Garmin G1000 NXi - Socata TBM 850 Reference guide

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Reference guide

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®
Pilot’s Guide
Daher TBM 850/900
System Software Version 3086.00 or later
190-02348-00 Rev. C
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
Copyright © 2017-2019 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 3086.00 or later for the G1000 NXi Daher TBM 850/900. Some differences
in operation may be observed when comparing the information in this manual to earlier or later software versions.
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®
NXi,
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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 if
AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to
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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.
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
190-02348-00 Rev. C
AC-U-KWIK and its related organizations (hereafter collectively AC-U-KWIK Organizations”) expressly disclaim all warranties with
respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of
merchantability and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or
make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the
maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related
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Printed in the U.S.A
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190-02348-00 Rev. C
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
i
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: Always obtain qualified instruction prior to operational use of this equipment.
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.
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
190-02348-00 Rev. Cii
WARNINGS, CAUTIONS, AND NOTES
WARNING: When using the autopilot to fly 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
:
Because of variation in the earth’s magnetic field, do not rely on the accuracy of attitude and
heading indications in the following geographic areas: 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.
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: 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.
190-02348-00 Rev. C
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
iii
WARNINGS, CAUTIONS, AND NOTES
CAUTION: Do not clean display surfaces with abrasive cloths or cleaners containing ammonia. They will
harm the anti-reflective coating.
CAUTION:
Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or
modifications could void both the warranty and affect the airworthiness of the aircraft.
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.
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.
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
190-02348-00 Rev. Civ
WARNINGS, CAUTIONS, AND NOTES
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.
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: The system supports approval of AC 120-76C Hardware Class 3, Software Type B Electronic Flight Bag
(EFB) electronic aeronautical chart applications. Possible additional requirements may make a secondary
source (traditional paper or additional electronic display) necessary onboard the aircraft. If the secondary
source is a Portable Electronic Device (PED), its use must be consistent with guidance in AC 120-76C.
190-02348-00 Rev. C
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
v
WARNINGS, CAUTIONS, AND NOTES
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.
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.
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
190-02348-00 Rev. Cvi
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.
190-02348-00 Rev. C
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
vii
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-02348-00 A 12/5/17 i - I-6 Initial release for GDU 20.51
B 1/5/18 i - I-6 GDU 20.80 Revision:
Aircraft icon change
Heading/Track added to PFD display
Split Screen Display Title changes
True Airspeed/Mach number display change
Software License information reduced
Sofkey descriptions added
SVT Unusual Attitudes added
Delineated which OEM TAS systems is/are being described
Appendix message modifications/additions
C 8/15/19 All Add Baro VNAV
Clerical Updates
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
190-02348-00 Rev. Cviii
REVISION INFORMATION
Blank Page
190-02348-00 Rev. C
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
ix
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 ..................................................... 10
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 .......................................................... 33
System Utilities ........................................................... 43
1.5 Display Backlighting ............................................... 47
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................... 52
Attitude Indicator ....................................................... 52
Airspeed Indicator ...................................................... 53
Altimeter ................................................................... 55
Vertical Speed Indicator (VSI) ....................................... 58
Vertical Deviation ....................................................... 59
Vertical Navigation (VNV) Indications ........................... 61
Angle of Attack (AOA) Indicator ................................... 62
Radar Altimeter .......................................................... 62
Horizontal Situation Indicator (HSI) .............................. 65
Course Deviation Indicator (CDI) .................................. 68
Turn Rate Indicator ..................................................... 74
Bearing Pointers and Information Windows ................... 75
DME Information Window ........................................... 76
2.2 Supplemental Flight Data ...................................... 77
Generic Timer ............................................................. 77
Temperature Displays .................................................. 77
Wind Data ................................................................. 78
2.3 PFD Annunciations and Alerting Functions .......... 79
Altitude Alerting ......................................................... 79
Low Altitude Annunciation .......................................... 79
Marker Beacon Annunciations...................................... 80
Minimum Descent Altitude/Decision Height Alerting ...... 80
2.4 Garmin SVT (Synthetic Vision Technology) ........... 82
SVT Operation ............................................................ 83
SVT Features .............................................................. 85
Field of View ..............................................................94
2.5 Abnormal Operations ............................................. 95
Abnormal GPS Conditions ........................................... 95
Comparator Annunciations .......................................... 96
Reversionary Sensor Annunciations .............................. 97
Unusual Attitudes ....................................................... 98
SVT Unusual Attitudes ................................................. 99
SECTION 3 ENGINE AND AIRFRAME SYSTEMS
3.1 Engine Display ....................................................... 102
3.2 Landing Field Elevation (LFE) (TBM 900 Only) ... 106
3.3 Synoptics ............................................................... 107
Electrical (ELEC) ........................................................ 107
Fuel (FUEL) .............................................................. 110
General System (GEN) ............................................... 111
3.4 EIS Display (Reversionary Mode) ........................ 113
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview ................................................................ 115
Audio Panel Volume Control ...................................... 115
PFD Controls and Frequency Display ........................... 116
Audio Panel Controls ................................................ 118
4.2 COM Operation...................................................... 120
COM Transceiver Manual Tuning ................................ 121
Auto-Tuning the COM Frequency ................................ 121
Frequency Spacing .................................................... 124
4.3 NAV Operation....................................................... 125
NAV Tuning Boxes..................................................... 125
NAV Radio Selection and Activation ........................... 126
NAV Receiver Manual Tuning ..................................... 126
Auto-Tuning a NAV Frequency from the MFD............... 127
Marker Beacon Receiver ............................................ 129
ADF/DME Tuning ...................................................... 130
4.4 Mode S Transponders ........................................... 133
Transponder Controls ................................................ 133
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
190-02348-00 Rev. Cx
TABLE OF CONTENTS
Transponder Mode Selection ...................................... 134
Entering a Transponder Code ..................................... 136
IDENT Function ........................................................ 136
4.5 Additional Audio Panel Functions ....................... 137
Power-Up ................................................................. 137
Mono/Stereo Headsets .............................................. 137
Speaker ................................................................... 137
Intercom .................................................................. 137
Passenger Address (PA) System .................................. 138
Simultaneous COM Operation .................................... 138
Clearance Recorder and Player ................................... 138
Entertainment Inputs ................................................ 139
4.6 Audio Panels Preflight Procedure ....................... 140
4.7 Abnormal Operation ............................................. 142
Stuck Microphone ..................................................... 142
COM Tuning Failure ................................................... 142
PFD Failure, Dual System ...........................................142
Audio Panel Fail-Safe Operation ................................. 143
Reversionary Mode ................................................... 143
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ........................................................... 145
Navigation Status Box and Data Bar ........................... 147
5.2 Using Map Displays .............................................. 149
Map Orientation ....................................................... 149
Map Range .............................................................. 152
Map Panning ............................................................ 153
Measuring Bearing and Distance ................................ 156
Topography .............................................................. 157
Map Symbols ........................................................... 160
Airways ................................................................... 165
Additional Navigation Map Items ............................... 167
5.3 Waypoints .............................................................. 170
Airports ................................................................... 171
Intersections ............................................................ 178
NDBs ....................................................................... 180
VORs ....................................................................... 182
VRPs ....................................................................... 184
User Waypoints ........................................................ 186
5.4 Airspaces ................................................................ 192
5.5 Direct-to-Navigation ........................................... 196
5.6 Flight Planning ...................................................... 201
Flight Plan Creation .................................................. 202
Flight Plan Import/Export........................................... 205
Adding Waypoints to an Existing Flight Plan ................ 211
Adding Airways to a Flight Plan ................................. 215
Adding Procedures to a Stored Flight Plan .................. 216
Flight Plan Storage ................................................... 222
Flight Plan Editing .................................................... 224
Along Track Offsets ................................................... 227
Parallel Track ............................................................ 228
Activating a Flight Plan Leg ....................................... 231
Inverting a Flight Plan ............................................... 231
Flight Plan Views ...................................................... 231
Closest Point of FPL .................................................. 234
Collapsing Airways ................................................... 234
User-Defined Holding Patterns ................................... 235
5.7 Vertical Navigation ............................................... 240
Altitude Constraints .................................................. 241
Vertical Situation Display (VSD) .................................. 244
5.8 Procedures ............................................................. 248
Departures ............................................................... 250
Arrivals ................................................................... 252
Approaches ............................................................. 254
5.9 Weight Planning .................................................... 262
Weight Caution And Warning Conditions .................... 264
5.10 Trip Planning .......................................................... 265
Trip Planning ............................................................ 265
5.11 Abnormal Operation ............................................. 269
SECTION 6 HAZARD AVOIDANCE
6.1 Data Link Weather ................................................ 272
Activating Data Link Weather Services ........................ 273
Weather Product Age ................................................ 276
Displaying Data Link Weather Products ....................... 281
Connext Data Requests ............................................. 290
Weather Product Overview ........................................ 294
FIS-B Weather Status................................................. 328
Abnormal Operations for Garmin Connext Weather ..... 330
6.2 Stormscope Lightning Detection System ........... 332
Using the Stormscope Page ....................................... 332
Setting Up Stormscope on the Navigation Map ........... 334
6.3 Airborne Color Weather Radar ............................ 338
System Description ................................................... 338
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Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
xi
TABLE OF CONTENTS
Principles of Pulsed Airborne Weather Radar ............... 338
Safe Operating Distance ............................................ 342
Basic Antenna Tilt Setup ............................................ 343
Practical Application Using the Basic Tilt Setup ............ 343
Ground Mapping and Interpretation ........................... 357
Additional Weather Radar Displays ............................. 358
System Status ........................................................... 360
6.4 Terrain Displays ..................................................... 362
Relative Terrain Symbology ........................................ 363
Terrain Page ............................................................. 366
Vertical Situation Display (VSD) Terrain ....................... 367
Terrain-SVT and TAWS-B Alerting Displays ................... 370
Forward Looking Terrain Avoidance ............................ 374
Additional TAWS-B Alerting ....................................... 376
System Status ........................................................... 378
6.5 Traffic Information Service (TIS) .......................... 380
Displaying Traffic Data .............................................. 381
Traffic Map Page ....................................................... 382
TIS Alerts ................................................................. 383
System Status ........................................................... 385
6.6 TAS Traffic ............................................................... 387
TAS Theory of Operation ............................................ 387
TAS Alerts ................................................................ 391
System Test .............................................................. 392
Operation ................................................................ 393
6.7 ADS-B Traffic .......................................................... 401
ADS-B System Overview ............................................ 401
Conflict Situational Awareness & Alerting (CSA) .......... 403
Airborne and Surface Applications .............................. 404
Traffic Description ..................................................... 405
Operation ................................................................ 405
ADS-B System Status ................................................ 411
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Overview ...................................................... 415
Additional AFCS Controls .......................................... 417
Basic Autopilot Operation .......................................... 418
7.2 Flight Director Operation ..................................... 419
Activating the Flight Director ..................................... 419
AFCS Status Box ....................................................... 420
Flight Director Modes ................................................ 421
Switching Flight Directors .......................................... 421
Command Bars ......................................................... 422
7.3 AFCS Modes ........................................................... 423
Vertical Modes ......................................................... 423
Lateral Modes .......................................................... 430
Combination modes (VNV, APR, NAV, BC, GA) ............. 435
7.4 Autopilot and Yaw Damper Operation ............... 446
Flight Control ........................................................... 446
Engagement ............................................................. 447
Control Wheel Steering ............................................. 447
Disengagement ........................................................ 448
7.5 AFCS Annunciations and Alerts ........................... 449
Overspeed Protection ................................................ 450
Underspeed Protection .............................................. 450
Level Mode (if installed) ............................................ 452
Emergency Descent Mode ......................................... 453
7.6 Abnormal Operation ............................................. 454
Suspected Autopilot malfunction ................................ 454
Overpowering Autopilot Servos .................................. 454
SECTION 8 ADDITIONAL FEATURES
8.1 SafeTaxi .................................................................. 456
8.2 Charts ..................................................................... 459
Split view ................................................................. 460
ChartView ................................................................ 461
FliteCharts ............................................................... 470
IFR/VFR Charts ......................................................... 475
Airport Directory ....................................................... 479
8.3 Database Cycle number and revisions ............... 480
Cycle Number and Revision ....................................... 480
8.4 SiriusXM Radio Entertainment ............................ 482
Activating SiriusXM Satellite Radio Services ................ 482
Using SiriusXM Radio ................................................ 483
8.5 Flight Data Logging .............................................. 486
8.6 Satellite Telephone and sms messaging ............ 488
Registering with Garmin Connext .............................. 488
Disable/Enable Iridium Transceiver.............................. 488
Telephone Communication ........................................ 489
Text Messaging (SMS) ............................................... 497
8.7 Connext Setup ....................................................... 509
8.8 Maintenance Logs ................................................. 511
8.9 Electronic Stability and Protection (ESP) ........... 512
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190-02348-00 Rev. Cxii
TABLE OF CONTENTS
Roll Engagement ...................................................... 513
Pitch Engagement..................................................... 515
Angle of Attack Protection ......................................... 516
High Airspeed Protection ........................................... 517
8.10 Electronic Checklists ............................................. 518
8.11 Abnormal Operation ............................................. 520
SiriusXM Data Link Receiver Troubleshooting .............. 520
APPENDICES
Annunciations and Alerts ............................................... 521
CAS Message Prioritization ........................................ 521
Audio Alerts ............................................................. 525
System Message Advisories ....................................... 526
Database Management .................................................. 541
Loading Updated Databases ...................................... 541
Magnetic Field Variation Database Update .................. 548
Garmin Aviation Glossary .............................................. 551
Frequently Asked Questions .......................................... 561
Miscellaneous
Map Symbols ......................................... 565
INDEX
Index .................................................................................. I-1
190-02348-00 Rev. C
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
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
850/900. The system is an integrated avionics system that presents flight instrumentation, position, navigation,
communication, and identification information to the pilot through large-format displays.
LINE REPLACEABLE UNITS (LRU)
GDU 1050A
(2) – Each unit is configured as a PFD that features a 10 inch, high resolution LED backlit
display unit. 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 high resolution LED backlit 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 74B
(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 77, using an ARINC 429 digital interface. The GDC 74B is designed to
operate in Reduced Vertical Separation Minimum (RVSM) airspace.
GRS 77
(2) – Provides aircraft attitude and heading information via ARINC 429 to both displays and both
GIA 63Ws. The GRS 77 contains advanced sensors (including accelerometers and rate sensors) and interfaces
with the GMU 44 to obtain magnetic field information, with the GDC 74B 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 77 unit for processing to determine
aircraft magnetic heading. The GMU 44 receives power directly from the GRS unit, and communicates with
the GRS 77 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
(1) – Provides the Flight Management System (FMS) controls for the MFD through an RS-232
digital interface.
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.
GTA 82 (1)
– The GTA 82 Trim Adapter is a remote mounted device that is used to allow the AFCS to drive
the yaw trim actuator.
190-02348-00 Rev. C
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
2
SYSTEM OVERVIEW
GTX 33 / 33D / 33 ES / 33D ES / 345 (2) – There are two transponders installed. Standard and alternate
transponder models and combinations are dependent upon aircraft locale and configuration. The GTX 33
is a solid state base model that provides Mode A, C, and S capability. The GTX 33D includes Mode S with
diversity (“D”) and the GTX 33 ES (Extended Squitter) provides Automatic Dependent Surveillance (ADS-B
out) transmission. The GTX 345 provides ADS-B In/Out. Only one transponder can be active at a time. Each
transponder communicates with the on-side GIA 63W through an RS-232 digital interface.
GSA 81 (4)
and
GSM 85 or 86
(4) – 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 85 and 86 servo gearboxes are responsible for transferring the output torque of the GSA 81 servo
actuator to the mechanical flight-control surface linkage.
GDL 69A or 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 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 or KTA 810
(1) (Optional) –
The Traffic Advisory System (TAS) uses active interrogations of Mode S
and C transponders to provide traffic information to the pilot independent of the air traffic control system.
GWX 68 or 70
(1) (Optional) – Provides airborne weather and ground mapped radar data to the MFD.
GRA 55, KRA 405B, or RA 4500
(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.
Flight Stream 210 or 510
(1) (Optional) - The Flight Stream 210 LRU or the 510 SD Card provide a Bluetooth
®
connection between the system and a mobile device. GPS, AHRS, ADS-B, traffic, Sirius XM audio, and FIS-B
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 also be performed using the Flight Stream WiFi link.
RA 3502
(1) (Optional) – Becker Automatic Direction Finder.
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:
FS 210 or 510
Flight Stream (SD Card)
GDL 69A or GDL 69A SXM
Data Link Receiver
GRA 55
Radar Altimeter
GSR 56
Iridium Transceiver
GTS 820 Traffic Avoidance System
GTS 820
Traffic Advisory System
GWX 68/70
Weather Radar
KN 63 DME
KRA 405B Honeywell Radar Altimeter
KTA 810 Traffic Avoidance System
RA 4500 Free Flight Radar Altimeter
RA 3502 Becker ADF
WX 500
Stormscope Lightning Sensor
Angle of Attack Sensor
Flight Data Recorder
190-02348-00 Rev. C
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
3
SYSTEM OVERVIEW
GDU 1050A
(PFD1)
#1 GIA 63W
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
AFCS Mode
Logic
Flight
Director
Servo
Management
#2 GIA 63W
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
AFCS Mode
Logic
Flight
Director
Servo
Management
GDU 1050A
(PFD2)
Non-Garmin Equipment
GSR 56
(Iridium
Transceiver)
GDU 1550
(MFD)
GEA 71
(Engine &
Airframe 1/2)
#1 GMU 44
(Magnetometer)
#2 GMU 44
(Magnetometer)
#1 GDC 74B
(Air Data
Computer)
Optional
Garmin Equipment
Optional
Non-Garmin Equipment
GTS 820
or
Garmin Equipment
GCU 475
(Display
Controller)
#1 GMA 1347D
(Audio Panel)
#2 GMA 1347D
(Audio Panel)
GMC 710
(AFCS
Controller)
GWX 68 or 70
(Weather Radar)
#1 GRS 77
(Attitude & Heading)
#2 GRS 77
(Attitude & Heading)
#1 GSA 81 (Pitch)
#2 GSA 81 (Yaw)
#3 GSA 81 (Roll)
RA 4500
(Radar
Altimeter)
#2 GDC 74B
(Air Data
Computer)
RA 3502
(ADF)
KN 63
(DME)
WX 500
Stormscope
#4 GSA 81
(Pitch Trim)
FS 510
(SD Card
Bluetooth
Link)
OAT Probe
OAT Probe
GTA 82
(Trim Adapter)
KTA 810
(TAS)
KRA 405B
or
GRA 55
or
GDL 69A or
GDL 69A SXM
(Weather Datalink)
FS 210
(Flight Stream)
GTX 33,
GTX 33 ES, or
GTX 345
(#2 Transponder)
Flight
Data
Recorder
AOA
Sensor
GTX 33D,
GTX 33D ES, or
GTX 345
(#1 Transponder)
Figure 1-1 System (LRU Configuration)
NOTE: For information on non-Garmin equipment, consult the applicable optional interface user’s guide.
This document assumes that the reader is already familiar with the operation of this additional equipment.
190-02348-00 Rev. C
Garmin G1000 NXi Pilot’s Guide for the Daher TBM 850/900
4
SYSTEM OVERVIEW
1.2 SYSTEM CONTROLS
NOTE: The Audio Panel (GMA 1347D Cabin) and AFCS controls (GMC 710) are described in the Audio & CNS
and AFCS sections respectively.
The system controls are located on the PFD and MFD bezels, MFD Control Unit, AFCS Control Unit and audio
panel. The controls for the PFD and MFD are discussed within the following pages of this section.
PFD CONTROLS
Figure 1-2 PFD Controls
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