Garmin | G1000 NXI: Socata TBM 910 | Garmin G1000 NXI: Socata TBM 910 G1000 NXI Cockpit Reference Guide for Socata TBM 910 - SSV 2883.00

Garmin G1000 NXI: Socata TBM 910 G1000 NXI Cockpit Reference Guide for Socata TBM 910 - SSV 2883.00
®
Cockpit Reference Guide
Daher TBM 910
System Software Version 2883.00 or later
FLIGHT INSTRUMENTS
ENGINE INDICATION SYSTEM (EIS)
NAV/COM/TRANSPONDER/AUDIO PANEL
FLIGHT MANAGEMENT SYSTEM
HAZARD AVOIDANCE
FLIGHT DIRECTOR
ADDITIONAL FEATURES
ABNORMAL OPERATIONS
ANNUNCIATIONS & ALERTS
APPENDIX
INDEX
Copyright © 2017 - 2019 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 2883.00 or later for the G1000
NXi Daher TBM 910 Series. Some differences in operation may be observed when comparing
the information in this manual to earlier or later software versions.
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190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
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“AOPA”) expressly disclaim all warranties, with respect to the AOPA information included in this
data, express or implied, including, but not limited to, the implied warranties of merchantability
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do not allow the limitation or exclusion of implied warranties or liability for incidental or
consequential damages so the above limitations or exclusions may not apply to licensee.
Printed in the U.S.A.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Warnings, Cautions & Notes
WARNING: Do not use terrain avoidance displays as the sole source
of information for maintaining separation from terrain and obstacles.
Garmin obtains terrain and obstacle data from third party sources and
cannot independently verify the accuracy of the information.
WARNING: Always refer to current aeronautical charts and NOTAMs
for verification of displayed aeronautical information. Displayed
aeronautical data may not incorporate the latest NOTAM information.
WARNING: Do not use geometric altitude for compliance with air traffic
control altitude requirements. The primary barometric altimeter must
be used for compliance with all air traffic control altitude regulations,
requirements, instructions, and clearances.
WARNING: Do not use basemap information (land and water data) as the
sole means of navigation. Basemap data is intended only to supplement
other approved navigation data sources and should be considered only
an aid to enhance situational awareness.
WARNING: Do not rely solely upon the display of traffic information to
accurately depict all of the traffic within range of the aircraft. Due to lack
of equipment, poor signal reception, and/or inaccurate information from
aircraft or ground stations, traffic may be present that is not represented
on the display.
WARNING: Do not use data link weather information for maneuvering
in, near, or around areas of hazardous weather. Information contained
within data link weather products may not accurately depict current
weather conditions.
WARNING: Do not operate this equipment without first obtaining
qualified instruction.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Warnings, Cautions & Notes
WARNING: Do not use the indicated data link weather product age
to determine the age of the weather information shown by the data
link weather product. Due to time delays inherent in gathering and
processing weather data for data link transmission, the weather
information shown by the data link weather product may be older than
the indicated weather product age.
WARNING: The displayed minimum safe altitude (MSAs) are only advisory
in nature and should not be relied upon as the sole source of obstacle
and terrain avoidance information. Always refer to current aeronautical
charts for appropriate minimum clearance altitudes.
WARNING: Do not use a QFE altimeter setting with this system. System
functions will not operate properly with a QFE altimeter setting. Use
only a QNH altimeter setting for height above mean sea level, or the
standard pressure setting, as applicable.
WARNING: Do not use GPS to navigate to any active waypoint identified
as a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’
waypoints are derived from an unknown map reference datum that may
be incompatible with the map reference datum used by GPS (known as
WGS84) and may be positioned in error as displayed.
WARNING: Do not rely on the autopilot to level the aircraft at the MDA/
DH when flying an approach with vertical guidance. The autopilot will
not level the aircraft at the MDA/DH even if the MDA/DH is set in the
altitude preselect.
WARNING: Do not use the Garmin SVT runway depiction as the sole
means for determining the proximity of the aircraft to the runway or for
maintaining the proper approach path angle during landing.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Warnings, Cautions & Notes
WARNING: Do not rely solely upon the display of traffic information for
collision avoidance maneuvering. The traffic display does not provide
collision avoidance resolution advisories and does not under any
circumstances or conditions relieve the pilot’s responsibility to see and
avoid other aircraft.
WARNING: Do not rely on the accuracy of attitude and heading indications
in the following geographic areas (due to variations in the earth’s
magnetic field): North of 72° North latitude at all longitudes; South
of 70° South latitude at all longitudes; North of 65° North latitude
between longitude 75° W and 120° W. (Northern Canada); North of
70° North latitude between longitude 70° W and 128° W. (Northern
Canada); North of 70° North latitude between longitude 85° E and 114°
E. (Northern Russia); South of 55° South latitude between longitude
120° E and 165° E. (Region south of Australia and New Zealand).
WARNING: Do not rely on information from a lightning detection system
display as the sole basis for hazardous weather avoidance. Range
limitations and interference may cause the system to display inaccurate
or incomplete information. Refer to documentation from the lightning
detection system manufacturer for detailed information about the
system.
WARNING: Use appropriate primary systems for navigation, and for
terrain, obstacle, and traffic avoidance. Garmin SVT is intended as an aid
to situational awareness only and may not provide either the accuracy
or reliability upon which to solely base decisions and/or plan maneuvers
to avoid terrain, obstacles, or traffic.
WARNING: Intruder aircraft at or below 500 ft. AGL may not appear on
the Garmin SVT display or may appear as a partial symbol.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Warnings, Cautions & Notes
WARNING: Do not operate the weather radar in a transmitting mode
when personnel or objects are within the MPEL boundary.
WARNING: Always position the weather radar gain setting to Calibrated
for viewing the actual intensity of precipitation. Changing the gain in
weather mode causes precipitation intensity to be displayed as a color
not representative of the true intensity.
WARNING: Do not use TAWS information for primary terrain or obstacle
avoidance. TAWS is intended only to enhance situational awareness.
WARNING: Do not use SurfaceWatch™ information as the primary method
of flight guidance during airborne or ground operations. SurfaceWatch
does not have NOTAM or ATIS information regarding the current active
runway, condition, or information about the position of hold lines.
CAUTION: Do not clean display surfaces with abrasive cloths or cleaners
containing ammonia. They will harm the anti-reflective coating.
CAUTION: Do not allow repairs to be made by anyone other than an
authorized Garmin service center. Unauthorized repairs or modifications
could void both the warranty and affect the airworthiness of the aircraft.
CAUTION: Never disconnect power to the system when loading a
database. Power interruption during the database loading process
could result in maintenance being required to reboot the system.
NOTE: Do not rely solely upon data link services to provide Temporary
Flight Restriction (TFR) information. Always confirm TFR information
through official sources such as Flight Service Stations or Air Traffic
Control.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Warnings, Cautions & Notes
NOTE: All visual depictions contained within this document, including
screen images of the system panel and displays, are subject to change
and may not reflect the most current system and aviation databases.
Depictions of equipment may differ slightly from the actual equipment.
NOTE: The United States government operates the Global Positioning
System and is solely responsible for its accuracy and maintenance. The
GPS system is subject to changes which could affect the accuracy and
performance of all GPS equipment. Portions of the system utilize GPS
as a precision electronic NAVigation AID (NAVAID). Therefore, as with
all NAVAIDs, information presented by the system can be misused or
misinterpreted and, therefore, become unsafe.
NOTE: This device complies with part 15 of the FCC Rules. Operation is
subject to the following two conditions: (1) this device may not cause
harmful interference, and (2) this device must accept any interference
received, including interference that may cause undesired operation.
NOTE: 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 system responds to a terminal procedure based on data
coded within that procedure in the Navigation Database. Differences in
system operation may be observed among similar types of procedures
due to differences in the Navigation Database coding specific to each
procedure.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Warnings, Cautions & Notes
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: Operating the system in the vicinity of metal buildings, metal
structures, or electromagnetic fields can cause sensor differences that
may result in nuisance miscompare annunciations during start up,
shut down, or while taxiing. If one or more of the sensed values are
unavailable, the annunciation indicates no comparison is possible.
NOTE: The FAA has asked Garmin to remind pilots who fly with Garmin
database-dependent avionics of the following:
• It is the pilot’s responsibility to remain familiar with all FAA regulatory and
advisory guidance and information related to the use of databases in the
National Airspace System.
• Garmin equipment will only recognize and use databases that are obtained
from Garmin or Jeppesen. Databases obtained from Garmin or Jeppesen
that have a Type 2 Letter of Authorization (LOA) from the FAA are assured
compliance with all data quality requirements (DQRs). A copy of the Type
2 LOA is available for each applicable database and can be viewed at
http://fly.garmin.com by selecting ‘Aviation Database Declarations.’
• Use of a current Garmin or Jeppesen database in your Garmin equipment
is required for compliance with established FAA regulatory guidance, but
does not constitute authorization to fly any and all terminal procedures
that may be presented by the system. It is the pilot’s responsibility to
operate in accordance with established AFM(S) and regulatory guidance or
limitations as applicable to the pilot, the aircraft, and installed equipment.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Warnings, Cautions & Notes
NOTE: The pilot/operator must review and be familiar with Garmin’s
database exclusion list as discussed in SAIB CE-14-04 to determine what
data may be incomplete. The database exclusion list can be viewed at
www.flygarmin.com by selecting ‘Database Exclusions List.’
NOTE: The pilot/operator must have access to Garmin and Jeppesen
database alerts and consider their impact on the intended aircraft
operation. The database alerts can be viewed at www.flygarmin.com by
selecting ‘Aviation Database Alerts.’
NOTE: If the pilot/operator wants or needs to adjust the database,
contact Garmin Product Support.
NOTE: Garmin requests the flight crew report any observed discrepancies
related to database information. These discrepancies could come
in the form of an incorrect procedure; incorrectly identified terrain,
obstacles and fixes; or any other displayed item used for navigation or
communication in the air or on the ground. Go to FlyGarmin.com and
select ‘Aviation Data Error Report’.
NOTE: Electronic aeronautical charts displayed on this system have been
shown to meet the guidance in AC 120-76D as a Type B Electronic Flight
Bag (EFB) for FlightCharts and ChartView. The accuracy of the charts is
subject to the chart data provider. Own-ship position on airport surface
charts cannot be guaranteed to meet the accuracy specified in AC 12076D. Possible additional requirements may make a secondary source
of aeronautical charts, such as traditional paper charts or an additional
electronic display, necessary on the aircraft and available to the pilot.
If the secondary source of aeronautical charts is a Portable Electronic
Device (PED), its use must be consistent with the guidance in AC 12076D.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Warnings, Cautions & Notes
NOTE: The navigation databases used in Garmin navigation systems
contain Special Procedures. Prior to flying these procedures, pilots
must have specific FAA authorization, training, and possession of the
corresponding current, and legitimately-sourced chart (approach plate,
etc.). Inclusion of the Special Procedure in the navigation database
DOES NOT imply specific FAA authorization to fly the procedure.
NOTE: Terrain and obstacle alerting is not available north of 89º North
latitude and south of 89º South latitude. This is due to limitations
present within the Terrain database and the system’s ability to process
the data representing the affected areas.
NOTE: The nose of the ‘own ship’ symbol represents the location of the
aircraft. The center of any traffic symbol represents the location of that
traffic. The traffic and own ship symbols are an abstract representation
and do not reflect the physical extent of the aircraft/traffic, and should
not replace other methods for identifying traffic.
NOTE: Intruder aircraft at or below 500 ft. AGL may not appear on the
Garmin SVT display or may appear as a partial symbol.
NOTE: When using Stormscope, there are several atmospheric phenomena
in addition to nearby thunderstorms that can cause isolated discharge
points in the strike display mode. However, clusters of two or more
discharge points in the strike display mode do indicate thunderstorm
activity if these points reappear after the screen has been cleared.
NOTE: Operate G1000 NXi system power through at least one cycle in
a period of four days of continuous operation to avoid an autonomous
system reboot.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Warnings, Cautions & Notes
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 system more easily. It is not intended to be a comprehensive operating
guide. Complete operating procedures for the system are found in the Pilot’s
Guide for this aircraft.
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Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Warnings, Cautions & Notes
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Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Software License Agreement
SOFTWARE LICENSE AGREEMENT
BY USING THE DEVICE, COMPONENT OR SYSTEM MANUFACTURED OR SOLD BY GARMIN
(“THE GARMIN PRODUCT”), YOU AGREE TO BE BOUND BY THE TERMS AND CONDITIONS
OF THE FOLLOWING SOFTWARE LICENSE AGREEMENT. PLEASE READ THIS AGREEMENT
CAREFULLY. Garmin Ltd. and its subsidiaries (“Garmin”) grants you a limited license to use the
software embedded in the Garmin Product (the “Software”) in binary executable form in the
normal operation of the Garmin Product. Title, ownership rights, and intellectual property rights
in and to the Software remain with Garmin and/or its third-party providers. You acknowledge
that the Software is the property of Garmin and/or its third-party providers and is protected
under the United States of America copyright laws and international copyright treaties. You
further acknowledge that the structure, organization, and code of the Software are valuable
trade secrets of Garmin and/or its third-party providers and that the Software in source code
form remains a valuable trade secret of Garmin and/or its third-party providers. You agree not
to reproduce, decompile, disassemble, modify, reverse assemble, reverse engineer, or reduce to
human readable form the Software or any part thereof or create any derivative works based on
the Software. You agree not to export or re-export the Software to any country in violation of
the export control laws of the United States of America.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Software License Agreement
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Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Record of Revisions
Part Number
190-02219-00
Change Summary
Initial Release
Revision Date of Revision Affected Pages
Description
A
March, 2017
All
Production release at GDU
20.51
B
April, 2017
All
Revision
- Added Split Screen Mode
- Updated CAS Messages
- Added Voice Message Alerts
- Updated ESP Information
- Added Electronic Checklists
C
September, 2019
All
Revision
- Added Baro VNAV
- Clerical Changes
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Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
RR-1
Record of Revisions
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RR-2
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Table of Contents
FLIGHT INSTRUMENTS................................................................................................................. 1
Configure Vspeed Bugs Individually...................................................................................... 1
Modifying Vspeeds as a Group (All On, All Off, Restore Defaults)................................. 1
Generic Timer.............................................................................................................................. 1
Enabling altitude units overlays............................................................................................ 2
Setting the Selected Altitude................................................................................................. 2
Selecting the Altimeter Barometric Pressure Setting....................................................... 2
Selecting Standard Barometric Pressure (29.92 in Hg)..................................................... 2
Change Altimeter Barometric Pressure Setting Units....................................................... 2
Synchronizing The Altimeter Barometric Pressure Settings............................................ 2
Synchronizing The CDIs............................................................................................................ 3
Setting Baro transition alerts................................................................................................. 3
Adjusting The Selected Heading............................................................................................ 4
Adjusting The Selected Course............................................................................................... 4
Changing The Navigation Angle Setting.............................................................................. 4
Selecting Bearing Display And Changing Sources............................................................. 4
Change Navigation Sources.................................................................................................... 5
Displaying The DME Information Window........................................................................... 5
Changing The Selected GPS CDI Setting............................................................................... 5
Enable/Disable OBS Mode While Navigating with A FMS Flight Plan............................ 5
Changing Temperature Display Units.................................................................................... 6
Selecting The AOA Indicator Display Mode......................................................................... 6
Set Barometric Minimum Descent Altitude/Decision Height........................................... 6
Displaying Wind Data............................................................................................................... 6
Enabling/Disabling Field Of View........................................................................................... 7
Synthetic Vision Technology.................................................................................................... 7
ENGINE INDICATION..................................................................................................................... 9
Engine Display............................................................................................................................ 9
Synoptics .................................................................................................................................. 12
Reversionary Mode EIS Display............................................................................................ 19
NAV/COM/TRANSPONDER/AUDIO PANEL........................................................................ 21
Entering A Flight ID................................................................................................................. 21
Tuning An ADF Frequency...................................................................................................... 21
Selecting An ADF Receiver Mode......................................................................................... 21
DME Tuning............................................................................................................................... 21
Selecting And Activating XPDR 1 or XPDR 2...................................................................... 21
Selecting Transponder Mode................................................................................................ 22
Entering a Transponder Code with Softkeys..................................................................... 22
Entering a transponder code with the PFD FMS Knob.................................................... 22
Selecting a COM Radio........................................................................................................... 22
Selecting a NAV Radio............................................................................................................ 22
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Table of Contents
NAV/COM Tuning...................................................................................................................... 23
Intercom..................................................................................................................................... 23
Passenger Address (PA) System............................................................................................ 23
Clearance Recorder and Player............................................................................................ 24
Setting The Audio Panels During Preflight........................................................................ 24
FLIGHT MANAGEMENT.............................................................................................................. 25
USING MAP DISPLAYS.............................................................................................................. 25
Changing The Navigation Map Orientation....................................................................... 25
Enabling/Disabling Auto North Up And Selecting The Minimum Switching Range.. 25
Configuring Automatic Zoom................................................................................................ 26
Panning The Map..................................................................................................................... 26
Reviewing Information For An Airport, NAVAID, Or User Waypoint............................ 27
Reviewing information for a special-use or controlled airspace................................. 27
Displaying/Removing Topographic Data On All MFD Pages Displaying Navigation
Maps........................................................................................................................................... 27
Displaying/Removing Topographic Data On The PFD Map............................................. 27
Displaying/Removing Topographic Data Using The Navigation Map Page Menu..... 28
Setting Up The ‘Land’, ‘Aviation’ Or ‘Airspace’ Group Items........................................... 28
Decluttering The Map............................................................................................................. 28
Decluttering The PFD Map..................................................................................................... 29
Displaying/Removing Airways.............................................................................................. 29
Selecting An Airway Range (Low ALT Airways or High ALT Airways)........................... 29
Setting Up Additional ‘Map’ Group Items.......................................................................... 29
WAYPOINTS................................................................................................................................. 30
Selecting An Airport For Review By Identifier, Facility Name, Or Location................ 30
Selecting A Runway................................................................................................................. 30
Viewing A Destination Airport............................................................................................. 30
Viewing Information For A Nearest Airport On The PFD................................................ 31
Viewing Information For A Nearest Airport On The MFD............................................... 31
Viewing Runway Information For A Specific Airport...................................................... 31
Selecting An Intersection....................................................................................................... 32
Selecting An NDB..................................................................................................................... 32
Selecting A VOR........................................................................................................................ 32
Selecting A VRP........................................................................................................................ 32
Selecting A User Waypoint.................................................................................................... 32
Creating User Waypoints From The User Waypoint Information Page........................ 33
Creating User Waypoints From Map Pages........................................................................ 33
Deleting a single user waypoint.......................................................................................... 34
AIRSPACES................................................................................................................................... 35
Changing The Altitude Buffer Distance Setting................................................................ 35
Turning An Airspace Alert On Or Off................................................................................... 35
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Table of Contents
Selecting And Viewing An Airspace Alert With Its Associated Information............... 35
Turning Smart Airspace On Or Off....................................................................................... 36
DIRECT-TO NAVIGATION.......................................................................................................... 36
Entering A Waypoint Identifier, Facility Name, Or City As A Direct-To Destination. 36
Selecting An Active Flight Plan Waypoint As A Direct-To Destination........................ 36
Selecting A Nearest, Recent Or User Waypoint As A Direct-To Destination............... 37
Cancelling A Direct-To............................................................................................................. 37
Selecting A Manual Direct-To Course.................................................................................. 37
Entering A VNV Altitude And Along-Track Offset For The Waypoint............................ 38
Removing A VNV Altitude Constraint.................................................................................. 38
FLIGHT PLANNING..................................................................................................................... 38
Creating An Active Flight Plan.............................................................................................. 38
Adding A Waypoint To The Active Flight Plan................................................................... 39
Creating And Adding User Waypoints To The Active Flight Plan................................... 39
Adding An Airway To A Flight Plan...................................................................................... 40
Collapse/Expand Airways in The active Flight Plan......................................................... 40
Storing An Active Flight Plan From The Active Flight Plan Page or the Active Flight
Plan Window............................................................................................................................. 40
Activating A Stored Flight Plan On The MFD..................................................................... 41
Inverting And Activating A Stored Flight Plan On The MFD.......................................... 41
Import a Flight Plan from an SD Card................................................................................. 41
Export a Flight Plan to an SD Card...................................................................................... 42
Previewing a flight plan transfer from a wireless connection...................................... 43
Ignoring a flight plan transfer from a wireless connection........................................... 43
Storing a pending flight plan................................................................................................ 43
Activating a pending flight plan.......................................................................................... 44
Deleting a pending flight plan............................................................................................. 44
Deleting all pending flight plans......................................................................................... 44
Deleting The Active Flight Plan and suspending navigation......................................... 45
Deleting An Individual Waypoint From The Active Flight Plan...................................... 45
Deleting An Entire Airway From The Active Flight Plan.................................................. 45
Deleting An Entire Procedure From The Active Flight Plan............................................ 46
Entering An Along Track Offset Distance........................................................................... 46
Activating Parallel Track........................................................................................................ 46
Cancelling Parallel Track........................................................................................................ 47
Activating A Flight Plan Leg.................................................................................................. 47
Inverting The Active Flight Plan........................................................................................... 47
Changing The Flight Plan View............................................................................................. 48
Viewing charts and active flight plan page in split screen mode................................ 48
Displaying the flight plan map on the active flight plan page in split mode........... 48
Determining The Closest Point Along The Active Flight Plan To A Selected Waypoint
49
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Table of Contents
Creating A User-Defined Hold At An Active Flight Plan Waypoint................................ 49
Creating A User-Defined Hold At The Aircraft Present Position.................................... 50
Creating A User-Defined Hold At A Direct-To Waypoint.................................................. 50
Exiting A User-Defined Hold Inserted Into The Active Flight Plan................................ 51
Removing A User-Defined Hold Inserted Into The Active Flight Plan.......................... 51
Removing A User-Defined Hold At An Off-Route Direct-To............................................ 51
VERTICAL NAVIGATION........................................................................................................... 51
Enabling/Disabling VNV Guidance....................................................................................... 51
Activating A Vertical Navigation Direct-To........................................................................ 52
Modifying The VS TGT And FPA............................................................................................. 52
Altitude Constraints................................................................................................................ 52
Manually Designating A Waypoint Altitude To Be Used For Vertical Guidance......... 54
Manually Designating A Procedure Waypoint Altitude To Be Used For Vertical Guidance............................................................................................................................................. 54
Entering/Modifying An Altitude Constraint....................................................................... 54
Deleting An Altitude Constraint Provided By The Navigation Database.................... 55
Deleting An Altitude Constraint That Has Been Manually Entered.............................. 55
Reverting A Manually Entered Altitude Constraint Back To The Navigation Database Value................................................................................................................................. 56
Modifying A System Calculated Altitude Constraint....................................................... 56
Enabling the Vertical Situation Display.............................................................................. 56
Disabling the Vertical Situation Display............................................................................. 57
PROCEDURES............................................................................................................................... 57
Viewing Available Procedures At An Airport..................................................................... 57
Loading A Procedure Into The Active Flight Plan From The <Procedure> Information Page.................................................................................................................................... 58
Loading A Departure Into The Active Flight Plan Using The PROC Key....................... 58
Removing A Departure Procedure From The Active Flight Plan................................... 59
Loading An Arrival Into The Active Flight Plan Using The PROC Key........................... 59
Removing An Arrival From The Active Flight Plan............................................................ 59
Approach Service levels......................................................................................................... 60
Loading An Approach Into The Active Flight Plan Using The PROC Key...................... 60
Loading an approach into the active flight plan from the ‘NRST - Nearest Airports’
Page............................................................................................................................................ 61
Activating A Previously Loaded Approach......................................................................... 62
Activating A Previously Loaded Approach With Vectors To Final................................. 62
Removing An Approach From The Active Flight Plan...................................................... 62
Activating A Missed Approach In The Active Flight Plan................................................ 63
Activating Temperature Compensated Altitude............................................................... 63
Cancelling Temperature Compensated Altitude............................................................... 63
iv
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Table of Contents
WEIGHT PLANNING................................................................................................................... 64
Entering Basic Empty Weight................................................................................................ 64
Entering A Pilot And Stores Weight..................................................................................... 64
Entering The Number Of Passengers................................................................................... 64
Entering The Average Passenger Weight........................................................................... 64
Entering The Cargo Weight.................................................................................................... 65
Entering A Fuel On Board Weight......................................................................................... 65
Synchronizing the fuel on board with the actual measured fuel on board............... 65
Entering Fuel Reserve............................................................................................................. 65
TRIP PLANNING.......................................................................................................................... 66
Selecting Automatic Or Manual Page Mode..................................................................... 66
Selecting Flight Plan Or Waypoint Mode........................................................................... 66
Selecting A Flight Plan And Leg For Trip Statistics.......................................................... 66
Selecting Waypoints For Waypoint Mode.......................................................................... 66
Entering Manual Data For Trip Statistics Calculations.................................................... 66
RAIM PREDICTION..................................................................................................................... 67
Predicting RAIM Availability At A Selected Waypoint..................................................... 67
Predicting RAIM Availability At The Aircraft Present Position...................................... 68
Disabling SBAS......................................................................................................................... 68
HAZARD AVOIDANCE................................................................................................................. 69
STORMSCOPE® (Optional)...................................................................................................... 69
SiriusXM Weather (Optional)................................................................................................ 70
Connext Weather (Optional)................................................................................................. 74
FIS-B Weather........................................................................................................................... 81
Airborne Color Weather Radar............................................................................................. 87
Traffic Systems......................................................................................................................... 93
Terrain Displays...................................................................................................................... 106
AUTOMATIC FLIGHT CONTROL SYSTEM......................................................................... 111
Activating The Flight Director............................................................................................ 111
Vertical Modes........................................................................................................................ 112
Lateral Modes......................................................................................................................... 112
Combination Modes (VNV, APR, NAV, BC, GA).................................................................. 113
ADDITIONAL FEATURES.......................................................................................................... 115
Terminal Procedure Charts.................................................................................................. 115
Airport Directory................................................................................................................... 117
SiriusXM™ Radio Entertainment......................................................................................... 118
Satellite Telephone and Data Link Services.................................................................... 120
Scheduler................................................................................................................................. 132
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
v
Table of Contents
Crew Profiles........................................................................................................................... 134
Connext Management.......................................................................................................... 137
Maintenance Logs.................................................................................................................. 138
Electronic Stability & Protection (ESP™) (Optional)..................................................... 139
Electronic Checklists............................................................................................................. 141
ABNORMAL OPERATION........................................................................................................ 143
Reversionary Mode............................................................................................................... 143
Abnormal COM Operation................................................................................................... 143
Hazard Displays with Loss of GPS Position...................................................................... 143
Unusual Attitudes.................................................................................................................. 144
Abnormal GPS Conditions Annunciated on the HSI....................................................... 145
Dead Reckoning..................................................................................................................... 145
Suspected Autopilot malfunction...................................................................................... 147
Overpowering Autopilot Servos........................................................................................ 147
ANNUNCIATIONS & ALERTS.................................................................................................. 149
CAS Messages......................................................................................................................... 149
System Annunciations.......................................................................................................... 151
Reversionary Sensor Annunciations.................................................................................. 153
Comparator Annunciations.................................................................................................. 154
Terrain-SVT Alerts.................................................................................................................. 155
Terrain-SVT System Status Annunciations....................................................................... 155
TAWS-B Alerts......................................................................................................................... 156
TAWS-B System Status Annunciations.............................................................................. 158
GDL 69A SXM Data Link Receiver Messages................................................................... 159
AFCS Alerts.............................................................................................................................. 160
Voice Alerts............................................................................................................................. 161
System Message Advisories................................................................................................ 162
Flight Plan Import/Export Messages................................................................................. 180
Crew Profile Import/Export Messages.............................................................................. 182
APPENDIX...................................................................................................................................... 183
PFD Softkey Map................................................................................................................... 183
MFD Softkey Map.................................................................................................................. 188
Loading Updated Databases............................................................................................... 190
INDEX..........................................................................................................................................Index-1
vi
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Instruments
Flight
Flight
Instruments
Instruments
FLIGHT INSTRUMENTS
CONFIGURE VSPEED BUGS INDIVIDUALLY
EISEIS
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
1) Press the Tmr/Ref Softkey.
2) Turn the large FMS Knob to highlight the desired Vspeed.
3) Use the small FMS Knob to change the highlighted Vspeed in 1-kt
increments. When a speed has been changed from its default value, an
asterisk appears next to the changed speed.
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’.
6)
To remove the window, press the CLR Key or the Tmr/Ref Softkey.
MODIFYING VSPEEDS AS A GROUP (ALL ON, ALL OFF, RESTORE DEFAULTS)
Press the Tmr/Ref Softkey.
5)
To remove the window, press the CLR Key or the Tmr/Ref Softkey.
AFCS
Press the MENU Key.
Turn the FMS Knob to highlight the desired selection.
Press the ENT Key.
GENERIC TIMER
2)
Turn the small FMS Knob to display the Up/Down window. Turn the FMS
Knob to select ‘Up’ or ‘Dn’, then press the ENT Key. ‘START?’ is now
highlighted.
3)
Press the ENT Key to START, STOP, or RESET the timer (if the timer is
counting down, it will start counting up after reaching zero). Press the CLR
Key or the Tmr/Ref Softkey to remove the window.
Appendix
Appendix
Press 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/Dn field is now highlighted.
Annun/Alerts
Annun/Alerts
1)
Additional Additional
Abnormal
AFCS Features
Features
Operation
1)
2)
3)
4)
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
1
ENABLING ALTITUDE UNITS OVERLAYS
2)
Press the ALT Units Softkey.
3)
Press the Meters or Feet Softkey to enable/disable the altitude overlays .
4)
Press the Back Softkey twice to return to the top-level softkeys.
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
Turn the BARO Knob to select the desired setting.
SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)
1)
Press the PFD Opt Softkey.
2)
Press the STD Baro Softkey to set standard barometric pressure.
CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS
1)
Press the PFD Opt Softkey to display the second-level softkeys.
2)
Press the ALT Units Softkey.
3)
Press the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Or:
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
Press the PFD Opt Softkey to display the second-level softkeys.
Turn the ALT SEL Knob to set the Selected Altitude.
Press the HPA Softkey to display the barometric pressure setting in
hectopascals.
4)
Press the BACK Softkey to return to the top-level softkeys.
SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS
Index
Index
Appendix
Appendix
1)
SETTING THE SELECTED ALTITUDE
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Flight Instruments
2
1)
Turn the large FMS Knob to select the ‘Aux - System Setup 1’ Page on the
MFD.
2)
If necessary, press the Setup 1 Softkey to display the System Setup 1 Page.
3)
Press the FMS Knob to activate the cursor.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Instruments
5)
Turn the small FMS Knob clockwise to ‘On’ or counterclockwise to ‘Off’.
6)
Press the ENT Key.
7)
Turn the small FMS Knob to change the altitude.
8)
Press the ENT Key.
9)
To cancel the selection, press the FMS Knob.
EISEIS
Turn the large FMS Knob to highlight ‘BARO’ in the ‘Synchronization’ box.
Flight
Flight
Instruments
Instruments
4)
Turn the large FMS Knob to select the ‘Aux - System Setup 1’ Page on the
MFD.
2)
If necessary, press the Setup 1 Softkey to display the System Setup 1 Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the ‘CDI Sync’ in the Synchronization
box.
5)
Turn the small FMS Knob clockwise to ‘On’ or counterclockwise to ‘Off’.
6)
Press the ENT Key.
7)
To cancel the selection, press the FMS Knob.
AFCS
1)
2)
Press the FMS Knob to activate the cursor.
3)
To enable/disable the Baro Transition Alert based on altitude, turn the large
FMS Knob to highlight the ‘On’ or ‘Off’ field for the BARO Transition Alert
Altitude in the BARO Transition Alert Box.
4)
If desired, turn the small FMS Knob to set the BARO Transition Alert
Altitude On or Off.
5)
Turn the large FMS Knob to highlight the Altitude field.
6)
Use the FMS Knobs to change the altitude and press the ENT Key to
accept or press the CLR Key to return to the previous altitude selection.
7)
Turn the large FMS Knob to highlight the ‘On’ or ‘Off’ field for the BARO
Transition Alert Level.
8)
If desired, turn the small FMS Knob to set the BARO Transition Alert Flight
Level On or Off.
Index
Index
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Appendix
Appendix
Use the FMS Knob to select the ‘Aux - System Setup 1’ Page on the MFD.
Annun/Alerts
Annun/Alerts
1)
Additional Additional
Abnormal
AFCS Features
Features
Operation
SETTING BARO TRANSITION ALERTS
190-02219-00 Rev. C
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
SYNCHRONIZING THE CDIS
3
Flight Instruments
Flight
Flight
Instruments
Instruments
9)
Turn the large FMS Knob to highlight the Flight Level field.
10) Use the FMS Knobs to change the Flight Level for the alert and press the
ENT Key to accept or press the CLR Key to return to the previous altitude
selection.
EISEIS
11) Push the FMS Knob to deactivate the cursor.
T urn the HDG Knob to set the Selected Heading.
P ress the HDG Knob to synchronize the bug to the current heading.
ADJUSTING THE SELECTED COURSE
Turn the CRS Knob to set the Selected Course.
Press the CRS Knob to re-center the CDI and return the course pointer to
the bearing of the active waypoint or navigation station.
CHANGING THE NAVIGATION ANGLE SETTING
1)
Use the FMS Knob to select the ‘Aux - System Setup 1’ Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight NAV Angle setting in the Display Units
box.
4)
Turn the small FMS Knob to highlight the desired setting and press the
ENT Key.
• Magnetic - Angles corrected to the computed magnetic variation (Mag
Var)
• True - References angles to true north (T)
SELECTING BEARING DISPLAY AND CHANGING SOURCES
1)
Press the PFD Opt Softkey.
2)
Press either Bearing 1 or Bearing 2 Softkey to display the desired bearing
pointer and information window with a NAV source.
3)
Press either Bearing 1 or Bearing 2 Softkey again to change the bearing
source to FMS.
4)
Press either Bearing 1 or Bearing 2 Softkey a third time to change the
bearing source to ADF (note: ADF radio installation is optional).
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
ADJUSTING THE SELECTED HEADING
4
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Instruments
To remove the bearing pointer and information window, press either
Bearing 1 or Bearing 2 Softkey again.
Flight
Flight
Instruments
Instruments
5)
CHANGE NAVIGATION SOURCES
2)
Press the CDI Softkey again to change to VOR2 or LOC2. This places the
cyan tuning box over the NAV2 standby frequency.
3)
Press the CDI Softkey a third time to return to GPS.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Press the CDI Softkey to change from FMS to VOR1 or LOC1. This places
the cyan tuning box over the NAV1 standby frequency in the upper left
corner of the PFD.
EISEIS
1)
DISPLAYING THE DME INFORMATION WINDOW
1)
Press the PFD Opt Softkey.
2)
Press the DME Softkey to display the DME Information Window above the
BRG1 Information Window.
3)
To remove the DME Information Window, press the DME Softkey again.
AFCS
CHANGING THE SELECTED GPS CDI SETTING
2)
If necessary, press the Setup 1 Softkey to display the System Setup 1 Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight ‘Selected’ in the ‘GPS CDI’ box.
5)
Turn the small FMS Knob to highlight the desired setting and press the
ENT Key.
6)
To cancel the selection, press the FMS Knob or the CLR Key.
ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH A FMS FLIGHT PLAN
2)
Turn a CRS Knob to select the desired course to/from the waypoint. Press
the CRS Knob to synchronize the Selected Course with the bearing to the
next waypoint.
3)
Press the OBS Softkey again to disable OBS Mode.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
Press the OBS Softkey to select OBS Mode.
Appendix
Appendix
1)
Annun/Alerts
Annun/Alerts
Turn the FMS Knob to select the ‘Aux - System Setup 1’ Page.
Additional Additional
Abnormal
AFCS Features
Features
Operation
1)
5
CHANGING TEMPERATURE DISPLAY UNITS
Select the ‘Aux - System Setup 1’ Page on the MFD using the FMS Knob.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the Temperature datafield in the
Display Units box.
4)
Turn the small FMS Knob to highlight either ‘Celsius’ or ‘Fahrenheit’ and
press the ENT Key to confirm the selection.
5)
To cancel the selection, press the FMS Knob or the CLR Key.
1)
Press the PFD Opt Softkey.
2)
The AOA Softkey displays the currently selected mode in cyan. Press the
AOA Softkey to choose either Off or Auto Mode.
SET BAROMETRIC MINIMUM DESCENT ALTITUDE/DECISION HEIGHT
1) Press the Tmr/Ref Softkey.
Additional Additional
Abnormal
Features
Operation
Features AFCS
Annun/Alerts
Annun/Alerts
2)
Turn the large FMS Knob to highlight the MINS datafield.
3)
Turn the small FMS Knob to select BARO, TEMP COMP, or RAD ALT. OFF
is selected by default. Press the ENT Key or turn the large FMS Knob to
highlight the next field.
4)
Use the small FMS Knob to enter the desired altitude (from zero to 16,000
feet when ‘BARO’ or ‘TEMP COMP’ is selected, or up to 2,500 feet when
‘RAD ALT’ is selected).
5)
If TEMP COMP was selected, press the ENT Key or turn the large FMS
Knob to highlight the next field and then enter the temperature (-59˚C to
59˚C)
6)
To remove the window, press the CLR Key or the Tmr/Ref Softkey.
DISPLAYING WIND DATA
Index
Index
Appendix
Appendix
1)
SELECTING THE AOA INDICATOR DISPLAY MODE
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Flight Instruments
6
1)
Press the PFD Opt Softkey.
2)
Press the Wind Softkey to display wind data below the Selected Heading.
3)
Press one of the Option softkeys to change how wind data is displayed:
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Instruments
Flight
Flight
Instruments
Instruments
• Option 1: Wind direction arrows with numeric headwind/tailwind and
crosswind components
• Option 2: Wind direction arrow with numeric speed
• Option 3: Wind direction arrow with numeric direction and speed
To remove the window, press the Off Softkey.
EISEIS
4)
1)
While viewing the Navigation Map Page, press the MENU Key to display
the Page Menu.
2)
Turn the large FMS Knob to highlight Map Settings and press the ENT Key.
3)
Turn the FMS Knob to select the Map Group and press the ENT Key.
4)
Turn the large FMS Knob to scroll through the Map Group options to Field
of View.
5)
Turn the small FMS Knob to select On or Off.
6)
Press the FMS Knob to return to the Navigation Map Page.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
ENABLING/DISABLING FIELD OF VIEW
AFCS
SYNTHETIC VISION TECHNOLOGY
NOTE: Do not use the flight path marker as a flight director.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
7
Index
Index
190-02219-00 Rev. C
Appendix
Appendix
NOTE: Terrain alerting is not available north of 89º North latitude and south
of 89º South latitude. This is due to limitations present within the Terrain
database and the system’s ability to process the data representing the affected
areas.
Annun/Alerts
Annun/Alerts
WARNING: Do not use SVT runway depiction as the sole means for
determining the proximity of the aircraft to the runway or for maintaining
the proper approach path angle during landing.
Additional Additional
Abnormal
AFCS Features
Features
Operation
WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. SVT is intended as an aid to situational
awareness only and may not provide the accuracy and/or fidelity upon which
to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or
traffic.
Flight Instruments
EISEIS
Flight
Flight
Instruments
Instruments
Activating and deactivating SVT:
1)
Press the PFD Opt Softkey.
2)
Press the SVT Softkey.
3)
Press the Terrain Softkey. The SVT display will cycle on or off with the
Terrain Softkey.
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
Activating and deactivating Pathways:
1)
Press the PFD Opt Softkey.
2)
Press the SVT Softkey.
3)
Press the Pathways Softkey. The Pathway feature will cycle on or off with
the Pathways Softkey.
Activating and deactivating Horizon Headings:
Press the PFD Opt Softkey.
2)
Press the SVT Softkey.
3)
Press the HDG LBL Softkey. The horizon heading display will cycle on or off
with the HDG LBL Softkey.
AFCS
1)
1)
Press the PFD Opt Softkey.
2)
Press the SVT Softkey.
3)
Press the APT Sign Softkey. Display of airport signs will cycle on or off
with the APT Sign Softkey.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
Activating and deactivating Airport Signs:
8
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Engine Indication System
EISEIS
10
4
2
2
Additional Additional
Abnormal
AFCS Features
Features
Operation
11
10
7
12
6
6
AFCS
5
5
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
8
1
1
Annun/Alerts
Annun/Alerts
Appendix
Appendix
Index
Index
9
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
3
4
9
3
Reversionary Mode
Normal Mode
Flight
Flight
Instruments
Instruments
ENGINE INDICATION
ENGINE DISPLAY
8
12
11
Engine Display
1
Torque (TRQ)
EISEIS
Flight
Flight
Instruments
Instruments
Engine Indication System
The Torque Gauge displays values from 0 to 130% of maximum safe
torque.
If the torque remains above 100% for more than 5 seconds or exceeds
the value indicated by the red tick mark, a warning condition occurs.
The maximum climb torque is displayed as a white triangle (bug).
The optimum cruise range is displayed as a white band.
Optimum Cruise Range
When bleed pressure reaches its upper limit, ‘BLEED HI’ is annunciated
above the Torque Gauge.
2
Propeller
Speed (PROP
RPM)
Displays propeller speed in revolutions per minute (rpm) from zero to
2200.
If propeller speed slows so that the gauge pointer enters the amber
range, a caution is issued.
If propeller speed exceeds the maximum safe operating speed, a warning
is indicated.
3
Generator
Speed (NG)
Generator speed is displayed as a percentage of maximum safe
operating speed (rpm), from 0 to 120%.
If generator speed exceeds 104% a warning condition occurs.
4
Interturbine
Temperature
(ITT °C)
The Interturbine Temperature (ITT) Gauge ranges differ for engine off/
start and running conditions. Engine starting temperature range:
Between 200 and 1200 degrees Celsius (°C), and ‘STRT’ annunciation is
shown above the ITT indication. Engine normal operating temperature
range: Between 200 to 900 Celsius (°C) with no annunciation shown
above the ITT indication.
When the engine is not running: ‘OFF’ annunciation above the ITT
displayed.
Red tick marking along the ITT gauge, indicate ITT exceedance limits.
5
Oil Pressure
(OIL PSI)
Displays engine oil pressure in pounds per square inch (psi)
6
Oil Temperature Displays oil temperature in degrees Celsius (°C)
(OIL °C)
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
Maximum Climb Torque
10
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Engine Indication System
8
Cabin Pressure
(ALT FT, RATE
FPM, DIFF PSI,
LFE FT)
Cabin pressurization information (cabin altitude, rate of change,
differential cabin pressure, and landing field elevation) is shown. Only
displays for cabin altitude and pressure differential are shown during
Reversionary Mode.
Cabin altitude (ALT FT) is shown on a color-coded scale labeled 0, 10,
and 15 in 1,000 of feet, with numerical digital values in feet displayed
below.
Cabin altitude change rate (RATE FPM) is displayed on a scale of 1,000ft from plus (+) 2 to minus (-) 2 fpm with numerical digital values in feet
displayed below. (Only displayed in normal mode).
Cabin pressure differential (DIFF PSI), is displayed in pounds per square
inch (psi) on a color-coded scale, with numerical digits in psi.
9
Oxygen
Pressure
(OXY PSI)
Crew oxygen system is displayed in pounds per square inch (psi) in
numerical digital readout. (Only displayed in normal mode).
11 Electrical
(AMPS, VOLTS)
Fuel quantity is displayed in United States gallons (USG).
In normal mode, fuel quantity for each tank is normally shown along a
color-coded scale with numerical digits. In reversionary mode, it is only
displayed in numerical digits.
Fuel flow usage is listed in gallons per hour (gph) in numerical digits.
Position (ELEV,
RUD,FLAPS)
Index
Index
190-02219-00 Rev. C
shown along slide bar scales (normal mode). Rudder and aileron trim
indications are not displayed in reversionary mode.
Flap trim indication is displayed using a rotating pointer, with positions
for takeoff, landing, and up (normal mode). Flap indications are only
displayed as UP, T/O, and LDG in reversionary mode. The elevator display
does not change in reversionary mode.
11
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Appendix
Appendix
12 Trims and Flaps Elevator (ELEV), rudder (RUD), and aileron (AIL) trim indications are
Annun/Alerts
Annun/Alerts
Electrical amps and volts are displayed with indications for battery and
the electrical generating system.
In normal mode, amps and volts are displayed along a color-coded scale,
with numerical digits. In reversionary mode, only the numerical digits are
displayed.
AMPS displays the battery (pointers labeled “B”) and generators (pointer
labeled “G” for primary generator, “S” for standby generator when
primary generator is offline) (normal mode only)
VOLTS displays the battery (pointers labeled “B”) and essential bus
(pointer labeled “E”) (normal mode only).
Additional Additional
Abnormal
AFCS Features
Features
Operation
(FUEL QTY,
GPH)
AFCS
10 Fuel Quantity
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Displays CAS messages. (Refer to the Appendices section for information
on the CAS display).
EISEIS
Crew Alerting
System (CAS)
Flight
Flight
Instruments
Instruments
7
Landing Field Elevation
Landing Field Elevation (LFE FT) is displayed in numerical digits in feet and is set
two ways.
Setting the displayed landing field elevation to the value for the
destination airport
1) Press the System Softkey.
2) Press the FMS LFE Softkey to set the LFE to the value for the destination
airport in the current flight plan.
Manually adjusting the displayed landing field elevation
1) Press the System Softkey.
2) Press the LFE MAN Softkey.
3) Use the +250, -250, +25, or -25 FT softkeys to set the desired elevation.
4)
To confirm the new LFE value, press the Accept Softkey.
SYNOPTICS
The Synoptics pages show current conditions of certain aircraft functionality
on aviation system diagrams, reducing workload by allowing the flight crew to
rapidly analyze the situation.
Electrical (ELEC)
Accessing the Sys-Electrical synoptics status
1)
Press the System Softkey.
2)
Press the ELEC Softkey.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Engine Indication System
12
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Engine Indication System
3
2
4
Flight
Flight
Instruments
Instruments
1
EISEIS
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
9
5
6
AFCS
7
8
Additional Additional
Abnormal
AFCS Features
Features
Operation
Sys - Electrical Page
6
DC Buses 1 through 4
2
Main Generator
7
Essential Bus Voltage
3
Ground Power Unit Door
8
Battery Bus Voltage
4
Battery
9
Amperage
5
Main Bus
Appendix
Appendix
Standby Generator
Annun/Alerts
Annun/Alerts
1
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
13
Engine Indication System
Flight
Flight
Instruments
Instruments
EISEIS
Main
Generator
Connected
Disconnected
Connected
Disconnected
Standby
Generator
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
Description
Unit
Door Closed
(No Indication)
Annun/Alerts
Annun/Alerts
GPU
Door Open Not
Selected
Index
Index
Appendix
Appendix
Door Open
Selected
14
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Engine Indication System
Flight
Flight
Instruments
Instruments
Description
Unit
EISEIS
Battery
Disconnected
Current Flow
from Battery
Connected
Disconnected
Current Flow to Current Flow to
Battery
Battery
Normal
Caution - Low
Voltage
Warning - Low Warning - High
Voltage
Voltage
Bus Energized
Bus not
Energized
Switch Down
- Essential Bus
connected to
Main Bus
Switch Up Essential Bus
connected to
Battery Bus
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Connected
Current Flow
from Battery
Battery
Overheat
Condition
Ess Bus/Batt
Bus
AFCS
Additional Additional
Abnormal
AFCS Features
Features
Operation
DC Buses
Annun/Alerts
Annun/Alerts
Appendix
Appendix
Ess Bus
Connections
Index
Index
Electrical System Synoptics
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
15
Engine Indication System
Flight
Flight
Instruments
Instruments
Fuel (FUEL)
1)
Select the System softkey.
2)
Select the FUEL softkey.
5
1
6
2
7
3
8
4
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Accessing the Sys-Fuel synoptics status
1
Auxiliary Boost Pump
5
Engine Driven Boost Pump
2
Left Fuel Tank
6
Right Fuel Tank
3
Left Fuel Line
7
Right Fuel Line
4
Fuel Flow Data
8
Fuel Selector
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Sys - Fuel Page
16
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Engine Indication System
Switching
Fuel Tank
Selection
Right Fuel
Tank Selected
On
Off (Auto)
Off (Manual)
Manual or
Unknown
Fuel Tank
Selection
Fuel Selector
Off
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Auxiliary Boost
Pump
Left Fuel Tank
Selected
Fuel System Synoptics
General System (GEN)
2)
Select the GEN softkey.
Additional Additional
Abnormal
AFCS Features
Features
Operation
Select the System softkey.
AFCS
Accessing the Sys-General synoptics status
1)
EISEIS
Fuel Selector
Description
Flight
Flight
Instruments
Instruments
Unit
Annun/Alerts
Annun/Alerts
Appendix
Appendix
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
17
Flight
Flight
Instruments
Instruments
Engine Indication System
9
8
1
7
EISEIS
2
6
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
3
4
5
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Sys - General Page
1
Forward Cargo Door Open
6
Stall Warning Sensor
2
Pitot Probe 1
7
Pitot Probe 2
3
Pilot Door Open
8
Windshield Heat On
4
Cabin Door Open
9
Propeller Heater
5
Rear Cargo Door Open
Appendix
Appendix
Unit
Description
Windshield Heat
Index
Index
On
Off
Left Heat On, Right
Heat Selected
Windshield Heat Synoptics
18
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Engine Indication System
In the event of a PFD or MFD display failure, the display(s) operating in Reversionary Mode are configured to present PFD symbology together with the EIS Display
(refer to the System Overview for information about display reversionary mode).
Flight
Flight
Instruments
Instruments
REVERSIONARY MODE EIS DISPLAY
EISEIS
EIS Display
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
AFCS
Additional Additional
Abnormal
AFCS Features
Features
Operation
Reversionary Mode (EIS Shown)
Annun/Alerts
Annun/Alerts
Appendix
Appendix
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
19
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Engine Indication System
Blank Page
20
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Nav/Com/XPDR/Audio Panel
Flight
Flight
Instruments
Instruments
NAV/COM/TRANSPONDER/AUDIO PANEL
ENTERING A FLIGHT ID
2)
Press the FMS Knob to activate the selection cursor, if not already
activated.
3)
Turn the large FMS Knob to scroll down to the Flight ID.
4)
Turn the small FMS Knob to enter the desired Flight ID.
5)
Press the ENT Key to complete Flight ID entry.
TUNING AN ADF FREQUENCY
Press the ADF/DME Softkey to display the ‘ADF/DME Tuning’ Window.
2)
Turn the large FMS Knob to place the selection cursor over the standby ADF
frequency field.
3)
Turn the small FMS Knob to begin data entry and change each digit.
4)
Turn the large FMS Knob to move the cursor to the next digit position.
5)
Press the ENT Key to complete data entry for the standby frequency.
AFCS
1)
Additional Additional
Abnormal
AFCS Features
Features
Operation
SELECTING AN ADF RECEIVER MODE
1)
Turn the large FMS Knob to place the selection cursor over the ADF mode
field.
2)
Turn the small FMS Knob to select the desired ADF receiver mode.
Annun/Alerts
Annun/Alerts
DME TUNING
Press the ADF/DME Softkey to display the ‘ADF/DME Tuning’ Window.
2)
Turn the small FMS Knob to select the DME tuning mode.
3)
Press the ENT Key to complete the selection.
Appendix
Appendix
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Press the TMR/REF Softkey to display the ‘References’ Window.
EISEIS
1)
SELECTING AND ACTIVATING XPDR 1 OR XPDR 2
Press the XPDR Softkey to display the Transponder Mode Selection Softkeys.
2)
Press the XPDR1 or XPDR2 Softkey to select and activate the desired
transponder.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
21
Index
Index
1)
SELECTING TRANSPONDER MODE
2)
Select the desired softkey to activate the transponder mode.
1)
Press the XPDR Softkey to display the transponder mode selection softkeys.
2)
Press the Code Softkey to display the transponder code selection softkeys,
for digit entry.
3)
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.
1)
Press the XPDR and the Code Softkeys as in the previous procedure to
enable code entry.
2)
Turn the small FMS Knob to enter the first two code digits.
3)
Turn the large FMS Knob to move the cursor to the next code field.
4)
Enter the last two code digits with the small FMS Knob.
5)
Press the ENT Key to complete code digit entry.
SELECTING A COM RADIO
Transmit/Receive
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
Press the XPDR Softkey to display the Transponder Mode Selection Softkeys.
ENTERING A TRANSPONDER CODE WITH THE PFD FMS KNOB
Press the COM1 MIC or COM2 MIC Key on the audio panel.
Receive Only
Press the COM1 or COM2 Key on the audio panel.
SELECTING A NAV RADIO
Index
Index
Appendix
Appendix
1)
ENTERING A TRANSPONDER CODE WITH SOFTKEYS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Nav/Com/XPDR/Audio Panel
22
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.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Nav/Com/XPDR/Audio Panel
2)
Turn the respective tuning knobs to enter the desired frequency into the
standby frequency field. The large knob enters MHz and the small knob
enters kHz.
3)
Press the Frequency Transfer Key to place the frequency into the active
frequency field.
INTERCOM
23
Index
Index
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Appendix
Appendix
190-02219-00 Rev. C
Annun/Alerts
Annun/Alerts
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.
A Push-to-talk (PTT) must be pressed to deliver PA announcements to the passengers over their headphones.
Additional Additional
Abnormal
AFCS Features
Features
Operation
PASSENGER ADDRESS (PA) SYSTEM
AFCS
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.
When the flight crew wants to communicate with the passengers, the pilot or copilot presses the CABIN Key to signal that communication is desired. The cabin signal
must be acknowledged to begin intercom conversation.
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.
•
When the MAN SQ Annunciator is extinguished (Automatic Squelch is on),
the ICS Knob controls only the volume (pressing the ICS Knob has no effect on the
VOL/SQ selection).
•
When the MAN SQ Annunciator is illuminated (Manual Squelch), the ICS
Knob controls either volume or squelch (selected by pressing the ICS Knob and indicated by the VOL or SQ annunciation).
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Press the small tuning knob to select the desired radio for tuning. A cyan
box highlights the radio frequency to be tuned.
EISEIS
1)
Flight
Flight
Instruments
Instruments
NAV/COM TUNING
When PA is selected on the Audio Panel, the annunciator flashes about once per
second while pressing the PTT, the COM MIC annunciator is no longer lit, and the
active COM frequency for that Audio Panel changes to white, indicating that there is
no COM selected.
CLEARANCE RECORDER AND PLAYER
NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio
to the Pilot. Pressing the play key on the Copilot’s Audio Panel plays recorded
audio to the Copilot.
Recorded COM audio is stored in separate memory blocks. Once 2.5 minutes
of recording time have been reached, the recorder begins recording over the stored
memory blocks, starting from the oldest block.
The PLAY Key controls the play function. The PLAY annunciator 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.
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.
SETTING THE AUDIO PANELS DURING PREFLIGHT
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Nav/Com/XPDR/Audio Panel
24
1)
Verify that the INTR COM Key is selected.
2)
Verify manual squelch is set to minimum.
3)
Turn the MSTR Knob (Master Volume Control) on both Audio Panels
clockwise two full turns. This sets the headset audio level to max volume
(least amount of attenuation).
4)
Adjust radio volume levels (COM, NAV, etc.) to a suitable level.
5)
Adjust the ICS volume Knob on each Audio Panel to the desired intercom
level.
6)
Reset squelch to automatic, or adjust to the appropriate level manually.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
Flight
Flight
Instruments
Instruments
FLIGHT MANAGEMENT
Changing A Field In The MFD Navigation Data Bar
Select the ‘Aux - System Setup 1’ Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3)
Turn the large FMS Knob to highlight the desired field number in the MFD
Data Bar Fields Box.
4)
Turn the small FMS Knob to display and scroll through the data options list
to select the desired data.
5)
Press the ENT Key. Pressing the Defaults Softkey returns all fields to the
default setting.
EISEIS
1)
CHANGING THE NAVIGATION MAP ORIENTATION
With the ‘Map - Navigation Map’ Page displayed, press the MENU Key.
The cursor flashes on the ‘Map Settings’ option.
2)
Press the ENT Key to display the Map Settings Window.
3)
Select the ‘Map’ group if necessary. Turn the large FMS Knob, or press the
ENT Key once, to select the ‘Orientation’ field.
4)
Turn the small FMS Knob to select the desired orientation.
5)
Press the ENT Key to select the new orientation.
6)
Press the FMS Knob to return to the base page.
AFCS
1)
Annun/Alerts
Annun/Alerts
Press the ENT Key.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
4)
Appendix
Appendix
1) Press the MENU Key with the ‘Map - Navigation Map’ Page displayed. The
cursor flashes on the ‘Map Settings’ option.
2) Press the ENT Key. The ‘Map Settings’ Window is displayed.
Select the ‘Map’ group.
Additional Additional
Abnormal
AFCS Features
Features
Operation
ENABLING/DISABLING AUTO NORTH UP AND SELECTING THE MINIMUM
SWITCHING RANGE
3)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
USING MAP DISPLAYS
25
Highlight the ‘North Up Above’ field.
6)
Select ‘On’ or ‘Off’ using the small FMS Knob.
7)
Press the ENT Key to accept the selected option. The flashing cursor
highlights the range field.
8)
Use the small FMS Knob to select the desired range.
9)
Press the ENT Key to accept the selected option.
CONFIGURING AUTOMATIC ZOOM
Additional Additional
Abnormal
Features
Operation
Features AFCS
1)
Press the MENU Key with the ‘Map - Navigation Map’ Page displayed. The
cursor flashes on the ‘Map Settings’ option.
2)
Press the ENT Key. The ‘Map Settings’ Window is displayed.
3)
Select the ‘Map’ group.
4)
Press the ENT Key.
5)
Highlight the ‘Auto Zoom’ on/off field, and select ‘Off’ or ‘On’ using the
small FMS Knob.
6)
Press the ENT Key to accept the selected option. The flashing cursor
highlights the ‘Auto Zoom’ display selection field.
7)
Select ‘MFD’, ‘PFD’, or ‘All’ using the small FMS Knob.
8)
Press the ENT Key to accept the selected option. The flashing cursor
highlights the ‘Max Look FWD’ field. Times are from zero to 999 minutes.
9)
Use the FMS Knobs to set the time. Press the ENT Key.
10) Repeat step 9 for ‘Min Look FWD’ (zero to 99 minutes) and ‘Time Out’ (zero
to 99 minutes).
11) Press the FMS Knob to return to the Navigation Map Page.
PANNING THE MAP
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
5)
10) Press the FMS Knob to return to the Navigation Map Page.
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Flight Management
26
1)
Push the Joystick to display the Map Pointer.
2)
Move the Joystick to move the Map Pointer around the map.
3)
Push the Joystick to remove the Map Pointer and recenter the map on the
aircraft’s current position.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
With the desired map page displayed, push the Joystick to display the
Map Pointer and place the Map Pointer on a waypoint.
2)
Press the ENT Key to display the Waypoint Information Page for the
selected waypoint.
3)
Press the Go Back Softkey, the CLR Key, or the ENT Key to exit the
Waypoint Information Page and return to the Navigation Map showing the
selected waypoint.
EISEIS
1)
2)
Press the ENT Key to display an options menu.
3)
‘Review Airspaces’ should already be highlighted, if not select it. Press the
ENT Key to display the Information Window for the selected airspace.
4)
Press the FMS Knob, the CLR Key, or the ENT Key to exit the Information
Window.
Additional Additional
Abnormal
AFCS Features
Features
Operation
With the desired map page displayed, push the Joystick to display the
Map Pointer and place the Map Pointer on an open area within the
boundaries of an airspace. (As the Map Pointer crosses the airspace
boundary, the boundary is highlighted and airspace information is shown.)
DISPLAYING/REMOVING TOPOGRAPHIC DATA ON ALL MFD PAGES
DISPLAYING NAVIGATION MAPS
Press the TER Softkey until ‘Topo’ is shown on the softkey to display
topographic data.
3)
Press the TER Softkey until ‘Off’ is shown on the softkey to remove
topographic data from the navigation map. When topographic data
is removed from the page, all navigation data is presented on a black
background.
Appendix
Appendix
2)
Annun/Alerts
Annun/Alerts
With the desired map page displayed, press the Map Opt Softkey.
DISPLAYING/REMOVING TOPOGRAPHIC DATA ON THE PFD MAP
Press the Map/HSI Softkey on the PFD.
2)
Press the TER Softkey until ‘Topo’ is shown on the softkey to display
topographic data.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
1)
AFCS
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
REVIEWING INFORMATION FOR A SPECIAL-USE OR CONTROLLED AIRSPACE
1)
Flight
Flight
Instruments
Instruments
REVIEWING INFORMATION FOR AN AIRPORT, NAVAID, OR USER WAYPOINT
27
Flight Management
1)
Press the MENU Key with the ‘Map - Navigation Map’ Page displayed. The
cursor flashes on the ‘Map Settings’ option.
2)
Press the ENT Key. The ‘Map Settings’ Window is displayed.
3)
Select the ‘Map’ group.
4)
Press the ENT Key.
5)
Highlight the ‘Terrain Display’ field.
6)
Select ‘Topo’ or ‘Off’.
7)
Press the FMS Knob to return to the ‘Map - Navigation Map’ Page.
SETTING UP THE ‘LAND’, ‘AVIATION’ OR ‘AIRSPACE’ GROUP ITEMS
Additional Additional
Abnormal
Features
Operation
Features AFCS
Annun/Alerts
Annun/Alerts
1)
Press the MENU Key with the ‘Map - Navigation Map’ Page displayed. The
cursor flashes on the ‘Map Settings’ option.
2)
Press the ENT Key. The ‘Map Settings’ Window is displayed.
3)
Turn the small FMS Knob to select the desired group.
4)
Press the ENT Key. The cursor flashes on the first field.
5)
Turn the large FMS Knob to select the desired option.
6)
Turn the small FMS Knob to select the desired setting (e.g. On/Off or
maximum range).
7)
Press the ENT Key to accept the selected option and move the cursor to the
next item.
8)
Repeat steps 5-7 as necessary.
9)
Press the FMS Knob to return to the ‘Map - Navigation Map’ Page.
DECLUTTERING THE MAP
Select the Detail Softkey with the Navigation Map Page displayed. The
current declutter level is shown. With each softkey selection, another level
of map information is removed.
Index
Index
Appendix
Appendix
Press the TER Softkey until ‘Off’ is shown on the softkey to remove
topographic data from the navigation map. When topographic data
is removed from the page, all navigation data is presented on a black
background.
DISPLAYING/REMOVING TOPOGRAPHIC DATA USING THE NAVIGATION MAP
PAGE MENU
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
3)
28
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
Press the Map/HSI Softkey on the PFD.
2)
Press the Detail Softkey. The current declutter level is shown. With each
selection, another level of map information is removed.
EISEIS
1)
Flight
Flight
Instruments
Instruments
DECLUTTERING THE PFD MAP
DISPLAYING/REMOVING AIRWAYS
With the desired map page displayed, press the Map Opt Softkey.
2)
Press the AWY Softkey. Both High and Low Altitude Airways are displayed
(AWY On).
3)
Press the softkey again to display Low Altitude Airways only (AWY LO).
4)
Press the softkey again to display High Altitude Airways only (AWY HI).
5)
Press the softkey again to remove High Altitude Airways. No airways are
displayed (AWY Off).
SELECTING AN AIRWAY RANGE (LOW ALT AIRWAYS OR HIGH ALT AIRWAYS)
Press the ENT Key. The ‘Map Settings’ Window is displayed.
3)
Turn the small FMS Knob to select the ‘Airways’ group, and press the ENT
Key.
4)
Highlight the ‘Low ALT Airways’ or ‘High ALT Airways’ range field.
5)
To change the range setting, turn the small FMS Knob to display the range
list.
6)
Select the desired range using the small FMS Knob.
7)
Press the ENT Key.
8)
Press the FMS Knob to return to the Navigation Map Page.
Annun/Alerts
Annun/Alerts
2)
Press the MENU Key with the ‘Map - Navigation Map’ Page displayed. The
cursor flashes on the ‘Map Settings’ option.
2)
Press the ENT Key. The ‘Map Settings’ Window is displayed.
3)
Turn the small FMS Knob to select the ‘Map’ group.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
1)
Appendix
Appendix
SETTING UP ADDITIONAL ‘MAP’ GROUP ITEMS
190-02219-00 Rev. C
Additional Additional
Abnormal
AFCS Features
Features
Operation
Press the MENU Key with the ‘Map - Navigation Map’ Page displayed. The
cursor flashes on the ‘Map Settings’ option.
AFCS
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
1)
29
Flight
Flight
Instruments
Instruments
Flight Management
4)
Press the ENT Key. The cursor flashes on the first field.
5)
Turn the large FMS Knob to select the desired option.
6)
Turn the small FMS Knob to select ‘On’ or ‘Off’.
If it is a data field, use the FMS Knob to select the range or time value.
Additional Additional
Abnormal
Features
Operation
Features AFCS
Press the ENT Key to accept the selected option and move the cursor to the
next item.
8)
Repeat steps 5-7 as necessary.
9)
Press the FMS Knob to return to the ‘Map - Navigation Map’ Page.
SELECTING AN AIRPORT FOR REVIEW BY IDENTIFIER, FACILITY NAME, OR
LOCATION
1)
From the ‘WPT - Airport Information’ Page, press the FMS Knob.
2)
Use the FMS Knobs and enter an identifier, facility name, or location.
3)
Press the ENT Key.
4)
Press the FMS Knob to remove the cursor.
SELECTING A RUNWAY
Annun/Alerts
Annun/Alerts
Appendix
Appendix
7)
WAYPOINTS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Or:
1)
With the ‘WPT - Airport Information’ Page 1 displayed, press the FMS Knob
to activate the cursor.
2)
Turn the large FMS Knob to place the cursor in the ‘Runways’ Box, on the
runway designator.
3)
Turn the small FMS Knob to display the desired runway (if more than one)
for the selected airport.
4)
To remove the flashing cursor, press the FMS Knob.
VIEWING A DESTINATION AIRPORT
From the Airport Information Page press the MENU Key. Select ‘View
Index
Index
Destination Airport’. The Destination Airport is displayed.
30
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
Flight
Flight
Instruments
Instruments
VIEWING INFORMATION FOR A NEAREST AIRPORT ON THE PFD
2)
Highlight the airport identifier with the FMS Knob and press the ENT Key
to display the ‘Airport Information’ Window.
3)
To return to the ‘Nearest Airports’ Window press the ENT Key (with the
cursor on ‘BACK’) or press the CLR Key. The cursor is now on the next
airport in the nearest airports list. (Repeatedly pressing the ENT Key moves
through the airport list, alternating between the ‘Nearest Airports’ Window
and the ‘Airport Information’ Window.)
4)
Press the CLR Key or the Nearest Softkey to close the PFD ‘Nearest Airports’
Window.
VIEWING INFORMATION FOR A NEAREST AIRPORT ON THE MFD
2)
Turn the small FMS Knob to select the ‘NRST - Nearest Airports’ Page (it is
the first page of the group, so it may already be selected). If there are no
Nearest Airports available, ‘None Within 200nm’ is displayed.
3)
Press the APT Softkey; or press the FMS Knob; or press the MENU Key,
highlight ‘Select Airport Window’ and press the ENT Key. The cursor is
placed in the ‘Nearest Airports’ Box. The first airport in the nearest airports
list is highlighted.
4)
Turn the FMS Knob to highlight the desired airport. (Pressing the ENT Key
also moves to the next airport.)
5)
Press the FMS Knob to remove the flashing cursor.
Annun/Alerts
Annun/Alerts
VIEWING RUNWAY INFORMATION FOR A SPECIFIC AIRPORT
With the ‘NRST - Nearest Airports’ Page displayed, press the RNWY
Softkey; or press the MENU Key, highlight ‘Select Runway Window’; and
press the ENT Key. The cursor is placed in the ‘Runways’ Box.
2)
Turn the small FMS Knob to select the desired runway.
3)
Press the FMS Knob to remove the flashing cursor.
Appendix
Appendix
1)
Additional Additional
Abnormal
AFCS Features
Features
Operation
Turn the large FMS Knob to select the NRST page group.
AFCS
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Press the Nearest Softkey to display the ‘Nearest Airports’ Window.
EISEIS
1)
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
31
SELECTING AN INTERSECTION
Additional Additional
Abnormal
Features
Operation
Features AFCS
With the ‘WPT - Intersection Information’ Page displayed, enter an identifier
in the ‘Intersection’ Box.
2)
Press the ENT Key.
3)
Press the FMS Knob to remove the flashing cursor.
1)
With the ‘WPT - NDB Information’ Page displayed, enter an identifier, the
name of the NDB, or the city in which it’s located in the ‘NDB’ Box.
2)
Press the ENT Key.
3)
Press the FMS Knob to remove the flashing cursor.
SELECTING A VOR
1)
With the ‘WPT - VOR Information’ Page displayed, enter an identifier, the
name of the VOR, or the city in which it’s located in the ‘VOR’ Box.
2)
Press the ENT Key.
3)
Press the FMS Knob to remove the flashing cursor.
SELECTING A VRP
1)
With the ‘WPT - VRP Information’ Page displayed, enter the identifier or
the name of the VRP in the ‘VRP’ Box.
2)
Press the ENT Key.
3)
Press the FMS Knob to remove the flashing cursor.
SELECTING A USER WAYPOINT
1)
With the ‘WPT - User WPT Information’ Page displayed, enter the name of
the User Waypoint, or scroll to the desired waypoint in the ‘User Waypoint
List’ Box using the large FMS Knob.
2)
Press the ENT Key.
3)
Press the FMS Knob to remove the flashing cursor.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
1)
SELECTING AN NDB
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Flight Management
32
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
Enter a user waypoint name (up to six characters).
3)
Press the ENT Key. The current aircraft position is the default location of
the new waypoint.
4)
If desired, define the type and location of the waypoint in one of the
following ways:
Select ‘RAD/DIS’ using the small FMS Knob, press the ENT Key, and
enter the reference waypoint identifier, the radial, and the distance into
the ‘Reference Waypoints’ Box using the FMS Knobs.
Or:
AFCS
2)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Press the New Softkey, or press the MENU Key and select ‘Create New
User Waypoint’.
EISEIS
1)
Flight
Flight
Instruments
Instruments
CREATING USER WAYPOINTS FROM THE USER WAYPOINT INFORMATION
PAGE
Select ‘RAD/RAD’ using the small FMS Knob, press the ENT Key,
and enter the two reference waypoint identifiers and radials into the
‘Reference Waypoints’ Box using the FMS Knobs.
Or:
Press the ENT Key to accept the new waypoint.
6)
If desired, change the storage method of the waypoint to temporary by
moving the cursor to ‘Temporary’ and selecting the ENT Key to check the
box.
7)
Press the FMS Knob to remove the flashing cursor.
Annun/Alerts
Annun/Alerts
5)
Additional Additional
Abnormal
AFCS Features
Features
Operation
Select ‘LAT/LON’ using the small FMS Knob, press the ENT Key, and
enter the latitude and longitude into the ‘Information’ Box using the
FMS Knobs.
CREATING USER WAYPOINTS FROM MAP PAGES
2)
Press the ENT Key. The ‘WPT - User WPT Information’ Page is displayed
with the captured position.
3)
Enter a user waypoint name (up to six characters).
4)
Press the ENT Key to accept the selected name. The first reference
waypoint box is highlighted.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
Push the Joystick to activate the panning function and pan to the map
location of the desired user waypoint.
Appendix
Appendix
1)
33
Flight Management
Flight
Flight
Instruments
Instruments
5)
EISEIS
Select ‘RAD/RAD’ using the small FMS Knob, press the ENT Key,
and enter the two reference waypoint identifiers and radials into the
‘Reference Waypoints’ Box using the FMS Knobs.
Or:
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
Select ‘RAD/DIS’ using the small FMS Knob, press the ENT Key, and
enter the reference waypoint identifier, the radial, and the distance into
the ‘Reference Waypoints’ Box using the FMS Knobs.
Or:
AFCS
Select ‘LAT/LON’ using the small FMS Knob, press the ENT Key, and
enter the latitude and longitude into the ‘Information’ Box using the
FMS Knobs.
6)
Press the ENT Key to accept the new waypoint.
7)
If desired, change the storage method of the waypoint to temporary by
moving the cursor to ‘Temporary’ and selecting the ENT Key to check or
uncheck the box.
8)
Press the FMS Knob to remove the flashing cursor.
9)
Press the Go Back Softkey to return to the map page.
DELETING A SINGLE USER WAYPOINT
1)
With the ‘WPT - User WPT Information’ Page displayed, press the FMS
Knob to activate the cursor.
2)
Highlight a User Waypoint in the ‘User Waypoint List’ Box, or enter a
waypoint in the ‘User Waypoint’ Box.
3)
Press the Delete Softkey or press the CLR Key. ‘Yes’ is highlighted in the
confirmation window.
4)
Press the ENT Key.
5)
Press the FMS Knob to remove the flashing cursor.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
If desired, define the type and location of the waypoint in one of the
following ways:
34
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
Flight
Flight
Instruments
Instruments
AIRSPACES
CHANGING THE ALTITUDE BUFFER DISTANCE SETTING
Use the FMS Knob to select the ‘Aux - System Setup 1’ Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3)
Turn the large FMS Knob to highlight the ‘Altitude Buffer’ Field in the
‘Airspace Alerts’ Box.
4)
Use the FMS Knob to enter an altitude buffer value and press the ENT Key.
5)
Press the FMS Knob to remove the flashing cursor.
EISEIS
1)
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3)
Turn the large FMS Knob to highlight the desired field in the ‘Airspace
Alerts’ Box.
4)
Turn the small FMS Knob clockwise to turn the airspace alert on or
counterclockwise to turn the alert off.
5)
Press the FMS Knob to remove the flashing cursor.
Additional Additional
Abnormal
AFCS Features
Features
Operation
Use the FMS Knob to select the ‘Aux - System Setup 1’ Page.
AFCS
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
TURNING AN AIRSPACE ALERT ON OR OFF
SELECTING AND VIEWING AN AIRSPACE ALERT WITH ITS ASSOCIATED
INFORMATION
2)
Press the Alerts Softkey; or press the FMS Knob; or press the MENU
Key, highlight ‘Select Alerts Window’, and press the ENT Key. The cursor is
placed in the ‘Airspace Alerts’ Box.
3)
Select the desired airspace.
4)
Press the FMS Knob to remove the flashing cursor.
Appendix
Appendix
Select the ‘NRST - Nearest Airspaces’ Page.
Annun/Alerts
Annun/Alerts
1)
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
35
TURNING SMART AIRSPACE ON OR OFF
Use the FMS Knob to select the ‘Map - Navigation Map’ Page.
2)
Press the MENU Key, and press the ENT Key. The cursor is placed in the
‘Group’ Box.
3)
Turn the small FMS Knob to highlight the ‘Airspace’ in the ‘Group’ Box and
press the ENT Key.
4)
Turn the large FMS Knob to highlight the ‘Smart Airspace’ Field in the ‘Map
Settings’ Window.
5)
Turn the small FMS Knob clockwise to turn Smart Airspace ‘On’ or
counterclockwise to turn smart airspace ‘Off’.
6)
Press the FMS Knob to remove the flashing cursor.
ENTERING A WAYPOINT IDENTIFIER, FACILITY NAME, OR CITY AS A DIRECTTO DESTINATION
Additional Additional
Abnormal
Features
Operation
Features AFCS
Annun/Alerts
Annun/Alerts
1)
Press the Direct-to Key. The ‘Direct To’ Window is displayed (with the
active flight plan waypoint as the default selection or a blank waypoint field
if no flight plan is active).
2)
Turn the small FMS Knob clockwise to begin entering a waypoint identifier
(turning it counter-clockwise brings up the waypoint selection submenu press the CLR Key to remove it), or turn the large FMS Knob to select the
facility name, or city field and turn the small FMS Knob to begin entering
a facility name or city. If duplicate entries exist for the entered facility or
city name, additional entries can be viewed by turning the small FMS Knob
during the selection process.
3)
Press the ENT Key. The ‘Activate?’ Field is highlighted.
4)
Press the ENT Key to activate the direct-to.
SELECTING AN ACTIVE FLIGHT PLAN WAYPOINT AS A DIRECT-TO
DESTINATION
1)
Index
Index
Appendix
Appendix
1)
DIRECT-TO NAVIGATION
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Flight Management
36
While navigating an active flight plan, press the Direct-to Key. The ‘Direct
To’ Window is displayed with the active flight plan waypoint as the default
selection.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
3)
Select the desired waypoint.
4)
Press the ENT Key. The cursor is now displayed on ‘Activate?’.
5)
Press the ENT Key again to activate the direct-to.
EISEIS
Turn the small FMS Knob counter-clockwise to display a list of flight plan
waypoints (the FPL list is populated only when navigating a flight plan).
Flight
Flight
Instruments
Instruments
2)
Press the Direct-to Key. The ‘Direct To’ Window is displayed (with the
active flight plan destination as the default selection or a blank destination
if no flight plan is active).
2)
Turn the small FMS Knob counter-clockwise to display a list of flight plan
waypoints (the FPL list is populated only when navigating a flight plan).
3)
Turn the small FMS Knob clockwise to display the Nearest, Recent or User
waypoints.
4)
Turn the large FMS Knob clockwise to select the desired waypoint.
5)
Press the ENT Key. The cursor is now displayed on ‘Activate?’.
6)
Press the ENT Key again to activate the direct-to.
AFCS
1)
Additional Additional
Abnormal
AFCS Features
Features
Operation
CANCELLING A DIRECT-TO
Press the Direct-to Key to display the ‘Direct To’ Window.
2)
Press the MENU Key.
3)
With ‘Cancel Direct-To NAV’ highlighted, press the ENT Key. If a flight
plan is still active, the system resumes navigating the flight plan along the
closest leg.
Annun/Alerts
Annun/Alerts
1)
SELECTING A MANUAL DIRECT-TO COURSE
2)
Highlight the course field.
3)
Enter the desired course.
4)
Press the ENT Key. The cursor is now displayed on ‘Activate?’.
5)
Press the ENT Key again to activate the direct-to.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
Press the Direct-to Key. The ‘Direct To’ Window is displayed with the
destination field highlighted.
Appendix
Appendix
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
SELECTING A NEAREST, RECENT OR USER WAYPOINT AS A DIRECT-TO
DESTINATION
37
ENTERING A VNV ALTITUDE AND ALONG-TRACK OFFSET FOR THE
WAYPOINT
1)
Press the Direct-to Key to display the ‘Direct To’ Window.
2)
Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field
(‘ALT’ field on the PFD).
3)
Enter the desired altitude.
4)
Press the ENT Key to accept the altitude constraint.
5)
If the selected waypoint is an airport, an additional choice is displayed. Turn
the small FMS Knob to choose ‘MSL’ or ‘AGL’.
6)
Press the ENT Key. The cursor is now flashing in the VNV offset distance
(‘Offset’ Field).
7)
Enter the desired along-track distance before the waypoint.
8)
Press the ENT Key. The ‘Activate?’ Field is highlighted.
9)
Press the ENT Key to activate.
REMOVING A VNV ALTITUDE CONSTRAINT
1)
Press the Direct-to Key to display the ‘Direct To’ Window.
2)
Press the MENU Key.
3)
With ‘Clear Vertical Constraints’ highlighted, press the ENT Key.
FLIGHT PLANNING
CREATING AN ACTIVE FLIGHT PLAN
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Flight Management
1)
Press the FPL Key. Press the FMS Knob to activate the cursor (only on
MFD).
2)
Select the departure airport and runway.
Appendix
Appendix
a) Highlight the departure airport identifier using the FMS Knob
b) Use the FMS Knob or the waypoint submenu to enter the identifier,
facility, or city name of the departure waypoint.
Index
Index
c) Press the ENT Key. The ‘Set Runway’ Window is displayed with the
‘Runway’ field highlighted.
38
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
e) Press the ENT Key again to add the departure airport/runway to the
flight plan.
Repeat step number 2 for the destination airport and runway.
4)
Select the enroute waypoints.
EISEIS
3)
b) Use the FMS Knob or the waypoint submenu to enter the identifier,
facility, or city name of the waypoint. The active flight plan is modified
as each waypoint is entered.
5)
Repeat step number 4 to enter each additional enroute waypoint.
6)
When all waypoints have been entered, press the FMS Knob to remove the
cursor (if required).
ADDING A WAYPOINT TO THE ACTIVE FLIGHT PLAN
AFCS
Press the FMS Knob to activate the cursor (not required on the PFD).
3)
Select the point in the flight plan before which to add the new waypoint.
The new waypoint is placed directly in front of the highlighted waypoint.
4)
Turn the small FMS Knob to display the Waypoint Information Window.
(Turning it clockwise displays a blank Waypoint Information Window,
turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan,
nearest, recent, user, or airway waypoints).
5)
Enter the identifier, facility, or city name of the waypoint or select a
waypoint from the submenu of waypoints and press the ENT Key. The
active flight plan is modified as each waypoint is entered.
Appendix
Appendix
2)
CREATING AND ADDING USER WAYPOINTS TO THE ACTIVE FLIGHT PLAN
Index
Index
Push the Joystick to activate the panning function on the Active Flight
Plan Page and pan to the map location of the desired user waypoint.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Annun/Alerts
Annun/Alerts
Press the FPL Key.
Additional Additional
Abnormal
AFCS Features
Features
Operation
1)
190-02219-00 Rev. C
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
a) Highlight the location to insert the waypoint using the FMS Knob (If
the enroute header is selected, the new waypoint is placed following
the header. If an enroute waypoint or the dashes are selected, the new
waypoint will be placed before the selected item).
1)
Flight
Flight
Instruments
Instruments
d) Turn the small FMS Knob to select the runway, and press the ENT Key.
39
Flight Management
Press the FPL Key.
2)
Press the FMS Knob to activate the cursor (not required on the PFD).
3)
Turn the large FMS Knob to highlight the waypoint after the desired airway
entry point. If this waypoint is not a valid airway entry point, a valid entry
point should be entered at this time.
4)
Turn the small FMS Knob one click clockwise and press the LD AIRWY
Softkey on the MFD, or press the MENU Key and select “Load Airway” on
the PFD. The Select Airway Page is displayed. The LD AIRWY Softkey or
the “Load Airway” menu item is available only when a valid airway entry
waypoint has been chosen (the waypoint ahead of the cursor position).
5)
Turn the FMS Knob to select the desired airway from the list, and press the
ENT Key. Low altitude airways are shown first in the list, followed by “all”
altitude airways, and then high altitude airways.
6)
Turn the FMS Knob to select the desired airway exit point from the list, and
press the ENT Key. ‘Load?’ is highlighted.
7)
Press the ENT Key. The system returns to editing the flight plan with the
new airway inserted.
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
1)
COLLAPSE/EXPAND AIRWAYS IN THE ACTIVE FLIGHT PLAN
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the MENU Key, highlight ‘Collapse Airways’ or ‘Expand Airways’, and
press the ENT Key. The airways are collapsed/expanded.
STORING AN ACTIVE FLIGHT PLAN FROM THE ACTIVE FLIGHT PLAN PAGE
OR THE ACTIVE FLIGHT PLAN WINDOW
Index
Index
Appendix
Appendix
Select the LD WPT Softkey; or press the MENU Key, select ‘Load Waypoint’,
and press the ENT Key. The user waypoint is created with a name of
USRxxx (using the next available in sequence) and is added to the end of
the active flight plan.
ADDING AN AIRWAY TO A FLIGHT PLAN
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
2)
40
1)
Press the MENU Key.
2)
Highlight ‘Store Flight Plan’.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
Press the ENT Key.
4)
With ‘OK’ highlighted, press the ENT Key. The flight plan is stored in the
next available position in the flight plan list on the Flight Plan Catalog Page.
EISEIS
ACTIVATING A STORED FLIGHT PLAN ON THE MFD
Press the FPL Key and turn the small FMS Knob to display the ‘FPL - Flight
Plan Catalog’ Page.
2)
Press the FMS Knob to activate the cursor, and turn the FMS Knob to
highlight the desired flight plan.
3)
Press the Activate Softkey; or press the ENT Key twice; or press the
MENU Key, highlight ‘Activate Flight Plan’, and press the ENT Key. The
‘Activate stored flight plan?’ Window is displayed.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the
CLR Key, or highlight ‘Cancel’ and press the ENT Key.
INVERTING AND ACTIVATING A STORED FLIGHT PLAN ON THE MFD
Press the FMS Knob to activate the cursor, and turn the FMS Knob to
highlight the desired flight plan.
3)
Press the Invert Softkey; or press the MENU Key, highlight ‘Invert &
Activate FPL?’, and press the ENT Key. The ‘Invert and activate stored flight
plan?’ Window is displayed.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the
CLR Key, or highlight ‘Cancel’ and press the ENT Key.
IMPORT A FLIGHT PLAN FROM AN SD CARD
2)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page on the MFD.
3)
Turn the small FMS Knob to select the ‘FPL - Flight Plan Catalog’ Page.
4)
Press the FMS Knob to activate the cursor.
5)
Turn either FMS Knob to highlight an empty or existing flight plan.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
Insert the SD card containing the flight plan in the top card slot on the
MFD.
Appendix
Appendix
1)
Annun/Alerts
Annun/Alerts
2)
Additional Additional
Abnormal
AFCS Features
Features
Operation
Press the FPL Key and turn the small FMS Knob to display the ‘FPL - Flight
Plan Catalog’ Page.
AFCS
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
1)
190-02219-00 Rev. C
Flight
Flight
Instruments
Instruments
3)
41
Flight Management
Flight
Flight
Instruments
Instruments
6)
If an empty slot is selected, a list of the available flight plans on the SD
card will be displayed.
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 the list of 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 flight plan slot, and press the Import Softkey
again.
7)
Turn the small FMS Knob to highlight the desired flight plan for importing.
8)
Press the ENT Key to initiate the import.
9)
Press the ENT Key again to confirm the import.
EXPORT A FLIGHT PLAN TO AN SD CARD
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Or:
1)
Insert the SD card into the top card slot on the MFD.
2)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page on the MFD.
3)
Turn the small FMS Knob to select the ‘FPL - Flight Plan Catalog’ Page.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to highlight the flight plan to be exported.
6)
Press the Export Softkey; or press the MENU Key, select “Export Flight
Plan”.
7)
If desired, change the name for the exported file by turning the large FMS
Knob to the left to highlight the name, then use the small and large FMS
knobs to enter the new name, and press the ENT Key.
8)
Press the ENT Key to initiate the export.
9) Press the ENT Key to confirm the export.
Flight plans can be transferred to or from a mobile device via the Flight Stream 510
Bluetooth wireless connection. Transfer of a flight plan to a mobile device is controlled
by the mobile device.
Index
Index
Appendix
Appendix
Press the Import Softkey; or press the MENU Key, select “Import Flight
Plan”, and press the ENT Key.
42
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
2)
Press the ENT Key to display the ‘FPL - Preview Flight Plan’ Page on the
MFD.
Or:
Press the Preview Softkey to display the ‘FPL - Preview Flight Plan’ Page
on the MFD.
IGNORING A FLIGHT PLAN TRANSFER FROM A WIRELESS CONNECTION
When a flight plan transfer has been initiated from a mobile device, a
‘PENDING FLIGHT PLAN’ pop-up alert appears in the lower right corner of the
MFD, and an Connext annunciation appears to the right of the MFD page name.
2)
Press the CLR Key to remove the pop-up alert and ignore the pending flight
plan. The pending flight plan will still be available on the ‘FPL - Flight Plan
Catalog’ page.
Additional Additional
Abnormal
AFCS Features
Features
Operation
Or:
Press the Ignore Softkey to remove the pop-up alert and ignore the
pending flight plan. The pending flight plan will still be available on the
‘FPL - Flight Plan Catalog’ page.
STORING A PENDING FLIGHT PLAN
Press the FPL Key.
2)
Turn the small FMS Knob to display the ‘FPL - Flight Plan Catalog’ Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the FMS Knob to highlight the pending flight plan.
5)
Press the ENT Key to display the ‘FPL - Preview Flight Plan’ Page on the
MFD.
6)
Press the Store Softkey to store the flight plan. The pending flight plan is
stored and the pending annunciation is removed.
Appendix
Appendix
43
Index
Index
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Annun/Alerts
Annun/Alerts
1)
190-02219-00 Rev. C
AFCS
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
When a flight plan transfer has been initiated from a mobile device, a
‘PENDING FLIGHT PLAN’ pop-up alert appears in the lower right corner of
the MFD, and an Connext annunciation appears to the right of the MFD
page name.
EISEIS
1)
Flight
Flight
Instruments
Instruments
PREVIEWING A FLIGHT PLAN TRANSFER FROM A WIRELESS CONNECTION
ACTIVATING A PENDING FLIGHT PLAN
Press the FPL Key and turn the small FMS Knob to display the ‘FPL - Flight
Plan Catalog’ Page.
2)
Press the FMS Knob to activate the cursor, and turn the FMS Knob to
highlight the pending flight plan.
3)
Press the ENT Key to display the ‘FPL - Preview Flight Plan’ Page on the
MFD.
4)
Press the Activate Softkey. The ‘Activate Flight Plan?’ Window is
displayed.
5)
With ‘OK’ highlighted, press the ENT Key to activate the pending flight
plan. The pending flight plan becomes the active flight plan and is removed
from the ‘FPL - Flight Plan Catalog’ Page. To cancel the request, press the
CLR Key, or highlight ‘Cancel’ and press the ENT Key.
Additional Additional
Abnormal
Features
Operation
Features AFCS
1)
Press the FPL Key.
2)
Turn the small FMS Knob to display the ‘FPL - Flight Plan Catalog’ Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the FMS Knob to highlight the desired pending flight plan.
5)
Press the Delete Softkey. The ‘Delete Flight Plan XX?’ Window is
displayed.
Or:
Press the CLR Key. The ‘Delete Flight Plan XX?’ Window is displayed.
Annun/Alerts
Annun/Alerts
6)
With ‘OK’ highlighted, press the ENT Key to delete the pending flight plan.
The pending flight plan is removed from the ‘FPL - Flight Plan Catalog’
Page. To cancel the request, press the CLR Key, or highlight ‘Cancel’ and
press the ENT Key.
DELETING ALL PENDING FLIGHT PLANS
Index
Index
Appendix
Appendix
1)
DELETING A PENDING FLIGHT PLAN
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Flight Management
44
1)
Press the FPL Key.
2)
Turn the small FMS Knob to display the ‘FPL - Flight Plan Catalog’ Page.
3)
Press the MENU Key.
4)
Turn the FMS Knob to highlight ‘Delete All Pending’.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
Press the ENT Key. A ‘Delete all pending flight plans?’ confirmation
window is displayed.
6)
With ‘OK’ highlighted, press the ENT Key to delete all pending flight plans.
To cancel the request, press the CLR Key, or highlight ‘Cancel’ and press
EISEIS
the ENT Key.
Flight
Flight
Instruments
Instruments
5)
DELETING THE ACTIVE FLIGHT PLAN AND SUSPENDING NAVIGATION
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or
the ‘Flight Plan’ Window (PFD).
2)
Press the MENU Key, highlight ‘Delete Flight Plan’, and press the ENT Key.
The ‘Delete all waypoints in flight plan?’ Window is displayed.
3)
With ‘OK’ highlighted, press the ENT Key to delete the active flight plan. To
cancel the request, press the CLR Key, or highlight ‘Cancel’ and press the
ENT Key.
DELETING AN INDIVIDUAL WAYPOINT FROM THE ACTIVE FLIGHT PLAN
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the waypoint to be deleted.
3)
Press the CLR Key. The ‘Remove XXXXX?’ Window is displayed.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the
CLR Key, or highlight ‘Cancel’ and press the ENT Key.
5)
Press the FMS Knob to remove the flashing cursor.
Additional Additional
Abnormal
AFCS Features
Features
Operation
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD)
and turn the large FMS Knob to highlight the header of the airway to be
deleted.
3)
Press the CLR Key. The ‘Remove <airway name> from flight plan?’
Window is displayed.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
Appendix
Appendix
1)
Annun/Alerts
Annun/Alerts
DELETING AN ENTIRE AIRWAY FROM THE ACTIVE FLIGHT PLAN
190-02219-00 Rev. C
AFCS
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
1)
45
With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the
CLR Key, or highlight ‘Cancel’ and press the ENT Key.
5)
Press the FMS Knob to remove the flashing cursor.
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the header of the procedure to be
deleted.
3)
Press the CLR Key. The ‘Remove <procedure name> from flight plan?’
Window is displayed.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the
CLR Key, or highlight ‘Cancel’ and press the ENT Key.
5)
Press the FMS Knob to remove the flashing cursor.
ENTERING AN ALONG TRACK OFFSET DISTANCE
Annun/Alerts
Annun/Alerts
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the waypoint for the along track
offset.
3)
Press the ATK OFS Softkey (MFD only); or press the MENU Key, highlight
‘Create ATK Offset WPT’, and press the ENT Key.
4)
Enter a positive or negative offset distance in the range of +/- 1 to 999 nm
(limited by leg distances).
5)
Press the ENT Key to create the offset waypoint.
6)
Press the FMS Knob to remove the flashing cursor.
ACTIVATING PARALLEL TRACK
Index
Index
Appendix
Appendix
4)
DELETING AN ENTIRE PROCEDURE FROM THE ACTIVE FLIGHT PLAN
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Flight Management
46
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or
the ‘Flight Plan’ Window (PFD).
2)
Press the MENU Key, highlight ‘Parallel Track’, and press the ENT Key. The
‘Parallel Track’ Window is displayed with the ‘Direction’ field highlighted.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
4)
Turn the small FMS Knob to enter a distance from 1- 99 nm and press the
ENT Key. ‘Activate Parallel Track?’ is highlighted.
5)
Press the ENT Key to activate parallel track. Press the FMS Knob or the
CLR Key to cancel the parallel track activation.
EISEIS
Turn the small FMS Knob to select ‘LEFT’ or ‘RIGHT’ and press the ENT Key.
The ‘Distance’ field is highlighted.
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the MENU Key, highlight ‘Parallel Track’, and press the ENT Key.
The ‘Parallel Track’ Window is displayed with ‘Cancel Parallel Track?’
highlighted.
3)
Press the ENT Key.
ACTIVATING A FLIGHT PLAN LEG
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the destination waypoint for the
desired leg.
3)
Press the ACT Leg Softkey (MFD only); or press the MENU Key, highlight
‘Activate Leg’, and press the ENT Key. A confirmation window is displayed
with ‘Activate’ highlighted.
4)
Press the ENT Key to activate the flight plan leg. To cancel, press the CLR
Key, or highlight ‘Cancel’ and press the ENT Key.
5)
Press the FMS Knob to remove the flashing cursor.
Press the FPL Key to display the ‘FPL - Active Flight Plan Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the MENU Key, highlight ‘Invert Flight Plan’, and press the ENT Key.
An ‘Invert active flight plan?’ confirmation window is displayed.
3)
Select ‘OK’.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
47
Index
Index
1)
Appendix
Appendix
INVERTING THE ACTIVE FLIGHT PLAN
Annun/Alerts
Annun/Alerts
2)
Additional Additional
Abnormal
AFCS Features
Features
Operation
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
AFCS
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
CANCELLING PARALLEL TRACK
190-02219-00 Rev. C
Flight
Flight
Instruments
Instruments
3)
4)
1) Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
3) Press the CUM Softkey to view cumulative waypoint distance, or press the
Leg-Leg Softkey to view leg-to-leg waypoint distance.
4) Press the Wide Softkey to display the wide view, or press the Narrow
Softkey to display the narrow view.
5) Press the Back Softkey to return to the top level active flight plan softkeys.
VIEWING CHARTS AND ACTIVE FLIGHT PLAN PAGE IN SPLIT SCREEN MODE
1) Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
2) Press the Charts Softkey. Split screen mode is now enabled showing the
Charts page alongside the Active Flight Plan Page, and Charts page is
bordered by a cyan box indicating it is the active display pane.
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
2) Press the View Softkey to display the Wide, Narrow, Leg-Leg, and CUM
Softkeys.
3) To quickly view the chart corresponding to the active flight plan leg, press
the AUTO Softkey.
DISPLAYING THE FLIGHT PLAN MAP ON THE ACTIVE FLIGHT PLAN PAGE IN
SPLIT MODE
1) Press the FPL Key on the MFD to display the ‘FPL - Active Flight Plan’ Page.
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
Press the ENT Key to invert and activate the active flight plan. To cancel,
press the CLR Key, or highlight ‘Cancel’ and press the ENT Key.
CHANGING THE FLIGHT PLAN VIEW
EISEIS
Flight
Flight
Instruments
Instruments
Flight Management
2) Press the Charts Softkey. Split screen mode is now enabled showing the
Charts page alongside the Active Flight Plan Page, and Charts page is
bordered by a cyan box indicating it is the active display pane.
Appendix
Appendix
3) Move the Joystick to select the Active Flight Plan page as the active display
pane.
4) Press the MENU Key. ‘Show Flight Plan Map’ is highlighted. Press the ENT
Key.
Index
Index
5)
48
To removed the Flight Plan Map, press the MENU Key and select ‘Hide
Flight Plan Map’. Press the ENT Key.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
Flight
Flight
Instruments
Instruments
DETERMINING THE CLOSEST POINT ALONG THE ACTIVE FLIGHT PLAN TO A
SELECTED WAYPOINT
2)
Press the MENU Key, highlight ‘Closest Point Of FPL’, and press the ENT
Key. A window appears with the reference waypoint field highlighted.
3)
Enter the identifier of the reference waypoint. The system displays the
bearing (BRG) and distance (DIS) to the closest point along the flight
plan to the selected reference waypoint and creates a user waypoint at
this location. Press the ENT Key. The name for the new user waypoint is
derived from the identifier of the reference waypoint.
CREATING A USER-DEFINED HOLD AT AN ACTIVE FLIGHT PLAN WAYPOINT
3)
Press the MENU Key, highlight ‘Hold At Waypoint’, and press the ENT Key.
The ‘Hold at’ Window appears with the ‘Course’ Field highlighted.
4)
Use the FMS Knobs to edit the course, and press the ENT Key.
5)
Use the small FMS Knob to select ‘Inbound’ or ‘Outbound’ course direction,
and press the ENT Key.
6)
Use the small FMS Knob to select ‘Time’ or ‘Distance’ length mode, and
press the ENT Key.
7)
Use the FMS Knobs to edit the length, and press the ENT Key.
8)
Use the small FMS Knob to select ‘Right’ or ‘Left’ turn direction, and press
the ENT Key.
9)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC Time),
and press the ENT Key.
Appendix
Appendix
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the waypoint for the hold.
Annun/Alerts
Annun/Alerts
2)
Additional Additional
Abnormal
AFCS Features
Features
Operation
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
AFCS
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
EISEIS
1)
10) Press the ENT Key while ‘Load?’ is highlighted to insert the hold into the
flight plan.
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
49
CREATING A USER-DEFINED HOLD AT THE AIRCRAFT PRESENT POSITION
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the MENU Key, highlight ‘Hold At Present Position’, and press the
ENT Key. The ‘Hold at’ Window appears with the ‘Course’ field highlighted.
3)
If desired, use the FMS Knobs to edit the course, and press the ENT Key.
4)
Use the small FMS Knob to select ‘Inbound’ or ‘Outbound’ course direction,
and press the ENT Key.
5)
Use the small FMS Knob to select ‘Time’ or ‘Distance’ length mode, and
press the ENT Key.
6)
Use the FMS Knobs to edit the length, and press the ENT Key.
7)
Use the small FMS Knob to select ‘Right’ or ‘Left’ turn direction, and press
the ENT Key.
8)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC Time),
and press the ENT Key.
9)
Press the ENT Key while ‘Activate?’ is highlighted to create an Offroute
Direct-to hold waypoint at the aircraft present position and activate the
hold.
CREATING A USER-DEFINED HOLD AT A DIRECT-TO WAYPOINT
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Flight Management
50
1)
Press a Direct-to Key and set up the direct-to waypoint as desired, but
select ‘Hold?’ instead of ‘Activate?’ when finished (MFD or PFD).
2)
Use the FMS Knobs to edit the course, and press the ENT Key.
3)
Use the small FMS Knob to select ‘Inbound’ or ‘Outbound’ course direction,
and press the ENT Key.
4)
Use the small FMS Knob to select ‘Time’ or ‘Distance’ length mode, and
press the ENT Key.
5)
Use the FMS Knobs to edit the length, and press the ENT Key.
6)
Use the small FMS Knob to select ‘Right’ or ‘Left’ turn direction, and press
the ENT Key.
7)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key.
8)
Press the ENT Key while ‘Activate?’ is highlighted to activate the direct-to
with the user-defined hold defined at the direct-to waypoint. (If the directto waypoint is part of the active flight plan, the HOLD is inserted into the
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
Flight
Flight
Instruments
Instruments
active flight plan. If the direct-to waypoint is not part of the active flight
plan, an off-route direct-to hold is created.)
EXITING A USER-DEFINED HOLD INSERTED INTO THE ACTIVE FLIGHT PLAN
EISEIS
Press the SUSP Softkey. The system will provide guidance to follow the
holding pattern to the inbound course and resume automatic waypoint
sequencing.
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the HOLD waypoint.
3)
Press the CLR Key. A ‘Remove Holding Pattern?’ confirmation window is
displayed.
4)
Select ‘OK’ and press the ENT Key. The holding pattern is removed from
the active flight plan. Select ‘Cancel’ and press the ENT Key to cancel the
removal of the holding pattern.
REMOVING A USER-DEFINED HOLD AT AN OFF-ROUTE DIRECT-TO
Press a Direct To Key to display the ‘Direct To’ Window (PFD or MFD).
2)
Press the MENU Key to display the ‘Page Menu’ Window with the cursor
on the ‘Cancel Direct-To NAV’ selection.
3)
Press the ENT Key. The holding pattern is removed.
Annun/Alerts
Annun/Alerts
1)
VERTICAL NAVIGATION
ENABLING/DISABLING VNV GUIDANCE
2)
Press the ENBL VNV Softkey; or press the MENU Key, highlight ‘Enable
VNV’, and press the ENT Key. Vertical navigation is enabled, and vertical
guidance begins with the waypoint shown in the ‘Active VNV Profile’ Box
(defaults first waypoint in the active flight plan with an altitude enabled for
vertical navigation (e.g., FALUR)).
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
51
Index
Index
Press the FPL Key on the MFD to display the ‘FPL- Active Flight Plan’ Page.
Appendix
Appendix
1)
190-02219-00 Rev. C
Additional Additional
Abnormal
AFCS Features
Features
Operation
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
AFCS
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
REMOVING A USER-DEFINED HOLD INSERTED INTO THE ACTIVE FLIGHT
PLAN
Flight Management
NOTE: The selected waypoint must have a designated altitude constraint
(cyan number) to be used. If not, the first waypoint in the flight plan with a
designated altitude constraint is selected.
AFCS
Additional Additional
Abnormal
Features
Operation
Features AFCS
Annun/Alerts
Annun/Alerts
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page on the MFD.
2)
Press the FMS Knob to activate the cursor and turn the FMS Knob to
highlight the desired waypoint.
3)
Press the VNV Direct-To Softkey; or press the MENU Key, highlight
‘VNV Direct-To’, and press the ENT Key. An ‘Activate vertical Direct-to to:
NNNNNFT at XXXXXX?’ confirmation window is displayed.
4)
Press the ENT Key. Vertical guidance begins to the altitude constraint for
the selected waypoint.
5)
Press the FMS Knob to remove the flashing cursor.
MODIFYING THE VS TGT AND FPA
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page on the MFD.
2)
Press the VNV Prof Softkey; or press the MENU Key, highlight ‘Select VNV
Profile Window’, and press the ENT Key. The cursor is now located in the
‘Active VNV Profile’ Box.
3)
Turn the FMS Knobs as needed to edit the values.
4)
Press the FMS Knob to remove the flashing cursor.
ALTITUDE CONSTRAINTS
The system can use altitude constraints associated with lateral waypoints to give
guidance for vertical navigation. These altitudes are, depending on the specific instance, manually entered or retrieved from the published altitudes in the navigation
database.
Index
Index
Appendix
Appendix
To disable VNV guidance, press the Cncl VNV Softkey; or press the MENU
Key, highlight ‘Cancel VNV’, and press the ENT Key. Vertical navigation is
disabled.
ACTIVATING A VERTICAL NAVIGATION DIRECT-TO
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
3)
52
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
EISEIS
White Text
Cyan Text
White Text
with Altitude
Restriction Bar
Altitude Constraint Examples
Cross AT 2,300 ft
Cross AT or ABOVE
5,000 ft
AFCS
5OOOFT
Temperature Compensated
5OOOFT
Altitude calculated by the system estimating
the altitude of the aircraft as it passes over the
navigation point. No white line above or below to
indicate a potential constraint.
Altitude is designated for use in
determining vertical guidance. A pencil
icon indicates manual designation or
manual data entry.
5OOOFT
5OOOFT
Altitude retrieved from the navigation database.
White line above or below indicates the type of
constraint, as shown in the preceding figure.
These altitudes are provided as a reference, and
are not designated to be used in determining
vertical guidance.
The system cannot use this altitude in
determining vertical guidance because of
an invalid constraint condition.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
5OOOFT
Appendix
Appendix
Cyan Text
Annun/Alerts
Annun/Alerts
White Text
190-02219-00 Rev. C
Additional Additional
Abnormal
AFCS Features
Features
Operation
3OOOFT
Cross AT or BELOW
3,000 ft
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Cyan Text with
Pencil Icon
23OOFT
Flight
Flight
Instruments
Instruments
Displayed Text
Examples
53
Altitudes associated with arrival and approach procedures are not “auto-designated”. This means the system does not automatically use the altitudes loaded with the
arrival or approach for giving vertical speed and deviation guidance. Note that these
altitudes are displayed as white text 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.
MANUALLY DESIGNATING A WAYPOINT ALTITUDE TO BE USED FOR
VERTICAL GUIDANCE
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page on the MFD.
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude.
3)
Turn the small FMS Knob to enter editing mode.
4)
Press the ENT Key. The altitude is now shown in cyan, indicating it is
usable for vertical guidance.
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page on the MFD.
2)
Press the FMS Knob, and highlight the desired waypoint altitude. Turn the
small FMS Knob to enter editing mode. .
3)
Press the ENT Key. The altitude is now shown in cyan, indicating it is
usable for vertical guidance.
ENTERING/MODIFYING AN ALTITUDE CONSTRAINT
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page on the MFD.
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude
constraint.
3)
Enter an altitude constraint value using the FMS Knobs. To enter altitudes
as a flight level, turn the small FMS Knob counter-clockwise past zero
or clockwise past 9 on the first character, and the system automatically
changes to show units of Flight Level. Turn the large FMS Knob clockwise
to highlight the first zero and enter the three digit flight level.
4)
Press the ENT Key to accept the altitude constraint; if the selected
waypoint is an airport, an additional choice is displayed. Turn the small
FMS Knob to choose ‘MSL’ or ‘AGL’, and press the ENT Key to accept the
altitude.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
1)
MANUALLY DESIGNATING A PROCEDURE WAYPOINT ALTITUDE TO BE USED
FOR VERTICAL GUIDANCE
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Flight Management
54
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
• The altitude constraint results in a TOD behind the aircraft present
position
• The constraint is within a leg type for which altitude constraints are not
supported
• The altitude constraint is added to the FAF of an approach that provides
vertical guidance (i.e., ILS or GPS SBAS approach)
AFCS
• The altitude constraint is added to a waypoint past the FAF
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page on the MFD.
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude
constraint.
3)
Press the CLR Key. A ‘Remove VNV altitude?’ confirmation window is
displayed.
4)
Select ‘OK’ and press the ENT Key.
DELETING AN ALTITUDE CONSTRAINT THAT HAS BEEN MANUALLY ENTERED
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude
constraint.
3)
Press the CLR Key. A ‘Remove or Revert to published VNV altitude of
nnnnnFT?’ confirmation window is displayed.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page on the MFD.
Appendix
Appendix
1)
Annun/Alerts
Annun/Alerts
1)
Additional Additional
Abnormal
AFCS Features
Features
Operation
DELETING AN ALTITUDE CONSTRAINT PROVIDED BY THE NAVIGATION
DATABASE
190-02219-00 Rev. C
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
• Meeting the constraint requires the maximum flight path angle or
maximum vertical speed to be exceeded
EISEIS
• Meeting the constraint requires the aircraft to climb
Flight
Flight
Instruments
Instruments
Altitudes that have been designated for use in vertical guidance can be “undesignated” using the CLR Key. The altitude is now displayed only as a reference. It
is not used to give vertical guidance. Other displayed altitudes may change due to
re-calculations or be rendered invalid as a result of manually changing an altitude to a
non-designated altitude.
An altitude constraint is invalid if:
55
4)
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page on the MFD.
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude
constraint.
3)
Press the CLR Key. A ‘Remove or Revert to published VNV altitude of
nnnnnFT?’ confirmation window is displayed.
4)
Select ‘Revert’ and press the ENT Key. The altitude is changed to the
navigation database value.
5)
Press the FMS Knob to remove the flashing cursor.
MODIFYING A SYSTEM CALCULATED ALTITUDE CONSTRAINT
Additional Additional
Abnormal
Features
Operation
Features AFCS
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page on the MFD.
2)
Press the FMS Knob, and turn to highlight the desired waypoint altitude
constraint.
3)
Press the CLR Key. An ‘Edit or Revert to published VNV altitude of
nnnnnFT?’ confirmation window is displayed.
4)
Select ‘Edit’ and press the ENT Key.
5)
Edit the value using the FMS Knobs, and press the ENT Key.
6)
Press the FMS Knob to remove the flashing cursor.
ENABLING THE VERTICAL SITUATION DISPLAY
1)
Select the ‘Map - Navigation Map’ Page.
2)
Press the Map Opt Softkey.
3)
Press the Inset Softkey.
4)
Press the VSD Softkey to enable the Vertical Situation Display.
5)
Press the VSD mode softkey to choose between Auto, FPL, or TRK.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Select ‘Remove’ and press the ENT Key. The manually entered altitude is
deleted (it is replaced by a system calculated altitude, if available).
REVERTING A MANUALLY ENTERED ALTITUDE CONSTRAINT BACK TO THE
NAVIGATION DATABASE VALUE
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Flight Management
56
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
Select the ‘Map - Navigation Map’ Page.
2)
Press the Map Opt Softkey.
3)
Press the Off Softkey.
EISEIS
1)
Flight
Flight
Instruments
Instruments
DISABLING THE VERTICAL SITUATION DISPLAY
PROCEDURES
1)
From the ‘WPT - Airport Information’ Page (first page in the WPT group):
Press the DP Softkey. The ‘WPT - Departure Information’ Page is displayed,
defaulting to the airport displayed on the Airport information Page.
Or:
Press the STAR Softkey. The ‘WPT - Arrival Information’ Page is displayed,
defaulting to the airport displayed on the Airport information Page.
Or:
AFCS
Press the APR Softkey. The ‘WPT - Approach Information’ Page is
displayed, defaulting to the airport displayed on the Airport information
Page.
4)
Turn the small FMS Knob to view the available procedures. Press the ENT
Key to select the procedure. The cursor moves to the next box (runway or
transition). The procedure is previewed on the map.
5)
Turn the small FMS Knob to view the available runway or transition. Press
the ENT Key to select the runway or transition. The cursor moves to the
next box (if available). The procedure is previewed on the map.
6)
Turn the small FMS Knob to view the available runway or transition. Press
the ENT Key to select the runway or transition. The cursor moves to the
‘Sequence’ Box or the ‘Minimums’ Box. The procedure is previewed on the
map.
7)
Press the Info 1 Softkey or the Info 2 Softkey to return to the ‘WPT Airport Information’ Page.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
57
Index
Index
Turn the large FMS Knob to highlight the procedure. The procedure is
previewed on the map.
Appendix
Appendix
3)
Annun/Alerts
Annun/Alerts
To select another airport, press the FMS Knob to activate the cursor, enter
an identifier/facility name/city, and press the ENT Key.
Additional Additional
Abnormal
AFCS Features
Features
Operation
2)
190-02219-00 Rev. C
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
VIEWING AVAILABLE PROCEDURES AT AN AIRPORT
LOADING A PROCEDURE INTO THE ACTIVE FLIGHT PLAN FROM THE
<PROCEDURE> INFORMATION PAGE
1)
From the ‘WPT- Airport Information’ Page (first page in the WPT group):
Press the DP Softkey. The ‘WPT - Departure Information’ Page is displayed,
defaulting to the airport displayed on the Airport information Page.
EISEIS
Flight
Flight
Instruments
Instruments
Flight Management
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
Or:
Press the STAR Softkey. The ‘WPT - Arrival Information’ Page is displayed,
defaulting to the airport displayed on the Airport information Page.
Or:
Press the APR Softkey. The ‘WPT - Approach Information’ Page is
displayed, defaulting to the airport displayed on the Airport information
Page.
2)
To select another airport, press the FMS Knob to activate the cursor, enter
an identifier/facility name/city, and press the ENT Key.
3)
Select a different procedure, if desired.
AFCS
a) Turn the large FMS Knob to highlight the procedure. The procedure is
previewed on the map.
Additional Additional
Abnormal
Features
Operation
Features AFCS
b) Turn the small FMS Knob to view the available procedures. Press the
ENT Key to select the procedure. The cursor moves to the next box
(runway or transition). The procedure is previewed on the map.
c) Turn the small FMS Knob to view the available runway or transition.
Press the ENT Key to select the runway or transition. The cursor moves
to the next box (if available). The procedure is previewed on the map.
4)
Press the MENU Key to display the <Procedure> Information Page Menu.
5)
Turn the FMS Knob to highlight ‘Load <procedure>’.
6)
Press the ENT Key to load the procedure into the active flight plan.
LOADING A DEPARTURE INTO THE ACTIVE FLIGHT PLAN USING THE PROC
KEY
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
d) Turn the small FMS Knob to view the available transitions. Press the
ENT Key to select the transition. The cursor moves to the ‘Sequence’
Box or the ‘Minimums’ Box. The procedure is previewed on the map.
58
1)
Press the PROC Key. The ‘Procedures’ Window is displayed.
2)
Highlight ‘Select Departure’.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
4)
Use the FMS Knob to select an airport, if necessary, and press the ENT Key.
5)
Select a departure from the list and press the ENT Key.
6)
Select a runway (if required) and press the ENT Key.
7)
Select a transition (if required) and press the ENT Key. ‘Load?’ is
highlighted.
8)
Press the ENT Key to load the departure procedure.
EISEIS
Press the ENT Key. The ‘PROC - Departure Loading’ Page is displayed.
1)
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the MENU Key, and highlight ‘Remove Departure’.
3)
Press the ENT Key. A confirmation window is displayed listing the
departure procedure.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight
‘Cancel’ and press the ENT Key.
2)
Highlight ‘Select Arrival’.
3)
Press the ENT Key. The ‘PROC - Arrival Loading’ Page is displayed.
4)
Use the FMS Knob to select an airport, if necessary, and press the ENT Key.
5)
Select an arrival from the list and press the ENT Key.
6)
Select a transition (if required) and press the ENT Key.
7)
Select a runway (if required) and press the ENT Key. ‘Load?’ is highlighted.
8)
Press the ENT Key to load the arrival procedure.
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
2)
Press the MENU Key, and highlight ‘Remove Arrival’.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
1)
Appendix
Appendix
REMOVING AN ARRIVAL FROM THE ACTIVE FLIGHT PLAN
Annun/Alerts
Annun/Alerts
Press the PROC Key. The ‘Procedures’ Window is displayed.
Additional Additional
Abnormal
AFCS Features
Features
Operation
1)
AFCS
LOADING AN ARRIVAL INTO THE ACTIVE FLIGHT PLAN USING THE PROC KEY
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
REMOVING A DEPARTURE PROCEDURE FROM THE ACTIVE FLIGHT PLAN
190-02219-00 Rev. C
Flight
Flight
Instruments
Instruments
3)
59
3)
Press the ENT Key. A confirmation window is displayed listing the arrival
procedure.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight
‘Cancel’ and press the ENT Key.
APPROACH SERVICE LEVELS
HSI Annunciation
LNAV
LNAV+V
L/VNAV 
LP 
Description
RNAV GPS approach using published LNAV minima
RNAV GPS approach using published LNAV minima 
RNAV GPS approach using published LNAV/VNAV minima 
RNAV GPS approach using published LP minima 
LP+V 
RNAV GPS approach using published LP minima 
LPV 
RNAV GPS approach using published LPV minima 
 available only if SBAS is available
 downgrades to LNAV/VNAV (Baro VNAV) if SBAS becomes unavailable
 downgrades to LNAV is SBAS is unavailable
 advisory vertical guidance provided
Approach Service Levels
LOADING AN APPROACH INTO THE ACTIVE FLIGHT PLAN USING THE PROC
KEY
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Flight Management
1)
Press the PROC Key. The ‘Procedures’ Window is displayed.
2)
Highlight ‘Select Approach’, and press the ENT Key. The ‘PROC - Approach
Loading’ Page is displayed.
3)
Select the airport and approach:
Appendix
Appendix
a) Use the FMS Knob to select an airport, if necessary, and press the ENT
Key.
b) Select an approach from the list and press the ENT Key.
Or:
Index
Index
a) If necessary, push the FMS Knob to exit the approach list, and use the
large FMS Knob to move the cursor to the ‘Approach Channel’ Field.
b) Use the FMS Knob to enter the approach channel number, and press
the ENT Key to accept the approach channel number. The airport and
60
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
4)
Select a transition (if required) and press the ENT Key.
5)
Minimums
Flight
Flight
Instruments
Instruments
approach are selected.
Or:
To skip setting minimums, press the ENT Key.
6)
Press the ENT Key with ‘Load?’ highlighted to load the approach
procedure; or turn the large FMS Knob to highlight ‘Activate’ and press the
ENT Key to load and activate the approach procedure.
2)
Press the FMS Knob, then turn the large FMS Knob to highlight the desired nearest airport. The
airport is previewed on the map.
3)
Press the APR Softkey; or press the MENU Key, highlight ‘Select Approach
Window’, and press the ENT Key.
4)
Turn the FMS Knob to highlight the desired approach.
5)
Press the LD APR Softkey; or press the MENU Key, highlight ‘Load
Approach’, and press the ENT Key. The ‘PROC - Approach Loading’ Page is
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
61
Index
Index
Select the ‘NRST - Nearest Airports’ Page.
Appendix
Appendix
1)
Annun/Alerts
Annun/Alerts
LOADING AN APPROACH INTO THE ACTIVE FLIGHT PLAN FROM THE ‘NRST NEAREST AIRPORTS’ PAGE
Additional Additional
Abnormal
AFCS Features
Features
Operation
NOTE: When GPS is not approved for the selected final approach course, the
message ‘NOT APPROVED FOR GPS’ is displayed. GPS provides guidance to
the approach, but the CDI must to be switched to a NAV receiver to fly the
final course of the approach.
AFCS
NOTE: If there is no arrival procedure in the active flight plan, loading an
approach after a destination airport has already been entered will result in a
duplicate destination airport waypoint being added to the end of the enroute
segment.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
b) If ‘TEMP COMP’ was selected, the cursor moves to the temperature
field. Turn the small FMS Knob to select the temperature, and press the
ENT Key.
EISEIS
a) To set ‘Minimums’, turn the small FMS Knob to select ‘BARO’, ‘TEMP
COMP’ or ‘RAD ALT’, and press the ENT Key. Turn the small FMS Knob
to select the altitude, and press the ENT Key.
Flight Management
Flight
Flight
Instruments
Instruments
displayed with the transitions field highlighted.
6)
Turn the FMS Knob to highlight the desired transition, and press the ENT
Key.
7)
Minimums
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
a) To set ‘Minimums’, turn the small FMS Knob to select ‘BARO’, ‘TEMP
COMP’, or ‘RAD ALT’ and press the ENT Key. Turn the small FMS Knob
to select the altitude, and press the ENT Key.
b) If ‘TEMP COMP’ was selected, the cursor moves to the temperature
field. Turn the small FMS Knob to select the temperature, and press the
ENT Key.
Or:
To skip setting minimums, press the ENT Key. The ‘LOAD?’ Field is
highlighted.
Press the ENT Key with ‘LOAD?’ highlighted to load the approach
procedure; or turn the large FMS Knob to highlight ‘ACTIVATE’ and press
the ENT Key to load and activate the approach procedure. The system
continues navigating the current flight plan until the approach is activated.
When GPS is not approved for the selected final approach course, the
message ‘NOT APPROVED FOR GPS’ is displayed. GPS provides guidance to
the approach, but the CDI must to be switched to a NAV receiver to fly the
final course of the approach.
ACTIVATING A PREVIOUSLY LOADED APPROACH
1)
Press the PROC Key. The ‘Procedures Window’ is displayed with ‘Activate
Approach’ highlighted.
2)
Press the ENT Key to activate the approach.
ACTIVATING A PREVIOUSLY LOADED APPROACH WITH VECTORS TO FINAL
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
8)
1)
Press the PROC Key to display the ‘Procedures’ Window.
2)
Highlight ‘Activate Vector-to-Final’ and press the ENT Key.
REMOVING AN APPROACH FROM THE ACTIVE FLIGHT PLAN
Index
Index
1)
62
Press the FPL Key to display the ‘FPL - Active Flight Plan’ Page (MFD) or the
‘Flight Plan’ Window (PFD).
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
Press the MENU Key, and highlight ‘Remove Approach’.
3)
Press the ENT Key. A confirmation window is displayed listing the
approach procedure.
4)
With ‘OK’ highlighted, press the ENT Key. To cancel the removal, highlight
‘Cancel’ and press the ENT Key.
Flight
Flight
Instruments
Instruments
2)
EISEIS
ACTIVATING A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN
Press the PROC Key.
2)
Turn the FMS Knob to highlight ‘Activate Missed Approach’.
3)
Press the ENT Key. The aircraft automatically sequences to the MAHP.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
1)
Or:
Fly past the MAP, and press the SUSP Softkey on the PFD.
Or:
Press the Go-Around Button.
ACTIVATING TEMPERATURE COMPENSATED ALTITUDE
AFCS
From the ‘FPL - Active Flight Plan’ Page, press the MENU Key. The ‘Page
Menu’ Window is displayed.
2)
Turn the FMS Knob to highlight ‘Temperature Compensation’.
3)
Press the ENT Key. The ‘Temperature Compensation’ Window is displayed.
4)
Use the small FMS Knob to select the temperature at the <airport>. The
compensated altitude is computed as the temperature is selected.
Press the ENT Key. ‘Activate Compensation?’ is highlighted.
6)
Press the ENT Key. The compensated altitudes for the approach are
Annun/Alerts
Annun/Alerts
5)
shown in the flight plan.
Appendix
Appendix
CANCELLING TEMPERATURE COMPENSATED ALTITUDE
From the ‘FPL - Active Flight Plan’ Page, press the MENU Key. The ‘Page
Menu’ Window is displayed.
2)
Turn the FMS Knob to highlight ‘Temperature Compensation’.
3)
Press the ENT Key. The ‘Temperature Compensation’ Window is displayed.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
63
Index
Index
1)
190-02219-00 Rev. C
Additional Additional
Abnormal
AFCS Features
Features
Operation
1)
5)
Press the ENT Key. The temperature compensated altitude at the FAF
ENTERING BASIC EMPTY WEIGHT
1)
Press the Empty WT Softkey; or press the MENU Key, highlight ‘Set Basic
Empty Weight’, and press the ENT Key to select the ‘Basic Empty Weight’
Field.
2)
Turn the small FMS Knob to enter the basic empty weight.
3)
Press the ENT Key to confirm the entry.
4)
Press the FMS Knob to remove the flashing cursor.
ENTERING A PILOT AND STORES WEIGHT
1)
Press the FMS Knob to activate the cursor and highlight the ‘Pilot & Stores’
Field.
2)
Turn the small FMS Knob to enter the pilot and stores weight.
3)
Press the ENT Key to confirm the entry.
4)
Press the FMS Knob to remove the flashing cursor.
ENTERING THE NUMBER OF PASSENGERS
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
Press the ENT Key. ‘Cancel Compensation?’ is highlighted.
WEIGHT PLANNING
1)
Press the FMS Knob to activate the cursor and highlight the ‘Passengers #’
Field.
2)
Turn the small FMS Knob to enter the number of passengers.
3)
Press the ENT Key to confirm the entry.
4)
Press the FMS Knob to remove the flashing cursor.
ENTERING THE AVERAGE PASSENGER WEIGHT
Index
Index
Appendix
Appendix
4)
is cancelled.
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Flight Management
64
1)
Press the FMS Knob to activate the cursor and highlight the passenger
weight (‘at’) field.
2)
Turn the small FMS Knob to enter the average passenger weight.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
Press the ENT Key to confirm the entry.
4)
Press the FMS Knob to remove the flashing cursor.
The total weight of passengers is calculated by multiplying the number of
passengers by the average passenger weight.
EISEIS
ENTERING THE CARGO WEIGHT
Press the FMS Knob to activate the cursor and highlight the ‘Cargo’ Field.
2)
Turn the small FMS Knob to enter the cargo weight.
3)
Press the ENT Key to confirm the entry.
4)
Press the FMS Knob to remove the flashing cursor.
The ‘Zero Fuel Weight’ is calculated by adding the basic empty, pilot and
stores, passenger, and cargo weights.
ENTERING A FUEL ON BOARD WEIGHT
2)
Turn the small FMS Knob to enter the fuel on board.
3)
Press the ENT Key to confirm the entry.
4)
Press the FMS Knob to remove the flashing cursor.
SYNCHRONIZING THE FUEL ON BOARD WITH THE ACTUAL MEASURED FUEL
ON BOARD
ENTERING FUEL RESERVE
2)
Turn the small FMS Knob to enter the fuel reserves amount.
3)
Press the ENT Key to confirm the entry.
4)
Press the FMS Knob to remove the flashing cursor
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
Press the FMS Knob to activate the cursor and highlight the ‘Fuel Reserves’
Field.
Appendix
Appendix
1)
Annun/Alerts
Annun/Alerts
Press the FOB Sync Softkey on the ‘Aux - Weight Planning’ Page. The
actual measured fuel on board is displayed in the ‘FUEL ON BOARD’ Field.
Additional Additional
Abnormal
AFCS Features
Features
Operation
Press the FMS Knob to activate the cursor and highlight the ‘Fuel on Board’
Field.
AFCS
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
1)
190-02219-00 Rev. C
Flight
Flight
Instruments
Instruments
3)
65
TRIP PLANNING
SELECTING AUTOMATIC OR MANUAL PAGE MODE
From the ‘Aux - Trip Planning’ Page, press the Auto Softkey or the Manual
Softkey; or press the MENU Key, highlight ‘Auto Mode’ or ‘Manual Mode’,
and press the ENT Key.
SELECTING FLIGHT PLAN OR WAYPOINT MODE
From the ‘Aux - Trip Planning’ Page, press the FPL Softkey or the WPTs
Softkey; or press the MENU Key, highlight ‘Flight Plan Mode’ or ‘Waypoints
Mode’, and press the ENT Key.
SELECTING A FLIGHT PLAN AND LEG FOR TRIP STATISTICS
1)
From the ‘Aux - Trip Planning’ Page, press the FMS Knob to activate the
cursor in the ‘FPL’ Field.
2)
Turn the small FMS Knob to select the desired flight plan number.
3)
Turn the large FMS Knob to highlight ‘CUM’ or ‘REM’. The statistics for
each leg can be viewed by turning the small FMS Knob to select the
desired leg. The Trip Planning map also displays the selected data.
SELECTING WAYPOINTS FOR WAYPOINT MODE
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Flight Management
1)
From the ‘Aux - Trip Planning’ Page, press the WPTs Softkey; or press the
MENU Key, highlight ‘Waypoints Mode’, and press the ENT Key. The cursor
is positioned in the waypoint field directly below the ‘FPL’ Field.
2)
Turn the FMS knobs to select the desired waypoint (or press the MENU
Key and highlight ‘Set WPT to Present Position’ if that is what is desired),
and press the ENT Key. The cursor moves to the second waypoint field.
3)
Turn the FMS knobs to select the desired waypoint, and press the ENT Key.
The statistics for the selected leg are displayed.
ENTERING MANUAL DATA FOR TRIP STATISTICS CALCULATIONS
Index
Index
1)
66
From the ‘Aux - Trip Planning’ Page, press the Manual Softkey or select
‘Manual Mode’ from the ‘Page Menu’ Window, and press the ENT Key. The
cursor may now be positioned in any field in the top right two boxes.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Flight Management
Turn the FMS Knobs to move the cursor onto the ‘Departure Time’
Field and enter the desired value. Press the ENT Key. The statistics
are calculated using the new value and the cursor moves to the next
entry field. Repeat until all desired values have been entered.
EISEIS
RAIM PREDICTION
Select the ‘Aux - GPS Status’ Page.
2)
If necessary, press the RAIM Softkey.
3)
Press the FMS Knob. The ‘Waypoint’ Field is highlighted.
4)
Turn the small FMS Knob to display the ‘Waypoint Information’ Window.
5)
Enter the desired waypoint:
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
PREDICTING RAIM AVAILABILITY AT A SELECTED WAYPOINT
1)
Use the FMS Knob to enter the desired waypoint by identifier, facility,
or city name and press the ENT Key.
b) Turn the small FMS Knob clockwise to display the Flight Plan, Nearest,
Recent, or User waypoints, if required.
c) Turn the large FMS Knob clockwise to select the desired waypoint. The
system automatically fills in the identifier, facility, and city fields with the
information for the selected waypoint.
Annun/Alerts
Annun/Alerts
d) Press the ENT Key to accept the waypoint entry.
7)
Use the FMS Knob to enter an arrival date and press the ENT Key.
8)
With the cursor highlighting ‘Compute RAIM?’, press the ENT Key. Once
RAIM availability is computed, one of the following is displayed:
Appendix
Appendix
Use the FMS Knob to enter an arrival time and press the ENT Key.
• ‘Compute RAIM?’—RAIM has not been computed for the current
waypoint, time, and date combination
Index
Index
• ‘Computing Availability’—RAIM calculation in progress
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Additional Additional
Abnormal
AFCS Features
Features
Operation
a) Turn the small FMS Knob counter-clockwise to display a list of flight
plan waypoints (the FPL list is populated only when navigating a flight
plan).
AFCS
Or:
6)
Flight
Flight
Instruments
Instruments
2)
67
Flight Management
• ‘RAIM not Available’—RAIM is predicted to be unavailable for the
specified waypoint, time, and date
PREDICTING RAIM AVAILABILITY AT THE AIRCRAFT PRESENT POSITION
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
• ‘RAIM Available’—RAIM is predicted to be available for the specified
waypoint, time, and date
Select the ‘Aux - GPS Status’ Page.
2)
If necessary, press the RAIM Softkey.
3)
Press the FMS Knob. The ‘Waypoint’ Field is highlighted.
4)
Press the MENU Key.
5)
With ‘Set WPT to Present Position’ highlighted, press the ENT Key.
6)
Press the ENT Key to accept the waypoint entry.
7)
Use the FMS Knob to enter an arrival time and press the ENT Key.
8)
Use the FMS Knob to enter an arrival date and press the ENT Key.
9)
With the cursor highlighting ‘Compute RAIM?’, press the ENT Key. Once
RAIM availability is computed, one of the following is displayed:
Additional Additional
Abnormal
Features
Operation
Features AFCS
• ‘Compute RAIM?’—RAIM has not been computed for the current
waypoint, time, and date combination
• ‘Computing Availability’—RAIM calculation in progress
• ‘RAIM Available’—RAIM is predicted to be available for the specified
waypoint, time, and date
• ‘RAIM not Available’—RAIM is predicted to be unavailable for the
specified waypoint, time, and date
DISABLING SBAS
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
1)
68
1)
Select the ‘Aux - GPS Status’ Page.
2)
If necessary, press the SBAS Softkey.
3)
Press the FMS Knob, and turn the large FMS Knob to highlight ‘EGNOS’,
‘MSAS’, or ‘WAAS’.
4)
Press the ENT Key to uncheck the box.
5)
Press the FMS Knob to remove the cursor.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
Flight
Flight
Instruments
Instruments
HAZARD AVOIDANCE
Customizing the Hazard Displays on the Navigation Map Page
2)
Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS
Knob to select ‘Weather’ to customize the display of weather features.
Select ‘Traffic’ to customize the display of traffic.
3)
Press the small FMS Knob to return to the Navigation Map Page.
STORMSCOPE® (OPTIONAL)
Additional Additional
Abnormal
AFCS Features
Features
Operation
Displaying Stormscope Lightning Data on the Navigation Map Page
1)
Select the Map Opt Softkey.
2)
Select the STRMSCP Softkey.
Symbol
Annun/Alerts
Annun/Alerts
Lightning Age
Strike is less than 6 seconds old
Strike is between 6 and 60 seconds old
Appendix
Appendix
Strike is between 1 and 2 minutes old
Strike is between 2 and 3 minutes old
Displaying Stormscope information on PFD maps
On the PFD, press the Map/HSI Softkey.
2)
Press the Lightning Softkey.
3)
Press the STRMSCP Softkey.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
1)
AFCS
WARNING: Do not rely on information from the lightning detection system
display as the sole basis for hazardous weather avoidance. Range limitations
and interference may cause the system to display inaccurate or incomplete
information. Refer to the documentation from the lightning detection system
manufacturer for detailed information about the system.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
With the Navigation Map Page displayed, press the MENU Key to display
the Navigation Map Page Menu. The cursor flashes on the ‘Map Settings’
option.
EISEIS
1)
69
Hazard Avoidance
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Selecting ‘cell’ or ‘strike’ mode on the Stormscope Page
Select the Stormscope Page.
2)
Select the Mode Softkey. The Cell and Strike softkeys are displayed.
3)
Select the Cell Softkey to display ‘CELL’ data or select the Strike Softkey to
display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’ is displayed in the mode box in the
upper right corner of the Stormscope Page.
4)
Press the Back Softkey to return to the top-level softkeys for the Stormscope
Page.
NOTE: “Cell mode” uses a clustering program to identify clusters of electrical
activity that indicate cells.
AFCS
Manually Clearing Stormscope Data on the Navigation Map Page
1)
Press the MENU Key.
2)
Turn the FMS Knob to highlight ‘Clear Stormscope® Lightning’.
3)
Press the ENT Key.
Manually Clearing Stormscope Data on the Stormscope Page
Press the Clear Softkey.
SIRIUSXM WEATHER (OPTIONAL)
WARNING: Do not use data link weather information for maneuvering in,
near or around areas of hazardous weather. Information contained within data
link weather products may not accurately depict current weather conditions.
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
1)
Index
Index
Appendix
Appendix
WARNING: Do not use the indicated data link weather product age to
determine the age of the weather information shown by the data link weather
product. Due to time delays inherent in gathering and processing weather
data for data link transmission, the weather information shown by the data
link weather product may be older than the indicated weather product age.
70
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
2)
If necessary, turn the small FMS Knob to select the Weather Data Link
Page. If the name of another source besides ‘(XM)’ is in the page title,
continue to Step 3.
3)
Press the MENU Key.
4)
If necessary, turn the large FMS Knob to highlight ‘Display XM Weather’
and press the ENT Key.
Displaying SiriusXM Weather on the Navigation Map Page
1)
Press the Map Opt Softkey.
2)
Press the NEXRAD or XM LTNG or METAR Softkey to display the desired
weather. Press the applicable softkey again to remove weather data from
the Navigation Map Page.
Displaying Sirius Weather Legends on the Navigation Map Page
Press the Map Opt Softkey.
2)
Press the Legend Softkey to display or remove the legend.
AFCS
1)
Turn the large FMS Knob to select the WPT Page Group.
2)
Turn the small FMS Knob to select the Airport Information Page.
3)
Press the WX Softkey to display METAR and TAF text.
4)
Press the FMS Knob to enable the cursor, then turn the small FMS Knob as
needed to FMS knob to scroll through the text.
5)
After viewing text, press the FMS Knob to disable the cursor.
Displaying Weather on the Weather Data Link (XM) Page
2)
Turn the small FMS Knob to select the Weather Data Link (XM) Page.
3)
Press the available softkeys to select the desired SiriusXM Weather product.
4)
Press 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.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
71
Index
Index
Turn the large FMS Knob to select the Map Page Group.
Appendix
Appendix
1)
Annun/Alerts
Annun/Alerts
1)
Additional Additional
Abnormal
AFCS Features
Features
Operation
Display METAR and TAF information on the Airport Information Page
190-02219-00 Rev. C
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
If necessary, turn the large FMS Knob to select the Map Page Group.
EISEIS
1)
Flight
Flight
Instruments
Instruments
Changing the Data Link Weather Source to Display SiriusXM Weather
Hazard Avoidance
Flight
Flight
Instruments
Instruments
Enabling/disabling NEXRAD Animation on the Weather Data Link (XM)
Page
1) Turn the large FMS Knob to select the Map Page Group.
EISEIS
2) Turn the small FMS Knob to select the Weather Data Link (XM) Page.
3) Press the MENU Key.
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
4) Turn the FMS Knob to select ‘Weather Setup’ and press the ENT Key.
5) Turn the large FMS Knob to highlight the NEXRAD Animation on/off field.
6) Turn the small FMS Knob to select ‘On’ or ‘Off’ then press the ENT Key.
Map Panning Information – Weather Data Link (XM) Page
Push in the Joystick to activate the Map Pointer.
2)
Move the Joystick to place the Map Pointer over graphical weather
information. For Cloud Tops, Echo Tops, METAR flags, Storm Cells, and
County Warnings, an information box appears near the Map Pointer. If the
Map Pointer has highlighted a SIGMET, AIRMET, PIREP, AIREP, or TFR, press
the ENT Key to view additional information such as report text, then press
the ENT Key or the CLR Key to remove the information.
AFCS
1)
Additional Additional
Abnormal
Features
Operation
Features AFCS
Note when a METAR flag or airport is highlighted, pressing the ENT Key
shows the WPT - Weather Information Page. The decoded and original
METAR text is available on this page as well as the TAF, if provided. When
finished, press the Go Back Softkey or press the CLR Key to return to the
Weather Data Link (XM) Page.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Enabling/disabling winds aloft data display in the Vertical Situation
Display (VSD):
72
1)
Select the Navigation Map Page.
2)
Press the MENU Key.
3)
With ‘Map Settings’ highlighted, press the ENT Key
4)
Turn the small FMS Knob to select the ‘VSD’ Group and press the ENT Key
5)
Turn the large FMS Knob to select the Winds On/Off field.
6)
7)
Turn the small FMS Knob to select ‘On’ or ‘Off’.
Press the FMS Knob or CLR Key to return to the Navigation Map Page with
the changed settings.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
EISEIS
SiriusXM Weather Products and Symbols
Refresh Rate
(Minutes)
NEXRAD
30
5 (U.S.)
10 (Canada)
Cloud Top (CLD TOP)
60
15 (69/69A)
Symbol
30 (69/69A SXM)
30
5
Cell Movement (CELL
MOV)
30
1.25
SIGMETs/AIRMETs (SIG/
AIR)
60
12
METARs
90
12
City Forecast (CITY)
90
12
Surface Analysis (SFC)
60
12
Freezing Levels (FRZ LVL)
120
12
Winds Aloft (WIND)
90
12
Appendix
Appendix
SiriusXM Lightning
(LTNG)
Annun/Alerts
Annun/Alerts
7.5
Additional Additional
Abnormal
AFCS Features
Features
Operation
30
AFCS
Echo Top (ECHO TOP)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Expiration Time
(Minutes)
Weather Product
Flight
Flight
Instruments
Instruments
NOTE: NEXRAD data cannot be displayed simultaneously on the same map
as relative terrain, echo tops, turbulence, icing, or airborne weather radar is
displayed.
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
73
Expiration Time
(Minutes)
Refresh Rate
(Minutes)
County Warnings
(COUNTY)
60
5
Cyclone Warnings
(CYCLONE)
60
12
90
22
90
12
90
12
180
12
No product image
30
5
No product image
No product image
60
60
12
12
Weather Product
Symbol
Icing Potential (CIP and
SLD) (ICNG)
Pilot Weather Report
(PIREPs)
Air Report
(AIREPs)
Turbulence
(TURB)
Radar Coverage Not
Available
TFRs
TAFs
CONNEXT WEATHER (OPTIONAL)
WARNING: Do not use data link weather information for maneuvering in,
near, or around areas of hazardous weather. Information contained within
data link weather products may not accurately depict current weather conditions.
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Hazard Avoidance
Index
Index
Appendix
Appendix
WARNING: Do not use the indicated data link weather product age to
determine the age of the weather information shown by the data link weather
product. Due to time delays inherent in gathering and processing weather
data for data link transmission, the weather information shown by the data
link weather product may be older than the indicated weather product age.
NOTE: To check the availability of Garmin Connext weather products offered
in a particular region, visit http://sites.garmin.com/connext.
74
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
Flight
Flight
Instruments
Instruments
Weather data is provided when the pilot initiates either a manual or automatic
Connext data request on the Weather Data Link (CNXT) Page on the MFD. No
weather data is displayed until the first Connext Weather Data Request is made.
Accessing Connext Weather Products
EISEIS
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Data Link (CNXT) Page.
30
Infrared Satellite
60
30
Datalink Lightning
30
Continuous
SIGMETs/AIRMETs
60
Continuous
METARs
90
Continuous
Winds Aloft
90
Continuous
Pilot Weather Report
(PIREPs)
90
Continuous
no product image
60
Continuous
Terminal Aerodrome
Reports TAFs)
no product image
60
Continuous
Appendix
Appendix
Temporary Flight
Restrictions (TFRs)
Annun/Alerts
Annun/Alerts
Radar Precipitation
U.S.: 3*
Canada: 3*†
Europe: 15
Australia: 15ˆ
Additional Additional
Abnormal
AFCS Features
Features
Operation
Refresh Rate
(Minutes)
Symbol
AFCS
Expiration Time
(Minutes)
Garmin Connext
Weather Product
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
1)
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
* The composite precipitation image is updated every 3 minutes, but individual radar sites may take
between 3 and 10 minutes to provide new data.
†
Canadian radar precipitation data provided by Environment Canada.
ˆ Australian radar precipitation data provided by the Australian Bureau of Meteorology.
75
Hazard Avoidance
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Setting up and customizing the Weather Data Link (CNXT) Page
1)
Select the Weather Data Link (CNXT) Page.
2)
Press the MENU Key.
3)
With ‘Weather Setup’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select ‘Product Group 1’ or ‘Product Group 2’,
and press the ENT Key.
5)
Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
6)
Turn the small FMS Knob to scroll through options for each product (ON/
OFF, maximum map range settings, etc.).
7)
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the Weather Data Link (CNXT)
Page with the changed settings.
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Restoring default Weather Data Link (CNXT) Page settings
1)
Select the Weather Data Link (CNXT) Page.
2)
Press the MENU Key.
3)
With ‘Weather Setup’ highlighted, press the ENT Key.
4)
Press the MENU Key.
5)
Highlight the desired default(s) to restore (all or for selection) and press
ENT Key.
1)
Select the Weather Data Link (CNXT) Page.
2)
Select the Legend Softkey to display the legends for the displayed weather
products.
3)
Turn the FMS Knob to scroll through the legends if more are available than
fit in the window.
4)
To remove the Legend Window, press the Legend Softkey, the ENT Key,
the CLR Key, or the FMS Knob.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Viewing Legends for Displayed Connext Weather Products on the
Weather Data Link (CNXT) Page
76
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
Select the Navigation Map Page.
2)
Press the Map Opt Softkey.
3)
Press the softkey to enable/disable the desired weather product.
EISEIS
1)
Flight
Flight
Instruments
Instruments
Displaying Data Link Weather Products on the Navigation Map Page
Showing/removing the weather legend on the Navigation Map Page
Select the Navigation Map Page.
2)
Press the Map Opt Softkey.
3)
Press the Legend Softkey to show the weather legends window.
4)
When finished, press the Legend Softkey again, or press the FMS Knob or
the CLR Key to remove the window.
Setting up and customizing weather data for the Navigation Map Page
Press the MENU Key.
3)
With ‘Map Settings’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select the ‘Weather’ Group and press the ENT
Key.
5)
Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
6)
Turn the small FMS Knob to scroll through options for each product (ON/
OFF, range settings).
7)
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the Navigation Map Page with
the changed settings.
Displaying Data Link Weather products on the PFD map
On the PFD, press the Map/HSI Softkey.
2)
Press the desired weather product softkey(s) to enable/disable the display
of data link products on the PFD map.
Appendix
Appendix
1)
Annun/Alerts
Annun/Alerts
2)
Additional Additional
Abnormal
AFCS Features
Features
Operation
Select the Navigation Map Page.
AFCS
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
1)
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
77
Hazard Avoidance
Flight
Flight
Instruments
Instruments
3)
a) Press the Datalink Softkey to enable data link lightning or press the
LTNG Off Softkey.
EISEIS
b) Press the Back Softkey twice to return to the top-level PFD Softkeys.
Enabling/disabling the weather product icon and age display (PFD
maps)
1)
On the PFD, press the Map/HSI Softkey.
2)
Press the WX LGND Softkey to enable/disable the weather product age,
source, and icon box display on PFD Maps.
Connext Weather Data Requests
The Connext Data Request Menu provides the pilot with the options to define
the requested weather coverage area(s), choose automatic weather update intervals
(if desired), and the ability to send or cancel weather data requests. A Request Status
Window inside the menu shows the status of the Connext Data Request.
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
To enable/disable a data link lightning weather product on a PFD, press the
Lightning Softkey.
Additional Additional
Abnormal
Features
Operation
Features AFCS
Manually Requesting Garmin Connext Weather information
1)
Select the Weather Data Link (CNXT) Page.
2)
Press the MENU Key.
3)
With ‘Connext Data Request’ highlighted, press the ENT Key.
4)
Turn the large FMS Knob to highlight the desired coverage option(s) and
press the ENT Key to show or hide a green check mark to select one of
more of the following coverage selections:
Annun/Alerts
Annun/Alerts
• Present Position – Requests data based on current location.
Appendix
Appendix
• Destination – Requests data based on the active flight plan
destination (Direct-To destinations excluded). See the Flight
Management section for more information about entering and
activating flight plans.
Index
Index
• FPL – Requests data along an active flight plan, if one currently
exists. Turn the small FMS Knob to select the desired flight plan lookahead distance option (or choose ‘Remaining FPL’ to request weather
data for the remainder of the flight plan), then press the ENT Key.
78
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
6)
Turn the large FMS Knob until the ‘Send Request’ field is highlighted. Press
the ENT Key to initiate the request immediately or press the FMS Knob to
return to the Weather Data Link (CNXT) Page without requesting weather
data.
Weather Request Status
Message
Description
A general error has occurred. If the error persists, the
system should be serviced.
Connext Comm Error [2]
A communications error has occurred with the GDL59 or
GIA. The system should be serviced.
Connext Comm Error [3]
A general error has occurred. If the error persists, the
system should be serviced.
Connext Comm Error [4]
This occurs if multiple automatic weather data requests
have recently failed, or the GDL 59 or a GIA is off-line.
Connext Comm Error [5]
This can occur if the GDL 59 is off-line or not configured, or
the Iridium or Garmin Connext services are not accessible.
Check Iridium signal strength. If this error persists, the
system should be serviced.
Connext Comm Error [6]
A communications error has occurred. It this error persists,
the system should be serviced.
Connext Comm Error [7]
A weather data transfer has timed out. Check Iridium
signal strength and re-send the data request.
Connext Comm Error [8]
A server error has occurred or invalid data received.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
Connext Comm Error [1]
Appendix
Appendix
The system will attempt another automatic weather data
request after an error occurred during the previous request.
Timer counts down until the next automatic request occurs.
Annun/Alerts
Annun/Alerts
Auto update retry: ## Seconds
Additional Additional
Abnormal
AFCS Features
Features
Operation
The system has disabled automatic weather data requests
due to excessive errors. Automatic weather data requests
have stopped. Send a manual weather data request to
resume automatic updates.
AFCS
Auto requests inhibited Send
manual request to reset.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Turn the large FMS Knob highlight to the ‘Diameter / Route Width’ distance
field and turn the small FMS Knob to select the desired diameter and route
width of the request, then press the ENT Key.
EISEIS
5)
Flight
Flight
Instruments
Instruments
• Waypoint – Requests data based on a waypoint (which may be offroute). Turn the large and small FMS Knobs to enter a waypoint, then
press the ENT Key.
79
Weather Request Status
Message
Description
Connext Comm Error [9]
An error occurred while reading or writing data. If the error
persists, the system should be serviced.
Connext Login Invalid
There is a problem with the Garmin Connext registration.
Contact Garmin at 1-866-739-5687 in the United States or
913-397-8200, wait for the operator, and request Extension
1135 for assistance.
Connext Server Temp Inop
The Garmin Connext Weather data server is temporarily out
of service, but is expected to return to service in less than
30 minutes.
Connext Server Inop
The Garmin Connext Weather data server will be out of
service for at least 30 minutes.
Invalid Coverage Area
The weather data request coverage area does not contain
at least one of the following: a waypoint, a flight plan, or a
flight plan destination. Verify at least one of the coverage
options is enabled (checked) and contains required criteria,
then re-send the data request.
No Connext Subscription
The system is not be currently subscribed to Garmin
Connext services or the access code is incorrect. Verify the
access code. Contact Garmin at 1-866-739-5687 in the
United States or 913-397-8200, wait for the operator, and
request Extension 1135 for assistance.
Reduce Request Area
The size of the received weather data has exceeded system
memory limits. Reduce the size of the coverage area and
issue another Connext Data Request to ensure all available
weather data has been received.
Request Canceled
The user has cancelled a Connext Data Request.
Request Failed - Try Again
The weather data request timed-out. Re-send data request.
Transfer Preempted
The GDL 59 is busy. Retry request later.
Abnormal Weather Data Request Status Messages
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Hazard Avoidance
Index
Index
Cancelling a Connext Data Request in Progress
80
1)
Select the Weather Data Link (CNXT) Page.
2)
Press the MENU Key.
3)
With ‘Connext Data Request’ highlighted, press the ENT Key.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
Turn the large FMS Knob to select the ‘Cancel Request’ field and press the
ENT Key. The request status box indicates ‘Request Cancelled’.
5)
Press the FMS Knob to return to the Weather Data Link (CNXT) Page.
Flight
Flight
Instruments
Instruments
4)
EISEIS
Enabling/disabling automatic Connext Data Requests
Select the Weather Data Link (CNXT) Page.
2)
Press the MENU Key.
3)
With ‘Connext Data Request’ highlighted, press the ENT Key.
4)
Choose the desired weather coverage options.
5)
Turn the large FMS Knob to select the ‘Update Rate’ field. Then turn the
small FMS Knob to highlight the desired automatic update frequency (Off,
5 Min, 10 Min, 15 Min, 20 Min, 30 Min, 45 Min, or 60 Min), then press the
ENT Key.
6)
The ‘Send Request’ field is highlighted and a countdown timer is displayed
in the ‘Request Status’ Window based on the currently selected update
rate. Press the ENT Key to immediately send an immediate Connext Data
Request.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
1)
AFCS
Or:
FIS-B WEATHER
Appendix
Appendix
WARNING: Do not use the indicated data link weather product age
to determine the age of the weather information shown by the data
link weather product. Due to time delays inherent in gathering and
processing weather data for data link transmission, the weather
information shown by the data link weather product may be older than
the indicated weather product age.
Annun/Alerts
Annun/Alerts
WARNING: Do not use data link weather information for maneuvering
in, near, or around areas of hazardous weather. Information contained
within data link weather products may not accurately depict current
weather conditions.
Additional Additional
Abnormal
AFCS Features
Features
Operation
Press the FMS Knob to return to the Weather Data Link (CNXT) Page.
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
81
The optional GTX 345R transponder receives Flight Information Services - Broadcast
(FIS-B) weather data from a network of UAT ground-based transceivers (GBTs).
FIS-B weather data reception requires the aircraft being within range and line-ofsight of an operating GBT broadcasting FIS-B weather data. Reception may be affected
by factors including altitude or terrain.
Reception of FIS-B weather data occurs automatically without any pilot action. FIS-B
broadcasts provide weather data in a repeating cycle which may take approximately
ten minutes to transmit all available weather data. Therefore, not all available weather
data may be available immediately upon initial FIS-B signal acquisition.
Viewing the Weather Data Link (FIS-B) Page
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Hazard Avoidance
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Data Link (FIS-B or XM)
Page.
3)
If the page title displays a weather data link weather source other than
‘FIS-B’, such as ‘XM’, proceed to the following steps to change the data link
weather source.
4)
Press the MENU Key.
5)
Turn the small FMS Knob to select ‘Display FIS-B Weather’.
6)
Press the ENT Key. The page title will display ‘Map - Weather Data Link
(FIS-B)’ to indicate FIS-B is now the selected data link weather source.
Enabling/Disabling FIS-B Weather
Annun/Alerts
Annun/Alerts
Appendix
Appendix
Index
Index
1)
1)
Select the Weather Data Link (FIS-B) Page.
2)
Press the MENU Key.
3)
Turn the small FMS Knob to highlight ‘Enable FIS-B Weather’ or ‘Disable
FIS-B Weather’, and press the ENT Key.
Expiration Time
(Minutes)
Broadcast Rate
(Minutes)
NEXRAD Composite (US)
30
15
NEXRAD Composite
(Regional)
30
2.5
Meteorological Aerodrome
Report (METARs)
90
5
FIS-B Weather Product
82
Symbol
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
90
10
Winds Aloft
(WIND)
90
10
SIGMETs/AIRMETs
(SIG/AIR)
60
5
No Radar Coverage
no product image
30
2.5
Terminal Aerodrome Forecast
no product image
60
10
Temporary Flight Restriction
(TFR)
no product image
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Pilot Weather Report
(PIREPs)
EISEIS
Broadcast Rate
(Minutes)
Symbol
Flight
Flight
Instruments
Instruments
Expiration Time
(Minutes)
FIS-B Weather Product
10
Weather Product Symbols and Data Timing
Setting Up and Customizing the Weather Data Link (FIS-B) Page
AFCS
Select the Weather Data Link Page.
2)
Press the MENU Key.
3)
Turn the FMS Knob to highlight ‘Weather Setup’, then press the ENT Key.
4)
Turn the small FMS Knob to select ‘Product Group 1’ or ‘Product Group 2’,
and press the ENT Key.
NOTE: ‘Product Group 2’ is only applicable to SiriusXM and Garmin
6)
Turn the small FMS Knob to scroll through options for each product (ON/
OFF, range settings, etc.).
7)
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the Weather Data Link (XM)
Page with the changed settings.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
Appendix
Appendix
5)
Annun/Alerts
Annun/Alerts
Connext Weather.
Additional Additional
Abnormal
AFCS Features
Features
Operation
1)
83
Hazard Avoidance
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Setting Up and Customizing FIS-B Weather on the Navigation Map
Page
1)
Select the Navigation Map Page.
2)
Press the MENU Key.
3)
With ‘Map Settings’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select the ‘Weather’ Group and press the ENT
Key.
5)
Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
6)
Turn the small FMS Knob to scroll through options for each product (ON/
OFF, range settings).
7)
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the Navigation Map Page with
the changed settings.
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Displaying/Removing the Weather Product Information Box on PFD
Maps
1)
On the PFD, press the Map/HSI Softkey.
2)
Press the Layout Softkey.
3)
Press the WX LGND Softkey to display/remove the weather product
information box.
Annun/Alerts
Annun/Alerts
Viewing Legends for Displayed Weather Products on the Weather Data
Link (FIS-B) Page
1)
Select the Weather Data Link (FIS-B) Page.
2)
Press the Legend Softkey to display the legends for the displayed weather
products.
Appendix
Appendix
Or:
a) Press the MENU Key.
b) Select ‘Weather Legend’ and press the ENT Key.
Index
Index
3)
84
To remove the Legend Window, press the Legend Softkey, the ENT or the
CLR Key, or press the FMS Knob.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
Flight
Flight
Instruments
Instruments
Viewing Legends for Displayed Weather Products on the Navigation
Map Page
2)
Press the Map Opt Softkey.
3)
Press the Legend Softkey (available if one or more FIS-B weather products
are enabled for display).
4)
To remove the Legend Window, press the Legend Softkey, the ENT or the
CLR Key, or press the FMS Knob.
Displaying Weather on the Weather Data Link (FIS-B) Page
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Data Link (FIS-B) Page.
3)
Press the available softkeys to enable/disable the display of the desired
FIS-B Weather product.
Displaying the NEXRAD weather product on the Weather Data Link
(FIS-B) Page
2)
Press the NEXRAD Softkey. Each softkey press cycles though a coverage
option as the softkey name changes (US, RGNL, or US/RGNL.)
Displaying the NEXRAD weather product on the Navigation Map Page
Press the Map Opt Softkey.
2)
Press the NEXRAD Softkey.
3)
To change the type of NEXRAD displayed, press the MENU Key.
4)
With ‘Map Settings’ highlighted, press the ENT Key.
5)
Turn the small FMS Knob to select the ‘Weather’ Group, then press the
ENT Key.
6)
Turn the large FMS Knob to highlight the NEXRAD Data Region field.
7)
Turn the small FMS Knob to highlight ‘CONUS’ (continental United States),
‘RGNL’ (regional), or ‘Combined’, then press the ENT Key. This selection
also affects display of NEXRAD on the PFD Maps.
8)
When finished, press the FMS Knob or press the CLR Key.
Index
Index
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Appendix
Appendix
190-02219-00 Rev. C
Annun/Alerts
Annun/Alerts
1)
Additional Additional
Abnormal
AFCS Features
Features
Operation
Select the Weather Data Link (FIS-B) Page.
AFCS
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Select the Navigation Map Page.
EISEIS
1)
85
Hazard Avoidance
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Display METAR and TAF information on the Airport Information Page
1)
Turn the large FMS Knob to select the WPT Page Group.
2)
Turn the small FMS Knob to select the Airport Information Page.
3)
Press the WX Softkey to display METAR and TAF text.
4)
Press the FMS Knob to enable the cursor, then turn the small FMS Knob as
needed to FMS knob to scroll through the text.
5)
After viewing text, press the FMS Knob to disable the cursor.
Map Panning Information – Weather Data Link (FIS-B) Page
1)
Push in the Joystick to activate the Map Pointer.
2)
Move the Joystick to place the Map Pointer over graphical weather
information. For Cloud Tops, Echo Tops, METAR flags, Storm Cells, and
County Warnings, an information box appears near the Map Pointer. If the
Map Pointer has highlighted a SIGMET, AIRMET, PIREP, or TFR, press the
ENT Key to view additional information such as report text, then press the
ENT Key or the CLR Key to remove the information.
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Note when a METAR flag or airport is highlighted, pressing the ENT Key
shows the WPT - Weather Information Page. The decoded and original
METAR text is available on this page as well as the TAF, if provided. When
finished, press the Go Back Softkey or press the CLR Key to return to the
Weather Data Link (XM) Page.
1)
Select the Navigation Map Page.
2)
Press the MENU Key.
3)
With ‘Map Settings’ highlighted, press the ENT Key
4)
Turn the small FMS Knob to select the ‘VSD’ Group and press the ENT Key
5)
Turn the large FMS Knob to select the Winds On/Off field.
6)
Turn the small FMS Knob to select ‘On’ or ‘Off’.
7)
Press the FMS Knob or CLR Key to return to the Navigation Map Page with
the changed settings.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Enabling/disabling winds aloft data display in the Vertical Situation
Display (VSD)
86
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
Displaying Weather on the Weather Radar Page
1)
Select the Weather Radar Page in the Map Page Group with the FMS Knob.
2)
Press the Mode Softkey.
3)
While on the ground, press the Standby Softkey. A one-minute warm-up
period is initiated (countdown is displayed on the screen). After the warmup is complete, the radar enters the Standby Mode.
a) Press the Weather Softkey. A confirmation window is displayed.
AFCS
b) Turn the small FMS Knob to highlight YES and press the ENT Key to
continue radar activation.
If the aircraft is airborne, select the Weather Softkey. After the warmup is complete, the radar begins transmitting.
Turn the Joystick to select the desired map range.
5)
The horizontal scan is initially displayed. If desired, select the Vertical
Softkey to change to vertical scanning.
Approximate
Precipitation Rate (in/hr.)
Black
< 23 dBZ
< .01
Green
23 dBZ to < 33 dBZ
.01 - 0.1
Yellow
33 dBZ to < 41 dBZ
0.1 - 0.5
Red
41 dBZ and greater
greater than 0.5
Appendix
Appendix
Intensity
Annun/Alerts
Annun/Alerts
Weather Mode Color
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
Precipitation Intensity Levels in Weather Mode (GWX 70)
190-02219-00 Rev. C
Additional Additional
Abnormal
AFCS Features
Features
Operation
Or: 4)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
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.
EISEIS
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 12 feet of the antenna.
Flight
Flight
Instruments
Instruments
AIRBORNE COLOR WEATHER RADAR
87
Hazard Avoidance
Flight
Flight
Instruments
Instruments
Vertically Scan a Storm Cell
NOTE: Vertical scanning of a storm cell should be done with the aircraft
wings level to avoid constant adjustment of the Bearing Line.
EISEIS
1)
While in the Horizontal Scan view, select the BRG Softkey. This places the
cursor in the Bearing field and displays the Bearing Line.
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
If the Bearing Line is not displayed, press the MENU Key and turn the large
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
FMS Knob to select Show Bearing Line. Press the ENT Key.
2)
Press the ENT Key.
3)
Turn the small FMS Knob to place the Bearing Line on the desired storm
cell or other area to be vertically scanned.
4)
Press the Vertical Softkey. A vertical scan of the selected area is now
displayed.
5)
The small FMS Knob may be used to move the scanned bearing line a few
degrees right or left.
6)
Turn the Joystick to adjust the range.
7)
Press the FMS Knob to remove the cursor.
8)
To select a new area to be vertically scanned, press the Horizon Softkey to
return to the Horizontal Scan view and repeat the previous steps.
Annun/Alerts
Annun/Alerts
Adjusting antenna tilt on the Horizontal Scan display
1)
Press the FMS Knob to activate the cursor in the Tilt field.
2)
Turn the small FMS Knob to select the desired antenna tilt angle.
3)
Press the ENT Key.
4)
Press the FMS Knob to remove the cursor.
Adjusting antenna tilt on the Vertical Scan display
Appendix
Appendix
1)
Press the Tilt Softkey to activate the cursor in the Tilt field and display the
Tilt Line.
If the Tilt Line is not displayed, press the MENU Key and turn the large
FMS Knob to select Show Tilt Line. Press the ENT Key.
Index
Index
2)
Turn the small FMS Knob to adjust the antenna tilt angle. The selected tilt
angle is implemented when Horizontal Scan is again selected.
The Joystick can also be used to adjust tilt.
88
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
1)
On the Weather Radar Page, select the Mode Softkey.
2)
Select the ACT ON Softkey. When ACT is enabled, ‘ACT ON’ is annunciated
in upper right corner of the Weather Radar Page. When ACT is disabled,
‘ACT OFF’ is annunciated.
Enabling/disabling manual gain adjustment
2)
Turn the small FMS Knob to adjust the gain for the desirable level. The
gain setting is visible in the Gain field as a movable horizontal bar in
a flashing box. The line pointer is a reference depicting the calibrated
position.
3)
Press the FMS Knob to remove the cursor.
4)
Press the Gain Softkey again to return to the calibrated gain setting.
‘Calibrated’ is displayed in the Gain field.
Annun/Alerts
Annun/Alerts
Press the Gain Softkey to activate the cursor in the Gain field.
Additional Additional
Abnormal
AFCS Features
Features
Operation
1)
AFCS
WARNING: Changing the gain in weather mode causes 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.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Enabling/Disabling Altitude Compensated Tilt (ACT)
EISEIS
The Altitude Compensated Tilt feature of the enables the system to automatically
adjust the antenna beam tilt angle setting based on aircraft altitude changes. For example, if the ACT feature is enabled and the aircraft climbs, the system compensates
by adjusting the tilt downward. As the aircraft descends with ACT enabled, the system
adjusts the antenna tilt upward.
Flight
Flight
Instruments
Instruments
Altitude Compensated Tilt (ACT)
Enabling/disabling Sector Scanning
1)
While in horizontal scan mode, select the BRG Softkey to display the
Bearing Line and place the cursor in the Bearing field. If the Bearing Line is
not displayed, press the MENU Key and turn the large FMS Knob to select
Show Bearing Line.
Appendix
Appendix
2)
Press the ENT Key.
Index
Index
3)
Turn the small FMS Knob to place the Bearing Line in the desired position.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
89
Hazard Avoidance
4)
Turn the large FMS Knob to place the cursor in the Sector Scan field.
5)
Turn the small FMS Knob to highlight the desired scan. Selecting ‘Full’
enables a 90º scan.
6)
If desired, readjust the Bearing Line as discussed previously to change the
center of the Sector Scan.
7)
Select the BRG Softkey again to remove the Bearing Line and cursor. The
bearing reference is reset to 0º.
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
The location of the Bearing Line becomes the center point of the Sector
Scan.
Enabling/disabling antenna stabilization
1)
On the Weather Radar Page, press the Mode Softkey.
2)
Select the STAB Softkey to enable/disable antenna stabilization. The
current stabilization condition is, ‘STAB On’ or ‘STAB Off’ is shown in the
upper right of the Weather Radar Page.
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Enabling/disabling the WATCH feature
1)
On the Weather Radar Page, select the Features Softkey.
2)
Select the Watch Softkey to enable/disable the WATCH feature.
3)
Select the Back Softkey to return to the top-level softkeys.
Annun/Alerts
Annun/Alerts
Enabling/disabling the Weather Alert feature
1)
On the Weather Radar Page, select the Features Softkey.
2)
Select the WX ALRT Softkey to enable/disable the Weathe Alert feature.
3)
Select the Back Softkey to return to the top-level softkeys.
Index
Index
Appendix
Appendix
Operation in Ground Map Mode
90
1)
On the Weather Radar Page, press the Mode Softkey.
2)
Select the Ground Softkey to place the radar in Ground Map mode.
3)
Select the Back Softkey.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to place the cursor in the Tilt field.
6)
Adjust the antenna tilt angle by turning the small FMS Knob to display
ground returns at the desired distance.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
Press the FMS Knob to remove the cursor.
Black
0 dB
> 0 dB to < 9 dB
9 dB to < 18 dB
18 dB to < 27 dB
27 dB and greater
Cyan
Yellow
Magenta
Blue
Ground Target Return Intensity Levels
Enabling/disabling Airborne Weather Radar Overlay on the Navigation
Map Page
1)
Select the Navigation Map Page.
2)
Select the Map Opt Softkey.
3)
Select the WX Radar Softkey.
AFCS
Adjusting the bearing and antenna tilt angle on the Navigation Map
Page
2)
Move the Joystick up to adjust the antenna tilt angle downward, or move
the Joystick up to adjust the antenna tilt angle upward.
3)
Move the Joystick left or right to adjust the bearing line in the desired
direction. A white dashed bearing line is displayed during and momentarily
after adjustment.
Controlling weather radar information on the HSI Map:
2)
On the PFD, press the Map/HSI Softkey.
3)
Press the Wx Radar Softkey to enable/disable the airborne weather radar
HSI Map overlay.
4)
Press the RDR Opt Softkey.
5)
To select a weather radar mode, press the Mode SEL Softkey
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
If necessary, enable the HSI Map on the PFD.
Appendix
Appendix
1)
Annun/Alerts
Annun/Alerts
With the weather radar overlay enabled, push the Joystick twice. The
bearing and tilt legend is displayed.
Additional Additional
Abnormal
AFCS Features
Features
Operation
1)
190-02219-00 Rev. C
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Intensity
EISEIS
Ground Map Mode Color
Flight
Flight
Instruments
Instruments
7)
91
Hazard Avoidance
Flight
Flight
Instruments
Instruments
a) Press a softkey for the desired mode: Off, Standby, Weather, or
Ground. The selected mode only affects the PFD on which the softkey is
selected.
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
b) When finished, press the Back Softkey.
7)
Move the PFD Joystick up to adjust the antenna tilt angle downward, or
move the Joystick down to adjust the antenna tilt angle upward.
8)
To access controls for enabling/disabling the Weather Alert, Antenna
Stabilization, or Altitude Compensated Tilt, press the Features Softkey:
b) Press the STAB Softkey to enable/disable the Antenna
Stabilization feature.
AFCS
c)
Press the ACT Softkey to enable/disable the Altitude
Compensated Tilt feature.
d) When finished, press the Back Softkey twice to return to the toplevel PFD softkeys.
System Status
The radar mode is annunciated in the upper left corner of the Weather Radar Page.
Additional information may be displayed in the center of the Weather Radar Page as a
banner annunciation.
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
Press the Gain- Softkey to decrease the gain setting or press the Gain+
Softkey to increase the gain setting in increments of 0.5 with each press, or
press and hold the softkey for continuous adjustment. A gain setting of 0.0
is equivalent to the calibrated gain setting.
a) Press the WX Alert Softkey to enable/disable the ‘WX Alert Possible severe weather ahead.” Alerts window message.
Appendix
Appendix
Index
Index
6)
Radar Mode
Radar Mode Annunciation Box†
Center Banner
Annunciation
Standby
STANDBY
STANDBY
Weather
WEATHER
None
Ground Mapping
GROUND MAPPING
None
Off
OFF
OFF
Radar Failed*
FAIL
RADAR FAIL
† Annunciations in this column appear in white text in the Weather Radar Mode box on the Navigation Map Page.
92
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
EISEIS
Radar Feature Status
Description
Altitude compensated tilt feature is enabled.
ACT OFF
Altitude compensated tilt feature is disabled.
STAB ON
Antenna stabilization is selected on.
STAB OFF
Antenna stabilization is selected off.
STAB INOP
The radar is not receiving pitch and roll information. The antenna
stabilization feature is inoperative.
If the unit fails, an annunciation as to the cause of the failure is shown as a banner
in the center of the Weather Radar Page.
RDR FAULT
RADAR FAIL
The radar configuration is invalid. The radar should be
serviced.
The radar unit is reporting a fault. The radar should be
serviced.
Additional Additional
Abnormal
AFCS Features
Features
Operation
BAD CONFIG
Description
AFCS
Weather Radar Page Center
Banner Annunciation
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
ACT ON
Flight
Flight
Instruments
Instruments
The system displays the status of the radar antenna stabilization feature in the upper right corner of the Weather Radar Page. For the GWX 70, the status of the Altitude
Compensated Tilt feature also appears in the upper right corner of the Weather Radar
Page.
The system is not receiving valid data from the radar
unit. The system should be serviced.
Appendix
Appendix
WARNING: Do not rely solely upon the display of traffic information for collision avoidance maneuvering. The traffic display does not provide collision
avoidance resolution advisories and does not under any circumstances or
conditions relieve the pilot’s responsibility to see and avoid other aircraft.
Annun/Alerts
Annun/Alerts
TRAFFIC SYSTEMS
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
93
Hazard Avoidance
Flight
Flight
Instruments
Instruments
Traffic Information Service (TIS)
NOTE: Mode S TIS is disabled if another traffic system such as TAS or Automatic Dependent Surveillance-Broadcast (ADS-B) is installed.
Traffic Information Service (TIS) is designed to help in detection and avoidance of
other aircraft. TIS uses the Mode S transponder for the traffic data link. TIS receives
traffic information from ground stations, and is updated every five seconds. The system displays TIS traffic with the symbology shown in the following table.
TIS Symbol
Description
Non-Threat Traffic
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
NOTE: TIS is available only when the aircraft is within the service volume of
a TIS-capable terminal radar site. Aircraft without an operating transponder
are invisible to both Traffic Advisory Systems (TAS), Traffic Alert and Collision
Avoidance Systems (TCAS) and TIS. Aircraft without altitude reporting capability are shown without altitude separation data or climb descent indication.
Additional Additional
Abnormal
Features
Operation
Features AFCS
Traffic Advisory (TA)
Traffic Advisory Off Scale
TIS Traffic Symbols
Annun/Alerts
Annun/Alerts
Enabling/disabling traffic overlays (MFD navigation maps)
1)
Select the Map Opt Softkey.
2)
Select the Traffic Softkey. Traffic is now displayed on the navigation map.
Index
Index
Appendix
Appendix
Enabling/disabling traffic information on the PFD Inset Map or HSI
Map
94
1)
On the PFD, press the Map/HSI Softkey.
2)
Press the Traffic Softkey to enable/disable the display traffic information on
the Inset Map or HSI Map.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
2)
Press the MENU Key.
3)
With ‘Map Setup’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select the ‘Traffic’ Group and press the ENT
Key.
5)
Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Select the Navigation Map Page.
EISEIS
1)
Flight
Flight
Instruments
Instruments
Customizing traffic display on the Navigation Map Page
• Traffic – Turns the display of traffic data on or off
• Traffic Mode – Selects the traffic mode for display; select from:
- All Traffic - Displays all traffic
- TA Only - Displays Traffic Alerts only
• Traffic Symbols – Selects the maximum range at which traffic
symbols are shown
Turn the small FMS Knob to scroll through options for each product (On/Off,
range settings, etc.).
7)
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the Navigation Map Page with
the changed settings.
Displaying traffic on the Traffic Map Page
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Traffic Map Page.
3)
Confirm TIS is in Operating Mode:
Annun/Alerts
Annun/Alerts
1)
a) Press the TIS OPER Softkey to begin displaying traffic.
Appendix
Appendix
Or:
a) Press the MENU Key.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
95
Index
Index
b) Select ‘Operate Mode’ (shown if TIS is in Standby Mode) and press the
ENT Key.
190-02219-00 Rev. C
Additional Additional
Abnormal
AFCS Features
Features
Operation
6)
AFCS
• Traffic Labels – Selects the maximum range at which traffic labels
are shown (with the option to turn off)
Hazard Avoidance
EISEIS
Flight
Flight
Instruments
Instruments
Switching between TIS modes
1)
Select the Traffic Map Page.
2)
Press the Standby or Operate Softkey to switch between modes. The mode
is displayed in the upper right corner of the Traffic Map Page.
TIS Alerts
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
When the number of TAs on the Traffic Map Page increases from one scan
to the next, the following occur:
• A single “Traffic” voice alert is generated.
• A ‘TRAFFIC’ Annunciation appears to the right of the airspeed tape,
flashes for five seconds, and remains displayed until no TAs are detected
in the area.
• The PFD Inset Map or HSI Map is automatically displayed with traffic.
AFCS
A “TIS Not Available” (TNA) voice alert is generated when the TIS service
becomes unavailable or is out of range.
Additional Additional
Abnormal
Features
Operation
Features AFCS
Muting the “TIS Not Available” voice alert
1)
Select the Traffic Map Page.
2)
Press the TNA Mute Softkey. The status is displayed in the upper left corner
of the Traffic Map Page.
Or:
a) Press the MENU Key.
Annun/Alerts
Annun/Alerts
b) Select ‘‘’Not Available” Mute On’ (shown if TNA muting is currently off)
and press the ENT Key.
Traffic Advisory System (TAS)
Index
Index
Appendix
Appendix
WARNING: Do not rely solely upon the display of traffic information for
collision avoidance maneuvering. The traffic display does not provide collision avoidance resolution advisories and does not under any circumstances
or conditions relieve the pilot’s responsibility to see and avoid other aircraft.
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Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
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Hazard Avoidance
TAS Symbol
Description
Annun/Alerts
Annun/Alerts
Non-Threat Traffic
Additional Additional
Abnormal
AFCS Features
Features
Operation
If a Garmin GTX 33 ES transponder is installed with this TAS, the system uses the
following symbols to represent traffic.
AFCS
NOTE: If Garmin GTX 345R transponder is installed, refer to the Automatic
Dependent Surveillance-Broadcast (ADS-B) Traffic discussion for more information about ADS-B traffic displays.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
NOTE: Pilots should be aware of traffic system limitations. Traffic systems
require transponders of other aircraft to respond to system interrogations.
If the transponders do not respond to interrogations due to phenomena
such as antenna shading or marginal transponder performance, traffic may
be displayed intermittently, or not at all. Aircraft without altitude reporting
capability are shown without altitude separation data or climb descent indication. Pilots should remain vigilant for traffic at all times.
EISEIS
NOTE: ADS-B traffic symbols are only displayed if the equipment installed
in the aircraft is capable of receiving ADS-In traffic reports.
Flight
Flight
Instruments
Instruments
WARNING: Do not rely solely upon the display of traffic information to
accurately depict all of the traffic within range of the aircraft. Due to lack
of equipment, poor signal reception, and/or inaccurate information from
aircraft or ground stations, traffic may be present that is not represented on
the display. .
Proximity Advisory (PA)
Appendix
Appendix
Traffic Advisory (TA)
Traffic Advisory Off Scale
Index
Index
TAS Symbol Description with GTX 33 ES/335 Transponder
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
97
If a Garmin GTX 345 transponder is installed with the TAS, the symbols in the following table depict traffic, and include Automatic Dependent Surveillance-Broadcast
(ADS-B) information. Refer to the ADS-B Traffic discussion later in this section for
more information.
Symbol
Description
Traffic Advisory with ADS-B directional information. Arrow points in the direction of the
intruder aircraft track.
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Hazard Avoidance
Traffic Advisory without directional information.
Traffic Advisory with ADS-B directional information is beyond the selected display range.
Displayed at outer range ring at proper bearing. Arrow points in the direction of the intruder
aircraft track.
Traffic Advisory out of the selected display range without directional information. Displayed
at outer range ring at proper bearing.
AFCS
Proximity Advisory with ADS-B directional information. Arrow points in the direction of the
aircraft track.
Additional Additional
Abnormal
Features
Operation
Features AFCS
Proximity Advisory without directional information.
Other Non-Threat traffic with ADS-B directional information. Arrow points in the direction of
the intruder aircraft track.
Other Non-Threat traffic without directional information.
Annun/Alerts
Annun/Alerts
Traffic located on the ground with ADS-B directional information. Arrow points in the
direction of the aircraft track. Ground traffic is only displayed when ADS-B is in Surface
(SURF) Mode or own aircraft is on the ground.
Appendix
Appendix
Ground traffic without ADS-B directional information. Ground traffic is only displayed when
ADS-B is in Surface (SURF) Mode or own aircraft is on the ground.
Non-aircraft ground traffic with ADS-B directional information. Pointed end indicates
direction of travel. Ground traffic is only displayed when ADS-B is in Surface (SURF) Mode or
own aircraft is on the ground.
Index
Index
Non-aircraft ground traffic without ADS-B directional information. Ground traffic is only
displayed when ADS-B is in Surface (SURF) Mode or own aircraft is on the ground.
ADS-B Traffic Symbology with GTX 345R Transponder
98
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
Turn the Joystick to set the range to 2/6 nm to allow for full test pattern to
be displayed during test.
4)
Press the Standby or TAS STBY Softkey.
5)
Press the Test Softkey. 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.
NOTE: Traffic surveillance is not available during the system test. Use
Appendix
Appendix
3)
Annun/Alerts
Annun/Alerts
Turn the small FMS Knob to select the Traffic Map Page.
Additional Additional
Abnormal
AFCS Features
Features
Operation
2)
AFCS
Turn the large FMS Knob to select the Map Page Group.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
1)
EISEIS
Testing the traffic system
Flight
Flight
Instruments
Instruments
TAS Alerts
When the TAS detects a new TA, the following occur:
• The system issues a single “Traffic!” voice alert, followed by additional voice
information about the bearing, relative altitude, and approximate distance from
the intruder that triggered the TA. For example, the announcement “Traffic! 12
o’clock, high, four miles,” would indicate the traffic is in front of own aircraft,
above own altitude, and approximately four nautical miles away.
• A TRAFFIC Annunciation appears at the right of the airspeed on the PFD, flashes
for five seconds, and remains displayed until no TAs are detected in the area.
• A PFD map is automatically displayed with TA traffic.
If the bearing of TA traffic cannot be determined, a yellow text banner will be displayed in the center of the Traffic Map Page and in the lower-left of the PFD inset map
instead of a TA symbol. The text will indicate “TA” followed by the distance, relative
altitude, and vertical trend arrow for the TA traffic, if known.
The traffic system provides a system test mode to verify the TAS is operating normally. The test takes about ten seconds to complete. When the system test is initiated,
a test pattern of traffic symbols appears on the Traffic Map Page. If system test passes, the system announces, “TAS System Test Passed” or “TAS System Test Failed.”
When the system test is complete, the traffic system enters Standby Mode.
caution when performing a system test during flight.
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
99
Hazard Avoidance
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
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 Traffic Map Page.
3)
Press the TAS OPER Softkey to begin displaying TAS traffic. ‘OPERATING’
is displayed in the Traffic Mode field.
4)
Press the ADS-B Softkey to begin display ADS-B traffic.
5)
Press the ALT Mode Softkey to change the altitude volume. Select the
desired altitude volume by pressing the Above, Normal, Below, or
UNREST (unrestricted) Softkey. The selection is displayed in the Altitude
Mode field. Press the Back Softkey to return to the previous level softkeys.
6)
Press the Motion Softkey.
7)
Press one of the following softkeys:
Absolute: Displays the motion vector pointing in the absolute direction.
Relative: Displays the motion vector relative to own aircraft
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Off: Disables the display of the motion vector.
8)
Press the Back Softkey to return to the previous level softkeys.
8)
Press the TAS STBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
9)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Annun/Alerts
Annun/Alerts
Enabling/disabling the display of Flight ID for traffic
1)
Select the Traffic Map Page.
2)
Select the FLT ID Softkey to enable/disable the display of Flight IDs for
displayed traffic.
1)
Select the Map Opt Softkey.
2)
Select the Traffic Softkey. Traffic is now displayed on the map.
Index
Index
Appendix
Appendix
Enabling/disabling traffic information (MFD maps other than the
Traffic Map Page)
100
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
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Hazard Avoidance
Flight
Flight
Instruments
Instruments
Customizing the traffic display on the Navigation Map Page
2)
Press the MENU Key.
3)
With ‘Map Settings’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select the Traffic Group and press the ENT Key.
5)
Turn the large FMS Knob or press the ENT Key to scroll through the
selections.
• Traffic – Turns the display of traffic data on or off
• Traffic Mode – Selects the traffic mode for display; select from:
- All Traffic - Displays all traffic
- TA/PA - Displays only Traffic Advisories and Proximity Advisories
- TA Only - Displays Traffic Advisories only
• Traffic Symbols – Selects the maximum range at which traffic
symbols are shown
Turn the small FMS Knob to scroll through options (On/Off, range settings,
etc.).
7)
Press the ENT Key to select an option.
8)
Press the FMS Knob or CLR Key to return to the Navigation Map Page.
Showing the HSI Traffic Map
Press the Map/HSI Softkey.
2)
Press the Layout Softkey.
3)
Press the HSI Trfc Softkey.
Annun/Alerts
Annun/Alerts
1)
Appendix
Appendix
Traffic information can also be overlaid on PFD navigation maps.
Enabling/disabling traffic overlay on PFD navigation maps
With the Inset Map or HSI Map displayed, press the Map/HSI Softkey on
the PFD.
2)
Press the Traffic Softkey to enable/disable the display traffic information.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
101
Index
Index
1)
190-02219-00 Rev. C
Additional Additional
Abnormal
AFCS Features
Features
Operation
6)
AFCS
• Traffic Labels – Selects the maximum range at which traffic
labels (relative altitude, vertical trend) are shown with the option to
turn off
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Select the Navigation Map Page.
EISEIS
1)
Flight
Flight
Instruments
Instruments
Hazard Avoidance
ADS-B Traffic
The symbols used to display ADS-B traffic are shown in the following table.
EISEIS
Symbol
Description
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
Traffic Advisory with directional information. Points in the direction of the intruder aircraft
track.
Traffic Advisory without directional information.
Traffic Advisory out of the selected display range with directional information. Displayed at
outer range ring at proper bearing.
Traffic Advisory out of the selected display range without directional information.
Displayed at outer range ring at proper bearing.
Proximity Advisory with directional information. Points in the direction of the aircraft track.
AFCS
Proximity Advisory without directional information.
Additional Additional
Abnormal
Features
Operation
Features AFCS
Other Non-Threat traffic with directional information. Points in the direction of the
intruder aircraft track.
Other Non-Threat traffic without directional information.
Annun/Alerts
Annun/Alerts
Traffic located on the ground with directional information. Points in the direction of the
aircraft track. Ground traffic is only displayed when ADS-B is in Surface (SURF) Mode or
own aircraft is on the ground.
Ground traffic without directional information. Ground traffic is only displayed when
ADS-B is in Surface (SURF) Mode or own aircraft is on the ground.
Appendix
Appendix
Non-aircraft ground traffic with ADS-B directional information. Pointed end indicates
direction of travel. Ground traffic is only displayed when ADS-B is in Surface (SURF) Mode
or own aircraft is on the ground.
Non-aircraft ground traffic without ADS-B directional information. Ground traffic is only
displayed when ADS-B is in Surface (SURF) Mode or own aircraft is on the ground.
Index
Index
ADS-B Traffic Symbology
102
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
1)
Select the Traffic Map Page.
2)
Select the ADS-B Softkey.
Flight
Flight
Instruments
Instruments
Enabling/disabling the display of ADS-B traffic
EISEIS
Testing the display of ADS-B traffic
Select the Traffic Map Page.
2)
If necessary, turn the Joystick to select a map range of 2 and 6 nm to
ensure full test pattern display.
3)
Ensure the ADS-B Softkey is disabled.
4)
If the optional TAS is installed, ensure the TAS STBY Softkey is enabled.
5)
Press the Test Softkey. A test pattern of traffic symbols appears during the
test, and a ‘TRAFFIC’ annunciation appears on the PFDs. At the conclusion
of the test, the system issues the voice alert “Traffic System Test”. If the
test pattern is displayed and the voice alert is heard, the system has passed
the test.
Changing the altitude range
2)
Select one of the following softkeys:
•
Normal: Displays Other Non-Threat and proximity traffic from 2700
feet above the aircraft to 2700 feet below the aircraft. Typically used
during enroute phase of flight.
•
Below: Displays Other Non-Threat and proximity traffic from 2700 feet
above the aircraft to 9900 feet below the aircraft. Typically used during
descent phase of flight.
•
UNREST (unrestricted): All traffic is displayed from 9900 feet above
and 9900 feet below the aircraft.
Appendix
Appendix
Above: Displays Other Non-Threat and proximity traffic from 9900 feet
above the aircraft to 2700 feet below the aircraft. Typically used during
climb phase of flight.
To return to the Traffic Map Page, select the Back Softkey.
Select the Traffic Map Page.
2)
Select the Motion Softkey.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
Enabling/disabling the Motion Vector display
1)
Annun/Alerts
Annun/Alerts
3)
•
Additional Additional
Abnormal
AFCS Features
Features
Operation
On the Traffic Map Page, select the ALT Mode Softkey.
AFCS
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
1)
103
Hazard Avoidance
EISEIS
Flight
Flight
Instruments
Instruments
3)
Select one of the following softkeys:
•
Absolute: Displays the motion vector pointing in the absolute
direction.
•
Relative: Displays the motion vector relative to own aircraft
•
Off: Disables the display of the motion vector.
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
Adjusting the duration for the Motion Vector projected time
1)
Select the Traffic Map Page.
2)
Select the Motion Softkey.
3)
Select the Duration Softkey.
4)
Select a softkey for the desired duration (30 SEC, 1 MIN, 2 MIN, 5 MIN).
5)
When finished, select the Back Softkey to return to the Traffic Map Page.
Showing additional traffic information
Select the Traffic Map Page.
2)
Press the FMS Knob. A cyan border appears on the first selected traffic
symbol. Additional information appears in a window in the lower-left
corner of the Traffic Map Page.
3)
To select a different aircraft symbol, turn the FMS Knob to move the cyan
border until another symol is selected.
4)
When finished, press the FMS Knob again to disable the traffic selection.
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
1)
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Changing the display range on the Traffic Map Page
104
1)
Turn the Joystick.
2)
The following range options are available:
•
500 feet
•
500 feet and 1000 feet
•
1000 feet and 2000 feet
•
2000 feet and 1 nm
•
1 and 2 nm
•
2 and 6 nm
•
6 and 12 nm
•
12 and 24 nm
•
24 and 40 nm
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Hazard Avoidance
1)
Turn the large FMS Knob to select the Aux Page Group.
2)
Turn the small FMS Knob to select the Aux - ADS-B Status Page.
Available to Run
Traffic application is not currently active, but application is ready to run when condition(s) determine the application should be active. Required
input data is available, and it meets performance
requirements.
Not Available
Traffic application is not available. Required input
data is available, but it does not meet performance requirements.
Fault
Traffic application is not available. Required input
data is not available or the application has failed.
Not Configured
Traffic application is not available, because it has
not been configured. If this annunciation persists,
the system should be serviced.
Traffic application status is invalid or unknown.
Available
The system is receiving the ADS-R coverage from
an FAA ground station.
Not Available
The system is not receiving the ADS-R coverage
from an FAA ground station.
---------------
ADS-R coverage is invalid or unknown.
External #1
The system is using the #1 GPS receiver for the
GPS position source.
External #2
The system is using the #2 GPS receiver for the
GPS position source.
Ground Uplink Status: Last
Uplink
The GPS source is invalid or unknown.
Aux-ADS-B Status Page Messages for ADS-B Traffic
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
105
Index
Index
Number of minutes, Displays the number of minutes since the last upor ‘------’
link from a ground station occurred. If no uplink
has been received, or the status is invalid, dashes
appear instead of the number of minutes.
Appendix
Appendix
---------
Annun/Alerts
Annun/Alerts
----------------
Additional Additional
Abnormal
AFCS Features
Features
Operation
Traffic application is currently on. Required
input data is available, and it meets performance
requirements.
AFCS
GPS Status: GPS Source
Description
On
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
TIS-B/ADS-R Coverage
EISEIS
ADS-B Status Page Item Status Message
Traffic Application Status:
Airborne (AIRB), Surface
(SURF), Airborne Alerts (CSA)
Flight
Flight
Instruments
Instruments
Viewing ADS-B Traffic Status
TERRAIN DISPLAYS
WARNING: Do not use terrain avoidance displays as the sole source of information for maintaining separation from terrain and obstacles. Garmin obtains
terrain and obstacle data from third party sources and cannot independently
verify the accuracy of the information.
EISEIS
Flight
Flight
Instruments
Instruments
Hazard Avoidance
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
NOTE: Terrain data is not displayed when the aircraft is outside of the installed
terrain database coverage area.
NOTE: Terrain and obstacle alerting is not available north of 89º North latitude
and south of 89º South latitude. This is due to limitations present within the
Terrain database and the system’s ability to process the data representing
the affected areas.
NOTE: Terrain and obstacle alerting requires the Terrain-SVT or TAWS-B option.
No terrain or obstacle alerting occurs for the Terrain Proximity feature.
Relative Terrain Symbology
The terrain system uses colors and symbols to represent terrain and obstacles (with
heights greater than 200 feet above ground level, AGL) present in the databases relative to aircraft altitude. The system dynamically adjusts these colors as the aircraft
altitude changes, and after takeoff and landing.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
One of the following terrain systems is installed on this aircraft:
• Terrain Proximity
• Terrain-SVT (included with the Garmin SVT option when the Terrain Awareness and Warning System Class-B (TAWS-B) is not installed; refer to the Flight
Instruments section for more information about Garmin SVT.)
• TAWS-B (optional)
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Hazard Avoidance
Flight
Flight
Instruments
Instruments
On-Ground Legend
In-Air Legend
EISEIS
Displaying terrain and obstacle information (MFD maps other than the
terrain page)
Press the Map Opt Softkey (for the PFD Inset Map, press the Map/HSI
Softkey).
2)
Press the TER Softkey until REL is shown to display terrain and obstacle
data.
AFCS
1)
Select the Navigation Map Page.
2)
Press the MENU Key.
3)
With ‘Map Settings’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key.
5)
Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
• Obstacle Data – Turns the display of obstacles on or off. The distance field selects
the maximum map range to display obstacle symbols before they are
removed from the map.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
Turn the small FMS Knob to scroll through options for each product (ON/
OFF, range settings).
Appendix
Appendix
• Terrain Display – Selects terrain ‘Off’ for no terrain, ‘Topo’ for topographic
information, or relative terrain ‘Rel’. The distance field selects the
maximum map range to display terrain information before it is removed
from the map.
Annun/Alerts
Annun/Alerts
1)
Additional Additional
Abnormal
AFCS Features
Features
Operation
Customizing terrain and obstacle display on the Navigation Map Page
6)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Relative Terrain Legend
107
Hazard Avoidance
Flight
Flight
Instruments
Instruments
7)
8)
Press the ENT Key to select an option.
Press the FMS Knob or CLR Key to return to the Navigation Map Page with
the changed settings.
Displaying the terrain page
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Map - Terrain Proximity/Terrain-SVT/
TAWS-B Page.
Showing/hiding aviation information on the terrain page
1)
Press the MENU Key.
2)
Select ‘Show Aviation Data’ or ‘Hide Aviation Data’ (choice dependent on
current state) and press the ENT Key.
Vertical Situation Display (VSD) Terrain
The system offers a Vertical Situation Display (VSD), which includes a
profile of terrain and obstacles in an inset window on the bottom of the
Navigation Map Page.
Enabling/Disabling the Vertical Situation Display (VSD)
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Terrain Page
1)
Select the Navigation Map Page.
2)
Select the Map Opt Softkey.
3)
Select the Inset Softkey.
4)
Select the VSD Softkey to enable or disable the VSD.
Flight Phase
Total VSD Width
Approach
0.6 nm
Departure
0.6 nm
Terminal
2.0 nm
Enroute
4.0 nm
Oceanic
4.0 nm
VSD Terrain Width Varies with Phase of Flight
108
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
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Hazard Avoidance
Flight
Flight
Instruments
Instruments
Selecting a VSD Mode
Select the Navigation Map Page.
2)
Select the Inset Softkey.
3)
Select the VSD Softkey displaying the VSD mode in cyan. Each press of the
softkey cycles through a mode selection: FPL (flight plan), TRK (track), or
Auto.
1)
Select the Navigation Map Page.
2)
Press the MENU Key.
3)
With ‘Map Settings’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select the ‘VSD’ Group and press the ENT Key.
5)
Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
Turn the small FMS Knob to scroll through options (On/Off range settings).
7)
8)
Press the ENT Key to select an option.
Press the FMS Knob or CLR Key to return to the Navigation Map Page with
the changed settings.
Terrain-SVT and TAWS-B Alerting Displays
1)
Select the Terrain Page.
2)
Select the Inhibit Softkey.
Appendix
Appendix
Inhibiting Terrain-SVT or TAWS-B FLTA and PDA Alerting
Annun/Alerts
Annun/Alerts
Alerts are issued when flight conditions meet parameters that are set within Terrain-SVT or TAWS-B software algorithms. Terrain alerts typically employ a CAUTION
or a WARNING alert severity level, or both. When an alert is issued, visual annunciations are displayed and voice alerts are simultaneously issued.
Additional Additional
Abnormal
AFCS Features
Features
Operation
6)
AFCS
• TRK Mode BNDRY – Enables/disables the display of the Track Mode
Boundary and sets maximum range at which Track Mode Boundary is
shown.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Customizing the Track Mode Boundary display on the Navigation Map
Page
EISEIS
1)
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
109
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Hazard Avoidance
Blank Page
110
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
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AFCS
NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.
Control Pressed
Modes Selected
Lateral
Vertical
PIT
AP Key
Roll Hold (default)
ROL
Pitch Hold (default)
PIT
CWS Button
Roll Hold (default)
ROL
Pitch Hold (default)
PIT
GA Button
Takeoff (on ground)
Go Around (in air)
TO
GA
Takeoff (on ground)
Go Around (in air)
TO
GA
ALT Key
Roll Hold (default)
ROL
Altitude Hold
ALT
VS Key
Roll Hold (default)
ROL
Vertical Speed
VS
VNV Key
Roll Hold (default)
ROL
Vertical Path Tracking*
VPTH
NAV Key
Navigation**
FMS
VOR
LOC
Pitch Hold (default)
PIT
BC Key
Backcourse***
BC
Pitch Hold (default)
PIT
APR Key
Approach**
FMS
VOR
LOC
Pitch Hold (default)
PIT
HDG Key
Heading Select
HDG
Pitch Hold (default)
PIT
LVL Button
Level
LVL
Level
LVL
Index
Index
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
**The selected navigation receiver must have a valid VOR or LOC signal or active FMS course before NAV
or APR Key press activates flight director.
***The selected navigation receiver must have a valid LOC signal before BC Key press activates flight director.
190-02219-00 Rev. C
111
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Appendix
Appendix
Pitch Hold (default)
Annun/Alerts
Annun/Alerts
ROL
Additional Additional
Abnormal
AFCS Features
Features
Operation
Roll Hold (default)
AFCS
FD Key
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
NOTE: If Underspeed Protection (USP) is installed, AP does not disconnect
upon selection of GA Button.
EISEIS
ACTIVATING THE FLIGHT DIRECTOR
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. The flight director
may be turned off and the Command Bars removed from the displays by pressing the
FD Key again. The FD Key is disabled when the autopilot is engaged.
Flight
Flight
Instruments
Instruments
AUTOMATIC FLIGHT CONTROL SYSTEM
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
AFCS
VERTICAL MODES
Vertical Mode
Description
Control Annunciation
Pitch Hold
Holds the current aircraft pitch attitude;
may be used to climb/descend to the
Selected Altitude
Selected Altitude
Capture
Captures the Selected Altitude
Altitude Hold
Holds the current Altitude Reference
ALT Key
ALT
nnnnn ft
Vertical Speed
Maintains the current aircraft vertical
speed; may be used to climb/descend to
the Selected Altitude
VS Key
VS
nnnn fpm
FLC
nnn kt
FLC
M .nnn
Flight Level Change,
Maintains the current aircraft airspeed (in
IAS Hold
IAS or Mach) while the aircraft is climbing/
Flight Level Change, descending to the Selected Altitude
Mach Hold
(default)
PIT
*
ALTS
FLC Key
* ALTS armed automatically when PIT, VS, FLC, TO, or GA active, and under VPTH when Selected
Altitude is to be captured instead of VNV Target Altitude
LATERAL MODES
Lateral Mode
Description
Control
Annunciation
Roll Hold
Holds the current aircraft roll attitude
or rolls the wings level, depending on
the commanded bank angle
(default)
ROL
Low Bank
Limits the maximum commanded roll
angle
BANK
Key
*
Heading Select**
Captures and tracks the Selected
HDG Key
Heading
Navigation, GPS Arm/
Capture/Track**
Navigation, VOR Enroute
Arm/Capture/Track**
Navigation, LOC Arm/
Capture/Track
(No Glideslope)
HDG
FMS
Captures and tracks the selected
NAV Key
navigation source (GPS, VOR, LOC)
VOR
LOC
* 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.
** The Heading, Navigation GPS and Navigation VOR mode maximum roll command limit will be
limited to the Low Bank mode value if it is engaged.
112
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
AFCS
Mode
Control
Annunciation
Vertical Path Tracking
Captures and tracks descent legs
of an active vertical profile
VNV Key
VPTH
VNV Target Altitude Capture
Captures the Vertical Navigation
(VNV) Target Altitude
*
ALTV
Glidepath
Captures and tracks the SBAS
glidepath on approach
Glideslope
Captures and tracks the ILS
glideslope on approach
Backcourse Arm/Capture/
Track
Captures and tracks a localizer
signal for backcourse approaches
EISEIS
Description
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
GP
APR Key
GS
BC Key
Approach, FMS Arm/Capture/
Track
BC
FMS
VAPP
APR Key
AFCS
LOC
TO
Go Around
Disengages the autopilot and
commands a constant pitch angle GA Button
and wings level in the air
GA
Annun/Alerts
Annun/Alerts
Takeoff
Disengages the autopilot and
commands a constant pitch angle
GA Button
and wings level on the ground in
preparation for takeoff
Additional Additional
Abnormal
AFCS Features
Features
Operation
Approach, VOR Arm/Capture/
Captures and tracks the selected
Track
navigation source (FMS, VOR,
Approach, ILS Arm/Capture/ LOC)
Track
(Glideslope Mode
automatically armed)
Flight
Flight
Instruments
Instruments
COMBINATION MODES (VNV, APR, NAV, BC, GA)
Autopilot
engages
and
commands pitch angle necessary LVL Button
LVL
to establish zero vertical fpm
* ALTV is armed automatically under VPTH when VNV Target Altitude is to be captured instead of
Selected Altitude.
Level
Appendix
Appendix
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
113
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
AFCS
Blank Page
114
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Additional Features
Flight
Flight
Instruments
Instruments
ADDITIONAL FEATURES
TERMINAL PROCEDURE CHARTS
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
115
Index
Index
FliteCharts® resemble the paper version of AeroNav Services terminal procedures
charts. The charts are displayed with high-resolution and in color for applicable
charts. The MFD depiction shows the aircraft position on the moving map in the plan
view of most approach charts and on airport diagrams.
Appendix
Appendix
FliteCharts®
Annun/Alerts
Annun/Alerts
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 Additional
Abnormal
AFCS Features
Features
Operation
ChartView
AFCS
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 Detail Softkey (declutter) once removes the taxiway markings and
airport identification labels. Pressing the Detail Softkey twice removes VOR station
ID, the VOR symbol, and intersection names if within the airport plan view. Pressing
the Detail Softkey a third time removes the airport runway layout, unless the airport
in view is part of an active route structure. Pressing the Detail Softkey again cycles
back to the original map detail.
The SafeTaxi database contains detailed airport diagrams for selected airports.
These diagrams provide the pilot with situational awareness by displaying the aircraft
position in relation to taxiways, ramps, runways, terminals, and services. This
information should not be used by the pilot as the basis for maneuvering the aircraft
on the ground. This database is updated on a 56-day cycle.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
SafeTaxi®
EISEIS
NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may
be necessary to carry another source of charts on-board the aircraft.
Flight
Flight
Instruments
Instruments
Additional Features
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.
While viewing the ‘MAP-Navigation Map’ Page, NRST-Nearest Airport’
Page, or ‘FPL-Flight Plan’ Page, select the Charts Softkey.
Or:
Additional Additional
Abnormal
Features
Operation
Features AFCS
Press the MENU Key to display the ‘Page Menu.’
2)
Turn the large FMS Knob to scroll through the ‘Options’ Menu to Charts.
3)
Press the ENT Key to display the chart.
1)
While viewing the Airport Taxi Diagram, select the Full SCN Softkey to
display the information windows (Airport, Info).
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the Airport, Info, Runways, or
Frequencies Box.
4)
Turn the small FMS Knob to select the Info Box choices. If multiple choices
are available, scroll to the desired choice with the large FMS Knob and
press the ENT Key to complete the selection.
5)
Press the FMS Knob again to deactivate the cursor.
Changing split view orientation
While in split view mode, pressing and holding Joystick for several seconds
toggles between narrow (vertical) split screens and wide (horizontal) split
screens.
Selecting full screen On or Off
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
1)
Selecting Additional Information:
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Selecting Terminal Procedures Charts:
1)
While viewing a terminal chart press the MENU Key to display the ‘Page
Menu’ Options.
2)
Turn the large FMS Knob to highlight the ‘Full Screen Off’ or ‘Full Screen
On’ Menu Option and press the ENT Key to toggle full screen off or on
respectively.
Or:
116
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Additional Features
While viewing a terminal chart press the CHRT Opt Softkey to display
additional chart view options.
2)
Press Full SCN Softkey to toggle full screen on or off for the selected chart.
EISEIS
Selecting Day, Night, or Automatic View:
While viewing a terminal chart press the MENU Key to display the ‘Page
Menu’ Options.
2)
Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and
press the ENT Key.
3)
Turn the large FMS Knob to move to the ‘Color Scheme’ Option.
4)
Turn the small FMS Knob to choose between ‘Day, Auto, and Night’ Options.
5)
If Auto Mode is selected, turn the large FMS Knob to select the percentage
field. Use the small FMS Knob to change the percentage value. The
percentage value is the day/night crossover point based on the percentage
of backlighting intensity. For example, if the value is set to 15%, the day/
night display changes when the display backlight reaches 15% of full
brightness.
AIRPORT DIRECTORY
1)
Appendix
Appendix
Selecting the Airport Directory Page:
Annun/Alerts
Annun/Alerts
The Aircraft Owners and Pilots Association (AOPA) or AC-U-KWIK Airport
Directory database offers detailed information regarding services, hours of operation,
lodging options, and more for various airports. This information is viewed on the
WPT-Airport Information Page.
The Airport Directory databases are revised every 56 days. The Airport Directory is
always available for use after the expiration date. Check fly.garmin.com for the current
database.
Additional Additional
Abnormal
AFCS Features
Features
Operation
Press the FMS Knob when finished to remove the ‘Chart Setup’ Menu.
AFCS
The display must be changed in order for the new setting to become active.
This may be accomplished by selecting another page or changing the
display range.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
1)
6)
Flight
Flight
Instruments
Instruments
1)
Turn the large FMS Knob to select the ‘WPT’ page group.
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
117
Turn the small FMS Knob to select the Airport Information Page. Initially,
information for the airport closest to the aircraft’s present position is
displayed.
3)
If necessary, select the Info softkey until Info 2 is displayed.
The XM Radio Page provides information and control of the audio entertainment
features of the SiriusXM™ Satellite Radio.
Selecting the XM Radio Page
1)
Turn the large FMS Knob to select the Auxiliary Page Group.
2)
Turn the small FMS Knob to select the displayed ‘Aux - XM Information’
Page.
3)
Select the Radio Softkey to show the ‘XM Radio’ Page where audio
entertainment is controlled.
Active Channel and Channel List
The Active Channel Box on the XM Radio Page displays the currently selected
channel. The Channels List Box of the XM Radio Page shows a list of the available
channels for the selected category.
Selecting a channel from the channel list
1)
While on the ‘AUX-XM Radio’ Page, select the Channel Softkey.
2)
Select the CH + Softkey to go up through the list in the ‘Channels’ Box, or
move down the list with the CH – Softkey.
Or:
1)
Press the FMS Knob to highlight the channel list and turn the large FMS
Knob to scroll through the channels.
2)
Press the ENT Key to activate the selected channel.
Selecting a channel directly:
Index
Index
Appendix
Appendix
2)
SIRIUSXM™ RADIO ENTERTAINMENT
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Additional Features
118
1)
While on the ‘AUX-XM Radio’ Page, select the Channel Softkey.
2)
Select the Direct CH Softkey. The channel number in the ‘Active Channel’
Box is highlighted.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Additional Features
Select the numbered softkeys located on the bottom of the display to
directly select the desired channel number.
4)
Press the ENT Key to activate the selected channel.
Flight
Flight
Instruments
Instruments
3)
Setting a preset channel number
On the ‘XM Radio’ Page, while listening to an ‘Active Channel’ that is
wanted for a preset, select the Presets Softkey to access the first five
preset channels (Preset 1 - Preset 5).
2)
Select the More Softkey to access the next five channels (Preset 6
– Preset 10), and again to access the last five channels (Preset 11 –
Preset 15). Selecting the More Softkey repeatedly cycles through the
preset channels.
3)
Select any one of the (Preset 1 - Preset 15) 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.
AFCS
1)
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.)
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
119
Index
Index
SiriusXM Radio volume may also be adjusted on each passenger headset.
Appendix
Appendix
With the ‘AUX-XM Radio’ Page displayed, select the Volume Softkey.
Annun/Alerts
Annun/Alerts
1)
Additional Additional
Abnormal
AFCS Features
Features
Operation
Adjusting Volume
190-02219-00 Rev. C
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
The Category Box of the XM Radio Page displays the currently selected category
of audio.
1) Select the Category Softkey on the ‘AUX-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 and press the ENT Key. Selecting
All Categories places all channels in the list.
EISEIS
Selecting a Category
Mute SiriusXM audio
1)
Select the ‘AUX-XM Radio’ Page or ‘AUX-XM Information’ Page.
2)
Select the Mute Softkey to mute the audio. Select the Mute Softkey again
to unmute the audio.
SATELLITE TELEPHONE AND DATA LINK SERVICES
NOTE: An account must be established to access the Iridium satellite network
for voice/SMS.
Operation of these features in the cockpit is accomplished through the AuxTelephone, Aux-Text Messaging, and Aux-Maintenance WI-FI Setup Pages. For
operation using the cabin handset, consult the instructions provided with the handset.
Registering with Garmin Connext
A subscriber account must be established prior to using the Iridium Satellite
System. Before setting up an Iridium account, obtain the serial number of the Iridium
Transceiver (GSR1) and the System ID by selecting the Aux- System Status Page.
Contact Garmin at 1-866-739-5687 in the United States or 913-397-8200, ext. 1135.
Disable/Enable Iridium Transceiver
Iridium telephone and data communications may be turned on or off by performing
these simple steps.
Disabling/enabling telephone and low speed data services:
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Additional Features
1)
Turn the large FMS Knob on the MFD to select the Aux page group.
2)
Turn the small FMS Knob to select the ‘Aux-Telephone’ Page.
3)
Press the MENU Key. The Page Menu window is now displayed.
4)
Turn the FMS Knob to select ‘Disable Iridium Transmission’ in the menu list.
5)
Press the ENT Key. The Iridium transceiver is now disabled.
6)
To enable the Iridium transceiver, repeat steps 1 through 3, then select
‘Enable Iridium Transceiver’.
Index
Index
Telephone Communication
The pilot or copilot can place and answer calls on the Iridium satellite network.
120
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Additional Features
Viewing the Telephone Page
2)
Turn the small FMS Knob to select the ‘Aux - Telephone’ or ‘Aux - Text
Messaging’ Page.
3)
If necessary, select the TEL Softkey to display the ‘Aux-Telephone’ Page.
Internal
Phone
External
Phone
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Turn the large FMS Knob on the MFD to select the Aux page group.
EISEIS
1)
Flight
Flight
Instruments
Instruments
Control and monitoring of telephone functions are accomplished through the AuxTelephone Page.
Description
Phone is Idle
Phone is ringing
AFCS
Phone has a dial tone (off hook) or connected to
another phone
Additional Additional
Abnormal
AFCS Features
Features
Operation
Phone dialed is busy
Phone is dialing another phone
Annun/Alerts
Annun/Alerts
Phone has failed
Phone status not known
Appendix
Appendix
Phone is disabled
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
121
Additional Features
Flight
Flight
Instruments
Instruments
Internal
Phone
External
Phone
EISEIS
Phone is reserved for data transmission
Calling other phone or incoming call from other phone
Other phone is on hold
Phones are connected
Contacts
The names, telephone number, and email addresses can be saved in a list of contacts for easy use when making telephone calls.
With the Aux - Telephone Page displayed, press the FMS Knob to display
the cursor.
Additional Additional
Abnormal
Features
Operation
Features AFCS
2)
If necessary, turn either FMS Knob to place the cursor on ‘New Entry’.
3)
Press the ENT Key. The cursor moves the ‘Name’ field of the ‘Contact
Details’ window.
4)
Enter the desired name of the new contact. Entry can be accomplished
through the alphanumeric keys on the MFD Controller, or the FMS Knobs
on the controller or the MFD.
5)
Press the ENT Key. The cursor moves to the ‘Phone Number’ field.
6)
Enter the desired telephone number. Entry can be accomplished through
the alphanumeric keys on the MFD Controller, or the FMS Knobs on the
controller or the MFD.
7)
Press the ENT Key. The cursor moves to the ‘Email’ field.
8)
Enter the desired email address. Entry can be accomplished through
the alphanumeric keys on the MFD Controller, or the FMS Knobs on the
controller or the MFD.
9)
Press the ENT Key. The Save button is highlighted.
Index
Index
AFCS
1)
Annun/Alerts
Annun/Alerts
Entering a new contact
Appendix
Appendix
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
Description
122
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Additional Features
Flight
Flight
Instruments
Instruments
10) Press the ENT Key. The new contact entry is added to the list of saved
contacts.
Deleting a contact
2)
Turn either FMS Knob to place the cursor on the desired contact name.
3)
Select the Delete Softkey. A confirmation window is displayed.
4)
With ‘OK’ highlighted, press the ENT Key to delete the selected contact.
Editing a contact:
With the Aux - Telephone Page displayed, press the FMS Knob to display
the cursor.
2)
Turn either FMS Knob to place the cursor on the desired contact name.
3)
Select the Edit Softkey. The cursor is placed in the ‘Name’ field. Enter the
desired changes. Entry can be accomplished through the alphanumeric keys
on the MFD Controller, or the FMS Knobs on the controller or the MFD.
4)
Press the ENT Key when each field is complete. The Save Button is now
highlighted.
5)
Press the ENT Key to save the changes.
AFCS
1)
Appendix
Appendix
Answering an Incoming Call in the Cockpit
Press the TEL Key on the appropriate audio panel.
2)
Select the Answer Softkey on the MFD.
Index
Index
Or:
190-02219-00 Rev. C
Annun/Alerts
Annun/Alerts
When viewing MFD pages other than the Aux-Telephone Page, a pop-up alert will
be displayed and an aural alert “Incoming Call” will be heard. If the call is from the
cabin, Cabin will be displayed. If the incoming call is an Iridium network call, Iridium
will be displayed. The pop-up alert may be inhibited at times, such as during takeoff.
In addition to the pop-up alert, a ringing phone symbol will be displayed to the right
of the MFD page title. Also, the voice alert “Incoming Call” will be heard on the
selected cockpit audio.
Additional Additional
Abnormal
AFCS Features
Features
Operation
Incoming Calls
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
With the Aux - Telephone Page displayed, press the FMS Knob to display
the cursor.
EISEIS
1)
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
123
While viewing the Aux-Telephone Page, press the TEL Key on the
appropriate audio panel.
2)
Press the MENU Key to display the Page Menu.
3)
Turn either FMS Knob to place the cursor on ‘Answer Incoming Call’.
4)
Press the ENT Key.
Selecting the Ignore Softkey will extinguish the pop-up window and leave the call
unanswered. Selecting the TEL Softkey will display the Aux-Telephone Page allowing
additional call information to be viewed before answering.
Muting Incoming Call Alerts
1)
With the ‘Aux-Telephone’ Page displayed, press the MENU Key on the MFD
to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Disable Incoming Call Alerts’.
3)
Press the ENT Key. The voice and pop-up alert will not be displayed now
when an incoming call is received.
Outgoing Calls
Voice calls can be made from the cockpit to an external phone through the Iridium
Satellite Network.
Making an External Call from the Cockpit
1)
Press the TEL Key on the appropriate audio panel.
2)
Select the Dial Softkey on the MFD.
3)
Turn the small FMS Knob to select ‘Iridium’.
4)
Press the ENT Key. The cursor has now moved to the phone number entry
field.
5)
Enter the desired telephone number (country code first) by selecting the
number softkeys on the MFD or by pressing the numeric keys on the MFD
Control Unit.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
1)
NOTE: The Push-to-Talk switch is not utilized for telephone communication.
The microphone is active after selecting the Answer Softkey, and stays active
until the call is terminated.
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Additional Features
124
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Additional Features
Country Code
870
Ellipso
Iridium
Globalstar
8812 or 8813
8816 or 8817
8818 or 8819
Flight
Flight
Instruments
Instruments
Satellite System
Inmarsat
ICO
8810 or 8811
7)
Press the ENT Key. The system will begin calling the number.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Press the ENT Key. ‘OK’ is highlighted.
EISEIS
6)
To exit the call, select the HANGUP Softkey.
Placing The Cockpit Phone on Hold
Select the Hold Softkey on the MFD.
Or:
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Put Current Call On Hold’.
3)
Press the ENT Key.
AFCS
1)
Text Messaging (SMS)
Turn the large FMS Knob on the MFD to select the Aux page group.
2)
Turn the small FMS Knob to select the ‘Aux-Telephone’ or ‘Aux-Text
Messaging’ Page.
3)
If necessary, select the SMS Softkey to display the Aux-Text Messaging
Page.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
1)
Appendix
Appendix
Viewing the Text Messaging Page
Annun/Alerts
Annun/Alerts
The pilot or copilot can send and receive text messages on the Iridium satellite
network. Messages may be sent to an email address or text message capable cellular
telephone. Message length is limited to 160 characters, including the email address.
Senders should address text messages to aircraft by entering [aircraft Iridium phone
number]@msg.iridium.com.
The text messaging user interface is mainly through the Aux-Text Messaging Page.
Additional Additional
Abnormal
AFCS Features
Features
Operation
Select the Hold Softkey again to resume the call.
125
Additional Features
Flight
Flight
Instruments
Instruments
Message Symbol
Received text message that has not been opened
Saved text message, draft not sent
System is sending text message
Text message has been sent
System failed to send text message
Predefined text message
Viewing a Text Message When Received
When viewing MFD pages other than the Aux-Text Messaging Page, a pop-up alert
will be displayed when a new text message is received.
Select the View Softkey to view the message. Selecting the Ignore Softkey will
extinguish the pop-up window and leave the text message unopened. Selecting the
Ignore All Softkey will extinguish the pop-window and ignore all future incoming
text messages. Selecting the SMS Softkey will display the Aux-Text Messaging Page.
The pop-up alerts may be enabled or disabled through the Page Menu.
Enabling/Disabling Incoming Text Message Pop-Up Alerts
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Received text message that has been opened
Appendix
Appendix
Index
Index
Description
1)
With the ‘Aux-Text Messaging’ Page displayed, press the MENU Key on the
MFD to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Disable New Message
Popups’ or ‘Enable New Message Popups’.
3)
Press the ENT Key. The pop-up alert will not be displayed when an
incoming text message is received.
Replying to a Text Message
While viewing the text message, select the Reply Softkey.
Or:
126
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Additional Features
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Reply To Message’.
3)
Press the ENT Key.
Flight
Flight
Instruments
Instruments
1)
1)
EISEIS
Sending a New Text Message
While viewing the ‘Aux-Text Messaging’ Page, select the NEW Softkey.
Or:
b) Turn either FMS Knob to place the cursor on ‘Draft New Message’.
c) Press the ENT Key.
3)
Press the ENT Key. The cursor is now displayed in the ‘Message’ field.
4)
Enter the desired message using any combination of entry methods as
described in step 2.
5)
Press the ENT Key.
6)
Select the Send Softkey to send the message immediately, or select the
Save Softkey to save the message in Outbox for sending at a later time.
Select the Cancel Softkey to delete the message.
Additional Additional
Abnormal
AFCS Features
Features
Operation
The SMS Text Message Draft Window is now displayed with the cursor in
the ‘TO’ field. Enter the desired telephone number or email address. Entry
can be accomplished through the alphanumeric keys on the MFD Controller,
or combination of the FMS Knob on the controller and softkeys on the
MFD. The FMS Knob is used to enter letters and numbers, or numbers can
be entered from the MFD by selecting the Numbers Softkey. Select the
CapsLock Softkey to create upper and lower case alpha characters. Special
characters can be accessed by selecting the Symbols Softkey.
Time and effort can be saved in typing text messages that are used repeatedly by
saving these messages as a predefined message.
Appendix
Appendix
Creating a Predefined Text Message
2)
Turn either FMS Knob to select ‘Edit Predefined Messages’.
3)
Press the ENT Key. The Predefined Messages view is now displayed.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
While viewing the ‘Aux-Text Messaging’ Page, press the MENU Key to
display the Page Menu.
Annun/Alerts
Annun/Alerts
Predefined Text Messages
1)
AFCS
2)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
a) Press the MENU Key to display the Page Menu.
127
Additional Features
Flight
Flight
Instruments
Instruments
4)
Select the NEW Softkey.
Or:
a) Press the MENU Key to display the Page Menu.
EISEIS
b) Turn either FMS Knob to place the cursor on ‘Draft New Predefined
Message’.
5)
The cursor is displayed in the ‘Title’ field. Enter the desired message
title. Entry can be accomplished through the alphanumeric keys on the
MFD Controller, or combination of the FMS Knob on the controller and
softkeys on the MFD. The FMS Knob is used to enter letters and numbers,
or numbers can be entered from the MFD by selecting the Numbers
Softkey. Select the CapsLock Softkey to create upper and lower case alpha
characters. Special characters can be accessed by selecting the Symbols
Softkey.
6)
Press the ENT Key. The cursor is now displayed in the ‘Message’ field.
7)
Enter the desired message using any combination of entry methods as
described in step 5.
8)
Press the ENT Key.
9)
Select the Save Softkey. The new predefined message is now shown in
the displayed list. Selecting the Cancel Softkey will delete the message
without saving.
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
c) Press the ENT Key. The Predefined SMS Text Message Window is now
displayed.
10) Press the MENU Key to display the Page Menu.
11) Turn either FMS Knob to place the cursor on ‘Cancel Drafting Message’.
Annun/Alerts
Annun/Alerts
12) Press the ENT Key.
Index
Index
Appendix
Appendix
Sending a Predefined Text Message
128
1)
While viewing the ‘Aux-Text Messaging’ Page, select the NEW Softkey.
2)
The Predefined SMS Text Message Window is now displayed with the
cursor in the ‘TO’ field. Enter the desired telephone number or email
address. Entry can be accomplished through the alphanumeric keys on the
MFD Controller, or combination of the FMS Knob on the controller and
softkeys on the MFD. The FMS Knob is used to enter letters and numbers,
or numbers can be entered from the MFD by selecting the Numbers
Softkey. Select the CapsLock Softkey to create upper and lower case alpha
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Additional Features
4)
Select the Predefined Softkey. The Predefined Message Menu Window is
displayed.
5)
Turn either FMS Knob to select the desired predefined message.
6)
Press the ENT Key. The predefined message text is inserted into the
message field. If desired, the message can be edited by using the FMS
Knobs.
7)
Press the ENT Key.
8)
Select the Send Softkey to transmit the message.
Text Message Boxes
Received text messages reside in the Inbox as ‘Read’ or ‘Unread’ messages. The
Outbox contains ‘Sent” and ‘Unsent’ text messages. Saved messages that are meant to
be sent later are stored as Drafts. Each text message box may be viewed separately, or
together in any combination.
AFCS
Showing Inbox Messages
Additional Additional
Abnormal
AFCS Features
Features
Operation
While viewing the ‘Aux-Text Messaging’ Page, select the Arrange Softkey,
then select the Inbox Softkey.
Or:
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Show Inbox Messages’.
3)
Press the ENT Key. The message box selected for viewing is indicated at
the bottom left of the list window.
Annun/Alerts
Annun/Alerts
1)
Showing Outbox Messages
Appendix
Appendix
While viewing the ‘Aux-Text Messaging’ Page, select the Arrange Softkey,
then select the Outbox Softkey.
Or:
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Show Outbox Messages’.
3)
Press the ENT Key. The message box selected for viewing is indicated at
the bottom left of the list window.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
1)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Press the ENT Key. The cursor is now displayed in the ‘Message’ field.
EISEIS
3)
Flight
Flight
Instruments
Instruments
characters. Special characters can be accessed by selecting the Symbols
Softkey.
129
Additional Features
Flight
Flight
Instruments
Instruments
Showing Draft Messages
While viewing the ‘Aux-Text Messaging’ Page, select the Arrange Softkey,
then select the Drafts Softkey.
1)
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Show Draft Messages’.
3)
Press the ENT Key. The message box selected for viewing is indicated at
the bottom left of the list window.
Managing Text Messages
The viewed messages may be listed according to the date/time the message was
sent or received, the type of message (read, unread, sent, unsent, etc.), or by message
address.
Viewing Messages Sorted by Message Date/Time:
While viewing the ‘Aux-Text Messaging’ Page, select the Arrange Softkey,
then select the Time Softkey.
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Or:
Additional Additional
Abnormal
Features
Operation
Features AFCS
Or:
1)
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Sort By Date/Time’.
3)
Press the ENT Key. The sorting selection is indicated at the bottom center
of the list window.
Viewing Messages Sorted by Message Type
Annun/Alerts
Annun/Alerts
While viewing the ‘Aux-Text Messaging’ Page, select the Arrange Softkey,
then select the Type Softkey.
Appendix
Appendix
Or:
1)
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Sort By Type’.
3)
Press the ENT Key. The sorting selection is indicated at the bottom center
of the list window.
Index
Index
Viewing Messages Sorted by Address:
While viewing the ‘Aux-Text Messaging’ Page, select the Arrange Softkey,
then select the Address Softkey.
130
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Additional Features
Flight
Flight
Instruments
Instruments
Or:
Press the MENU Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Sort By Address’.
3)
Press the ENT Key. The sorting selection is indicated at the bottom center
of the list window.
EISEIS
1)
Viewing The Content of a Text Message
While viewing the ‘Aux-Text Messaging’ Page, select the desired message
box.
2)
Press the FMS Knob to activate the cursor.
3)
Turn either FMS Knob to select the desired message.
4)
Select the VIEW Softkey.
Or:
Press the ENT Key.
Or:
b) Turn either FMS Knob to place the cursor on ‘View Selected Message’.
Additional Additional
Abnormal
AFCS Features
Features
Operation
c) Press the ENT Key.
Message content is displayed.
5)
To close the text message, select the Close Softkey.
Or:
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Close Message’.
Annun/Alerts
Annun/Alerts
c) Press the ENT Key.
Marking Selected Message As Read
While viewing the Inbox on the ‘Aux-Text Messaging’ Page, press the FMS
Knob to activate the cursor.
2)
Turn either FMS Knob to select the desired message.
3)
Select the MRK Read Softkey.
Index
Index
Or:
Appendix
Appendix
1)
190-02219-00 Rev. C
AFCS
a) Press the MENU Key to display the Page Menu.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
1)
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
131
Additional Features
Flight
Flight
Instruments
Instruments
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Mark Selected Message
As Read’.
EISEIS
c) Press the ENT Key.
The message symbol now indicates the message has been opened.
Additional Additional
Abnormal
Features
Operation
Features AFCS
Annun/Alerts
Annun/Alerts
Appendix
Appendix
Index
Index
1)
While viewing the Inbox on the ‘Aux-Text Messaging’ Page, press the MENU
Key to display the Page Menu.
2)
Turn either FMS Knob to place the cursor on ‘Mark All New Messages As
Read’.
3)
Press the ENT Key. A confirmation window is displayed.
4)
With cursor highlighting ‘YES’, press the ENT Key. The message symbols
now indicate all the message have been opened.
Deleting a Message
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
Marking All Messages As Read
1)
While viewing the Inbox on the ‘Aux-Text Messaging’ Page, press the FMS
Knob to activate the cursor.
2)
Turn either FMS Knob to select the desired message.
3)
Select the Delete Softkey.
Or:
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Delete Selected Message’.
c) Press the ENT Key.
SCHEDULER
The Scheduler feature can be used to enter and display reminder messages (e.g.,
Update Databases, Switch fuel tanks, or Altimeter-Transponder Check) in the Alerts
Window on the PFD. Messages can be set to display based on a specific date and time
(event), once the message timer reaches zero (one-time; default setting), or recurrently
whenever the message timer reaches zero (periodic). Message timers set to periodic
alerting automatically reset to the original timer value once the message is displayed.
When power is cycled, all messages are retained until deleted, and message timer
countdown is resumed
132
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Additional Features
Flight
Flight
Instruments
Instruments
Entering a scheduler message:
1) Select the ‘Aux - Utility’ Page.
3)
Turn the large FMS Knob to highlight the first empty scheduler message
naming field.
4)
Use the FMS Knob to enter the message text to be displayed in the PFD
Alerts Window and press the ENT Key.
5)
Press the ENT Key again or use the large FMS Knob to move the cursor to
the field next to ‘Type’.
6)
Turn the small FMS Knob to select set the message alert type:
• Event—Message issued at the specified date/time
• One-time—Message issued when the message timer reaches zero
(default setting)
• Periodic—Message issued each time the message timer reaches zero
8)
For periodic and one-time message, use the FMS Knob to enter the timer
value (HHH:MM:SS) from which to countdown and press the ENT Key.
9)
For event-based messages:
a) Use the FMS Knob to enter the desired date (DD-MM-YYYY) and press
the ENT Key.
b) Press the ENT Key again or use the large FMS Knob to move the cursor
to the next field.
10) Press the ENT Key again or use the large FMS Knob to move the cursor to
enter the next message.
Appendix
Appendix
Deleting a scheduler message:
1) Select the ‘Aux - Utility’ Page.
Press the FMS Knob momentarily to activate the flashing cursor.
3)
Turn the large FMS Knob to highlight the name field of the scheduler
message to be deleted.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
2)
Annun/Alerts
Annun/Alerts
c) Use the FMS Knob to enter the desired time (HH:MM) and press the
ENT Key.
Additional Additional
Abnormal
AFCS Features
Features
Operation
Press the ENT Key again or use the large FMS Knob to move the cursor to
the next field.
AFCS
7)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Press the FMS Knob momentarily to activate the flashing cursor.
EISEIS
2)
133
4)
Press the CLR Key to clear the message text. If the CLR Key is pressed
again, the message is restored.
5)
Press the ENT Key to confirm message deletion.
CREW PROFILES
When the system is powered on, the last selected pilot profile is shown on the MFD
power-up screen. The system can store up to 25 profiles; the currently active profile,
the amount of memory used, and the amount of memory available are shown at the
top of the Aux - System Setup page in the box labeled ‘Pilot Profile’.
Creating a profile:
1) Select the ‘Aux - System Setup (X)’ Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight ‘Create’ in the Crew Profile Box.
4)
Press the ENT Key. A ‘Create Profile’ Window is displayed.
5) Use the FMS Knob to enter a profile name up to 16 characters long and
press the ENT Key. Crew profile names cannot begin with a blank as the
first letter.
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Additional Features
6)
In the next field, use the small FMS Knob to select the desired settings
upon which to base the new profile. Profiles can be created based on
Garmin factory defaults, default profile settings (initially based on Garmin
factory defaults unless edited by the pilot), or other previously created
profile settings.
7)
Press the ENT Key.
Annun/Alerts
Annun/Alerts
8) With ‘Create’ highlighted, press the ENT Key to create the profile
Or:
Appendix
Appendix
Use the large FMS Knob to select ‘Create & Activate’ and press the ENT
Key to activate the new profile.
9)
To cancel the process, select ‘Cancel’ with the large FMS Knob and press
the ENT Key.
Index
Index
Selecting an active profile:
1) Select the ‘Aux - System Setup (X)’ Page.
2)
134
Press the FMS Knob momentarily to activate the flashing cursor.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Additional Features
Profile’ Box.
4) Turn the small FMS Knob to display the crew profile list and highlight the
Flight
Flight
Instruments
Instruments
3) Turn the large FMS Knob to highlight the active profile field in the ‘Crew
desired profile.
the selected profile.
1) Select the ‘Aux - System Setup (X)’ Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight ‘Rename’ in the ‘Crew Profile’ Box.
4)
Press the ENT Key.
5) In the ‘Rename Profile’ Window, turn the FMS Knob to select the profile to
rename.
6)
Press the ENT Key.
AFCS
7) Use the FMS Knob to enter a new profile name up to 16 characters long
and press the ENT Key.
To cancel the process, use the large FMS Knob to select ‘Cancel’ and press
the ENT Key.
Deleting a profile:
1) Select the ‘Aux - System Setup (X)’ Page.
Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight ‘Delete’ in the ‘Crew Profile’ Box.
4)
Press the ENT Key.
delete.
6)
Press the ENT Key.
Appendix
Appendix
5) In the ‘Delete Profile’ Window, turn the FMS Knob to select the profile to
Annun/Alerts
Annun/Alerts
2)
Additional Additional
Abnormal
AFCS Features
Features
Operation
8) With ‘Rename’ highlighted, press the ENT Key.
9)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Renaming a profile:
EISEIS
5) Press the ENT Key. The system loads and displays the system settings for
7) With ‘Delete’ highlighted, press the ENT Key.
To cancel the process, use the large FMS Knob to select ‘Cancel’ and press
the ENT Key.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
135
Index
Index
8)
Importing a profile from an SD card:
1)
Insert an SD card containing the crew profile(s) into the top card slot on the
MFD.
2)
Turn the FMS Knob to select the ‘Aux - System Setup (X)’ Page.
3)
Press the Import Softkey.
4)
The system displays the ‘Crew Profile Importing’ Window with ‘Import’
highlighted. Turn the large FMS Knob to highlight the ‘Profile Name’ Field,
then scroll to the desired profile name with the large and small FMS Knobs,
then press the ENT Key. Then press the ENT Key with ‘Import’ highlighted.
5)
If the imported profile name is the same as an existing profile on the
system, the system displays an ‘Overwrite existing profile? OK or Cancel’
prompt. Press the ENT Key to replace profile on the system with the profile
imported from the SD card, or turn the FMS Knob to highlight ‘Cancel’ and
press the ENT Key to return to the ‘Crew Profile Importing’ Window.
6)
If successful, the system displays ‘Crew profile import succeeded.’ in the
window below. With ‘OK’ highlighted, press the ENT or CLR Keys or press
the FMS Knob to return to the ‘Aux - System Setup (X)’ Page. The imported
profile becomes the active profile.
Exporting a profile to an SD card:
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Additional Features
136
1)
Insert the SD card for storing the Crew Profile into the top card slot on the
MFD.
2)
Turn the FMS Knob to select the ‘Aux - System Setup (X)’ Page.
3)
Press the Export Softkey. The system displays the ‘Crew Profile Exporting’
Window.
4)
To export the crew profile using the current selected profile, press the ENT
Key with ‘Export’ highlighted. To change the selected profile, turn the large
FMS Knob to highlight the ‘Profile Name’ ield, then scroll to the desired
profile name with the large and small FMS Knobs, then press the ENT Key.
Then press the ENT Key with ‘Export’ highlighted.
5)
If the selected profile to be exported is the same as an existing profile file
name on the SD card, the system displays an ‘Overwrite existing profile?
OK or Cancel’ prompt. Press the ENT Key to replace the profile on the SD
card with the profile to be exported, or turn the FMS Knob to highlight
‘Cancel’ and press the ENT Key to return to the ‘Pilot Profile Exporting’
Window without exporting the profile.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Additional Features
If successful, the window displays ‘Crew profile export succeeded.’ With
‘OK’ highlighted, press the ENT or CLR Keys, or press the FMS Knob to
return to the ‘Aux - System Setup (X)’ Page.
Flight
Flight
Instruments
Instruments
6)
1)
Turn the large FMS Knob on the MFD to select the Aux page group.
2)
Turn the small FMS Knob to select the Connext Setup page.
AFCS
Changing the Bluetooth Name
2)
Turn the large FMS Knob to place the cursor in the ‘Bluetooth Name’ field.
3)
Enter the desired name by using the large FMS Knob to select the character
field, and the small FMS Knob select the desired alphanumeric character
for that field.
4)
Press the ENT Key. The cursor is removed and the new name is displayed.
Enabling/Disabling Flight Plan Importing from Garmin Pilot
While viewing the Connext Setup Page, press the FMS Knob to activate the
cursor.
2)
Turn the large FMS Knob to place the cursor in the ‘Flight Plan Import’
field.
3)
Turn the small FMS Knob to select ‘Enabled’ or ‘Disabled’.
4)
Press the FMS Knob to remove the cursor.
Index
Index
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Appendix
Appendix
1)
Annun/Alerts
Annun/Alerts
While viewing the Connext Setup Page, press the FMS Knob to activate the
cursor.
Additional Additional
Abnormal
AFCS Features
Features
Operation
1)
190-02219-00 Rev. C
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Viewing the Connext Setup Page
EISEIS
CONNEXT MANAGEMENT
The Connext Setup Page allows for setting up the installed optional Flight Stream
device for a Bluetooth connection between the system and a mobile device running the
Garmin Pilot™ application.
The mobile device must be ‘paired’ with the system in order to use the various
functions. Pairing is accomplished by first placing the system in pairing mode by
displaying the Connext Setup Page. The system is ‘discoverable’ whenever this page is
displayed. The pairing operation is completed from the mobile device and the Garmin
Pilot application. See the device Bluetooth pairing instructions and the connection
instructions in the Garmin Pilot application.
137
Enabling/Disabling WiFi Database Importing from Garmin Pilot
Annun/Alerts
Annun/Alerts
While viewing the Connext Setup Page, press the FMS Knob to activate the
cursor.
2)
Turn the large FMS Knob to place the cursor in the ‘WiFi Database Import’
field.
3)
Turn the small FMS Knob to select ‘Enabled’ or ‘Disabled’.
4)
Press the FMS Knob to remove the cursor.
1)
While viewing the Connext Setup Page, press the FMS Knob to activate the
cursor.
2)
Turn the large FMS Knob to highlight the desired paired device.
3)
Turn the small FMS Knob to select ‘Enabled’ or ‘Disabled’. Selecting
‘Enabled’ allows the system to automatically connect to a previously paired
device when detected.
4)
Press the FMS Knob to remove the cursor.
Remove a Specific Paired Device from the List of Paired Devices:
1)
While viewing the Connext Setup Page, press the FMS Knob to activate the
cursor.
2)
Turn the large FMS Knob to highlight the desired paired device.
3)
Press the Remove Softkey. A confirmation screen is displayed.
4)
If necessary, turn the large FMS Knob to select ‘Yes’.
5)
Press the ENT Key to remove the device from the list of paired devices.
MAINTENANCE LOGS
The system provides recording of CAS, CMC, exceedances, and other critical aircraft data that occur while the aircraft is on the ground or in flight.
The Maintenance Logs feature is accessible by entering a password. No pilot action
is required.
Viewing the Maintenance Logs Page
Index
Index
Appendix
Appendix
1)
Enabling/Disabling Automatic Reconnection of a Specific Paired Device
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Additional Features
138
1)
Turn the large FMS Knob on the MFD to select the Aux page group.
2)
Turn the small FMS Knob to select ‘Maintenance Logs’. The Aux Maintenance Logs Page is now displayed.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Additional Features
AFCS
2)
Turn the small FMS Knob to select the System Setup Page.
3)
If necessary, select the SETUP 2 Softkey to display the Aux-System Setup 2
Page. If the Aux-System Setup 2 is already displayed, proceed to step 4.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to place the cursor in the Stability & Protection
field.
6)
Turn the small FMS Knob to select ‘Enabled’ or ‘Disabled’.
7)
Press the FMS Knob to remove the cursor.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
139
Index
Index
Roll Limit Indicators are displayed on the roll scale at 45° right and left, indicating
where ESP will engage. As roll attitude exceeds 45°, ESP will engage and the on-side
Roll Limit Indicator will move to 30°. The Roll Limit Indicator is now showing where
ESP will disengage as roll attitude decreases to within the desirable roll attitude range.
Appendix
Appendix
Roll Engagement
Annun/Alerts
Annun/Alerts
Turn the large FMS Knob to select the Aux Page Group.
Additional Additional
Abnormal
AFCS Features
Features
Operation
1)
190-02219-00 Rev. C
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Enabling or disabling ESP
EISEIS
ESP engages when the aircraft exceeds one or more conditions (pitch, roll, Vmo,
Mmo, and/or angle of attack) beyond the normal flight parameters. Enhanced stability
for each condition is provided by applying a force to the appropriate control surface to
return the aircraft to the normal flight envelope. This is perceived by the pilot as resistance to control movement in the undesired direction when the aircraft approaches a
steep attitude, high airspeed, or when a stall is imminent.
When ESP™ has been engaged for more than ten seconds (cumulative; not necessarily consecutive seconds) of a 20-second interval, the autopilot is automatically entgaged
with the flight director in Level Mode, bringing the aircraft into level flight. An aural
“Engaging Autopilot” alert is played and the flight director mode annunciation will indicate ‘LVL’ for vertical and lateral modes.
The pilot can interrupt ESP by pressing and holding either the Control Wheel Steering (CWS) or Autopilot Disconnect (AP DISC) switch. Upon releasing the CWS or AP
DISC switch, ESP force will again be applied, provided aircraft attitude and/or airspeed
are within their respective engagement limits. ESP can also be overridden by overpowering the servo’s mechanical torque limit. ESP is not functional when Trim/Servo has failed.
Flight
Flight
Instruments
Instruments
ELECTRONIC STABILITY & PROTECTION (ESP™) (OPTIONAL)
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Additional Features
Once engaged, ESP force will be applied between 30° and 75°. The force increases
as roll attitude increases and decreases as roll attitude decreases. The applied force
is intended to encourage pilot input that returns the airplane to a more normal roll
attitude. As roll attitude decreases, ESP will disengage at 30°.
ESP is automatically disengaged if the aircraft reaches the autopilot roll engagement
attitude limit of 75°.
Pitch Engagement
ESP™ engages at 20° nose-up and 22° nose-down. Once ESP™ is engaged, it will
apply increasing opposing force between 15° and 50° nose-up and between 12° and
50° nose-down, as indicated in the following figure. Maximum opposing force is
applied between 25° and 50° nose-up and between 27° and 50° nose-down. ESP™
disengages when 50° is exceeded in a nose-up or nose-down attitude.
With ESP™ engaged, and the aircraft in a nose-up condition, opposing force steadily decreases from 25° nose-up to 15° nose-up as aircraft pitch moves toward zero
degrees. ESP™ disengages at 15° nose-up. With ESP™ engaged, and the aircraft in a
nose-down condition, opposing force steadily decreases from 27° nose-down to 12°
nose-down as aircraft pitch moves toward zero degrees. ESP™ disengages at 12° nosedown.
The opposing force increases or decreases depending on the pitch angle and the
direction of pitch travel. This force is intended to encourage movement in the pitch
axis in the direction of the normal pitch attitude range for the aircraft.
There are no indications marking the pitch ESP™ engage and disengage limits in
these nose-up/nose-down conditions.
Angle of Attack Protection
When a compatible lift computer is installed with the G1000NXi retrofit, angle of
attack protection is provided as part of the ESP feature. ESP force may be applied if
the lift computer determines a stall warning condition is imminent. In this condition,
the Pitch Limit Indicator will be initially displayed 4° below this computed pitch
attitude. When pitch attitude equals that indicated by the Pitch Limit Indicator, ESP
will engage, applying a force in the direction necessary to lower the nose of the aircraft.
High Airspeed Protection
Exceeding 268 kts IAS will result in ESP™ applying force to raise the nose of the
aircraft. When the indicated airspeed decreases to below 256 kts, ESP™ force is no
longer applied.
140
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Additional Features
The MFD is able to display optional electronic checklists which allow a pilot to
quickly find the proper procedure on the ground and during each phase of flight. The
system accesses the checklists from an SD card inserted into the bezel slot. If the SD
card contains an invalid checklist file or no checklist, the Power-up Page messages display ‘Checklist File: Invalid’ or ‘Checklist File: N/A’ (not available) and the Checklist
Softkey is not available.
AFCS
Accessing and navigating checklists
From any page on the MFD (except the EIS Pages), press the Checklist
Softkey or turn the large FMS Knob to select the Checklist Page.
2)
Turn the large FMS Knob to select the ‘Group’ field.
3)
Turn the small FMS Knob to select the desired procedure and press the
ENT Key.
4)
Turn the large FMS Knob to select the ‘Checklist’ field.
5)
Turn the FMS Knob to select the desired checklist and press the ENT Key.
The selected checklist item is indicated with white text surrounded by a
white box.
6)
Press the ENT Key or Check Softkey to check the selected checklist item.
The line item turns green and a checkmark is placed in the associated box.
The next line item is automatically selected for checking.
Additional Additional
Abnormal
AFCS Features
Features
Operation
1)
141
Index
Index
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Appendix
Appendix
Press the CLR Key or Uncheck Softkey to remove a check mark from an
item.
Annun/Alerts
Annun/Alerts
Either FMS Knob can be used to scroll through the checklist and select the
desired checklist item.
190-02219-00 Rev. C
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
NOTE: Garmin is not responsible for the content of checklists. Checklists
are created by the aircraft manufacturer. Modifications or updates to the
checklists are coordinated through the aircraft manufacturer. The user cannot
edit these checklists.
EISEIS
NOTE: The optional checklists presented here are for example only and may
differ from checklists available for the aircraft. The information described in
this section is not intended to replace the checklist information described in
the AFM or the Pilot Safety and Warning Supplements document.
Flight
Flight
Instruments
Instruments
ELECTRONIC CHECKLISTS
7)
When all checklist items have been checked, ‘*Checklist Finished*’ is
displayed in green text at the bottom left of the checklist window. If all
items in the checklist have not be checked, ‘*Checklist Not Finished*’ will
be displayed in yellow text.
8)
Press the ENT Key. ‘Go To Next Checklist?’ will be highlighted by the
cursor.
9)
Press the ENT Key to advance to the next checklist.
10) Press the Exit Softkey to exit the Checklist Page and return to the page last
viewed.
Accessing emergency procedures
1)
From any page on the MFD (except the EIS Pages), press the Checklist
Softkey or turn the large FMS Knob to select the Checklist Page.
2)
Press the EMER Softkey.
3)
Turn the FMS Knob to select the desired emergency checklist and press the
ENT Key.
4)
Press the ENT Key or Check Softkey to check the selected emergency
checklist item. The line item turns green and a checkmark is placed in the
box next to it. The next line item is automatically highlighted for checking.
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Additional Features
Either FMS Knob can be used to scroll through the checklist and select the
desired checklist item.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Press the CLR Key or Uncheck Softkey to remove a check mark from an
item.
142
5)
When all checklist items have been checked, ‘*Checklist Finished*’ is
displayed in green text at the bottom left of the checklist window. If all
items in the checklist have not be checked, ‘*Checklist Not Finished*’ will
be displayed in yellow text.
6)
Press the ENT Key. ‘Go To Next Checklist?’ will be highlighted by the
cursor.
7)
Press the ENT Key to advance to the next checklist.
8)
Press the Return Softkey to return to the previous checklist.
9)
Press the Exit Softkey to exit the Checklist Page and return to the page last
viewed.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Abnormal Operation
Flight
Instruments
ABNORMAL OPERATION
REVERSIONARY MODE
AFCS
Additional
Features
NOTE: The Daher TBM 910 Pilot’s Operating Handbook/Airplane Flight
Manual (POH/AFM) always takes precedence over the information found in
this section.
Hazard
Avoidance
• PFD2 – By pressing the DISPLAY BACKUP button on the right audio
panel.
Flight
Management
• MFD – By pressing the DISPLAY BACKUP button on the left or the right
audio panel.
Nav/Com/
XPDR/Audio
• PFD1 – By pressing the DISPLAY BACKUP button on the left audio panel.
EIS
Reversionary mode is a mode of operation in which all important flight information is presented identically on at least one of the remaining displays. Transition to
reversionary mode should be straightforward for the pilot, for flight parameters are
presented in the same format as in normal mode.
Reversionary mode can be activated manually by pressing the dedicated DISPLAY
BACKUP button at the bottom of the audio panel (refer to the Audio Panel section for
further details). Pressing this button again deactivates reversionary mode.
Each display can be configured to operate in reversionary mode, as follows:
ABNORMAL COM OPERATION
Appendix
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.
Annun/Alerts
HAZARD DISPLAYS WITH LOSS OF GPS POSITION
Abnormal
Operation
When a COM tuning failure is detected by the system, the emergency frequency
(121.500 MHz) is automatically loaded into the active frequency field of the COM
radio for which the tuning failure was detected. In the event of a failure of both PFD
and MFD, the emergency frequency (121.500 MHz) automatically becomes the active
frequency on both COM radios.
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
143
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
• Outside Air Temperature (OAT)
• International Standard Atmosphere
Temperature (ISA)
• DME Information
Window (optional)
• Wind data
• Transponder Status
Box
• PFD Setup Menu
• Windows displayed
in the lower right
corner of the PFD:
– Timer/References
– Nearest Airports
– Flight Plan
– Alerts
– Procedures
– DME Tuning
(optional)
• Minimum Descent
Altitude/Decision
Height readout
• Vertical Deviation,
Glideslope, and
Glidepath Indicators
• Altimeter Barometric Setting
• Selected Altitude
• VNV Target Altitude
• System Time
Annun/Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Abnormal Operation
Index
Appendix
Extreme Pitch Indication
144
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Abnormal Operation
Annunciation
Flight
Instruments
ABNORMAL GPS CONDITIONS ANNUNCIATED ON THE HSI
Right of
HSI
Loss of Integrity Monitoring–GPS integrity is insufficient for the
current phase of flight
Right of
HSI
Integrity OK–GPS integrity has been restored to within normal
limits (annunciation displayed for 5 seconds)
Lower left
of aircraft
symbol
Dead Reckoning–System is using projected position rather than
GPS position to compute navigation data and sequence active
flight plan waypoints
Flight
Management
DEAD RECKONING
Annun/Alerts
Appendix
Index
145
Abnormal
Operation
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Additional
Features
DR Mode is indicated on the system by the appearance of the letters ‘DR’
superimposed in yellow over the ‘own aircraft’ symbol as shown in the following
figure. In addition, ‘DR’ is prominently displayed, also in yellow, on the HSI slightly
above and to the right of the aircraft symbol on the CDI as shown in the following
figure. The CDI deviation bar is displayed in yellow, but will be removed from the
display after 20 minutes. Lastly, but at the same time, a ‘GPS NAV LOST’ alert message
appears on the PFD.
Normal navigation using GPS/SBAS source data resumes automatically once a valid
GPS solution is restored.
It is important to note that estimated navigation data supplied by the system in
DR Mode may become increasingly unreliable and must not be used as a sole means
of navigation. If, while in DR Mode, airspeed and/or heading data is also lost or
not available, the DR function may not be capable of estimating your position and,
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 system stops
navigating in GPS Mode.
Hazard
Avoidance
While in Enroute or Oceanic phase of flight, if the system 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 system 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.
190-02219-00 Rev. C
Nav/Com/
XPDR/Audio
Description
EIS
Location
consequently, the system may display a path that is different than the actual movement
of the aircraft. Estimated position information displayed by the system through
DR while there is no heading and/or airspeed data available should not be used for
navigation.
DR Mode is inherently less accurate than the standard GPS/SBAS Mode due to the
lack of satellite measurements needed to determine a position. Changes in wind speed
and/or wind direction compounds the relative inaccuracy of DR Mode. Because of this
degraded accuracy, the crew must maintain position awareness using other navigation
equipment until GPS-derived position data is restored.
Hazard
Avoidance
Flight
Management
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Abnormal Operation
AFCS
CDI ‘DR’ Indication on PFD
Symbolic Aircraft
(Map pages and Inset Map)
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 system is in DR Mode, the autopilot will couple to GPS for up to 20
minutes. 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
Dead Reckoning Indications
146
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Abnormal Operation
NOTE: Consult the aircraft documentation for the location of circuit breakers
as well as specifics that may supplement or amplify this procedure.
Firmly grasp the control wheel.
2)
Press and hold the AP DISC Switch. The autopilot will disconnect and
power is removed from the trim motor. Power is also removed from all
primary servo motors and engaged solenoids. Note the visual and aural
alerting indicating autopilot disconnect.
3)
Retrim the aircraft as needed. Substantial trim adjustment may be needed.
4)
Pull the appropriate circuit breaker(s) to electrically isolate the servo and
solenoid components.
5)
Release the AP DISC Switch.
Nav/Com/
XPDR/Audio
1)
EIS
If an autopilot failure or trim failure is suspected to have occurred, perform the
following steps:
Flight
Instruments
SUSPECTED AUTOPILOT MALFUNCTION
Flight
Management
Hazard
Avoidance
AFCS
OVERPOWERING AUTOPILOT SERVOS
Additional
Features
Abnormal
Operation
Annun/Alerts
Appendix
In the context of this discussion, “overpowering” refers to any pressure or force
applied to the pitch controls when the autopilot is engaged. A small amount of
pressure or force on the pitch controls can cause the autopilot automatic trim to run
to an out-of-trim condition. Therefore, any application of pressure or force to the
controls should be avoided when the autopilot is engaged.
Overpowering the autopilot during flight will cause the autopilot’s automatic trim
to run, resulting in an out-of-trim condition or cause the trim to hit the stop if the
action is prolonged. In this case, larger than anticipated control forces are required
after the autopilot is disengaged.
The following steps should be added to the preflight check:
1) Check for proper autopilot operation and ensure the autopilot can be
overpowered.
2) Note the forces required to overpower the autopilot servo clutches.
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
147
Index
Appendix
Annun/Alerts
Abnormal
Operation
Additional
Features
AFCS
Hazard
Avoidance
Flight
Management
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Abnormal Operation
Blank Page
148
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Annunciations & Alerts
Flight
Flight
Instruments
Instruments
ANNUNCIATIONS & ALERTS
CAS MESSAGES
EISEIS
Warning Messages
Additional Additional
Abnormal
AFCS Features
Features
Operation
Annun/Alerts
Annun/Alerts
OIL PRESS
O2 CYL CLOSED
PARK BRAKE
PRESSU OFF
USP ACTIVE
Loss of GPS navigation. Abort approach
Aural warning system failure due to non-communicating LRUs
Aural warning failure of one LRU
Cabin altitude over 10,000 ft
Cabin pressure differential over 6.2 psi
Pilot or cabin door open
Feathering system failure
Autopilot has activated emergency descent mode
Engine compartment fire (temperature over 200°C; if installed)
Dissymmetry between left- and right-hand flaps
Fuel tank selectors set to “Off”
Fuel pressure below 10 psi
Gears are in an unsafe configuration
Engine start: ITT over 1000°C, 870°C (5 s), or 840°C (20 s)
Engine running: ITT over 840°C
Oil pressure below 60 psi
Oxygen cylinder closed
Parking brake applied
No Bleed air provided to cabin
Underspeed protection is active
AFCS
ITT
Description
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Message
ABORT APR
AURAL WRN FAIL
AURAL WARN 1 CHNL
CABIN ALTITUDE
CABIN DIFF PRESS
DOOR
ELEC FEATH FAULT
EDM
FIRE
FLAPS ASYM
FUEL OFF
FUEL PRESS
GEAR UNSAFE
Caution Messages
Description
APR DWNGRADE
The autopilot is ON while the Yaw Damper is OFF
Approach downgraded , vertical guidance generated by SBAS is
unavailable.
Fuel timer off or out of service
Electric fuel pump running (manual or automatic mode)
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
AUTO SEL
AUX BOOST PMP ON
190-02219-00 Rev. C
Appendix
Appendix
Message
AP ON YD OFF
149
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Annunciations & Alerts
Message
BAT AMP
BAT OFF
CARGO DOOR
CHIP
Description
Battery current over 50 A while on ground
Battery off
Forward cargo door open
Oil chip detector on (if installed)
Electronic Stability and Protection (ESPTM))) angle of attack (AOA)
ESP DEGRADED - AOA
mode is inoperative. The system should be serviced
Electronic Stability and Protection (ESPTM))) indicated air speed (IAS)
ESP DEGRADED - IAS
mode is inoperative. The system should be serviced
The ESP function has failed and is inoperative. The system should be
ESP FAIL
serviced
Fuel tanks imbalanced by more than 15 USGAL for >30 seconds
FUEL IMBALANCE
Fuel quantity less than or equal to 9.1 USGAL in specified tank
FUEL LOW L-R*
Global Air System needs servicing
GAS EVENT
Global Air System failure. The system should be serviced.
GAS DEGRADED
GPU receptacle door not closed
GPU DOOR
The GDU is not receiving status packet from the GWX 68/GWX 70
is reporting a fault. The GWX 68/GWX 70 radar system should be
GWX FAIL
serviced
Ignition exciter running
IGNITION
Inertial separator failure
INERT SEP FAIL
Low fuel level sensor failure for specified tank
LOW LVL FAIL L-R*
Battery voltage below 26 V
LOW VOLTAGE
Starter generator unconnected
MAIN GEN
Generator speed is more than 103%
NG HI
Oil pressure between 60 and 100 psi
OIL PRESS
Oil temperature below 0°C or above 104°C
OIL TEMP
Specified pitot heat (left or right) on while engine off
PITOT HT ON L-R*
Specified pitot heat (left or right) off
PITOT NO HT L-R*
GASC cannot compute optimal cabin altitude (cabin altitude default
PRESSU BACKUP
value is set at 9800 feet)
Prop deice selected and not on
PROP DEICE FAIL
Prop deice on while engine off
PROP DEICE ON
REAR CARGO DOOR The rear cargo door is open
STALL HEAT ON
STALL NO HEAT
150
Stall heat on while engine off
Stall warning heat off
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Annunciations & Alerts
TCAS has failed and is inoperative. The system should be serviced
Traffic has failed and is inoperative. The system should be serviced
Vacuum pressure less than 3.75 in Hg
Cabin altitude high
EISEIS
ADS-B of XPDR1 is inoperative. The transponder may not be receiving
a valid GPS position. Other transponder functions may be available.
Service when possible.
XPDR1 has failed and is inoperative. The system should be serviced
ADS-B of XPDR2 is inoperative. The transponder may not be receiving
a valid GPS position. Other transponder functions may be available.
Service when possible.
XPDR2 has failed and is inoperative. The system should be serviced
XPDR2 FAIL
* Only affected side (L, R, or L-R) displayed in CAS message; applicable messages listed here display
L-R for example
Advisory Messages
Description
Emergency Descent Mode has been overridden by the crew
Electronic Stability and Protection has been disabled on the
Avionics Settings Screen
Inertial separator extended
Cabin pressurization system in MAX DIFF MODE.
Starter generator running
INERT SEP ON
MAX DIFF MODE
STARTER
Additional Additional
Abnormal
AFCS Features
Features
Operation
ESP OFF
AFCS
Message
EDM OVERRIDE
When an LRU or an LRU function fails, a large red “X” is typically displayed on
windows associated with the failed data. Refer to the Daher TBM 910 POH/AFM for
additional information regarding pilot responses to these annunciations
Appendix
Appendix
Comment
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
Air Data, Attitude and Heading Reference System is aligning.
190-02219-00 Rev. C
Annun/Alerts
Annun/Alerts
SYSTEM ANNUNCIATIONS
System Annunciation
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
XPDR1 FAIL
XPDR2 ADS-B FAIL
Description
Flight
Flight
Instruments
Instruments
Message
TCAS FAIL
TRAFFIC FAIL
VACUUM LOW
USE OXYGEN MASK
XPDR1 ADS-B FAIL
151
System Annunciation
Comment
Display system is not receiving attitude information from the AHRS.
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Annunciations & Alerts
AHRS calibration incomplete or configuration module failure.
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
GPS information is either not present or is invalid for navigation
use. Note that AHRS utilizes GPS inputs during normal operation.
AHRS operation may be degraded if GPS signals are not present
(see POH).
Annun/Alerts
Annun/Alerts
Display system is not receiving airspeed input from the air data
computer.
Appendix
Appendix
Display system is not receiving vertical speed input from the air
data computer.
Index
Index
Display system is not receiving valid heading input from the AHRS
or magnetometer.
152
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Annunciations & Alerts
Comment
Flight
Flight
Instruments
Instruments
System Annunciation
EISEIS
Display system is not receiving altitude input from the air data
computer.
Display system is not receiving valid OAT information from the air
data computer.
Display system is not receiving valid transponder information.
Other Various Red X
Indications
A red ‘X’ through any other display field (such as engine
instrumentation fields) indicates that the field is not receiving valid
data.
AFCS
REVERSIONARY SENSOR ANNUNCIATIONS
Condition
BOTH ON ADC1
Both PFDs are displaying data from the number one Air Data Computer.
BOTH ON ADC2
Both PFDs are displaying data from the number two Air Data Computer.
Both PFDs are displaying data from the number one GPS receiver.
BOTH
ON GPS2
Both PFDs are displaying data from the number two GPS receiver.
PFD2 is displaying data from the #1 Air Data Computer.
USING ADC2
PFD1 is displaying data from the #2 Air Data Computer.
USING AHRS1
PFD2 is displaying data from the #1 AHRS.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
USING ADC1
Appendix
Appendix
BOTH
ON GPS1
Annun/Alerts
Annun/Alerts
BOTH ON AHRS2
Both PFDs are displaying data from the number one Attitude & Heading
Reference System.
Both PFDs are displaying data from the number two Attitude & Heading
Reference System.
Additional Additional
Abnormal
AFCS Features
Features
Operation
Reversionary Sensor
Annunciation
BOTH ON AHRS1
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Display system is not receiving valid ISA information from the air
data computer.
153
Reversionary Sensor
Annunciation
Condition
USING AHRS2
PFD1 is displaying data from the #2 AHRS.
USING
GPS1
PFD2 is displaying data from the #1 GPS.
USING
GPS2
PFD1 is displaying data from the #2 GPS.
COMPARATOR ANNUNCIATIONS
Comparator
Annunciation
Difference in altitude sensors is > 200 ft.
IAS
If both airspeed sensors detect < 35 knots, this is inhibited.
If either airspeed sensor detects > 35 knots, and the difference in sensors is >
10 knots.
If either airspeed sensor detects > 80 knots, and the difference in sensors is >
7 knots.
HDG
Difference in heading sensors is > 6 degrees.
Additional Additional
Abnormal
Features
Operation
Features AFCS
Annun/Alerts
Annun/Alerts
PIT
Difference in pitch sensors is > 5 degrees.
ROL
Difference in roll sensors is > 6 degrees.
VDI
Difference in temperature compensated altitudes is > 50 ft.
ALT
No data from one or both altitude sensors.
IAS
No data from one or both airspeed sensors.
HDG
No data from one or both heading sensors.
PIT
No data from one or both pitch sensors.
ROL
No data from one or both roll sensors.
VDI
No temperature compensated altitude data available.
Index
Index
Appendix
Appendix
Condition
ALT
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Annunciations & Alerts
154
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Annunciations & Alerts
Flight
Flight
Instruments
Instruments
TERRAIN-SVT ALERTS
TERRAIN
WARNING - TERRAIN
“Warning; Terrain,
Terrain”
Imminent Terrain Impact
Warning (ITI)
TERRAIN
WARNING - TERRAIN
“Warning; Terrain,
Terrain”
Reduced Required Obstacle
Clearance Warning (ROC)
TERRAIN
WARNING - OBSTACLE
“Warning; Obstacle,
Obstacle”
Imminent Obstacle Impact
Warning (IOI)
TERRAIN
WARNING - OBSTACLE
“Warning; Obstacle,
Obstacle”
Reduced Required Terrain
Clearance Caution (RTC)
TERRAIN
CAUTION - TERRAIN
“Caution; Terrain,
Terrain”
Imminent Terrain Impact
Caution (ITI)
TERRAIN
CAUTION - TERRAIN
“Caution; Terrain,
Terrain”
Reduced Required Obstacle
Clearance Caution (ROC)
TERRAIN
CAUTION - OBSTACLE
“Caution; Obstacle,
Obstacle”
Imminent Obstacle Impact
Caution (IOI)
TERRAIN
CAUTION - OBSTACLE
“Caution; Obstacle,
Obstacle”
TERRAIN-SVT SYSTEM STATUS ANNUNCIATIONS
TER TEST
TERRAIN TEST
None
None
None
“Terrain
System Test
OK”
Terrain Alerting Inhibited
TER INH
None
None
No GPS position
TER N/A
NO GPS POSITION
“Terrain
System Not
Available”*
Excessively degraded GPS signal;
or Out of database coverage
area
TER N/A
None
“Terrain
System Not
Available”*
System Test in Progress
System Test Pass
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
155
Index
Index
Voice Alert
Appendix
Appendix
Terrain-SVT Page Center
Banner Annunciation
Annun/Alerts
Annun/Alerts
PFD/MFD†
Alert
Annunciation
Alert Type
Additional Additional
Abnormal
AFCS Features
Features
Operation
Reduced Required Terrain
Clearance Warning (RTC)
AFCS
Voice Alert
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
MFD
Pop-Up Alert (except
Terrain-SVT Page)
EISEIS
PFD/MFD* Alert
Annunciation
Alert Type
Annunciations & Alerts
Terrain-SVT Page Center
Banner Annunciation
Voice Alert
Terrain System Test Fail; Terrain
or Obstacle database unavailable
or invalid; Invalid software
configuration; or System audio
fault
TER FAIL
TERRAIN FAIL
“Terrain
System
Failure”
MFD Terrain or Obstacle
database unavailable or invalid,
TERRAIN DATABASE FAILURE
and Terrain-SVT operating
None
None
with PFD Terrain or Obstacle
databases
† Annunciation is shown on Terrain-SVT Page and the Navigation Map Page when Terrain is enabled.
* “Terrain System Available” will be heard when sufficient GPS signal is received, or Terrain database
coverage area re-entered.
TAWS-B ALERTS
Alert Type
PFD/MFD**
TAWS Page
Annunciation
MFD Map Page
Pop-Up Alert
Voice Message
Excessive
Descent Rate
Warning
(EDR)
PULL UP
PULL-UP
“Pull Up”
PULL UP
TERRAIN - PULL-UP
or
TERRAIN AHEAD - PULL-UP
“Terrain, Terrain; Pull Up,
Pull Up”
or
“Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”*
PULL UP
TERRAIN - PULL-UP
or
TERRAIN AHEAD - PULL-UP
“Terrain, Terrain; Pull Up,
Pull Up”*
or
“Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
Reduced
Required
Terrain
Clearance
Warning
(RTC)
Imminent
Terrain
Impact
Warning (ITI)
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Alert Type
PFD/MFD†
Alert
Annunciation
156
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Annunciations & Alerts
MFD Map Page
Pop-Up Alert
Voice Message
PULL UP
OBSTACLE - PULL-UP
or
OBSTACLE AHEAD - PULL-UP
*
“Obstacle, Obstacle; Pull
Up, Pull Up”
or
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”*
PULL UP
OBSTACLE - PULL-UP
or
OBSTACLE AHEAD - PULL-UP
“Obstacle, Obstacle; Pull
Up, Pull Up”*
or
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
TERRAIN
CAUTION - TERRAIN
or
TERRAIN AHEAD
“Caution, Terrain;
Caution, Terrain”
or
“Terrain Ahead; Terrain
Ahead”*
TERRAIN
CAUTION - TERRAIN
or
TERRAIN AHEAD
“Caution, Terrain;
Caution, Terrain”*
or
“Terrain Ahead; Terrain
Ahead”
TERRAIN
CAUTION - OBSTACLE
or
OBSTACLE AHEAD
“Caution, Obstacle;
Caution, Obstacle”
or
“Obstacle Ahead;
Obstacle Ahead”*
Imminent
Obstacle
Impact
Caution (IOI)
TERRAIN
CAUTION - OBSTACLE
or
OBSTACLE AHEAD
“Caution, Obstacle;
Caution, Obstacle”*
or
“Obstacle Ahead;
Obstacle Ahead”
Premature
Descent
Alert Caution
(PDA)
TERRAIN
TOO LOW - TERRAIN
“Too Low, Terrain”
Reduced
Required
Terrain
Clearance
Caution (RTC)
Additional Additional
Abnormal
AFCS Features
Features
Operation
Reduced
Required
Obstacle
Clearance
Caution
(ROC)
AFCS
Imminent
Terrain
Impact
Caution (ITI)
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Imminent
Obstacle
Impact
Warning (IOI)
EISEIS
Reduced
Required
Obstacle
Clearance
Warning
(ROC)
Flight
Flight
Instruments
Instruments
PFD/MFD**
TAWS Page
Annunciation
Alert Type
Annun/Alerts
Annun/Alerts
Appendix
Appendix
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
157
Alert Type
PFD/MFD**
TAWS Page
Annunciation
MFD Map Page
Pop-Up Alert
Voice Message
Altitude Voice
Callout (VCO)
“500”
None
None
“Five-Hundred”
Excessive
Descent Rate
Caution (EDR)
TERRAIN
SINK RATE
“Sink Rate”
TERRAIN
DONT SINK
or
TOO LOW - TERRAIN
“Don’t Sink”*
or
“Too Low, Terrain”
Negative
Climb Rate
Caution
(NCR)
* Alerts with multiple messages are configurable at installation and are installation-dependent. Alerts
for the default configuration when more than one option is available are indicated with asterisks.
** Annunciation is displayed on the MFD when terrain display is enabled.
TAWS-B SYSTEM STATUS ANNUNCIATIONS
Alert Type
PFD/MFD Alert
Annunciation
TAWS-B Page Annunciation
Aural Message
TAWS TEST
None
None
“TAWS System
Test Test OK”
None
None
NO GPS POSITION
“TAWS Not
Available”
Excessively degraded
GPS signal; or Out of
database coverage area
None
“TAWS Not
Available”
TAWS-B System Test
Fail; Terrain or Obstacle
database unavailable or
invalid; Invalid software
configuration; or System
audio fault
TAWS FAIL
“TAWS System
Failure”
System Test in progress
System Test pass
TAWS-B FLTA Alerting
Inhibited
No GPS position
None
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Annunciations & Alerts
158
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Annunciations & Alerts
TAWS-B Page Annunciation
Aural Message
MFD Terrain or Obstacle
database unavailable or
invalid. TAWS operating
with PFD Terrain or
Obstacle databases
None
TERRAIN DATABASE FAILURE
None
EISEIS
PFD/MFD Alert
Annunciation
GDL 69A SXM DATA LINK RECEIVER MESSAGES
Message Location
Description
CHECK ANTENNA
XM Information Page (MFD)
Data Link Receiver antenna
error; service required
UPDATING
XM Information Page (MFD))
Data Link Receiver updating
encryption code
NO SIGNAL
XM Information Page Weather Loss of signal; signal strength
Datalink Page (MFD)
too low for receiver
Acquiring channel audio or
information
OFF AIR
XM Radio Page (MFD)
Channel not in service
--------
XM Radio Page (MFD)
Missing channel information
WEATHER DATA LINK FAILED
No communication from Data
Weather Datalink Page (MFD) Link Receiver within last 5
minutes
XM Information Page (MFD)
Sirius SXM subscription is not
activated
DETECTING ACTIVATION
Weather Datalink Page (MFD)
Sirius SXM subscription is
activating.
Sirius SXM subscription
Weather Datalink Page (MFD) confirmed downloading
weather data.
Appendix
Appendix
WAITING FOR DATA...
Annun/Alerts
Annun/Alerts
ACTIVATION REQUIRED
Additional Additional
Abnormal
AFCS Features
Features
Operation
XM Radio Page (MFD)
AFCS
Message
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
† Annunciation is shown on TAWS-B Page and the Navigation Map Page when Terrain is enabled.
* “TAWS Available” will be heard when sufficient GPS signal is received, or Terrain database coverage area re-entered.
LOADING
Flight
Flight
Instruments
Instruments
Alert Type
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
159
AFCS ALERTS
Condition
Annunciation Description
Pitch Failure
PTCH
Pitch axis control failure. AP is inoperative.
Roll Failure
ROLL
Roll axis control failure. AP is inoperative.
PTRM
If annunciated when AP is engaged, take control of the
aircraft and disengage the autopilot. If annunciated
when AP is not engaged, move each half of the MEPT
switch separately to check if a stuck switch is causing the
annunciation.
(or stuck MEYT
Switch)
Yaw Damper
Failure
YTRM
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
YAW
YD control failure; AP also inoperative
System Failure
AFCS
AP and MEPT are unavailable. FD may still be available.
Elevator Mistrim
Up
↑ELE
A condition has developed causing the pitch servo to
provide a sustained force. Be prepared to apply nose up
control wheel force upon autopilot disconnect.
↓ELE
A condition has developed causing the pitch servo to
provide a sustained force. Be prepared to apply nose down
control wheel force upon autopilot disconnect.
Aileron Mistrim
Left
←AIL
A condition has developed causing the roll servo to provide
a sustained left force. Ensure the slip/skid indicator is
centered and observe any maximum fuel imbalance limits.
Aileron Mistrim
Right
AIL→
A condition has developed causing the roll servo to provide a
sustained right force. Ensure the slip/skid indicator is centered
and observe any maximum fuel imbalance limits.
Rudder Mistrim
Left
←RUD
A condition has developed causing the yaw servo to provide
a sustained force. Ensure the slip/skid indicator is centered
and observe any maximum fuel imbalance limits.
Rudder Mistrim
Right
RUD→
A condition has developed causing the yaw servo to
provide a sustained force. Ensure the slip/skid indicator is
centered and observe any maximum fuel imbalance limits.
MEPT Switch
Stuck, or Pitch
Trim Axis Control
Failure
Yaw Trim Failure
Elevator Mistrim
Down
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Annunciations & Alerts
160
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Annunciations & Alerts
Annunciation Description
PFT
Preflight system test has failed.
VOICE ALERTS
“Airspeed”
Played when the indicated airspeed is below a given threshold for a
given aircraft configuration. Note, this alert may be heard under normal
conditions during the landing flare.
“Aural Warning OK”
Played when both audio paths are OK, following a previous audio path or
audio processing issue.
“Engaging Autopilot”
Played when ESP has been engaged for more than 10 seconds cumulative
of a 20 second interval, and the autopilot is automatically engaged.
“Incoming Call”
Satellite telephone is receiving a call.
“Landing Gear, Landing Gear” Gear up in landing condition.
“Minimums, minimums”
The aircraft has descended below the preset barometric minimum
descent altitude.
“Overspeed, Overspeed”
Airspeed has exceeded 265 Kts.
Combination of airplane in stall condition and gear up in landing
condition.
“Stall, Stall”
Annun/Alerts
Annun/Alerts
“Stall, Landing Gear”
Airplane in stall condition.
“Traffic”
Played when a Traffic Advisory (TA) is issued with the TIS system.
The aircraft is outside the Traffic Information Service (TIS) coverage area.
“Traffic, Traffic”
Played when a Traffic Advisory (TA) is issued with a TAS system.
Played when the TAS system fails a pilot-initiated self test.
“TAS System Test Passed”
Played when the TAS system passes a pilot-initiated self test.
“Use Oxygen Mask, Use
Oxygen Mask”
Played in conjuction with associated CAS messages when cabin altiude
exceeds 10,000 ft.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
161
Index
Index
“TAS System Test Failed”
Appendix
Appendix
“TIS Not Available”
Additional Additional
Abnormal
AFCS Features
Features
Operation
Description
AFCS
Voice Alert
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
PFT
EISEIS
Preflight Test
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.
Flight
Flight
Instruments
Instruments
Condition
Annunciations & Alerts
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Voice Alert
Description
“Vertical track”
The aircraft is one minute from Top of Descent. Issued only when vertical
navigation is enabled.
“One o’clock” through
“Twelve o’clock” or “No
Bearing”
Played to indicate bearing of traffic from own aircraft (GTS 820 only).
“High”, “Low”, “Same
Played to indicate altitude of traffic relative to own aircraft (GTS 820
Altitude” (if within 200 feet of only).
own altitude), or “Altitude not
available”
“Less than one mile”,
“One Mile” through “Ten
Miles”, or “More than ten
miles”
Played to indicate distance of traffic from own aircraft (GTS 820 only).
SYSTEM MESSAGE ADVISORIES
Message
Comments
ADC1 ALT EC – ADC1 altitude
error correction is unavailable.
GDC1 is reporting that the altitude error correction is
unavailable.
ADC1 AS EC – ADC1 airspeed
error correction is unavailable.
GDC1 is reporting that the airspeed error correction is
unavailable.
ADC2 ALT EC – ADC2 altitude
error correction is unavailable.
GDC2 is reporting that the altitude error correction is
unavailable.
ADC2 AS EC – ADC2 airspeed
error correction is unavailable.
GDC2 is reporting that the airspeed error correction is
unavailable.
AHRS MAG DB – AHRS magnetic The #1 AHRS and #2 AHRS magnetic model database versions
model database version mismatch. do not match.
AHRS1 CAL – AHRS1 calibration
version error. Srvc req’d.
The AHRS1 calibration version error. The system should be
serviced.
AHRS1 CONFIG– AHRS1 config
error. Config service req’d.
AHRS configuration settings do not match those of backup
configuration memory. The system should be serviced.
AHRS1 GPS – AHRS1 not
receiving any GPS information.
The #1 AHRS is not receiving any or any useful GPS
information. Check AFMS limitations. The system should be
serviced.
AHRS1 GPS – AHRS1 not
The #1 AHRS is not receiving backup GPS information. The
receiving backup GPS information. system should be serviced.
162
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190-02219-00 Rev. C
Annunciations & Alerts
Comments
Flight
Flight
Instruments
Instruments
Message
The #1 AHRS is operating exclusively in no-GPS mode. The
system should be serviced.
AHRS1 GPS – AHRS1 using
backup GPS source.
The #1 AHRS is using the backup GPS path. Primary GPS path
has failed. The system should be serviced when possible.
AHRS1 SRVC – AHRS1 Magneticfield model needs update.
The #1 AHRS earth magnetic field model is out of date.
Update magnetic field model when practical.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
AHRS1 TAS – AHRS1 not receiving The #1 AHRS is not receiving true airspeed from the air data
airspeed.
computer. The AHRS relies on GPS information to augment
the lack of airspeed. The system should be serviced.
AHRS2 CAL – AHRS2 calibration
version error. Srvc req’d.
The AHRS2 calibration version error. The system should be
serviced.
AHRS2 CONFIG– AHRS2 config
error. Config service req’d.
AHRS configuration settings do not match those of backup
configuration memory. The system should be serviced.
AHRS2 GPS – AHRS2 not
receiving any GPS information.
The #2 AHRS is not receiving any or any useful GPS
information. Check AFMS limitations. The system should be
serviced.
AFCS
AHRS2 GPS – AHRS2 not
The #2 AHRS is not receiving backup GPS information. The
receiving backup GPS information. system should be serviced.
The #2 AHRS is operating exclusively in no-GPS mode. The
system should be serviced.
AHRS2 GPS – AHRS2 using
backup GPS source.
The #2 AHRS is using the backup GPS path. Primary GPS path
has failed. The system should be serviced when possible.
AHRS2 SRVC – AHRS2 Magneticfield model needs update.
The #2 AHRS earth magnetic field model is out of date.
Update magnetic field model when practical.
Annun/Alerts
Annun/Alerts
AHRS2 TAS – AHRS2 not receiving The #2 AHRS is not receiving true airspeed from the air data
airspeed.
computer. The AHRS relies on GPS information to augment
the lack of airspeed. The system should be serviced.
APR ADVISORY – SBAS VNAV not SBAS is not available. The system is calculating the VNAV
available. Using Baro VNAV.
profile using Baro VNAV.
Special use airspace is ahead of aircraft. The aircraft will
penetrate the airspace within 10 minutes.
ARSPC NEAR – Airspace near –
less than 2 nm.
Special use airspace is within 2 nm of the aircraft position.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
ARSPC AHEAD – Airspace ahead
less than 10 minutes.
Appendix
Appendix
The system notifies the pilot that the loaded approach is not
active. Activate approach when required.
Additional Additional
Abnormal
AFCS Features
Features
Operation
AHRS2 GPS – AHRS2 operating
exclusively in no-GPS mode.
APR INACTV – Approach is not
active.
EISEIS
AHRS1 GPS – AHRS1 operating
exclusively in no-GPS mode.
163
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Annunciations & Alerts
Message
Comments
ARSPC NEAR – Airspace near and
Special use airspace is near and ahead of the aircraft position.
ahead.
AUDIO MANIFEST Audio software mismatch,
communication halted.
The GDC 74B has incorrect software installed. The system
should be serviced.
CHECK CRS – Database course
for LOC1 / [LOC ID] is [CRS]°.
Selected course for LOC1 differs from published localizer
course by more than 10 degrees.
CHECK CRS – Database course
for LOC2 / [LOC ID] is [CRS]°.
Selected course for LOC2 differs from published localizer
course by more than 10 degrees.
CNFG MODULE – PFD1
configuration module is
inoperative.
The PFD1 configuration module backup memory has failed.
The system should be serviced.
COM1 CONFIG – COM1 config
error. Config service req’d.
The COM1 configuration settings do not match backup
configuration memory. The system should be serviced.
COM 1 MANIFEST –
COM1 software mismatch,
communication halted.
The COM1 has incorrect software installed. The system
should be serviced.
COM1 PTT – COM1 push-to-talk
key is stuck.
The COM1 external push-to-talk switch is stuck in the enable
(or “pressed”) position. Press the PTT switch again to cycle
its operation.
If the problem persists, the system should be serviced.
COM1 RMT XFR – COM1 remote
transfer key is stuck.
The COM1 transfer switch is stuck in the enabled (or
“pressed”) position. Press the transfer switch again to cycle
its operation. If the problem persists, the system should be
serviced.
COM1 SERVICE – COM1 needs
service. Return unit for repair.
The system has detected a failure in COM1. COM1 may still
be usable. The system should be serviced when possible.
COM1 TEMP – COM1 over temp.
Reducing transmitter power.
The system has detected an over temperature condition in
COM1. The transmitter is operating at reduced power. If the
problem persists, the system should be serviced.
COM2 CONFIG – COM2 config
error. Config service req’d.
The COM2 configuration settings do not match backup
configuration memory. The system should be serviced.
COM 2 MANIFEST –
COM2 software mismatch,
communication halted.
The COM2 has incorrect software installed. The system
should be serviced.
164
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Annunciations & Alerts
Comments
COM2 RMT XFR – COM2 remote
transfer key is stuck.
The 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 system should be
serviced.
COM2 SERVICE – COM2 needs
service. Return unit for repair.
The system has detected a failure in COM2. COM2 may still
be usable. The system should be serviced when possible.
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
The system has detected an over temperature condition in
COM2. The transmitter is operating at reduced power. If the
problem persists, the system should be serviced.
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.
DB CHANGE – Database
changed. Verify stored airways.
This occurs when a stored flight plan contains an airway that
is no longer consistent with the navigation database. This
alert is issued only after an navigation database update.
Verify use of airways in stored flight plans and reload airways
as needed.
DB MISMATCH – Navigation
database mismatch. Xtalk is off.
The PFDs and MFD have different navigation database versions
or regions installed. Crossfill is off. Check the Aux-System
Status Page to determine versions or regions. Also, check
the Aux-System Status Page for a database synchronization
function not completed. After synchronization is complete,
power must be turned off, then on.
Appendix
Appendix
This occurs when a stored flight plan contains procedures that
have been manually edited. This alert is issued only after an
navigation database update. Verify that the user-modified
procedures in stored flight plans are correct and up to date.
Annun/Alerts
Annun/Alerts
DB CHANGE – Database
changed. Verify user modified
procedures.
Additional Additional
Abnormal
AFCS Features
Features
Operation
The pilot profile data was lost. System reverts to default pilot
profile and settings. The pilot may reconfigure the MFD &
PFDs with preferred settings, if desired.
AFCS
DATA LOST – Pilot stored data
was lost. Recheck settings.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
The 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 system should be serviced.
EISEIS
COM2 PTT – COM2 push-to-talk
key is stuck.
Flight
Flight
Instruments
Instruments
Message
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
165
Message
The PFDs and MFD have different obstacle database versions
or regions installed. Check the Aux-System Status Page to
determine versions or regions. Also, check the Aux-System
Status Page for a database synchronization function not
completed. After synchronization is complete, power must be
turned off, then on.
DB MISMATCH – Standby
Navigation database mismatch.
The PFDs and MFD have different standby navigation database
versions or regions installed. Check the Aux-System Status
Page to determine versions or regions. Also, check the AuxSystem Status Page for a database synchronization function
not completed. After synchronization is complete, power must
be turned off, then on.
DB MISMATCH – Terrain
database mismatch.
The PFDs and MFD have different terrain database versions
or regions installed. Check the Aux-System StatusPage to
determine versions or regions. Also, check the Aux-System
Status Page for a database synchronization function not
completed. After synchronization is complete, power must be
turned off, then on.
DME CHECK RANGE – DME
range disagreement. Check
position sensors.
A failure or disagreement has been detected in a DME
receiver. Check position sensors.
ECS – Service required.
The Environmental Control System has failed.
EPS – Service required.
Electrical Power System needs servicing.
EPS – S/G speed sensor failed.
Starter Generator speed sensor has failed.
ESP CONFIG– ESP config error.
Config service req’d.
ESP is not configured properly. The system should be serviced.
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
AFCS
Additional Additional
Abnormal
Features
Operation
Features AFCS
Annun/Alerts
Annun/Alerts
EXCEEDANCE – Exceedance data
is being logged.
An exceedance log has been captured.
FAILED PATH – A data path has
failed.
A data path connected to the GDU or the GIA 63/W has
failed.
Index
Index
Appendix
Appendix
Comments
DB MISMATCH – Obstacle
database mismatch.
EISEIS
Flight
Flight
Instruments
Instruments
Annunciations & Alerts
166
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190-02219-00 Rev. C
Annunciations & Alerts
Comments
FPL WPT MOVE – Flight plan
waypoint moved.
The system has detected that a waypoint coordinate has
changed due to a new navigation database update. Verify
that stored flight plans contain correct waypoint locations.
FPL TRUNC – Flight plan has been This occurs when a newly installed navigation database
truncated.
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.
AFCS
FS510 CARD ERROR – FS510 not The SD card was removed from the bottom card slot of the
detected in MFD Bottom Slot.
MFD. The SD card needs to be reinserted.
G/S2 FAIL – G/S2 is inoperative.
A failure has been detected in glideslope receiver 2. The
system should be serviced.
G/S2 SERVICE – G/S2 needs
service. Return unit for repair.
A failure has been detected in glideslope receiver 2. The
receiver may still be available. The system should be serviced
when possible.
GCU CNFG – GCU Config error.
Config service req’d.
GCU 475 configuration settings do not match those of backup
configuration memory. The system should be serviced.
GCU FAIL – GCU is inoperative.
A failure has been detected in the GCU 475. The GCU 475 is
unavailable.
GCU KEYSTK – GCU [key name]
Key is stuck.
A key is stuck on the GCU 475 bezel. Attempt to free the
stuck key by pressing it several times. The system should be
serviced if the problem persists.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
A failure has been detected in glideslope receiver 1. The
receiver may still be available. The system should be serviced
when possible.
Appendix
Appendix
G/S1 SERVICE – G/S1 needs
service. Return unit for repair.
Annun/Alerts
Annun/Alerts
A failure has been detected in glideslope receiver 1. The
system should be serviced.
Additional Additional
Abnormal
AFCS Features
Features
Operation
G/S1 FAIL – G/S1 is inoperative.
190-02219-00 Rev. C
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Upon power-up, the system detects that a stored flight plan
waypoint is locked. This occurs when an navigation database
update eliminates an obsolete waypoint. The flight plan
cannot find the specified waypoint and flags this message.
This can also occur with user waypoints in a flight plan that
is deleted.
Remove the waypoint from the flight plan if it no longer exists
in any database,
Or
update the waypoint name/identifier to reflect the new
information.
EISEIS
FPL WPT LOCK – Flight plan
waypoint is locked.
Flight
Flight
Instruments
Instruments
Message
167
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Annunciations & Alerts
Message
Comments
GCU MANIFEST – GCU software
mismatch, communication halted.
The GCU 475 has incorrect software installed. The system
should be serviced.
GDC1 MANIFEST – GDC1
software mismatch,
communication halted.
The GDC 74B has incorrect software installed. The system
should be serviced.
GDC2 MANIFEST – GDC2
software mismatch,
communication halted.
The GDC 74B has incorrect software installed. The system
should be serviced.
GDL MANIFEST – GDL software
mismatch, communication halted.
The GDL 69A SXM has incorrect software installed. The
system should be serviced.
GDL69 CONFIG – GDL 69 config
error. Config service req’d.
GDL 69A SXM configuration settings do not match those of
backup configuration memory. The system should be serviced.
GDL69 FAIL – GDL 69 has failed.
A failure has been detected in the GDL 69A SXM. The
receiver is unavailable. The system should be serviced
GEA1 CONFIG – GEA1 config
error. Config service req’d.
The GEA1 configuration settings do not match those of
backup configuration memory. The system should be serviced.
GEA1 MANIFEST – GEA1
software mismatch,
communication halted.
The #1 GEA 71 has incorrect software installed. The system
should be serviced.
GEA2 CONFIG – GEA2 config
error. Config service req’d.
The GEA2 configuration settings do not match those of
backup configuration memory. The system should be serviced.
GEA2 MANIFEST – GEA2
software mismatch,
communication halted.
The #2 GEA 71 has incorrect software installed. The system
should be serviced.
GEO LIMITS – AHRS1 too
far North/South, no magnetic
compass.
GEO LIMITS – AHRS2 too
far North/South, no magnetic
compass.
The aircraft is outside geographical limits for approved AHRS
operation. Heading is flagged as invalid.
GFC MANIFEST – GFC software
mismatch, communication halted.
Incorrect servo software is installed, or gain settings are
incorrect.
GIA1 CONFIG – GIA1 audio
config error. Config service req’d.
The GIA1 have an error in the audio configuration. The
system should be serviced.
GIA1 CONFIG – GIA1 config error. The GIA1 configuration settings do not match backup
Config service req’d.
configuration memory. The system should be serviced.
168
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Annunciations & Alerts
Comments
The GIA1 temperature is too high. If problem persists, the
system should be serviced.
GIA1 COOLING – GIA1
temperature too low.
he GIA1 configuration settings do not match backup
configuration memory. The system should be serviced.
GIA1 MANIFEST – GIA1 software The GIA1 has incorrect software installed. The system should
mismatch, communication halted. be serviced.
The GIA1 self-test has detected a problem in the unit. The
system should be serviced.
GIA2 CONFIG – GIA2 config error. The GIA2 configuration settings do not match backup
Config service req’d.
configuration memory. The system should be serviced.
GIA2 CONFIG – GIA2 audio
config error. Config service req’d.
The GIA2 have an error in the audio configuration. The
system should be serviced.
GIA2 COOLING – GIA2
temperature too low.
The GIA2 temperature is too low to operate correctly. Allow
units to warm up to operating temperature.
GIA2 COOLING – GIA2 over
temperature.
The GIA2 temperature is too high. If problem persists, the
system should be serviced.
GMA XTALK – GMA crosstalk
error has occurred.
An error has occurred in transferring data between the two
GMAs. The system should be serviced.
GMA1 AUX MANIFEST – GMA
1 AUX software mismatch,
communication halted.
The digital audio controller has incorrect software installed.
The system should be serviced.
GMA1 CONFIG – GMA1 config
error. Config service req’d.
The audio panel configuration settings do not match backup
configuration memory. The system should be serviced.
GMA1 FAIL – GMA1 is
inoperative.
The audio panel self-test has detected a failure. The audio
panel is unavailable. The system should be serviced.
GMA1 SERVICE – GMA1 needs
service. Return unit for repair.
The audio panel self-test has detected a problem in the unit.
Certain audio functions may still be available, and the audio
panel may still be usable. The system should be serviced when
possible.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
190-02219-00 Rev. C
The audio panel has incorrect software installed. The system
should be serviced.
Appendix
Appendix
GMA1 MANIFEST – GMA1
software mismatch, communication
halted.
Annun/Alerts
Annun/Alerts
The GIA2 self-test has detected a problem in the unit. The
system should be serviced.
Additional Additional
Abnormal
AFCS Features
Features
Operation
GIA2 SERVICE – GIA2 needs
service. Return the unit for repair.
AFCS
GIA2 MANIFEST – GIA2 software The GIA 2 has incorrect software installed. The system should
mismatch, communication halted. be serviced.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
GIA1 SERVICE – GIA1 needs
service. Return the unit for repair.
EISEIS
GIA1 COOLING – GIA1 over
temperature.
Flight
Flight
Instruments
Instruments
Message
169
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Annunciations & Alerts
Message
Comments
GMA2 CONFIG – GMA2 config
error. Config service req’d.
The audio panel configuration settings do not match backup
configuration memory. The system should be serviced.
GMA2 FAIL – GMA2 is
inoperative.
The audio panel self-test has detected a failure. The audio
panel is unavailable. The system should be serviced.
GMA2 MANIFEST – GMA2
software mismatch, communication
halted.
GMA2 SERVICE – GMA2 needs
service. Return unit for repair.
GMC CONFIG – GMC Config
error. Config service req’d.
The audio panel has incorrect software installed. The system
should be serviced.
The audio panel self-test has detected a problem in the unit.
Certain audio functions may still be available, and the audio
panel may still be usable. The system should be serviced when
possible.
Error in the configuration of the GMC 710.
GMC FAIL – GMC is inoperative.
A failure has been detected in the GMC 710. The GMC 710
is unavailable.
GMC KEYSTK – GMC [key name]
Key is stuck.
A key is stuck on the GMC 710 bezel. Attempt to free the
stuck key by pressing it several times. The system should be
serviced if the problem persists.
GMC MANIFEST – GMC software The GMC 710 has incorrect software installed. The system
mismatch. Communication halted. should be serviced.
GMU1 MANIFEST –
GMU1 software mismatch,
communication halted.
The GMU 44 has incorrect software installed. The system
should be serviced.
GMU2 MANIFEST –
GMU2 software mismatch,
communication halted.
he GMU 44 has incorrect software installed. The system
should be serviced.
GPS NAV LOST – Loss of GPS
navigation. Insufficient satellites.
Loss of GPS navigation due to insufficient satellites.
GPS NAV LOST – Loss of GPS
navigation. Position error.
Loss of GPS navigation due to position error.
GPS NAV LOST – Loss of GPS
navigation. GPS fail.
Loss of GPS navigation due to GPS failure.
GPS1 SERVICE – GPS1 needs
service. Return unit for repair.
GPS2 SERVICE – GPS2 needs
service. Return unit for repair.
170
A failure has been detected in the GPS1 and/or GPS2 receiver.
The receiver may still be available. The system should be
serviced.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Annunciations & Alerts
Comments
Flight
Flight
Instruments
Instruments
Message
GRA1 has improper calibration. The system should be
serviced.
GRA1 CONFIG – GRA1 config
error. Config service req’d.
The GRA and GDU have incompatible configurations.
GRA1 MANIFEST – GRA1
software mismatch,
communication halted.
The GRA has incorrect software installed. The system should
be serviced.
GRA1 SERVICE – GRA1 needs
service. Return unit for repair
The GRA self-test has detected a problem in the unit. The
system should be serviced.
GRA1 TEMP – GRA1 over
temperature.
The system has detected an over temperature condition in
GRA1.
GRS1 CONFIG – GRS1 config
error. Config service req’d.
GRS configuration settings do not match those of backup
configuration memory. The system should be serviced.
GRS1 MANIFEST – GRS1
software mismatch,
communication halted.
The #1 AHRS has incorrect software installed. The system
should be serviced.
GRS2 CONFIG – GRS2 config
error. Config service req’d.
GRS configuration settings do not match those of backup
configuration memory. The system should be serviced.
GRS2 MANIFEST – GRS2
software mismatch,
communication halted.
The #2 AHRS has incorrect software installed. The system
should be serviced.
AFCS
The AHRS1 should be serviced when practical.
Additional Additional
Abnormal
AFCS Features
Features
Operation
A failure has been detected in the #1 GSR 56. The system
should be serviced.
GTS CONFIG – GTS config error.
Config service req’d.
The GTS and GDU have incompatible configurations. This
alert is also set when the GTS has an invalid mode S address
configured or the mode S address does not match both XPDR
mode S addresses.
GTS MANIFEST – GTS software
mismatch, communication halted.
The GTS has incorrect software installed. The system should
be serviced.
GTX1 MANIFEST – GTX1
software mismatch,
communication halted.
The transponder has incorrect software installed. The system
should be serviced.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
171
Index
Index
GSR1 FAIL – GSR1 has failed.
Appendix
Appendix
The AHRS1 should be serviced when practical.
Annun/Alerts
Annun/Alerts
GRS2 SERVICE – GRS1 needs
service. Return unit for repair.
190-02219-00 Rev. C
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
GRS1 SERVICE – GRS1 needs
service. Return unit for repair.
EISEIS
GRA1 CAL – GRA1 calibration.
Service req’d.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Annunciations & Alerts
Message
GTX2 MANIFEST – GTX2
software mismatch,
communication halted.
GWX CONFIG – GWX config
error. Config service req’d.
Comments
The transponder has incorrect software installed. The system
should be serviced.
GWX 68 or GWX 70 configuration settings do not match
those of the GDU configuration. The system should be
serviced.
GWX MANIFEST – GWX software The GWX 68/GWX 70 has incorrect software installed. The
mismatch, communication halted. system should be serviced.
GWX SERVICE – GWX needs
service. Return unit for repair.
A failure has been detected in the GWX 68 or GWX 70. The
GWX 68 or GWX 70may still be usable.
HDG FAULT – AHRS1
magnetometer fault has occurred.
A fault has occurred in the #1 GMU 44. Heading is flagged
as invalid. The AHRS uses GPS for backup mode operation.
The system should be serviced.
HDG FAULT – AHRS2
magnetometer fault has occurred.
A fault has occurred in the #2 GMU 44. Heading is flagged
as invalid. The AHRS uses GPS for backup mode operation.
The system should be serviced.
HOLD EXPIRED – Holding EFC
time expired.
Expect Further Clearance (EFC) time has expired for the User
Defined Hold.
HW MISMATCH – GIA hardware
mismatch. GIA1 communication
halted.
A GIA mismatch has been detected, where only one is SBAS
capable.
HW MISMATCH – GIA hardware
mismatch. GIA2 communication
halted.
A GIA mismatch has been detected, where only one is SBAS
capable.
INSIDE ARSPC – Inside airspace.
The aircraft is inside the special use airspace.
INVALID ADM – Invalid ADM:
ATN communication halted.
Data link avionics were not configured correctly and therefore
will not be able to communicate with the ground network.
LOCKED FPL – Cannot navigate
locked flight plan.
This occurs when the pilot attempts to activate a stored flight
plan that contains locked waypoint. Remove locked waypoint
from flight plan. Update flight plan with current waypoint.
LOI – GPS integrity lost.
Crosscheck with other NAVS.
GPS integrity is insufficient for the current phase of flight.
LOSS OF GPS NAVIGATION –
Poor Satellite Coverage.
Loss of GPS navigation due to insufficient/poor satellite
coverage.
LOW BANK ACTIVE – Disengage
for approach.
Low Bank mode is active. Disengage to continue approach.
172
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Annunciations & Alerts
Comments
Flight
Flight
Instruments
Instruments
Message
LRG MAG VAR – Verify all course
angles.
The GDU’s internal model cannot determine the exact
magnetic variance for geographic locations near the magnetic
poles. Displayed magnetic course angles may differ from the
actual magnetic heading by more than 2°.
MFD1 CONFIG – MFD1 config
error. Config service req’d.
The MFD configuration settings do not match backup
configuration memory. The system should be serviced.
MFD1 COOLING – MFD1 has
poor cooling. Reducing power
usage.
The MFD is overheating and is reducing power consumption
by dimming the display. If problem persists, the system
should be serviced.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Low Bank mode is active. Disengage to continue RNP 1.0.
MFD1 DB ERR – MFD1 navigation The MFD detected a failure in the navigation database.
database error exists.
Attempt to reload the navigation database. If problem
persists, the system should be serviced.
The MFD detected a failure in the basemap database.
MFD1 DB ERR – MFD1 basemap
database is incompatible.
The MFD detected a that the basemap database is
incompatible.
MFD1 DB ERR – MFD1 terrain
database error exists.
The MFD detected a failure in the terrain database. Ensure
that the terrain card is properly inserted in display. Replace
terrain card. If problem persists, The system should be
serviced.
MFD1 DB ERR – MFD1 terrain
database missing.
The terrain database is present on another LRU, but is missing
on the specified LRU.
AFCS
MFD1 DB ERR – MFD1 basemap
database error exists.
The MFD detected a failure in the Airport Directory database.
Ensure the data card is properly inserted. Replace data card. If
problem persists, the system should be serviced.
MFD1 DB ERR – MFD1 obstacle
database error exists.
The MFD detected a failure in the obstacle database. Ensure
that the data card is properly inserted. Replace data card. If
problem persists, The system should be serviced.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
173
Index
Index
MFD1 DB ERR – MFD1 Airport
Directory database error exists.
Appendix
Appendix
The MFD detected a failure in the FliteCharts database
(optional feature). Ensure the data card is properly inserted.
Replace data card. If problem persists, the system should be
serviced.
Annun/Alerts
Annun/Alerts
MFD1 DB ERR – MFD1
FliteCharts database error exists.
Additional Additional
Abnormal
AFCS Features
Features
Operation
MFD1 DB ERR – MFD1 Chartview The MFD detected a failure in the ChartView database
database error exists.
(optional feature). Ensure the data card is properly inserted.
Replace data card. If problem persists, the system should be
serviced.
190-02219-00 Rev. C
EISEIS
LOW BANK ACTIVE – Disengage
for RNP less than 1.0.
Message
Comments
MFD1 DB ERR – MFD1 obstacle
database missing.
The obstacle database is present on another LRU, but is
missing on the specified LRU.
MFD1 DB ERR – MFD1 Safe Taxi
database error exists.
The MFD detected a failure in the Safe Taxi database. Ensure
that the data card is properly inserted. Replace data card. If
problem persists, The system should be serviced.
MFD1 KEYSTK – MFD [key name] A key is stuck on the PFD and/or MFD bezel. Attempt to free
Key is stuck.
the stuck key by pressing it several times. The system should
be serviced if the problem persists.
MFD1 MANIFEST – MFD1
software mismatch,
communication halted.
The MFD has incorrect software installed. The system should
be serviced.
MFD1 SERVICE – MFD1 needs
service. Return unit for repair.
The MFD self-test has detected a problem. The system should
be serviced.
MFD1 VOLTAGE – MFD1 has low
voltage. Reducing power usage
The MFD voltage is low. The system should be serviced.
NAV1 MANIFEST – NAV1
software mismatch,
communication halted.
The NAV1 has incorrect software installed. The system should
be serviced.
NAV1 RMT XFR – NAV1 remote
transfer key is stuck.
The remote NAV1 transfer switch is stuck in the enabled (or
“pressed”) state. Press the transfer switch again to cycle
its operation. If the problem persists, the system should be
serviced.
NAV1 SERVICE – NAV1 needs
service. Return unit for repair.
A failure has been detected in the NAV1 receiver. The receiver
may still be available. The system should be serviced.
NAV2 MANIFEST – NAV2
software mismatch,
communication halted.
The NAV2 has incorrect software installed. The system should
be serviced.
NAV2 RMT XFR – NAV2 remote
transfer key is stuck.
The remote NAV2 transfer switch is stuck in the enabled (or
“pressed”) state. Press the transfer switch again to cycle
its operation. If the problem persists, the system should be
serviced.
NAV2 SERVICE – NAV2 needs
service. Return unit for repair.
A failure has been detected in the NAV2 receiver. The receiver
may still be available. The system should be serviced.
NAV DB UPDATED – Active
navigation database updated.
System has updated the active navigation database from the
standby navigation database.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Annunciations & Alerts
174
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190-02219-00 Rev. C
Annunciations & Alerts
Comments
Flight
Flight
Instruments
Instruments
Message
NON WGS84 WPT – Do not use
GPS for navigation to [xxxx]
The position of the selected waypoint [xxxx] is not calculated
based on the WGS84 map reference datum and may be
positioned in error as displayed. Do not use GPS to navigate
to the selected non-WGS84 waypoint.
PFD POSITIONS DIFFERENT –
PFD positions mismatch. Check
position sensors.
There is a mismatch in the position sensed by the PFDs. Check
position sensor settings. If message persists the system should
be serviced.
PFD1 CONFIG – PFD1 config
error. Config service req’d.
The PFD configuration settings do not match backup
configuration memory. The system should be serviced.
PFD1 COOLING – PFD1 has poor
cooling. Reducing power usage.
The PFD is overheating and is reducing power consumption by
dimming the display. If problem persists, the system should
be serviced.
The PFD detected a failure in the basemap database.
PFD1 DB ERR – PFD1 multiple
database errors exists.
The PFD detected a failure in more than one database. If
problem persists, the system should be serviced.
PFD1 DB ERR – PFD1
navigation database error exists.
The PFD detected a failure in the navigation database.
Attempt to reload the navigation database. If problem
persists, the system should be serviced.
PFD1 DB ERR – PFD1 obstacle
database error exists.
The PFD detected a failure in the obstacle database. Ensure
that the data card is properly inserted. Replace data card. If
problem persists, The system should be serviced.
PFD1 DB ERR – PFD1 obstacle
database missing.
The obstacle database is present on another LRU, but is
missing on the specified LRU.
PFD1 DB ERR – PFD1 Safe Taxi
database error exists.
The PFD detected a failure in the Safe Taxi database. Ensure
that the data card is properly inserted. Replace data card. If
proble m persists, the system should be serviced.
PFD1 DB ERR – PFD1 terrain
database error exists.
The 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 system should be
serviced.
PFD1 DB ERR – PFD1 terrain
database missing.
The terrain database is present on another LRU, but is missing
on the specified LRU.
Annun/Alerts
Annun/Alerts
Appendix
Appendix
175
Index
Index
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Additional Additional
Abnormal
AFCS Features
Features
Operation
190-02219-00 Rev. C
AFCS
PFD1 DB ERR – PFD1 basemap
database error exists.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Navigation angle is not set to MAGNETIC at power-up.
EISEIS
NON-MAG UNITS– Nonmagnetic NAV ANGLE display
units are active.
Message
Comments
PFD1 KEYSTK – PFD1 [key name]
is stuck.
A key is stuck on the PFD bezel. Attempt to free the stuck key
by pressing it several times. The system should be serviced if
the problem persists.
PFD1 CARD 1 REM – Card 1 was
removed. Reinsert card.
The SD card was removed from the top card slot of the
specified PFD or MFD. The SD card needs to be reinserted.
PFD1 CARD 2 REM – Card 2 was
removed. Reinsert card.
The SD card was removed from the bottom card slot of the
specified PFD or MFD. The SD card needs to be reinserted.
PFD1 CARD 1 ERR – Card 1 is
invalid.
The SD card in the top card slot of the specified PFD or MFD
contains invalid data.
PFD1 CARD 2 ERR – Card 2 is
invalid.
The SD card in the bottom card slot of the specified PFD or
MFD contains invalid data.
PFD1 SERVICE – PFD1 needs
service. Return unit for repair.
The PFD self-test has detected a problem. The system should
be serviced.
PFD1 VOLTAGE – PFD1 has low
voltage. Reducing power usage
The PFD1 voltage is low. The system should be serviced.
PFD2 CARD 1 REM – Card 1 was
removed. Reinsert card.
The SD card was removed from the top card slot of the
specified PFD or MFD. The SD card needs to be reinserted.
PFD2 CARD 2 REM – Card 2 was
removed. Reinsert card.
The SD card was removed from the bottom card slot of the
specified PFD or MFD. The SD card needs to be reinserted.
PFD2 CARD 1 ERR – Card 1 is
invalid.
The SD card in the top card slot of the specified PFD or MFD
contains invalid data.
PFD2 CARD 2 ERR – Card 2 is
invalid.
The SD card in the bottom card slot of the specified PFD or
MFD contains invalid data.
PFD2 CONFIG – PFD2 config
error. Config service req’d.
The PFD configuration settings do not match backup
configuration memory. The system should be serviced.
PFD2 COOLING – PFD2 has poor
cooling. Reducing power usage.
The PFD is overheating and is reducing power consumption by
dimming the display. If problem persists, the system should
be serviced.
PFD2 DB ERR – PFD2 basemap
database error exists.
The PFD detected a failure in the basemap database.
PFD2 DB ERR – PFD2 basemap
database is incompatible.
The PFD detected a that the basemap database is
incompatible.
PFD2 DB ERR – PFD2 navigation
database error exists.
The PFD detected a failure in the navigation database.
Attempt to reload the navigation database. If problem
persists, the system should be serviced.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Annunciations & Alerts
176
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Annunciations & Alerts
Comments
The PFD detected a failure in the obstacle database. Ensure
that the data card is properly inserted. Replace data card. If
problem persists, The system should be serviced.
PFD2 DB ERR – PFD2 obstacle
database missing.
The obstacle database is present on another LRU, but is
missing on the specified LRU.
PFD2 DB ERR – PFD2 Safe Taxi
database error exists.
The PFD detected a failure in the Safe Taxi database. Ensure
that the data card is properly inserted. Replace data card. If
problem persists, The system should be serviced.
PFD2 DB ERR – PFD2 terrain
database error exists.
The 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 system should be
serviced.
PFD2 DB ERR – PFD2 terrain
database missing.
The terrain database is present on another LRU, but is missing
on the specified LRU.
PFD2 KEYSTK – PFD2 [key name]
Key is stuck.
A key is stuck on the PFD bezel. Attempt to free the stuck key
by pressing it several times. The system should be serviced if
the problem persists.
PF2 MANIFEST – PFD2 software
mismatch, communication halted.
The PFD has incorrect software installed. The system should
be serviced.
PFD2 SERVICE – PFD2 needs
service. Return unit for repair.
The PFD self-test has detected a problem. The system should
be serviced.
PFD2 VOLTAGE – PFD2 has low
voltage. Reducing power usage
The PFD2 voltage is low. The system should be serviced.
PILOT RADIOS MUTED – Pilot
radios are muted.
The pilot radios are set on mute.
PTK FAIL – Parallel track
unavailable: invalid leg type.
Invalid leg type for parallel offset.
PTK FAIL – Parallel track
unavailable: past IAF.
IAF waypoint for parallel offset has been passed.
PTK FAIL – Parallel track
unavailable: bad geometry.
Bad parallel track geometry.
RAIM UNAVAIL – RAIM is not
available from FAF to MAP
waypoints.
GPS satellite coverage is insufficient to perform Receiver
Autonomous Integrity Monitoring (RAIM) from the FAF to the
MAP waypoints.
EISEIS
PFD2 DB ERR – PFD2 obstacle
database error exists.
AFCS
Additional Additional
Abnormal
AFCS Features
Features
Operation
Annun/Alerts
Annun/Alerts
Appendix
Appendix
Index
Index
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
RECORDER SERVICE REQUIRED
The CVDR should be serviced.
- The CVDR needs service.
190-02219-00 Rev. C
Flight
Flight
Instruments
Instruments
Message
177
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Annunciations & Alerts
Message
Comments
REGISTER CONNEXT – Data
services are inoperative, register
w/ Connext.
The system is not registered with Garmin Connext, or its
current registration data has failed authentication.
SCHEDULER [#] – <message>.
Message criteria entered by the user.
SLCT FREQ – Select appropriate
frequency for approach.
The system notifies the pilot to load the approach frequency
for the appropriate NAV receiver. Select the correct frequency
for the approach.
SLCT MAG– Select MAGNETIC
NAV ANGLE display units.
The system notifies the pilot to set the Nav Angle units on the
Avioncs Settings Screen to Magnetic.
SLCT NON-MAG– Select
alternate NAV ANGLE display
units.
The system notifies the pilot to set the Nav Angle units on the
Avioncs Settings Screen to True.
STEEP TURN – Steep turn ahead.
A steep turn is 15 seconds ahead. Prepare to turn.
STRMSCP FAIL – Stormscope has
failed.
Stormscope has failed. The system should be serviced.
SVT – SVT DISABLED: Out of
available terrain region.
Synthetic Vision is disabled because the aircraft is not within
the boundaries of the installed terrain database.
SVT – SVT DISABLED: Terrain DB
resolution too low.
Synthetic Vision is disabled because a terrain database of
sufficient resolution (9 arc-second or better) is not currently
installed.
SW MISMATCH – GDU software
version mismatch. Xtalk is off.
The MFD and PFDs have different software versions installed.
The system should be serviced.
TERRAIN DSP – [PFD1, PFD2 or
MFD1] Terrain awareness display
unavailable.
One of the terrain, or obstacle databases required for TAWS in
the specified PFD or MFD is missing or invalid.
TIMER EXPIRD – Timer has
expired.
The system notifies the pilot that the timer has expired.
UNABLE V WPT – Can’t reach
current vertical waypoint.
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.
VNV UNAVAILABLE – Excessive
crosstrack error.
The current crosstrack exceeds the limit, causing vertical
deviation to go invalid.
VNV UNAVAILABLE –
The current track angle error exceeds the limit, causing the
Unavailable. Excessive track angle
vertical deviation to go invalid.
error.
178
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Annunciations & Alerts
Comments
Flight
Flight
Instruments
Instruments
Message
The lateral flight plan contains a procedure turn, vector,
or other unsupported leg type prior to the active vertical
waypoint. This prevents vertical guidance to the active vertical
waypoint.
WPT ARRIVAL – Arriving at
waypoint -[xxxx]
Arriving at waypoint [xxxx], where [xxxx] is the waypoint
name.
WX ALERT – Possible severe
weather ahead.
The GWX 68/GWX 70 indicates severe weather within ±10º
of the aircraft heading at a range of 80 to 320 nm.
XPDR1 ADS-B 1090 – Datalinik:
ADS-B 1090 receiver has failed.
A failure has been detected in the 1090 receiver.
XPDR1 ADS-B NO POS –
Transponder: ADS-B is not
transmitting position.
The transponder is not able to receive position information.
XPDR1 ADS-B TRFC –
Transponder: ADS-B traffic has
failed
The Transponder is incapable of processing traffic information.
XPDR1 ADS-B UAT – Datalink:
ADS-B in UAT receiver has failed.
A failure has been detected in the UAT receiver.
Additional Additional
Abnormal
AFCS Features
Features
Operation
XPDR1 CONFIG – XPDR1 config
error. Config service req’d.
AFCS
VNV UNAVAILABLE –
Unsupported leg type in flight
plan.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
A parallel course has been selected, causing the vertical
deviation to go invalid.
EISEIS
VNV UNAVAILABLE – Parallel
course selected.
The transponder configuration settings do not match those
of backup configuration memory. The system should be
serviced.
XPDR2 ADS-B 1090 – Datalinik:
ADS-B 1090 receiver has failed.
A failure has been detected in the 1090 receiver.
XPDR2 ADS-B NO POS –
Transponder: ADS-B is not
transmitting position.
The transponder is not able to receive position information.
Appendix
Appendix
The #1 transponder should be serviced when possible.
Annun/Alerts
Annun/Alerts
XPDR1 SRVC – XPDR1 needs
service. Return unit for repair.
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
179
Message
Comments
XPDR2 ADS-B TRFC –
Transponder: ADS-B traffic has
failed
The Transponder is incapable of processing traffic information.
XPDR2 ADS-B UAT – Datalink:
ADS-B in UAT receiver has failed.
A failure has been detected in the UAT receiver.
XPDR2 CONFIG – XPDR2 config
error. Config service req’d.
The transponder configuration settings do not match those
of backup configuration memory. The system should be
serviced.
XPDR2 SRVC – XPDR2 needs
service. Return unit for repair.
The #2 transponder should be serviced when possible.
XTALK ERROR – A flight display
crosstalk error has occurred.
The MFD and PFDs are not communicating with each other.
The system should be serviced.
FLIGHT PLAN IMPORT/EXPORT MESSAGES
In some circumstances, some messages may appear in conjunction with others.
Description
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.
Index
Index
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
‘Flight plan successfully imported.’
Annun/Alerts
Annun/Alerts
Flight Plan Import/Export Results
Appendix
Appendix
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Annunciations & Alerts
180
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Annunciations & Alerts
Description
Flight
Flight
Instruments
Instruments
Flight Plan Import/Export Results
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.
‘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.
EISEIS
‘Too many points. Flight plan truncated.’
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
AFCS
Additional Additional
Abnormal
AFCS Features
Features
Operation
Annun/Alerts
Annun/Alerts
Appendix
Appendix
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
181
CREW PROFILE IMPORT/EXPORT MESSAGES
Crew Profile Import/
Export Results
Description
‘No pilot profile plan files found
to import.’
Displayed if the SD card does not have one or more valid pilot
profile filenames.
‘Overwrite existing profile?’
Displayed if the profile name matches the name of existing
profile.
‘Profile name invalid. Enter a
different profile name.’
Displayed if the profile name is invalid.
‘All available pilot profiles in use.
Delete a profile before importing
another.’
Displayed if the maximum number for pilot profiles has been
reached.
‘Pilot profile import failed.’
Displayed if the importing operation fails for any other reason.
‘Pilot profile import succeeded.’
Displayed if the importing operation succeeds.
‘Overwrite existing file?’
Displayed if the filename matches the name of an existing file
on the SD card.
‘Pilot profile export failed.’
Displayed if the export operation fails.
‘Pilot profile export succeeded.’
Displayed if the export operation succeeds.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Annunciations & Alerts
182
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Appendix
Flight
Flight
Instruments
Instruments
APPENDIX
PFD SOFTKEY MAP
Level 2
Level 3
Level 4
Map/HSI
Description
EISEIS
Level 1
Displays the PFD Map display settings
softkeys.
Displays the PFD Map selection softkeys.
Map Off
Removes the PFD map from display (Inset
or Traffic).
Inset Map
Displays the Inset Map.
HSI Map
Inset Trfc
Displays the HSI Map.
HSI Trfc
Replaces the Inset Map with a dedicated
traffic display.
Replaces the HSI Map with a dedicated
traffic display.
Traffic
TER
Displays traffic information on PFD Map.
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
183
Index
Index
PFD Softkey Map
Appendix
Appendix
Displays/removes the name of the selected
data link weather provider (SiriusXM) and
the weather product icon and age box (for
enabled weather products).
Annun/Alerts
Annun/Alerts
Displays terrain on the PFD map; cycles
through the following:
Off: No terrain information shown on PFD
Map.
Topo: Displays topographical data (e.g.,
coastlines, terrain, rivers, lakes).
REL: Displays relative terrain information on
the PFD Map.
Additional Additional
Abnormal
AFCS Features
Features
Operation
Selects desired amount of map detail:
All (No Declutter): All map features visible
Detail 3: Declutters land data
Detail 2: Declutters land and SUA data
Detail 1: Removes everything except for
the active flight plan
AFCS
Detail
WX LGND
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Layout
Flight
Flight
Instruments
Instruments
Appendix
Level 1
Level 2
Level 3
Level 4
PRECIP
Displays Connext weather and coverage on
PFD Map.
Or:
Displays XM NEXRAD weather and coverage
on PFD Map (subscription optional).
or
EISEIS
NEXRAD
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
METAR
Displays METAR information on Inset Map
(subscription optional).
Lightning
Adds/removes the display of SiriusXM
lightning information on PFD Map.
Disables lightning function on PFD Map.
The softkey annunciator is green when the
lightning function is off.
Datalink
Selects the data link weather source for the
PFD Map.
STRMSCP
Adds or removes the display of Stormscope
information on the PFD Map. The softkey
annunciator is green when the function
is on. When the function is off, the
annunciator is gray (optional).
AFCS
LTNG Off
Wx
Radar
RDR Opt
Additional Additional
Abnormal
Features
Operation
Features AFCS
Description
When enabled, displays the airborne
weather radar overlay on HSI Map.
Displays softkeys for airborne weather radar
options.
Mode
SEL
Displays softkeys for weather radar mode
selection.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Standby Selects Standby weather radar mode.
Weather Activates Weather radar mode.
Ground Activates Ground Map weather radar mode.
Gain Gain +
WX ALRT
Decreases weather radar gain setting.
STAB
ACT
Activates antenna stabilization feature.
Increases weather radar gain setting.
When enables, displays weather alerts as
system messages.
Activates Altitude Compensated Tilt feature.
PFD Softkey Map
184
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Appendix
Level 2
Level 3
Level 4
Description
Flight
Flight
Instruments
Instruments
Level 1
Replaces the PFD Map with a dedicated
traffic display.
PFD Opt
Displays second-level softkeys for additional
PFD options.
SVT
Displays additional SVT overlay softkeys.
Displays Pathway Boxes on the Synthetic
Vision Display.
Terrain
HDG LBL
Enables synthetic terrain depiction.
APT Sign
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.
Displays compass heading along the ZeroPitch line.
Wind
Displays the wind option softkeys.
Option 2
Option 3
Wind direction arrow and speed.
Headwind/Tailwind and crosswind
components.
Wind direction arrow with direction and
speed.
Displays DME Information Window
(optional).
Cycles the Bearing 1 Information Window
through NAV1, NAV2, GPS/waypoint
identifier and GPS-derived distance
information, ADF/frequency, and Off.
Appendix
Appendix
Bearing 1
Wind information not displayed.
Annun/Alerts
Annun/Alerts
DME
Off
Option 1
Additional Additional
Abnormal
AFCS Features
Features
Operation
Selects the display mode for the Angle of
Attack (AOA) indicator on the PFD:
Auto: Displays AOA indicator on the PFD.
Off: Removes AOA indicator from the PFD.
AFCS
AOA
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Pathways
EISEIS
TFC Map
PFD Softkey Map
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
185
Flight
Flight
Instruments
Instruments
Appendix
Level 1
Level 2
Level 3
Level 4
Sensors
Displays the sensor selection softkeys.
ADC
EISEIS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
AHRS
Selects the #1 ADC.
Selects the #2 ADC.
Displays the AHRS selection softkeys.
AHRS 1
AHRS 2
Selects the #1 AHRS.
Selects the #2 AHRS.
Bearing 2
Cycles the Bearing 2 Information Window
through NAV1, NAV2, GPS/waypoint identifier
and GPS-derived distance information, ADF/
frequency, and Off.
ALT Units
Displays softkeys to select altitude unit
parameters.
AFCS
Meters
IN
HPA
Additional Additional
Abnormal
Features
Operation
Features AFCS
Annun/Alerts
Annun/Alerts
Appendix
Appendix
Displays ADC selection softkeys.
ADC 1
ADC 2
STD Baro
When enabled, displays altimeter in meters.
Press to display the BARO setting as inches
of mercury.
Press to display the BARO setting as
hectopascals.
Sets barometric pressure to 29.92 in Hg
(1013 hPa if metric units are selected).
OBS
Selects OBS mode on the CDI when
navigating by GPS (only available with
active leg). When OBS is on, the softkey
annunciator is green.
CDI
Cycles through FMS, NAV1, and NAV2
navigation modes on the CDI.
ADF/DME
Displays the ADF/DME Tuning Window,
allowing tuning and selection of the ADF/
DME (optional).
XPDR
Displays the transponder selection softkeys.
XPDR 1
XPDR 2
Index
Index
Description
Selects the #1 transponder as active.
Selects the #2 transponder as active.
PFD Softkey Map
186
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
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Appendix
Level 2
Level 3
Standby
Activates transponder (transponder replies
to identification interrogations).
ALT
Altitude Reporting Mode (transponder
replies to identification and altitude
interrogations).
VFR
Automatically enters the VFR code (1200 in
the U.S.A. only).
Code
Displays transponder code selection softkeys
0-7.
Use numbers to enter code.
BKSP
Removes numbers entered, one at a time.
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen.
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen.
Displays Timer/References Window.
Annun/Alerts
Annun/Alerts
Appendix
Appendix
Displays the Alerts Window when
pressed. System generated messages
cause the Alerts Softkey label to
change to a flashing ‘Message’ label.
Pressing the Message Softkey opens
the Alerts Window, acknowledges the
message, and the softkey reverts to
the ‘Alerts’ label.
PFD Softkey Map
Additional Additional
Abnormal
AFCS Features
Features
Operation
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen.
AFCS
0-7
Ident
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Alerts
or
Message
Selects transponder Standby Mode
(transponder does not reply to any
interrogations).
EISEIS
Tmr/Ref
Description
On
Ident
Ident
Level 4
Flight
Flight
Instruments
Instruments
Level 1
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
187
Flight
Flight
Instruments
Instruments
Appendix
MFD SOFTKEY MAP
Level 1
Level 2
Level 3
CAS
Accesses the Synoptics page softkeys and the Landing
Field Elevation softkeys.
CAS ↑
and
CAS ↓
LFE MAN
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
System
Additional Additional
Abnormal
Features
Operation
Features AFCS
Annun/Alerts
Annun/Alerts
Scroll up or down (displayed only when a sufficient
number of items are displayed in the Crew Alerting
System display to warrant scrolling).
Displays the manual landing field elevation softkeys.
+ 250 FT
Adds 250 feet to the previously selected or default LFE
value.
- 250 FT
Subtracts 250 feet to the previously selected or default
LFE value.
+ 25 FT
Adds 25 feet to the previously selected or default LFE
value.
- 25 FT
Subtracts 25 feet to the previously selected or default
LFE value.
Accept
Press to accept the adjustments to the LFE value.
FMS LFE
Sets the landing field elevation to the destination
airport elevation.
ELEC
Displays the electrical synoptics page.
FUEL
Displays the fuel synoptics page.
GEN
Displays the general synoptics page for the anti-ice
system and doors.
Map Opt
Displays system oil pressure and temperature, fuel
calculations, and electrical system information.
Traffic
Inset
Appendix
Appendix
Description
Displays traffic information on Navigation Map Page.
Displays inset window second level softkeys.
Off
Removes VSD inset from Navigation Map Page.
Index
Index
MFD Softkey Map
188
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Appendix
Level 2
VSD
Displays VSD profile information of terrain/obstacles along
the current track, vertical track vector, and selected altitude.
Auto: Automatically displays either VSD profile information
for active flight plan information or along current track with
no active flight plan.
FPL: Displays VSD profile information for active flight plan.
TRK: Displays VSD profile information along current track.
Displays terrain on the map; cycles through the following:
Off: No terrain information shown on MFD Map.
Topo: Displays topographical data (e.g., coastlines, terrain,
rivers, lakes) and elevation scale on MFD Map.
REL: Displays relative terrain information on the MFD Map.
AWY
Displays airways on the map; cycles through the following:
Off: No airways are displayed.
On: All airways are displayed.
LO: Only low altitude airways are displayed.
HI: Only high altitude airways are displayed.
Displays Stormscope information on Navigation Map
(optional).
NEXRAD
Displays XM NEXRAD weather and coverage on Navigation
Map Page (optional).
XM LTNG
Displays XM lightning information on Navigation Map Page
(optional).
Displays METAR information on Inset Map (subscription
optional).
Legend
Displays legends for the displayed XM Weather products
(optional).
Wx Radar
Annun/Alerts
Annun/Alerts
METAR
Additional Additional
Abnormal
AFCS Features
Features
Operation
STRMSCP
AFCS
TER
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Description
EISEIS
Level 3
Flight
Flight
Instruments
Instruments
Level 1
Displays weather information.
Appendix
Appendix
MFD Softkey Map
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
189
Level 1
Level 2
Charts
When available, displays optional airport and terminal
procedure charts.
CHRT Opt
AUTO
Info
DP
STAR
APR
NOTAM
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
Description
Selects desired amount of map detail; cycles through the
following levels:
Detail All: All map features visible.
Detail-3: Declutters land data.
Detail-2: Declutters land and SUA data.
Detail-1: Removes everything except for the active flight
plan.
Checklist
Displays chart display settings softkeys (if available).
Displays the most pertinent chart based on the phase of
flight and loaded procedures in the active flight plan.
Pressing the Info 1 or Info 2 Softkey returns to the airport
diagram when the view is on a different chart.
Displays departure procedure chart.
Displays standard terminal arrival procedure chart.
Displays approach procedure chart.
Displays NOTAM information for selected airport, when
available.
When available, displays optional checklists
MFD Softkey Map
LOADING UPDATED DATABASES
CAUTION: Never disconnect power to the system when loading a database.
Power interruption during the database loading process could result in maintenance being required to reboot the system.
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
Level 3
Detail
EISEIS
Flight
Flight
Instruments
Instruments
Appendix
Index
Index
Appendix
Appendix
NOTE: When loading database updates, the ‘DB Mismatch’ system messages will be displayed until database synchronization is complete, followed
by turning system power off, then on. Synchronization can be monitored on
the Aux-Database Page.
190
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Appendix
Additional Additional
Abnormal
AFCS Features
Features
Operation
Annun/Alerts
Annun/Alerts
Appendix
Appendix
Index
Index
191
AFCS
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
190-02219-00 Rev. C
EISEIS
Databases may be loaded from an SD card, or through Garmin Pilot and Flight
Stream 510. When loading databases through Garmin Pilot and the Flight Stream
510, it must be enabled on the system and the multimedia card inserted in the bottom
SD slot of the MFD.
The cycles and dates for both standby and active databases are displayed on the
“Aux – Databases” page on the MFD. Any active databases with expiration dates in
the past will be highlighted with amber text. When an expired active database has a
standby database that is ready to become effective, a cyan double-sided arrow will be
displayed between the database cycles. When this arrow is visible, it indicates that
the standby and active databases in that row will be switched on the next power cycle,
activating the current standby database. Databases can also be manually selected (or
deselected) by highlighting a list item and pressing the ENT key, provided a valid, verified standby database is present.
In some cases it may be necessary to obtain an unlock code from Garmin in order
to make the database product functional. It may also be necessary to have the system
configured by a Garmin authorized service facility in order to use some database features.
The navigation database contains the aeronautical data used by the system for the
flight management and flight planning functions. Included is detailed data for waypoints, procedures (arrivals, departures, approaches), and airways. The navigation database is updated every 28 days.
The basemap database contains data for the topography and land features, such as
rivers, lakes, and towns. It is updated only periodically, with no set schedule. There
is no expiration date.
The terrain database contains the terrain mapping data. These databases are updated periodically and have no expiration date.
The obstacle database contains data for obstacles, such as towers, that pose a potential hazard to aircraft. Obstacles 200 feet and higher are included in the obstacle
database. It is very important to note that not all obstacles are necessarily charted and
therefore may not be contained in the obstacle database. This database is updated on
a 56-day cycle.
Flight
Flight
Instruments
Instruments
NOTE: Loading a database in the system prior to its effective date will result
in the expiration date on the power-up screen and the effective date on the
Aux – Databases Page being displayed in amber.
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.
The AOPA or AC-U-KWIK Airport Directory provides data on airports and heliports throughout the U.S. or worldwide, respectively. The AOPA Directory offers
detailed information for over 5,300 U. S. airports, along with the names and phone
numbers of thousands of FBOs. These databases are updated every 56 days. The
AC-U-KWIK Directory offers detailed information for more than 8,000 airports with
runways longer than 3,000 feet worldwide.
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.
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.
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. The ChartView database must be purchased directly from Jeppesen, but can be
updated at www.jeppesen.com or www.flygarmin.com.
Updating Databases using an SD Card
With the system OFF, remove an SD Card from the bottom SD card slot of the
MFD.
2) Download and install the databases on an SD card.
1)
3)
Put the SD Card in the bottom SD card slot of the MFD.
4)
Turn the system ON.
5)
Press the ENT Key or the right most softkey on MFD display to
acknowledge the startup screen.
6)
Turn the large FMS Knob to select the Aux page group on the MFD.
7)
Turn the small FMS Knob to select the Database page group on the MFD.
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Appendix
192
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190-02219-00 Rev. C
Appendix
11) Remove the SD card from the bottom slot of the MFD.
12) After restarting the system, turn the large FMS Knob and select the Aux
page group on the MFD.
13) Turn the small FMS Knob and select the Databases page.
14) Verify that the standby databases transferred and are now in the active
database column.
b) Turn the small FMS Knob as necessary to select the database title.
c) Press the ENT Key. A cyan double-sided arrow will appear indicating
that the standby database will become active.
d) Remove and reapply power to the system.
17) Remove power from the system.
Appendix
Appendix
Updating Databases using Flight Stream 510 from any MFD page
(except the Aux - Databases page)
Insert the Flight Stream Mutimedia Card in the bottom slot of the MFD.
2)
3)
Press the Update softkey when the Database Update screen appears.
The Flight Stream 510 will enter WI-FI mode. A Starting Database Update
window will appear.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
193
Index
Index
1)
190-02219-00 Rev. C
Annun/Alerts
Annun/Alerts
e) Verify that the standby databases transferred and are now in the active
database column.
Additional Additional
Abnormal
AFCS Features
Features
Operation
a) Press the FMS Knob. The first database title on the screen will be
selected.
AFCS
15) To view database information for an individual display, press and then turn
the FMS Knob to select the database, and then press the Details Softkey.
Press the ENT Key or the FMS Knob to exit.
16) To manually activate any databases that did not transfer to the active
column:
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
10) Remove power from the system.
EISEIS
9)
Monitor the Sync Status on the Database page. Wait for all databases to
complete syncing, indicated by ‘Sync Complete’ being displayed. A cyan
double arrow will appear between the Standby and Active columns to show
which Standby databases will be transferred to Active at the next power
cycle.
Verify the correct database cycle information is shown in the Standby
Database column.
Flight
Flight
Instruments
Instruments
8)
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Appendix
4)
Put the mobile device in WI-FI mode (refer to the Additional Features
section).
5)
Connect the mobile device to the Flight Stream 510 WI-FI (refer to the
Additional Features section). The ‘WI-FI Not Connected’ screen will close
when the WI-FI connection is established.
6)
7)
When the transfer is complete, the following screen will appear.
Press the Close softkey.
9)
Remove power from the system.
10) After restarting the system, turn the large FMS Knob and select the Aux
page group on the MFD.
11) Turn the small FMS Knob and select the Databases page.
12) Verify that the standby databases transferred and are now in the active
database column.
AFCS
13) To view database information for an individual display, press and then turn
the FMS Knob to select the database, and then press the Details Softkey.
Press the ENT Key or the FMS Knob to exit.
14) To manually activate any databases that did not transfer to the active
column:
b) Turn the small FMS Knob as necessary to select the database title.
c) Press the ENT Key. A cyan double-sided arrow will appear indicating
that the standby database will become active.
d) Remove and reapply power to the system.
e) Verify that the standby databases transferred and are now in the active
database column.
Updating Databases using Flight Stream 510 from the Aux - Databases
page
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
a) Press the FMS Knob. The first database title on the screen will be
selected.
1)
With the system OFF, insert the Flight Stream Mutimedia Card in the bottom
Index
Index
slot of the MFD.
194
2)
Turn the large FMS Knob to select the Aux page group on the MFD.
3)
Turn the small FMS Knob to select the Database page group on the MFD.
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Appendix
5)
The Aux - Databases page will show the databases connected to the mobile
device in place of the active databases on the system. Databases selected
to load will be indicated by a cyan arrow.
6)
Press the Update softkey. The Flight Stream 510 will enter WI-FI mode.
7)
Put the mobile device in WI-FI mode (refer to the Additional Features
section).
8)
Connect the mobile device to the Flight Stream 510 WI-FI (refer to the
Additional Features section).
9)
The Database Update status will appear in the Status window at the top of
the page.
EISEIS
Press the Device Softkey.
Flight
Flight
Instruments
Instruments
4)
11) After restarting the system, turn the large FMS Knob and select the Aux
page group on the MFD.
12) Turn the small FMS Knob and select the Databases page.
15) To manually activate any databases that did not transfer to the active
column:
a) Press the FMS Knob. The first database title on the screen will be
selected.
c) Press the ENT Key. A cyan double-sided arrow will appear indicating
that the standby database will become active.
d) Remove and reapply power to the system.
Appendix
Appendix
e) Verify that the standby databases transferred and are now in the active
database column.
Annun/Alerts
Annun/Alerts
b) Turn the small FMS Knob as necessary to select the database title.
Additional Additional
Abnormal
AFCS Features
Features
Operation
14) To view database information for an individual display, press and then turn
the FMS Knob to select the database, and then press the Details Softkey.
Press the ENT Key or the FMS Knob to exit.
AFCS
13) Verify that the standby databases transferred and are now in the active
database column.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
10) Remove power from the system.
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
195
Magnetic Field Variation Database Update
A copy of the current magnetic field variation database (MV DB) is included with
the navigation database. At startup, the system compares this version of the MV DB
with that presently being used by each AHRS (GRS1 and GRS2). If the system determines the MV DB needs to be updated, a prompt is displayed on the MFD.
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Appendix
GRS1 Magnetic Field Variation Database Update Prompt
Loading the magnetic field variation database update
With ‘OK’ highlighted, press the ENT Key on the MFD. A progress monitor
is displayed.
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
1)
Index
Index
Appendix
Appendix
Uploading Database to GRS1
196
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Appendix
When the upload is complete, the prompt for the next GRS upload is
displayed.
Flight
Flight
Instruments
Instruments
2)
EISEIS
3)
With ‘OK’ highlighted, press the ENT Key on the MFD. A progress monitor
is displayed. When the upload is complete, the system is ready for use.
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
GRS2 Magnetic Field Variation Database Update Prompt
AFCS
Additional Additional
Abnormal
AFCS Features
Features
Operation
Uploading Database to GRS2
Annun/Alerts
Annun/Alerts
Appendix
Appendix
Index
Index
190-02219-00 Rev. C
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
197
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Appendix
Blank Page
198
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Index
Barometric Altitude Minimums 6
Baro VNAV 60
Basic Empty Weight 64
Battery 13
Alerts 150
Bearing Line 88, 89, 90
Bluetooth 42, 137, 138
C
Cabin Door Open 18
Cabin pressure altitude
Warning 149
Cargo 65
CDI 5, 22
ChartView 115
Checklists 141–142
Closest Point 49
Code selection softkeys 22
COM 22, 23, 143
AFCS
Additional Additional
Abnormal
AFCS Features
Features
Operation
D
Data Link Receiver 159
Day/Night views 117
DB Mismatch 190
Dead Reckoning 145
Declutter 144
Deleting
An entire airway 45
An entire procedure 46
An individual waypoint 45, 46
Departure
Procedure 58, 59
Select 58, 59, 60
Detail Softkey 115
Differential cabin pressure
Warning 149
Appendix
Appendix
Index
Index
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Annun/Alerts
Annun/Alerts
190-02219-00 Rev. C
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
Active Channel 118
AC-U-KWIK 117, 192
ADF 22
AHRS 172
AHRS2 163
Air Data Computer 153
Airport
Information 31
Airport Directory 117, 192
Airway
Collapse/Expand Airways 40
Alerts, Aircraft 149
Along Track Offset 46
ALT 100
Altimeter setting 2
Altitude
Constraints 52
Altitude Compensated Tilt (ACT) 89
Altitude mode 100
Altitude volume 100
AOPA 117, 192
AP 160
Approach
Activating 61, 62
Loading 60, 61
Removing 62
Approach channel 60
APR softkey 61, 66
Arrival procedure 59, 60
Attitude & Heading Reference System
(AHRS) 153
Audio panel controls
NAV1, NAV2 22
Autopilot 160
Auxiliary Boost Pump 16
EISEIS
B
Flight
Flight
Instruments
Instruments
A
Index-1
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Index
Direct-to 25, 36, 37
Display backup 143
DME 21, 22
DR mode 145, 146
H
E
I
Electronic Checklists 141, 142
Electronic Stability and Protection (ESP)
139, 140
Emergency Checklist 142
Engine Driven Boost Pump 16
ESP 139, 140
Export a Flight Plan 42
Import a Flight Plan 41
Intercom 23
Interturbine Temperature (ITT) 10
Warning 149
Inverting a flight plan 41
IOI 155, 157
Iridium 125
Iridium satellite network 120, 125
F
Flap position
Asymmetrical deflection warning 149
Flight Director FD) 111, 160
Flight Plan, Active
Creating 38
Flight plan import/export messages 180
Flight Plan Map 48
Flight Stream 510 42, 137
FliteCharts 115
Forward Cargo Door Open 18
FPA 52
Frequency Transfer 23
Fuel
Alerts 149–150
Fuel Flow Data 16
Fuel on Board 65
G
Garmin Pilot 137, 138
GCU Configuration Error 167
GIA Hardware Mismatch 172
GMC Connfiguration Error 170
Ground Mapping, Weather Radar 90
Index-2
Horizontal Scan 88
Horizontal Situation Indicator (HSI) 60
J
Jeppesen 115
L
Left Fuel Tank 16
Level Mode 139
Low speed data 120
M
Main Bus 13
Main Generator 13
Map panning 72, 86
MET 160
METAR 71, 86
Minimums 161
Missed Approach 63
Mistrim 160
Mode selection softkeys 21, 22
N
NAV 1/2 5, 22
Navigation
Database 52
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Index
P
190-02219-00 Rev. C
U
User-Defined Holding Pattern 51
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
Index
Index
SafeTaxi 115
SBAS 68, 149, 172
Scheduler 132
Appendix
Appendix
S
Annun/Alerts
Annun/Alerts
RAIM 67, 68
Rear Cargo Door Open 18
ROC 155, 157
Additional Additional
Abnormal
AFCS Features
Features
Operation
R
TA 161
TAF 71, 86
TAS 99, 100, 161, 163
TAS Traffic
Non-Threat Traffic 97
PA 97
Proximity Advisory 97
TAWS 156
Telephone 120, 121
Terminal procedures charts 116
Terrain 166
Terrain Proximity 106
Text message 125, 126, 127, 129
Tilt, Antenna 88
Tilt Line 88
Timer 1
Torque 10
Traffic 69
Traffic Advisory 161
Traffic map page 100
Transponder 21, 22, 187
AFCS
Pairing 137
Parallel Track 47
Passenger Address (PA) System 23
Passenger(s) 64, 65
Pending flight plan 43, 44
Pilot and Stores Weight 64
Pitot Tube 1 18
Power-up Page 141
Predefined message 127, 128, 129
Propeller Speed 10
T
Nav/Com/
Nav/Com/
Flight Flight
Hazard Hazard
XPDR/Audio Management
Management Avoidance
Avoidance
XPDR/Audio
OBS 5
Obstacles Database Mismatch 166
Oil, engine
Alerts 149
Oil Pressure (OIL PSI) 10
Overspeed Protection 112
Oxygen
Warning 149
EISEIS
O
Sector Scan 90
Secure Digital (SD) card 141
Sensor 153
SiriusXM Weather 71, 85
Softkeys 185
Split Screen 48
Stabilization, Antenna 90
Standby Generator 13
Standby Navigation Database 193
Stormscope lightning data 70
SVT 178
Flight
Flight
Instruments
Instruments
Nearest
Airport 31, 61
Airports Page 31
NEXRAD 71
No Compare 154
Index-3
V
Vertical Navigation (VNAV) 38, 52
Direct-to 52
Vertical track 162
VNV guidance 53
Disabling 52
Enabling 51
Voice alerts, TIS Traffic 96
VRP 32
Vspeed 1
VS TGT 52
W
Waypoint Selection Submenu 39
Waypoint Submenu 36, 38
Weather Attenuated Color Highlight 91
Weather radar 87
Index
Index
Appendix
Appendix
Annun/Alerts
Annun/Alerts
Additional Additional
Abnormal
Features
Operation
Features AFCS
AFCS
Hazard Hazard
Flight Flight
Nav/Com/
Nav/Com/
Avoidance
Avoidance Management
Management XPDR/Audio
XPDR/Audio
EISEIS
Flight
Flight
Instruments
Instruments
Index
Index-4
Garmin G1000 NXi Cockpit Reference Guide for the Daher TBM 910
190-02219-00 Rev. C
Garmin International, Inc.
1200 East 151st Street
Olathe, Kansas 66062, U.S.A.
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Garmin Corporation
No. 68, Zhangshu 2nd Road
Xizhi District, New Taipei City, Taiwan
Contact Garmin Product Support or view
warranty information at www.flygarmin.com.
© 2017 - 2019 Garmin Ltd. or its subsidiaries
190-02219-00 Rev. C
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