With the desired channel highlighted, press the ENT Key.
Abnormal
Operation
Entering a Channel Directly
1) While on the XM Radio Page, select the CHNL Softkey.
Appendix
3) Select the numbered softkeys located on the bottom of the display to
directly select the desired channel number.
Annun/
Alerts
2) Select the DIR CH Softkey. The channel number in the Active Channel Box
is highlighted.
4) Press the ENT Key to activate the selected channel.
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
59
Additional Features
Flight
Instruments
Assigning Channel Presets
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
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). Pressing the
MORE Softkey repeatedly cycles through the preset channels.
3) Select any one of the (PS1 - PS15) softkeys to assign a number to the
active channel.
4) Select the SET Softkey on the desired channel number to save the channel
as a preset.
Adjusting Volume
Flight
Planning
1) With the XM Radio Page displayed, select the VOL Softkey.
Procedures
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.)
Hazard
Avoidance
3) Select the MUTE Softkey to mute the audio. Select the MUTE Softkey
again to unmute the audio.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
XM Radio volume may also be adjusted on each passenger headset.
60
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Abnormal Operation
Flight
Instruments
Abnormal Operation
Reversionary Mode
Flight
Planning
NOTE: The Socata TBM 850 Airplane Flight Manual (AFM) always takes
precedence over the information found in this section.
GPS Nav
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
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Index
Loss of Hazard Functions with Loss of GPS
Position
61
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
• Selected Altitude
• VNV Target Altitude
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Abnormal Operation
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Extreme Pitch Indication
62
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Abnormal Operation
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
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/WAAS 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 is 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/WAAS 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.
AFCS
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.
Nav/Com/
XPDR/Audio
EAS
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.
Flight
Instruments
Dead Reckoning
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
63
EAS
Flight
Instruments
Abnormal Operation
Symbolic Aircraft
(Map pages and Inset Map)
Dead Reckoning Indications
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-SVS, and TAWS are also disabled. Additionally,
the accuracy of all nearest information (airports, airspaces, and waypoints) is
questionable. Finally, airspace alerts continue to function, but with degraded
accuracy.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
CDI ‘DR’ Indication on PFD
64
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Annunciations & Alerts
Flight
Instruments
Annunciations & Alerts
CAS Messages
EAS
Warning Messages
Nav/Com/
XPDR/Audio
Abnormal
Operation
Annun/
Alerts
TORQUE
Additional
Features
OIL PRESS
OXYGEN
PARK BRAKE
Hazard
Avoidance
ITT
X
Procedures
FLAPS ASYM
FUEL OFF
FUEL PRESS
X
Flight
Planning
FIRE
Battery temperature over 70°C
Bleed temperature high
X
Cabin altitude over 10,000 ft
Cabin pressure differential over 6.2 psi
X
Pilot or cabin door open
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
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
GPS Nav
BAT OVERHEAT
BLEED TEMP
CABIN ALTITUDE
CABIN DIFF PRESS
DOOR
Comments
AFCS
Messages
ENGINE OFF
ENGINE ON
GROUND
TOPI
AIR
LOPI
Inhibits
Appendix
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
65
Annunciations & Alerts
Flight
Instruments
Caution Messages
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Messages
Comments
ENGINE OFF
ENGINE ON
GROUND
TOPI
AIR
LOPI
Nav/Com/
XPDR/Audio
EAS
Inhibits
X
AUTO SEL
Fuel timer off or out of service
Electric fuel pump running (manual or
AUX BOOST PMP ON
automatic mode)
BAT AMP
Battery current over 50 A while on ground
BAT OFF
Battery off
Flow control and shut-off valve/shut-off
BLEED OFF
valve closed
CHIP
Oil chip detector on (if installed)
FRONT CARGO DOOR Forward baggage door open
Fuel tanks imbalanced by more than 15
FUEL IMBALANCE
USGAL for >30 seconds
Fuel quantity less than or equal to 9.1
FUEL LOW L-R*
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 fuel level sensor failure for specified
LOW LVL FAIL L-R*
tank
LOW VOLTAGE
Battery voltage below 26 V
MAIN GEN
Starter generator unconnected
OIL PRESS
Oil pressure between 60 and 100 psi
Oil temperature below 0°C or above
OIL TEMP
104°C
Specified pitot heat (left or right) on while
PITOT HT ON L-R*
engine off
PITOT NO HT L-R* Specified pitot heat (left or right) off
PROP DEICE FAIL
Prop deice selected and not on
PROP DEICE ON
Prop deice on while engine off
66
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
X X X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
190-00708-02 Rev. A
Annunciations & Alerts
X
Nav/Com/
XPDR/Audio
X
X
X
AFCS
Rear cargo door open
Stall warning heat on while engine off
Stall warning heat off
Starter generator running
Vacuum pressure less than 3.75 in Hg
X
Inhibits prevent certain CAS messages from being displayed during the following
conditions:
GPS Nav
* Only affected side (L, R, or L-R) displayed in CAS message; applicable messages listed here display
L-R for example
Flight
Planning
•Aircraft in air (AIR)
•Engine on
•Landing Operation Phase Inhibit
(LOPI)
Hazard
Avoidance
•Takeoff Operation Phase Inhibit
(TOPI)
Procedures
•Engine off
•Aircraft on ground (Ground)
EAS
REAR CARGO DOOR
STALL HEAT ON
STALL NO HEAT
STARTER
VACUUM LOW
Comments
ENGINE OFF
ENGINE ON
GROUND
TOPI
AIR
LOPI
Messages
Flight
Instruments
Inhibits
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
67
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
Comparator Annunciations
Comparator
Window Text
ALT MISCOMP
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Difference in altitude sensors is > 200 ft.
If both airspeed sensors detect < 35 knots, this is inhibited.
IAS MISCOMP
If either airspeed sensor detects > 35 knots, and the difference in sensors is > 10
kts.
If either airspeed sensor detects > 80 knots, and the difference in sensors is > 7
kts.
HDG MISCOMP Difference in heading sensors is > 6 degrees.
PIT MISCOMP
Index
Condition
Difference in pitch sensors is > 5 degrees.
ROL MISCOMP Difference in roll sensors is > 6 degrees.
ALT NO COMP
No data from one or both altitude sensors.
IAS NO COMP
No data from one or both airspeed sensors.
HDG NO COMP No data from one or both heading sensors.
PIT NO COMP
No data from one or both pitch sensors.
ROL NO COMP No data from one or both roll sensors.
Reversionary Sensor Annunciations
Reversionary
Sensor Window
Text
Condition
BOTH ON ADC1
BOTH ON ADC2
BOTH ON AHRS1
Both PFDs are displaying data from the number one Air Data Computer.
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
USING AHRS1
Both PFDs are displaying data from the number one GPS receiver.
68
Both PFDs are displaying data from the number two Air Data Computer.
Both PFDs are displaying data from the number one Attitude & Heading Reference
System.
Both PFDs are displaying data from the number two GPS receiver.
PFD2 is displaying data from the #1 Air Data Computer.
PFD1 is displaying data from the #2 Air Data Computer.
PFD2 is displaying data from the #1 AHRS.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Annunciations & Alerts
PFD1 is displaying data from the #2 AHRS.
EAS
PFD2 is displaying data from the #1 GPS.
PFD1 is displaying data from the #2 GPS.
Nav/Com/
XPDR/Audio
USING AHRS2
USING GPS1
USING GPS2
Condition
Flight
Instruments
Reversionary
Sensor Window
Text
AFCS Alerts
Rudder Mistrim Left
Aileron Mistrim Left
Elevator Mistrim Up
(or stuck MEPT Switch)
Yaw Damper Failure
YD control failure; AP still operative
Pitch Failure
Pitch axis control failure; AP inoperative
Appendix
Roll axis control failure; AP inoperative
Annun/
Alerts
Roll Failure
System Failure
Abnormal
Operation
(or stuck MEYT Switch)
If AP engaged, take control of the aircraft and
disengage AP
If AP disengaged, move MEPT switches separately
to check if a stuck switch is causing the annunciation
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
Additional
Features
Yaw Trim Failure
Pitch servo providing sustained force in the
indicated direction
Hazard
Avoidance
Pitch Trim Failure
Roll servo providing sustained force in the
indicated direction
Procedures
Elevator Mistrim Down
Yaw servo providing sustained force in the
indicated direction
Flight
Planning
Aileron Mistrim Right
Description
GPS Nav
Rudder Mistrim Right
Annunciation
AFCS
Alert Condition
AP and MEPT are unavailable; FD may still be
available
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
69
Annunciations & Alerts
EAS
Flight
Instruments
Alert Condition
Annunciation
Description
Performing preflight system test; aural alert sounds
at completion
Do not press the AP DISC Switch during servo
power-up and preflight system tests as this may
cause the preflight system test to fail or never to
start (if servos fail their power-up tests). Power
must be cycled to the servos to remedy the
situation.
Preflight system test failed; aural alert sounds at
failure
AFCS
Nav/Com/
XPDR/Audio
Preflight Test
GPS Nav
Terrain-SVS Alerts
MFD
Pop-Up Alert
Aural
Message
Reduced Required Terrain
Clearance Warning (RTC)
“Warning; Terrain,
Terrain”
Imminent Terrain Impact
Warning (ITI)
“Warning; Terrain,
Terrain”
Reduced Required Obstacle
Clearance Warning (ROC)
“Warning; Obstacle,
Obstacle”
Imminent Obstacle Impact
Warning (IOI)
“Warning; Obstacle,
Obstacle”
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”
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
Alert Type
PFD/MFD
TERRAIN-SVS
Page
Annunciation
70
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Annunciations & Alerts
System Test fail
Aural Message
EAS
PFD/MFD
TERRAIN-SVS Page
Annunciation
Alert Type
Flight
Instruments
Terrain-SVS System Status Annunciations
“Terrain System Failure”
None
No GPS position or excessively
degraded GPS signal
System Test pass
None
Chime
PFD/MFD
TAWS-B Page
Annunciation
MFD
Pop-Up Alert
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
71
Index
“Obstacle, Obstacle; Pull
Up, Pull Up”
or
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
Appendix
190-00708-02 Rev. A
or
Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up,
Pull Up”
Annun/
Alerts
Reduced Required
Obstacle Clearance
Warning (ROC)
or
“Terrain, Terrain; Pull Up,
Pull Up”
or
“Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
Abnormal
Operation
Imminent Terrain
Impact Warning (ITI)
or
Additional
Features
Reduced Required
Terrain Clearance
Warning (RTC)
“Pull Up”
Hazard
Avoidance
Excessive Descent
Rate Warning (EDR)
Aural Message
Procedures
Alert Type
Flight
Planning
TAWS Alerts
GPS Nav
System Test in progress
AFCS
“Terrain System Not Available”
“Terrain Available” will be
heard when sufficient GPS
signal is re-established.
None
Nav/Com/
XPDR/Audio
Terrain Alerting is disabled
Alert Type
PFD/MFD
TAWS-B Page
Annunciation
Imminent Obstacle
Impact Warning
(IOI)
MFD
Pop-Up Alert
or
Reduced Required
Terrain Clearance
Caution (RTC)
or
Imminent Terrain
Impact Caution (ITI)
or
Reduced Required
Obstacle Clearance
Caution (ROC)
or
Imminent Obstacle
Impact Caution (IOI)
or
Premature Descent
Alert Caution (PDA)
Altitude Callout
“500”
None
Negative Climb
Rate Caution (NCR)
Aural Message
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
or
“Obstacle, Obstacle; Pull
Up, Pull Up”
“Caution, Terrain; Caution,
Terrain”
or
“Terrain Ahead; Terrain
Ahead”
“Terrain Ahead; Terrain
Ahead”
or
“Caution, Terrain; Caution,
Terrain”
“Caution, Obstacle; Caution, Obstacle”
or
“Obstacle Ahead; Obstacle
Ahead”
“Obstacle Ahead; Obstacle
Ahead”
or
“Caution, Obstacle; Caution, Obstacle”
“Too Low, Terrain”
None
Excessive Descent
Rate Caution (EDR)
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
“Five-Hundred”
“Sink Rate”
or
“Don’t Sink”
or
“Too Low, Terrain”
* Default configuration
72
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Annunciations & Alerts
PFD/MFD
TAWS-B Page
Annunciation
Aural Message
TAWS System Test Fail
None
“TAWS System Failure”
TAWS Alerting is disabled
None
None
No GPS position or
excessively degraded GPS
signal
None
System Test in progress
None
None
None
Chime
Nav/Com/
XPDR/Audio
“TAWS Not Available”
“TAWS Available” will be
heard when sufficient GPS
signal is re-established.
GPS Nav
None
AFCS
System Test pass
EAS
MFD
Pop-Up Alert
Alert Type
Flight
Instruments
TAWS System Status Annunciations
Flight
Planning
“Vertical track”
Additional
Features
Abnormal
Operation
Annun/
Alerts
“Traffic”
“Traffic Not Available”
“Traffic, Traffic”
“TAS System Test OK”
“TAS System Test
Failed”
Description
The aircraft has descended below the preset barometric minimum
descent altitude.
The aircraft is one minute from Top of Descent. Issued only when
vertical navigation is enabled.
Played when a Traffic Advisory (TA) is issued with the TIS system.
The aircraft is outside the Traffic Information Service (TIS) coverage area.
Played when a Traffic Advisory (TA) is issued with a TAS system.
Played when the TAS system passes a pilot-initiated self test.
Played when the TAS system fails a pilot-initiated self test.
Hazard
Avoidance
Voice Alert
“Minimums, minimums”
Procedures
Voice Alerts
Appendix
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
73
MFD & PFD Message Advisories
Message
Comments
DATA LOST – Pilot stored data was The pilot profile data was lost. System reverts
lost. Recheck settings.
to default pilot profile and settings. The pilot
may reconfigure the MFD & PFDs with preferred
settings, if desired.
XTALK ERROR – A flight display
The MFD and PFDs are not communicating
crosstalk error has occurred.
with each other. The G1000 system should be
serviced.
PFD1 SERVICE – PFD1 needs
service. Return unit for repair.
PFD2 SERVICE – PFD2 needs
The PFD and/or MFD self-test has detected a
service. Return unit for repair.
problem. The G1000 system should be serviced.
MFD1 SERVICE – MFD1 needs
service. Return unit for repair.
MANIFEST – PFD1 software
mismatch, communication halted.
MANIFEST – PFD2 software
The PFD and/or MFD has incorrect software
mismatch, communication halted. installed. The G1000 system should be serviced.
MANIFEST – MFD1 software
mismatch, communication halted.
PFD1 CONFIG – PFD1 config error.
The PFD configuration settings do not match
Config service req’d.
backup configuration memory. The G1000
PFD2 CONFIG – PFD2 config error. system should be serviced.
Config service req’d.
MFD1 CONFIG – MFD1 config
The MFD configuration settings do not match
error. Config service req’d.
backup configuration memory. The G1000
system should be serviced.
SW MISMATCH – GDU software
The MFD and PFDs have different software
version mismatch. Xtalk is off.
versions installed. The 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
74
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Annunciations & Alerts
Comments
EAS
The PFD and/or MFD is overheating and is
reducing power consumption by dimming the
display. If problem persists, the G1000 system
should be serviced.
Nav/Com/
XPDR/Audio
AFCS
A key is stuck on the PFD and/or MFD bezel.
Attempt to free the stuck key by pressing it
several times. The G1000 system should be
serviced if the problem persists.
GPS Nav
Flight
Planning
The PFD1 configuration module backup memory
has failed. The G1000 system should be
serviced.
The PFD1 voltage is low. The G1000 system
should be serviced.
The PFD2 voltage is low. The G1000 system
should be serviced.
The MFD voltage is low. The G1000 system
should be serviced.
Procedures
Hazard
Avoidance
Additional
Features
Message
PFD1 COOLING – PFD1 has poor
cooling. Reducing power usage.
PFD2 COOLING – PFD2 has poor
cooling. Reducing power usage.
MFD1 COOLING – MFD1 has poor
cooling. Reducing power usage.
PFD1 KEYSTK – PFD1 [key name]
Key is stuck.
PFD2 KEYSTK – PFD2 [key name]
Key is stuck.
MFD1 KEYSTK – MFD [key name]
Key is stuck.
CNFG MODULE – PFD1
configuration module is
inoperative.
PFD1 VOLTAGE – PFD1 has low
voltage. Reducing power usage
PFD2 VOLTAGE – PFD2 has low
voltage. Reducing power usage
MFD1 VOLTAGE – MFD1 has low
voltage. Reducing power usage
Flight
Instruments
MFD & PFD Message Advisories (Cont.)
Abnormal
Operation
Database Message Advisories
The MFD and/or PFD detected a failure in
the aviation database. Attempt to reload the
aviation database. If problem persists, the
G1000 system should be serviced.
Index
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Appendix
190-00708-02 Rev. A
Comments
Annun/
Alerts
Message
MFD1 DB ERR – MFD1 aviation
database error exists.
PFD1 DB ERR – PFD1 aviation
database error exists.
PFD2 DB ERR – PFD2 aviation
database error exists.
75
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
Database Message Advisories (Cont.)
Message
MFD1 DB ERR – MFD1 basemap
database error exists.
PFD1 DB ERR – PFD1 basemap
database error exists.
PFD2 DB ERR – PFD2 basemap
database error exists.
MFD1 DB ERR – MFD1 terrain
database error exists.
PFD1 DB ERR – PFD1 terrain
database error exists.
PFD2 DB ERR – PFD2 terrain
database error exists.
MFD1 DB ERR – MFD1 terrain
database missing.
PFD1 DB ERR – PFD1 terrain
database missing.
PFD2 DB ERR – PFD2 terrain
database missing.
MFD1 DB ERR – MFD1 obstacle
database error exists.
PFD1 DB ERR – PFD1 obstacle
database error exists.
PFD2 DB ERR – PFD2 obstacle
database error exists.
MFD1 DB ERR – MFD1 obstacle
database missing.
PFD1 DB ERR – PFD1 obstacle
database missing.
PFD2 DB ERR – PFD2 obstacle
database missing.
76
Comments
The MFD and/or PFD detected a failure in the
basemap database.
The MFD and/or PFD detected a failure in the
terrain database. Ensure that the terrain card is
properly inserted in display. Replace terrain card.
If problem persists, The G1000 system should be
serviced.
The terrain database is present on another LRU,
but is missing on the specified LRU.
The MFD and/or PFD detected a failure in the
obstacle database. Ensure that the data card is
properly inserted. Replace data card. If problem
persists, The G1000 system should be serviced.
The obstacle database is present on another LRU,
but is missing on the specified LRU.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Annunciations & Alerts
Comments
The MFD and/or PFD detected a failure in the
airport terrain database. Ensure that the data
card is properly inserted. Replace data card. If
problem persists, The G1000 system should be
serviced.
EAS
Nav/Com/
XPDR/Audio
AFCS
The airport terrain database is present on
another LRU, but is missing on the specified LRU.
Flight
Planning
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
77
Hazard
Avoidance
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Procedures
The MFD and/or PFD detected a failure in the
Safe Taxi database. Ensure that the data card is
properly inserted. Replace data card. If problem
persists, The G1000 system should be serviced.
The MFD detected a failure in the ChartView
database (optional feature). Ensure that the
data card is properly inserted. Replace data card.
If problem persists, The G1000 system should be
serviced.
MFD1 DB ERR – MFD1 FliteCharts The MFD detected a failure in the FliteCharts
database error exists.
database (optional feature). Ensure that the
data card is properly inserted. Replace data card.
If problem persists, The G1000 system should be
serviced.
DB MISMATCH – Aviation
The PFDs and MFD have different aviation
database version mismatch. Xtalk database versions installed. Crossfill is off.
is off.
Install correct aviation database version in all
displays.
190-00708-02 Rev. A
GPS Nav
Message
MFD1 DB ERR – MFD1 airport
terrain database error exists.
PFD1 DB ERR – PFD1 airport
terrain database error exists.
PFD2 DB ERR – PFD2 airport
terrain database error exists.
MFD1 DB ERR – MFD1 airport
terrain database missing.
PFD1 DB ERR – PFD1 airport
terrain database missing.
PFD2 DB ERR – PFD2 airport
terrain database missing.
MFD1 DB ERR – MFD1 Safe Taxi
database error exists.
PFD1 DB ERR – PFD1 Safe Taxi
database error exists.
PFD2 DB ERR – PFD2 Safe Taxi
database error exists.
MFD1 DB ERR – MFD1 Chartview
database error exists.
Flight
Instruments
Database Message Advisories (Cont.)
Database Message Advisories (Cont.)
Message
DB MISMATCH – Aviation
database type mismatch. Xtalk is
off.
Comments
The PFDs and MFD have different aviation
database types installed (Americas, European,
etc.). Crossfill is off. Install correct aviation
database type in all displays.
DB MISMATCH – Terrain database The PFDs and MFD have different terrain
version mismatch.
database versions installed. Install correct terrain
database version in all displays.
DB MISMATCH – Terrain database The PFDs and MFD have different terrain
type mismatch.
database types installed. Install correct terrain
database type in all displays.
DB MISMATCH – Obstacle
The PFDs and MFD have different obstacle
database version mismatch.
database versions installed. Install correct
obstacle database version in all displays.
DB MISMATCH – Airport Terrain
The PFDs and MFD have different airport terrrain
database mismatch.
databases installed. Install correct airport terrain
database in all displays.
GMA 1347D Message Advisories
Message
Comments
GMA1 FAIL – GMA1 is inoperative. The audio panel self-test has detected a failure.
GMA2 FAIL – GMA2 is inoperative. The audio panel is unavailable. The G1000
system should be serviced.
GMA XTALK – GMA crosstalk error An error has occurred in transferring data
has occurred.
between the two GMAs. The G1000 system
should be serviced.
GMA1 CONFIG – GMA1 config
The audio panel configuration settings do not
error. Config service req’d.
match backup configuration memory. The
GMA2 CONFIG – GMA2 config
G1000 system should be serviced.
error. Config service req’d.
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
78
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Annunciations & Alerts
Comments
The audio panel has incorrect software installed. The
G1000 system should be serviced.
Nav/Com/
XPDR/Audio
AFCS
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.
GPS Nav
GIA 63W Message Advisories
The GIA1 and/or GIA2 configuration settings do
not match backup configuration memory. The
G1000 system should be serviced.
Procedures
The GIA1 and/or GIA2 have an error in the audio
configuration. The G1000 system should be
serviced.
Additional
Features
Abnormal
Operation
The GIA1 and/or GIA2 temperature is too low
to operate correctly. Allow units to warm up to
operating temperature.
Appendix
Index
The GIA1 and/or GIA2 self-test has detected a
problem in the unit. The G1000 system should
be serviced.
Annun/
Alerts
The GIA1 and/or GIA2 temperature is too high.
If problem persists, the G1000 system should be
serviced.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Hazard
Avoidance
190-00708-02 Rev. A
Comments
Flight
Planning
Message
GIA1 CONFIG – GIA1 config error.
Config service req’d.
GIA2 CONFIG – GIA2 config error.
Config service req’d.
GIA1 CONFIG – GIA1 audio config
error. Config service req’d.
GIA2 CONFIG – GIA2 audio config
error. Config service req’d.
GIA1 COOLING – GIA1
temperature too low.
GIA2 COOLING – GIA2
temperature too low.
GIA1 COOLING – GIA1 over
temperature.
GIA2 COOLING – GIA2 over
temperature.
GIA1 SERVICE – GIA1 needs
service. Return the unit for repair.
GIA2 SERVICE – GIA2 needs
service. Return the unit for repair.
EAS
Message
MANIFEST – GMA1 software
mismatch, communication halted.
MANIFEST – GMA2 software
mismatch, communication halted.
GMA1 SERVICE – GMA1 needs
service. Return unit for repair.
GMA2 SERVICE – GMA2 needs
service. Return unit for repair.
Flight
Instruments
GMA 1347D Message Advisories (Cont.)
79
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
GIA 63W Message Advisories (Cont.)
Message
HW MISMATCH – GIA hardware
mismatch. GIA1 communication
halted.
HW MISMATCH – GIA hardware
mismatch. GIA2 communication
halted.
MANIFEST – GIA1 software
mismatch, communication halted.
MANIFEST – GIA2 software
mismatch, communication halted.
MANIFEST – GFC software
mismatch, communication halted.
COM1 TEMP – COM1 over temp.
Reducing transmitter power.
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
Comments
COM1 SERVICE – COM1 needs
service. Return unit for repair.
COM2 SERVICE – COM2 needs
service. Return unit for repair.
COM1 PTT – COM1 push-to-talk
key is stuck.
COM2 PTT – COM2 push-to-talk
key is stuck.
The system has detected a failure in COM1
and/or COM2. COM1 and/or COM2 may still be
usable. The G1000 system should be serviced
when possible.
COM1 RMT XFR – COM1 remote
transfer key is stuck.
COM2 RMT XFR – COM2 remote
transfer key is stuck.
80
A GIA mismatch has been detected, where only
one is WAAS capable.
The GIA1 and/or GIA 2 has incorrect software
installed. The G1000 system should be serviced.
Incorrect servo software is installed, or gain
settings are incorrect.
The system has detected an over temperature
condition in COM1 and/or COM2. The
transmitter is operating at reduced power. If the
problem persists, the G1000 system should be
serviced.
The COM1 and/or COM2 external push-to-talk
switch is stuck in the enable (or “pressed”)
position. Press the PTT switch again to cycle its
operation.
If the problem persists, the G1000 system should
be serviced.
The COM1 and/or COM2 transfer switch is stuck
in the enabled (or “pressed”) position. Press the
transfer switch again to cycle its operation. If
the problem persists, the G1000 system should
be serviced.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Annunciations & Alerts
Abort approach due to loss of GPS navigation.
Vertical guidance generated by WAAS is
unavailable, use LNAV only minimums.
Displayed after passing the first waypoint of a
true north approach when the nav angle is set
to ‘AUTO’.
Flight
Planning
Procedures
A failure has been detected in the GPS1
and/or GPS2 receiver. The receiver may still be
available. The G1000 system should be serviced.
Annun/
Alerts
Appendix
Index
A failure has been detected in glideslope
receiver 1 and/or receiver 2. The G1000 system
should be serviced.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Abnormal
Operation
The remote NAV1 and/or NAV2 transfer switch
is stuck in the enabled (or “pressed”) state.
Press the transfer switch again to cycle its
operation. If the problem persists, the G1000
system should be serviced.
Additional
Features
A failure has been detected in the NAV1
and/or NAV2 receiver. The receiver may still be
available. The G1000 system should be serviced.
Hazard
Avoidance
190-00708-02 Rev. A
Loss of GPS navigation due to GPS failure.
GPS Nav
G/S2 FAIL – G/S2 is inoperative.
AFCS
G/S1 FAIL – G/S1 is inoperative.
Loss of GPS navigation due to position error.
Nav/Com/
XPDR/Audio
GPS1 SERVICE – GPS1 needs
service. Return unit for repair.
GPS2 SERVICE – GPS2 needs
service. Return unit for repair.
NAV1 SERVICE – NAV1 needs
service. Return unit for repair.
NAV2 SERVICE – NAV2 needs
service. Return unit for repair.
NAV1 RMT XFR – NAV1 remote
transfer key is stuck.
NAV2 RMT XFR – NAV2 remote
transfer key is stuck.
Comments
GPS integrity is insufficient for the current phase
of flight.
Loss of GPS navigation due to insufficient
satellites.
EAS
Message
LOI – GPS integrity lost. Crosscheck
with other NAVS.
GPS NAV LOST – Loss of GPS
navigation. Insufficient satellites.
GPS NAV LOST – Loss of GPS
navigation. Position error.
GPS NAV LOST – Loss of GPS
navigation. GPS fail.
ABORT APR – Loss of GPS
navigation. Abort approach.
APR DWNGRADE – Approach
downgraded.
TRUE APR – True north approach.
Change HDG reference to TRUE.
Flight
Instruments
GIA 63W Message Advisories (Cont.)
81
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
GIA 63W Message Advisories (Cont.)
Message
G/S1 SERVICE – G/S1 needs
service. Return unit for repair.
G/S2 SERVICE – G/S2 needs
service. Return unit for repair.
Comments
A failure has been detected in glideslope
receiver 1 and/or receiver 2. The receiver may
still be available. The G1000 system should be
serviced when possible.
GEA 71 Message Advisories
Message
Comments
GEA1 CONFIG – GEA1 config error. The GEA1 configuration settings do not match
Config service req’d.
those of backup configuration memory. The
G1000 system should be serviced.
GEA2 CONFIG – GEA2 config error. The GEA2 configuration settings do not match
Config service req’d.
those of backup configuration memory. The
G1000 system should be serviced.
MANIFEST – GEA1 software
The #1 GEA 71 has incorrect software installed.
mismatch, communication halted. The G1000 system should be serviced.
MANIFEST – GEA2 software
The #2 GEA 71 has incorrect software installed.
mismatch, communication halted. The G1000 system should be serviced.
GTX 33/33D Message Advisories
Message
XPDR1 CONFIG – XPDR1 config
error. Config service req’d.
XPDR2 CONFIG – XPDR2 config
error. Config service req’d.
MANIFEST – GTX1 software
mismatch, communication halted.
MANIFEST – GTX2 software
mismatch, communication halted.
82
Comments
The transponder configuration settings do not
match those of backup configuration memory.
The G1000 system should be serviced.
The transponder configuration settings do not
match those of backup configuration memory.
The G1000 system should be serviced.
The transponder has incorrect software installed.
The G1000 system should be serviced.
The transponder has incorrect software installed.
The G1000 system should be serviced.
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Annunciations & Alerts
Comments
The #1 transponder should be serviced when
possible.
The #2 transponder should be serviced when
possible.
There is no communication with the #1
transponder.
There is no communication with the #2
transponder.
EAS
Nav/Com/
XPDR/Audio
AFCS
Message
XPDR1 SRVC – XPDR1 needs
service. Return unit for repair.
XPDR2 SRVC – XPDR2 needs
service. Return unit for repair.
XPDR1 FAIL – XPDR1 is
inoperative.
XPDR2 FAIL – XPDR2 is
inoperative.
Flight
Instruments
GTX 33/33D Message Advisories (Cont.)
GPS Nav
GRS 77 Message Advisories
83
Index
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Appendix
190-00708-02 Rev. A
Annun/
Alerts
AHRS2 GPS – AHRS2 not receiving
any GPS information.
Abnormal
Operation
AHRS1 GPS – AHRS1 not receiving
any GPS information.
Additional
Features
AHRS2 GPS – AHRS2 using backup
GPS source.
Hazard
Avoidance
AHRS1 GPS – AHRS1 using backup
GPS source.
Procedures
AHRS2 TAS – AHRS2 not receiving
valid airspeed.
Comments
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 #2 AHRS is not receiving true airspeed from
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed.
The G1000 system should be serviced.
The #1 AHRS is using the backup GPS path.
Primary GPS path has failed. The G1000 system
should be serviced when possible.
The #2 AHRS is using the backup GPS path.
Primary GPS path has failed. The G1000 system
should be serviced when possible.
The #1 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
G1000 system should be serviced.
The #2 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
G1000 system should be serviced.
Flight
Planning
Message
AHRS1 TAS – AHRS1 not receiving
valid airspeed.
GRS 77 Message Advisories (Cont.)
Message
Comments
AHRS1 GPS – AHRS1 not receiving The #1 AHRS is not receiving backup GPS
backup GPS information.
information. The G1000 system should be
serviced.
AHRS2 GPS – AHRS2 not receiving The #2 AHRS is not receiving backup GPS
backup GPS information.
information. The G1000 system should be
serviced.
AHRS1 GPS – AHRS1 operating
The #1 AHRS is operating exclusively in no-GPS
exclusively in no-GPS mode.
mode. The G1000 system should be serviced.
AHRS2 GPS – AHRS2 operating
The #2 AHRS is operating exclusively in no-GPS
exclusively in no-GPS mode.
mode. The G1000 system should be serviced.
AHRS MAG DB – AHRS magnetic
The #1 AHRS and #2 AHRS magnetic model
model database version mismatch. database versions do not match.
AHRS1 SRVC – AHRS1 Magnetic- The #1 AHRS earth magnetic field model is out
field model needs update.
of date. Update magnetic field model when
practical.
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.
GEO LIMITS – AHRS1 too far
North/South, no magnetic compass. The aircraft is outside geographical limits for
approved AHRS operation. Heading is flagged
GEO LIMITS – AHRS2 too far
as invalid.
North/South, no magnetic compass.
MANIFEST – GRS1 software
The #1 AHRS has incorrect software installed.
mismatch, communication halted.
The G1000 system should be serviced.
MANIFEST – GRS2 software
The #2 AHRS has incorrect software installed.
mismatch, communication halted.
The 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
84
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Annunciations & Alerts
AFCS
GPS Nav
The GMU 44 has incorrect software installed.
The G1000 system should be serviced.
Flight
Planning
MANIFEST – GMU1 software
mismatch, communication halted.
MANIFEST – GMU2 software
mismatch, communication halted.
Nav/Com/
XPDR/Audio
HDG FAULT – AHRS2
magnetometer fault has occurred.
Comments
A fault has occurred in the #1 GMU 44.
Heading is flagged as invalid. The AHRS uses
GPS for backup mode operation. The G1000
system should be serviced.
A fault has occurred in the #2 GMU 44.
Heading is flagged as invalid. The AHRS uses
GPS for backup mode operation. The G1000
system should be serviced.
EAS
Message
HDG FAULT – AHRS1
magnetometer fault has occurred.
Flight
Instruments
GMU 44 Message Advisories
GDL 69A Message Advisories
Additional
Features
Abnormal
Operation
MANIFEST – GDL software
mismatch, communication halted.
Comments
GDL 69 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.
A failure has been detected in the GDL 69.
The receiver is unavailable. The G1000 system
should be serviced
The GDL 69 has incorrect software installed.
The G1000 system should be serviced.
Hazard
Avoidance
GDL69 FAIL – GDL 69 has failed.
Procedures
Message
GDL69 CONFIG – GDL 69 config
error. Config service req’d.
Annun/
Alerts
Appendix
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
85
GWX 68 Alert Messages
Message
GWX CONFIG – GWX config error.
Config service req’d.
GWX FAIL – GWX is inoperative.
GWX SERVICE – GWX needs
service. Return unit for repair.
MANIFEST – GWX software
mismatch, communication halted.
WX ALERT – Possible severe
weather ahead.
Comments
GWX 68 configuration settings do not match
those of the GDU configuration. The G1000
system should be serviced.
The GDU is not recieving status packet from the
GWX 68 or the GWX 68 is reporting a fault.
The GWX 68 radar system should be serviced.
A failure has been detected in the GWX 68. The
GWX 68 may still be usable.
The GWX 68 has incorrect software installed.
The G1000 system should be serviced.
Possible severe weather detected within +/- 10
degrees of the aircraft heading at a range of 80
to 320 nm.
GDC 74B Message Advisories
Message
ADC1 ALT EC – ADC1 altitude error
correction is unavailable.
ADC2 ALT EC – ADC2 altitude error
correction is unavailable.
ADC1 AS EC – ADC1 airspeed error
correction is unavailable.
ADC2 AS EC – ADC2 airspeed error
correction is unavailable.
MANIFEST – GDC1 software
mismatch, communication halted.
MANIFEST – GDC2 software
mismatch, communication halted.
Comments
GDC1 or GDC2 is reporting that the altitude
error correction is unavailable.
GDC1 or GDC2 is reporting that the airspeed
error correction is unavailable.
The GDC 74B has incorrect software installed.
The 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
86
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Annunciations & Alerts
Flight
Planning
Comments
Procedures
Error in the configuration of the GMC 710.
Hazard
Avoidance
A failure has been detected in the GMC 710.
The GMC 710 is unavailable.
The GMC 710 has incorrect software installed.
The G1000 system should be serviced.
A key is stuck on the GMC 710 bezel. Attempt
to free the stuck key by pressing it several
times. The G1000 system should be serviced if
the problem persists.
Additional
Features
Abnormal
Operation
MANIFEST – GMC software
mismatch. Communication halted.
GMC KEYSTK – GMC [key name]
Key is stuck.
GPS Nav
GMC 710 Message Advisories
Message
GMC CONFIG – GMC Config error.
Config service req’d.
GMC FAIL – GMC is inoperative.
AFCS
MANIFEST – GCU software
mismatch, communication halted.
GCU KEYSTK – GCU [key name]
Key is stuck.
Nav/Com/
XPDR/Audio
GCU FAIL – GCU is inoperative.
Comments
GCU 475 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.
A failure has been detected in the GCU 475.
The GCU 475 is unavailable.
The GCU 475 has incorrect software installed.
The G1000 system should be serviced.
A key is stuck on the GCU 475 bezel. Attempt
to free the stuck key by pressing it several times.
The G1000 system should be serviced if the
problem persists.
EAS
Message
GCU CNFG – GCU Config error.
Config service req’d.
Flight
Instruments
GCU 475 Message Advisories
Annun/
Alerts
Appendix
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
87
Miscellaneous Message Advisories
Message
FPL WPT LOCK – Flight plan
waypoint is locked.
Comments
Upon power-up, the G1000 system detects
that a stored flight plan waypoint is locked.
This occurs when an aviation 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.
FPL WPT MOVE – Flight plan
The system has detected that a waypoint
waypoint moved.
coordinate has changed due to a new aviation
database update. Verify that stored flight plans
contain correct waypoint locations.
TIMER EXPIRD – Timer has expired. The system notifies the pilot that the timer has
expired.
DB CHANGE – Database changed. This occurs when a stored flight plan contains
Verify user modified procedures.
procedures that have been manually edited.
This alert is issued only after an aviation
database update. Verify that the user-modified
procedures in stored flight plans are correct and
up to date.
DB CHANGE – Database changed. This occurs when a stored flight plan contains
Verify stored airways.
an airway that is no longer consistent with
the aviation database. This alert is issued only
after an aviation database update. Verify use
of airways in stored flight plans and reload
airways as needed.
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
88
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Annunciations & Alerts
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
89
GPS Nav
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
AFCS
190-00708-02 Rev. A
Nav/Com/
XPDR/Audio
Comments
This occurs when a newly installed aviation
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.
LOCKED FPL – Cannot navigate
This occurs when the pilot attempts to activate
locked flight plan.
a stored flight plan that contains locked
waypoint. Remove locked waypoint from flight
plan. Update flight plan with current waypoint.
WPT ARRIVAL – Arriving at
Arriving at waypoint [xxxx], where [xxxx] is the
waypoint -[xxxx]
waypoint name.
STEEP TURN – Steep turn ahead.
A steep turn is 15 seconds ahead. Prepare to
turn.
INSIDE ARSPC – Inside airspace.
The aircraft is inside the airspace.
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 and Special use airspace is near and ahead of the
ahead.
aircraft position.
ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the
than 2 nm.
aircraft position.
APR INACTV – Approach is not
The system notifies the pilot that the loaded
active.
approach is not active. Activate approach when
required.
SLCT FREQ – Select appropriate
The system notifies the pilot to load the
frequency for approach.
approach frequency for the appropriate NAV
receiver. Select the correct frequency for the
approach.
SLCT NAV – Select NAV on CDI for The system notifies the pilot to set the CDI to
approach.
the correct NAV receiver. Set the CDI to the
correct NAV receiver.
EAS
Message
FPL TRUNC – Flight plan has been
truncated.
Flight
Instruments
Miscellaneous Message Advisories (Cont.)
Miscellaneous Message Advisories (Cont.)
Message
PTK FAIL – Parallel track unavailable:
bad geometry.
PTK FAIL – Parallel track unavailable:
invalid leg type.
PTK FAIL – Parallel track unavailable:
past IAF.
UNABLE V WPT – Can’t reach
current vertical waypoint.
VNV – Unavailable. Unsupported
leg type in flight plan.
VNV – Unavailable. Excessive track
angle error.
VNV – Unavailable. Excessive
crosstrack error.
VNV – Unavailable. Parallel course
selected.
NO WGS84 WPT – Non WGS 84
waypoint for navigation -[xxxx]
TRAFFIC FAIL – Traffic device has
failed.
FAILED PATH – A data path has
failed.
Comments
Bad parallel track geometry.
Invalid leg type for parallel offset.
IAF waypoint for parallel offset has been
passed.
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.
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.
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 selected waypoint [xxxx] does not use the
WGS 84 datum. Cross-check position with
alternate navigation sources.
The G1000 is no longer receiving data from
the traffic system. The traffic device should be
serviced.
A data path connected to the GDU or the GIA
63/W has failed.
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
90
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Annunciations & Alerts
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Comments
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°.
SVS – SVS DISABLED: Out of
Synthetic Vision is disabled because the aircraft
available terrain region.
is not within the boundaries of the installed
terrain database.
SVS – SVS 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.
SCHEDULER [#] – <message>.
Message criteria entered by the user.
ECS – Service required.
The environmental control system has failed.
CRUISE I – Cruise I conditions met. Cruise I engine trend data log has been
captured.
CRUISE II – Cruise II conditions met. Cruise II engine trend data log has been
captured.
EXCEEDANCE – Engine exceedance
An engine exceedance log has been captured.
data is being logged.
EAS
Message
MAG VAR WARN – Large magnetic
variance. Verify all course angles.
Flight
Instruments
Miscellaneous Message Advisories (Cont.)
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
91
Flight Plan Import/Export Messages
In some circumstances, some messages may appear in conjunction with others.
Flight Plan Import/Export
Results
Appendix
Index
Description
‘Flight plan successfully imported.’
A flight plan file stored on the SD card was successfully
imported as a stored flight plan.
‘File contained user waypoints only.
User waypoints imported successfully. No stored flight plan data was
modified.’
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.
‘No flight plan files found to import.’
The SD card contains no flight plan data.
‘Flight plan import failed.’
Flight plan data was not successfully imported from the SD card.
‘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.
‘User waypoint database full. Not all
loaded.’
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.
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Annunciations & Alerts
‘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.
‘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.
92
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Appendix
Flight
Instruments
Appendix
PFD Softkey Map
EAS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Top Level PFD Softkeys
Flight
Planning
Procedures
TRFC-1
Hazard
Avoidance
Select the BACK or OFF Softkey
to return to the top-level softkeys.
TRFC-2
Additional
Features
Inset Map Softkeys
Level 2
Level 3
Description
Displays Inset Map in PFD lower left corner
INSET
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
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
93
Index
DCLTR (3)
Appendix
Removes Inset Map
Annun/
Alerts
OFF
Abnormal
Operation
Level 1
Level 1
Level 2
Level 3
Nav/Com/
XPDR/Audio
TOPO
AFCS
TERRAIN
Displays NEXRAD weather and coverage
information on Inset Map (optional feature)
Displays XM lightning information on Inset
Map (optional feature)
NEXRAD
XM LTNG
Procedures
Flight
Planning
GPS Nav
Description
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
TRAFFIC
EAS
Flight
Instruments
Appendix
ADC1
ADC2
Hazard
Avoidance
Additional
Features
BACK
AHRS2
MSG
Select the BACK Softkey to
return to the top level softkeys.
Sensor Softkeys
Level 1
Level 2
Description
ADC1
ADC2
Selects the #2 Air Data Computer
AHRS1
Selects the #1 AHRS
AHRS2
Selects the #2 AHRS
Index
Appendix
Level 3
Displays softkeys for selecting the #1 and
#2 AHRS and Air Data Computers
Selects the #1 Air Data Computer
SENSOR
Annun/
Alerts
Abnormal
Operation
AHRS1
94
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Appendix
SYN VIS
Flight
Instruments
ADF/DME
ALT UNIT
HSI FMT
EAS
Select the BACK Softkey
to return to the top-level softkeys
Nav/Com/
XPDR/Audio
IN
HPA
Flight
Planning
PATHWAY
BACK
ARC HSI
GPS Nav
METERS
AFCS
360 HSI
SYN TERR HRZN HDG APTSIGNS
Procedures
PFD Configuration Softkeys
Level 2
Level 3
PFD
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Index
190-00708-02 Rev. A
Appendix
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.
Annun/
Alerts
SYN TERR
Abnormal
Operation
PATHWAY
Displays second-level softkeys for
additional PFD configurations
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
Additional
Features
SYN VIS
Description
Hazard
Avoidance
Level 1
95
Level 1
Level 2
Level 3
DFLTS
WIND
EAS
Flight
Instruments
Appendix
Nav/Com/
XPDR/Audio
OPTN 1
OPTN 2
AFCS
OPTN 3
Procedures
Flight
Planning
GPS Nav
OFF
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
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
Hazard
Avoidance
Additional
Features
BRG2
Abnormal
Operation
Wind direction arrow with direction
and speed
Information not displayed
Select to display the DME information
window
360 HSI
ARC HSI
Appendix
Annun/
Alerts
ALT UNIT
Index
Resets PFD to default settings, including
changing units to standard
Displays softkeys to select wind data
parameters
Wind direction arrows with headwind
and crosswind components
Wind direction arrow and speed
DME
HSI FRMT
STD BARO
96
Description
METERS
When enabled, displays altimeter in
meters
IN
Select to display the BARO setting as
inches of mercury
HPA
Select to display the BARO setting as
hectopacals
Sets altimeter setting to standard
barometric pressure
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Appendix
Flight
Instruments
MSG
EAS
Select the BACK Softkey to return
to the top-level softkeys.
Nav/Com/
XPDR/Audio
MSG
AFCS
Select the BACK Softkey to return
to the top-level softkeys.
Transponder Softkeys
Level 2
Level 3
GPS Nav
Level 1
Description
ALT
GND
VFR
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
97
Index
190-00708-02 Rev. A
Appendix
CODE
Annun/
Alerts
Removes numbers entered, one at a time
ON
Abnormal
Operation
BKSP
STBY
Additional
Features
0—7
Displays transponder mode selection
softkeys
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)
Manually selects Ground Mode, the
transponder does not allow Mode A
and Mode C replies, but it does permit
acquisition squitter and replies to discretely
addressed Mode S 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
Hazard
Avoidance
XPDR
Procedures
Displays the ADF/DME Tuning Window
Flight
Planning
ADF/DME
Level 1
Level 2
Level 3
Description
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
IDENT
MFD Softkey Map
CAS ↑
CAS ↓
DCLTR
MAP
(optional)
(optional)
SHW CHRT
CHKLIST
DCLTR-1
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Appendix
DCLTR-2
Procedures
DCLTR-3
Hazard
Avoidance
TRAFFIC
TOPO
TERRAIN
Select the BACK Softkey on this level to
return to the top softkey level.
AIRWAYS
(optional)
(optional)
NEXRAD
XM LTNG
BACK
AIRWY ON
Additional
Features
AIRWY LO
AIRWAY HI
Level 1
Appendix
CAS ↑
CAS ↓
Index
Annun/
Alerts
Abnormal
Operation
MFD Softkeys
MAP
98
Level 2
Description
Scroll up (Displayed only when a sufficient
number of items are displayed in the Crew
Alerting System Display to warrant scrolling)
Scroll down (Displayed only when a sufficient
number of items are displayed in the Crew Alerting System Display to warrant scrolling)
Enables second-level Navigation Map softkeys
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Appendix
Level 2
Description
Flight
Instruments
Level 1
TRAFFIC Displays traffic information on Navigation Map
Displays topographical data (e.g., coastlines,
terrain, rivers, lakes) and elevation scale on
Navigation Map
TERRAIN Displays terrain information on Navigation Map
TOPO
EAS
Nav/Com/
XPDR/Audio
Procedures
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
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
CHKLIST
Flight
Planning
SHW CHRT
GPS Nav
DCLTR (3)
AFCS
AIRWAYS 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
NEXRAD Displays NEXRAD weather and coverage
information on Navigation Map (optional feature)
XM LTNG Displays XM lightning information on Navigation
Map (optional feature)
Returns to top-level softkeys
BACK
Appendix
Index
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
99
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
100
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Index
E
Edit a flight plan 34
Enable Terrain 48
Engine display 5
Essential bus voltage 5
Procedures
Hazard
Avoidance
F
Annun/
Alerts
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Abnormal
Operation
Flap position 5
Asymmetrical deflection warning 65
Flight Director 15
Flight ID 11
Flight path marker 55
FliteCharts® 56, 57
Frequency Transfer 12
Fuel
Alerts 65–66
Flow 5
Pressure 5
Quantity 5
Additional
Features
190-00708-02 Rev. A
Flight
Planning
Cabin pressure altitude 5
Warning 65
CDI 1, 2, 12, 89
Cell 41, 42
Cell mode 42
Channel Presets 60
GPS Nav
C
AFCS
Barometric Altitude Minimums 3
Battery
Alerts 66
Current 5
Overheat warning 65
Voltage 5
Bearing line 51, 52, 53
DCLTR Softkey 56
Dead Reckoning 63
Declutter 62, 93, 99
Designated altitudes 22
Differential cabin pressure 5
Warning 65
Direct-to 19
DME 11, 12
Door status 9
DR mode 63, 64
Nav/Com/
XPDR/Audio
B
D
EAS
Activate a flight plan 20
Active Channel 59
ADF 11, 12, 62
AHRS 83, 84, 85, 87
Airport Signs 55, 56
Airways 99
Air Data Computer 68
Alert messages 86
ALT 46
Altimeter setting 1, 62
Altitude mode 46
Altitude volume 46
Antenna stabilization 53
Antenna tilt 51
Attitude & Heading Reference System
68
Audio panel controls
NAV1, NAV2 12
ChartView 56, 57
Code selection softkeys 12
COM 12, 61
Flight
Instruments
A
Index-1
G
N
Gain 52
Generator
Current 5
Speed 5
NACO 57
NAV 12
NAV1 2, 12
NAV2 2, 12
Navigation database 21, 22
NEXRAD 43, 44, 94, 99
H
Horizontal scan 52
Horizon heading 55
I
Inhibit 48, 50
Inhibit TAWS 50
Inhibit Terrain 48
Inset Map 93, 94
Interturbine Temperature (ITT) 5
Warning 65
IOI 70, 72
J
OBS 2
Obstacles 78, 80
Oil, engine
Alerts 65
Pressure 5
Temperature 5
Overspeed Protection 16
Oxygen
Pressure 5
Warning 65
P
Lightning 41, 42
Pathways 55, 56
PIT 68
Propeller speed 5
M
R
Map panning 43
Message advisories 74–79, 81–85,
87–91
METAR 43
Minimums 73
MISCOMP 68
Mode S 97
Mode selection softkeys 12
Multi Function Display (MFD)
Softkeys 98
Reversionary Mode
EICAS 5
Reversionary mode 61
ROC 70, 71, 72
Index
Appendix
Annun/
Alerts
Additional
Features
Jeppesen 57
O
Abnormal
Operation
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EAS
Flight
Instruments
Index
L
Index-2
S
SafeTaxi® 56
Sector scan 53
Sensor 68
STAB 53
Standby 51
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
Index
X
EAS
XM lightning 94, 99
XM weather 43
Nav/Com/
XPDR/Audio
T
Weather data link page 43
Weather radar 50
Wind data 96
Flight
Instruments
Store Flight Plan 34
Stormscope lightning data 41, 42
Strike 41
Strike mode 42
SVS 55, 91
Synthetic Vision System 55
AFCS
TA 73
TAF 43
TAS 45, 46, 73, 83
TAWS 49, 50, 71, 73
TAWS-B 49
Terrain 46, 47, 49, 78, 94, 99
Terrain-SVS 47, 48
Tilt line 51
Timer 2, 88
Topographical data 94, 99
Torque 5
Warning 65
Traffic 41, 45, 99
Traffic advisory 45
Traffic Advisory 73
Traffic map page 45, 46, 47
Transponder 11, 12, 97, 98
Trim 5
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
V
Annun/
Alerts
Vertical speed guidance 22
Vertical track 73
VNV 19, 62, 90
Vspeed 2
Appendix
W
190-00708-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
Index
WAAS 80
WATCH® 53
Weather Attenuated Color Highlight 53
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
190-00708-02 Rev. A
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, Bulls Copse Road
Hounsdown Business Park
Southampton, SO40 9RB, U.K.
p: 44/0870.8501241 f: 44/0870.8501251
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 Garmin Ltd. or its subsidiaries
190-00708-02 Rev. A