Garmin G1000 NXi - Socata TBM 910 Reference guide

Type
Reference guide
®
Pilot’s Guide
Daher TBM 910
System Software Version 2883.00 or later
190-02218-00 Rev. E
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910
Copyright © 2017-2020 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. Some differences in
operation may be observed when comparing the information in this manual to earlier or later software versions.
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with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties
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representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for
any incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even
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the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual
or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for
incidental or consequential damages so the above limitations or exclusions may not apply to you.
190-02218-00 Rev. EGarmin G1000 NXi Pilot’s Guide for the Daher TBM 910
AC-U-KWIK and its related organizations (hereafter collectively AC-U-KWIK Organizations”) expressly disclaim all warranties with
respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of
merchantability and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or
make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to
the maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses
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Printed in the U.S.A.
190-02218-00 Rev. E
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910
iii
WARNINGS, CAUTIONS, AND 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 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 operate this equipment without first obtaining qualified instruction.
WARNING: Do not use a QFE altimeter setting with this system. System functions will not operate properly
with a QFE altimeter setting. Use only a QNH altimeter setting for height above mean sea level, or the
standard pressure setting, as applicable.
190-02218-00 Rev. EGarmin G1000 NXi Pilot’s Guide for the Daher TBM 910iv
WARNINGS, CAUTIONS, AND NOTES
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 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: 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.
WARNING: Intruder aircraft at or below 500 ft. AGL may not appear on the Garmin SVT display or may
appear as a partial symbol.
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.
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Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910
v
WARNINGS, CAUTIONS, AND NOTES
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.
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.
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WARNINGS, CAUTIONS, AND 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 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.
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.
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.
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WARNINGS, CAUTIONS, AND NOTES
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 120-76D. 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 120-76D.
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.
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WARNINGS, CAUTIONS, AND NOTES
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Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910
SOFTWARE LICENSE AGREEMENT
ix
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.
190-02218-00 Rev. EGarmin G1000 NXi Pilot’s Guide for the Daher TBM 910
SOFTWARE LICENSE AGREEMENT
x
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xi
RECORD OF REVISIONS
Record of Revisions
Part Number Revision Date Page Range Description
190-02218-00 A 3/27/17 i – I-6 Initial Release for GDU 20.51
B 4/10/17 i – I-6 Revision
- Added support for Split Screen Mode
- Updated CAS Messages
- Added Voice Message Alerts
- Updated ESP Information
- Added support for Electronic Checklists
C 9/5/19 All Revision
- Added support for Baro-VNAV
- Clerical changes
D 10/2/20 All Revision
- Added support for Visual Approach
- Added support for VNAV auto-nomination
- Removed Broadcast Rate/Refresh Rate column from Tables 6-1,
6-2, and 6-3
E 12/10/20 All Revision
- Added (if equipped) to Visual Approach and Baro VNAV
discussions
190-02218-00 Rev. EGarmin G1000 NXi Pilot’s Guide for the Daher TBM 910xii
RECORD OF REVISIONS
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TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ..............................................1
Line Replaceable Units (LRU) ..............................................1
1.2 System Controls ...................................................4
PFD Controls .......................................................................4
Controls Associated With the MFD ...................................... 6
Secure Digital Cards ............................................................ 8
1.3 System Operation ................................................9
System Power-up ................................................................9
Normal Operation .............................................................10
Reversionary Mode ...........................................................11
System Annunciations .......................................................12
System Status....................................................................14
AHRS Operation ................................................................15
GPS Receiver Operation ....................................................16
1.4 Accessing System Functionality .........................21
Softkey Function ...............................................................21
Menus ............................................................................... 27
MFD Page Groups .............................................................28
Split Screen Functionality .................................................. 31
System Settings .................................................................32
System Utilities .................................................................41
1.5 Display Backlighting ..........................................46
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ..............................................50
Airspeed Indicator ............................................................. 50
Attitude Indicator ..............................................................53
Altimeter ........................................................................... 54
Vertical Speed Indicator (VSI) ............................................57
Vertical Deviation ..............................................................57
Horizontal Situation Indicator (HSI) ...................................60
Course Deviation Indicator (CDI) .......................................64
Angle of Attack (AOA) Indicator ........................................ 72
Radar Altimeter ................................................................. 73
2.2 Supplemental Flight Data ..................................75
Temperature Displays ........................................................ 75
Wind Data ......................................................................... 76
Vertical Navigation (VNV) Indications ............................... 77
2.3 PFD Annunciations and Alerting Functions ........78
Marker Beacon Annunciations ..........................................78
Altitude Alerting ................................................................78
Low Altitude Annunciation ................................................ 79
Minimum Descent Altitude/Decision Height Alerting ........79
2.4 Garmin SVT (Synthetic Vision Technology) .........81
SVT Operation ................................................................... 82
SVT Features .....................................................................84
Field of View .....................................................................92
2.5 Abnormal Operations .........................................93
Abnormal GPS Conditions .................................................93
Comparator Annunciations ...............................................94
Reversionary Sensor Annunciations ..................................95
Unusual Attitudes .............................................................96
SECTION 3 ENGINE INDICATION SYSTEM
3.1 Engine Display ...................................................98
3.2 Landing Field Elevation ...................................101
3.3 Synoptics .........................................................102
Electrical (ELEC) ..............................................................102
Fuel (FUEL) ...................................................................... 105
General System (GEN) .....................................................106
3.4 EIS Display (Reversionary Mode) .....................108
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview .......................................................... 109
Audio Panel Volume Control ...........................................109
PFD Controls and Frequency Display ............................... 110
Audio Panel Controls ......................................................112
4.2 COM Operation ................................................114
COM Transceiver Manual Tuning ..................................... 115
Auto-Tuning the COM Frequency ....................................115
Frequency Spacing .........................................................118
4.3 NAV Operation .................................................119
NAV Tuning Boxes ...........................................................119
NAV Radio Selection and Activation................................120
NAV Receiver Manual Tuning ..........................................120
Auto-Tuning a NAV Frequency from the MFD .................121
Marker Beacon Receiver .................................................123
ADF/DME Tuning .............................................................124
4.4 Mode S Transponders .......................................127
Transponder Controls ......................................................127
Transponder Mode Selection ........................................... 128
Entering a Transponder Code ..........................................130
IDENT Function ...............................................................131
4.5 Additional Audio Panel Functions ....................132
Power-Up ........................................................................132
Mono/Stereo Headsets .................................................... 132
Speaker ...........................................................................132
Intercom ..........................................................................132
Passenger Address (PA) System ....................................... 133
Simultaneous COM Operation ........................................133
Clearance Recorder and Player .......................................133
Entertainment Inputs ......................................................134
4.6 Audio Panels Preflight Procedure ....................135
4.7 Abnormal Operation ........................................137
Stuck Microphone ...........................................................137
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TABLE OF CONTENTS
COM Tuning Failure ......................................................... 137
PFD Failure, Dual System ................................................. 137
Audio Panel Fail-Safe Operation ......................................138
Reversionary Mode .........................................................138
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction .....................................................139
Navigation Status Box and Data Bar ............................... 141
5.2 Using Map Displays ..........................................143
Map Orientation .............................................................143
Map Range .....................................................................145
Map Panning ...................................................................147
Measuring Bearing and Distance ....................................149
Topography .....................................................................150
Map Symbols ..................................................................153
Airways ...........................................................................158
Additional Navigation Map Items ...................................160
IFR/VFR Charts ................................................................163
5.3 Waypoints ........................................................166
Airports ...........................................................................167
Intersections ...................................................................174
NDBs ............................................................................... 176
VORs ...............................................................................178
VRPs ...............................................................................180
User Waypoints ...............................................................182
5.4 Airspaces .......................................................... 188
5.5 Direct-to-Navigation .......................................192
5.6 Flight Planning .................................................197
Flight Plan Creation ........................................................198
Flight Plan Import/Export ................................................201
Adding Waypoints to an Existing Flight Plan ...................206
Adding Airways to a Flight Plan ......................................210
Adding Procedures to a Stored Flight Plan ...................... 212
Flight Plan Storage ..........................................................217
Flight Plan Editing ........................................................... 220
Along Track Offsets .........................................................223
Parallel Track ...................................................................225
Activating a Flight Plan Leg ............................................227
Inverting a Flight Plan ..................................................... 227
Flight Plan Views .............................................................227
Closest Point of FPL.........................................................230
Collapsing Airways .......................................................... 231
User-Defined Holding Patterns ........................................231
5.7 Vertical Navigation ..........................................236
Altitude Constraints ........................................................237
Vertical Situation Display (VSD) ......................................240
5.8 Procedures .......................................................244
Departures ......................................................................246
Arrivals ...........................................................................248
Approaches ....................................................................250
5.9 Weight Planning ............................................... 259
Weight Caution And Warning Conditions ........................ 261
5.10 Trip Planning ....................................................262
Trip Planning ...................................................................262
5.11 Abnormal Operation ........................................266
SECTION 6 HAZARD AVOIDANCE
6.1 Data Link Weather............................................270
Activating Data Link Weather Services ............................ 271
Weather Product Age ......................................................274
Displaying Data Link Weather Products ..........................279
Connext Data Requests ...................................................288
Weather Product Overview .............................................292
FIS-B Weather Status .......................................................329
Abnormal Operations for Garmin Connext Weather .......331
6.2 Stormscope Lightning Detection System ......... 333
Using the Stormscope Page .............................................333
Setting Up Stormscope on the Navigation Map ..............335
6.3 Airborne Color Weather Radar .........................339
System Description ..........................................................339
Principles of Pulsed Airborne Weather Radar ..................339
Safe Operating Distance .................................................343
Basic Antenna Tilt Setup ..................................................344
Practical Application Using the Basic Tilt Setup ...............344
Weather Mapping and Interpretation .............................346
Ground Mapping and Interpretation ............................... 357
Additional Weather Radar Displays ................................. 357
System Status..................................................................360
6.4 Terrain Displays ................................................361
Relative Terrain Symbology .............................................362
Terrain Page ....................................................................365
Vertical Situation Display (VSD) Terrain ........................... 366
Terrain-SVT and TAWS-B Alerting Displays ......................370
Forward Looking Terrain Avoidance ................................373
Additional TAWS-B Alerting ............................................375
System Status..................................................................377
6.5 Traffic Information Service (TIS) ......................379
Displaying Traffic Data ....................................................380
Traffic Map Page .............................................................381
TIS Alerts ......................................................................... 382
System Status..................................................................384
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TABLE OF CONTENTS
6.6 TAS Traffic .........................................................386
TAS Theory of Operation .................................................386
TAS Alerts ........................................................................390
System Test .....................................................................391
Operation ........................................................................ 392
6.7 ADS-B Traffic ....................................................399
ADS-B System Overview .................................................399
Conflict Situational Awareness & Alerting (CSA) ............. 401
Airborne and Surface Applications ..................................403
Traffic Description ...........................................................404
Operation ........................................................................ 404
ADS-B System Status.......................................................410
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Overview .................................................413
Additional AFCS Controls ................................................ 415
Basic Autopilot Operation ...............................................416
7.2 Flight Director Operation ................................. 417
Activating the Flight Director ..........................................417
AFCS Status Box..............................................................418
Flight Director Modes......................................................419
Switching Flight Directors ...............................................419
Command Bars ...............................................................420
7.3 AFCS Modes .....................................................421
Vertical Modes ................................................................421
Lateral Modes .................................................................428
Combination modes (VNV, APR, NAV, BC, GA) ................433
7.4 Autopilot and Yaw Damper Operation .............444
Flight Control ..................................................................444
Engagement ....................................................................445
Control Wheel Steering ...................................................445
Disengagement ............................................................... 446
7.5 AFCS Annunciations and Alerts ........................ 447
Overspeed Protection ...................................................... 448
Underspeed Protection ....................................................448
Level Mode .....................................................................450
Emergency Descent Mode ...............................................451
7.6 Abnormal Operation ........................................452
Suspected Autopilot malfunction ....................................452
Overpowering Autopilot Servos ......................................452
SECTION 8 ADDITIONAL FEATURES
8.1 SafeTaxi ............................................................ 454
8.2 Charts ............................................................... 457
Split view ........................................................................458
ChartView .......................................................................459
FliteCharts .......................................................................468
IFR/VFR Charts ................................................................473
Airport Directory .............................................................474
8.3 Database Cycle number and revisions .............475
Cycle Number and Revision ............................................475
8.4 SiriusXM Radio Entertainment .........................477
Activating SiriusXM Satellite Radio Services ...................477
Using SiriusXM Radio ......................................................478
8.5 Flight Data Logging .........................................481
8.6 Satellite Telephone and sms messaging ..........483
Registering with Garmin Connext
®
................................483
Disable/Enable Iridium Transceiver .................................. 483
Telephone Communication..............................................484
Text Messaging (SMS) ..................................................... 491
8.7 Connext Setup..................................................503
8.8 Maintenance Logs ............................................ 505
8.9 Electronic Stability and Protection (ESP
) ....... 506
Roll Engagement .............................................................507
Pitch Engagement ........................................................... 508
Angle of Attack Protection ..............................................510
High Airspeed Protection ................................................510
8.10 Electronic Checklists ........................................511
8.11 Abnormal Operation ........................................513
SiriusXM Data Link Receiver Troubleshooting .................513
APPENDICES
Annunciations and Alerts .........................................515
CAS Message Prioritization ............................................. 516
CAS Messages.................................................................518
Audio Alerts ....................................................................520
System Message Advisories ............................................521
Database Management ............................................535
Loading Updated Databases ...........................................535
Magnetic Field Variation Database Update .....................542
Garmin Aviation Glossary ......................................... 545
Frequently Asked Questions .....................................555
Map Symbols ............................................................559
INDEX
Index ......................................................................... I-1
190-02218-00 Rev. EGarmin G1000 NXi Pilot’s Guide for the Daher TBM 910xvi
TABLE OF CONTENTS
Blank Page
190-02218-00 Rev. E
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910
1
SYSTEM OVERVIEW
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section provides an overview of the G1000 NXi Integrated Avionics System as installed in the Daher TBM
910. The system is an integrated avionics system that presents flight instrumentation, position, navigation,
communication, and identification information to the pilot through large-format displays.
The system is comprised of several Line Replaceable Units along with an optional Flight Stream 510 device.
The Flight Stream 510 provides a Bluetooth
®
connection between the system and a mobile device. GPS, AHRS,
ADS-B, traffic, SiriusXM audio, and weather data can then be shared with the mobile device, and flight plans can
be transferred to or from the mobile device. Also, database updates may be performed using the Flight Stream
510 WiFi link.
LINE REPLACEABLE UNITS (LRU)
- GDU 1050A (2) – Each unit is configured as a PFD that features a 10.5-inch LCD display. The unit installed
on the left/pilot side is designated as PFD1, and the one installed on the right/copilot side is designated
as PFD2. These units communicate with each other, the MFD, and with the on-side GIA 63W Integrated
Avionics Unit through a High-Speed Data Bus (HSDB) connection.
- GDU 1550 (1) – This unit features a 15-inch LCD display and is configured as an MFD. This unit is linked
to both PFDs via HSDB connection.
- GIA 63W (2) – Functions as the main communication hub, linking all LRUs with the PFD and MFD. Each
GIA 63W contains a GPS SBAS receiver, VHF COM/NAV/GS receivers, a flight director (FD) and system
integration microprocessors. Each GIA 63W is paired with the PFD and MFD via High Speed Database
connection. The GIA 63Ws are not paired together and do not communicate with each other directly.
- GDC 72B (2) – Processes data from the pitot/static system as well as the OAT probe. This unit provides
pressure altitude, airspeed, vertical speed and OAT information to the system, and it communicates with the
GIA 63Ws, the displays, and the GRS 79, using an ARINC 429 digital interface. The GDC 72B is designed to
operate in Reduced Vertical Separation Minimum (RVSM) airspace.
- GRS 79 (2) – Provides aircraft attitude and heading information via ARINC 429 to both displays and both
GIA 63Ws. The GRS 79 contains advanced sensors (including accelerometers and rate sensors) and interfaces
with the GMU 44 to obtain magnetic field information, with the GDC 72B to obtain air data, and with both
GIA 63Ws to obtain GPS information. AHRS modes of operation are discussed later in this document.
- GMU 44 (2) – Measures local magnetic field. Data is sent to the GRS 79 unit for processing to determine
aircraft magnetic heading. The GMU 44 receives power directly from the GRS unit, and communicates with
the GRS 79 unit using an RS-485 digital interface.
- GMA 1347D (2) – Integrates NAV/COM digital audio, intercom system and marker beacon controls, and is
installed in dual configuration on the outboard side of PFD1 and PFD2. This unit also enables the manual
control of the display reversionary mode (red DISPLAY BACKUP button) and communicates with the on-
side GIA 63W, using an RS-232 digital interface.
- GMC 710 (1) – Provides the controls for the Garmin AFCS through an RS-232 digital interface allowing
communication with both PFDs.
- GCU 475 – Provides the Flight Management System (FMS) controls for the MFD through an RS-232 digital
interface.
190-02218-00 Rev. EGarmin G1000 NXi Pilot’s Guide for the Daher TBM 9102
SYSTEM OVERVIEW
- GTX 33D ES (1), or the GTX 345R (optional) (1 or 2) – Solid state transponders that provide Mode A,
C, S capability. The standard GTX 33D includes Mode S with diversity and Extended Squitter Automatic
Dependent Surveillance (ADS-B out) transmission, and is indicated as ‘XPDR1’. The optional GTX 345R
provides ADS-B In/Out. The optional GTX 345R may be installed in addition to the GTX 33D, in which
case, it is indicated as ‘XPDR2’. The system may instead accommodate an optional dual set of GTX 345R
transponders as well, occupying ‘XPDR1’ and ‘XPDR2’. Only one transponder can be active at a time. Each
transponder communicates with the on-side GIA 63W through an RS-232 digital interface. If installed, the
(#1) GTX 345R communicates with the PFD via High Speed Database connection.
- GEA 71 (2) – Receives and processes signals from the engine and airframe sensors. This unit communicates
with both GIA 63Ws using an RS-485 digital interface.
- GSA 81
(4)
, and GSM 86 (1) – The GSA 81 servos are used for the automatic control of roll, yaw, pitch, and
pitch trim. These units interface with each GIA 63W.
- The GSM 86 servo gearbox is responsible for transferring the output torque of the GSA 81 servo actuator
to the mechanical flight-control surface linkage.
- GTA 82 – The GTA 82 Trim Adapter is a remote mounted device that is used to allow the AFCS to drive the
yaw trim actuator.
- GDL 69A SXM (1) (Optional) – A satellite radio receiver that provides data link weather information to the
MFD (and, indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL 69A
SXM communicates with the MFD via HSDB connection. Subscriptions to the SiriusXM Weather or SiriusXM
Satellite Radio services are required to enable the GDL 69A SXM capability.
- GTS 820 (Optional) – The GTS 820 Traffic Advisory System (TAS) uses active interrogations of Mode S and
Mode C transponders to provide traffic information to the pilot independent of the air traffic control system.
- GWX 70 (1) (Optional) – Provides airborne weather and ground mapped radar data to the MFD via HSDB
connection.
- GRA 55
(1) (Optional) – The optional Radar Altimeter provides altitude above the ground information and
rate of change of radar altitude information.
- GSR 56 (1) (Optional) - The Iridium Transceiver provides voice communications by means of a telephone
handset in the cabin and pilot and copilot headsets in the cockpit. The transceiver can also send and receive
short message service (SMS) text messages. The GSR 56 also receives data link weather products from the
Garmin Connext weather service through the Iridium satellite network.
Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are also shown in Figure
1-1. The system is capable of interfacing with the following optional equipment:
- GDL 69A SXM
Data Link Receiver
- GTS 820 Traffic Advisory System
- FS 510 Flight Stream (SD Card)
- GRA 55 Radio Altimeter
- GSR 56 Iridium Transceiver
-
WX 500
Stormscope Lightning Sensor
- KN 63 DME
- Becker ADF 3502
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Garmin G1000 NXi - Socata TBM 910 Reference guide

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