Garmin G1000 NXi: Diamond DA40NG User guide

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User guide

This manual is also suitable for

Pilot’s Guide
190-02452-00
Revision A
Garmin International, Inc.
1200 East 151st Street
Olathe, Kansas 66062, U.S.A.
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
Garmin Corporation
No. 68, Zhangshu 2nd Road
Xizhi District,
New Taipei City, Taiwan
Contact Garmin Product Support at: www.flygarmin.com
For warranty information refer to: www.flygarmin.com
Cirrus SR2x
G1000
®
NXi Pilot’s Guide Diamond DA40NG
Diamond DA40NG
®
SYSTEM OVERVIEW
FLIGHT INSTRUMENTS
EIS
AUDIO PANEL & CNS
FLIGHT MANAGEMENT
HAZARD AVOIDANCE
AFCS
ADDITIONAL FEATURES
APPENDICES
INDEX
190-02452-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA40NG
Copyright © 2018 Garmin Ltd. or its subsidiaries. All rights reserved..
This manual reflects the operation of System Software version 1929.10 or later for the Diamond DA40NG. Some differences in operation
may be observed when comparing the information in this manual to earlier or later software versions.
Garmin International, Inc.
1200 East 151st Street
Olathe, Kansas 66062, U.S.A.
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 at www.flygarmin.com.
For warranty information refer to www.flygarmin.com.
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored
in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download
a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for
personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice
and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin
®
G1000
®
NXi, FliteCharts
®
, and SafeTaxi
®
are registered trademarks of Garmin International, Inc. or its subsidiaries. Garmin ESP
,
Garmin SVT
, Connext
, and WireAware
are trademarks of Garmin International, Inc. or its subsidiaries. These trademarks may not be
used without the express permission of Garmin.
Skywatch
®
and Stormscope
®
are registered trademarks of L-3 Communications. Ryan
®
, TCAD
®
and Avidyne
®
are registered trademarks of
Avidyne Corporation. CO Guardian is a trademark of CO Guardian, Inc. AC-U-KWIK
®
is a registered trademark of Penton Business Media
Inc. Bendix/King
®
and Honeywell
®
are registered trademarks of Honeywell International, Inc. Becker
®
is a registered trademark of Becker
Flugfunkwerk GmbH. NavData
®
is a registered trademark of Jeppesen, Inc.; Wi-Fi
®
is a registered trademark of the Wi-Fi Alliance. Sirius,
XM, and all related marks and logos are trademarks of Sirius XM Radio, Inc. and its subsidiaries. The Bluetooth
®
word mark and logos are
owned by the Bluetooth SIG, Inc. and any use of such marks by Garmin is under license.
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively AOPA”) expressly disclaim all warranties,
with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties
of merchantability and fitness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any
representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any
incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if
AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to
the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual
or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for
incidental or consequential damages so the above limitations or exclusions may not apply to you.
Garmin G1000 NXi Pilot’s Guide for the Diamond DA40NG
190-02452-00 Rev. A
AC-U-KWIK and its related organizations (hereafter collectively AC-U-KWIK Organizations”) expressly disclaim all warranties with
respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of
merchantability and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or
make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the
maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related
to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some jurisdictions
do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations
or exclusions may not apply to licensee.
Printed in the U.S.A.
190-02452-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA40NG
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: Do not rely on the displayed minimum safe altitude (MSAs) 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.
Garmin G1000 NXi Pilot’s Guide for the Diamond DA40NG
190-02452-00 Rev. Aii
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: 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.
190-02452-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA40NG
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:
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.
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 Diamond DA40NG
190-02452-00 Rev. Aiv
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
current version of the pertinent flight manual 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: Operate G1000NXi system power through at least one cycle in a period of four days of continuous
operation to avoid an autonomous system reboot.
190-02452-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA40NG
v
WARNINGS, CAUTIONS, AND NOTES
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: 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: Intruder aircraft at or below 500 ft. AGL may not appear on the Garmin SVT display or may appear as
a partial symbol.
Garmin G1000 NXi Pilot’s Guide for the Diamond DA40NG
190-02452-00 Rev. A
SOFTWARE LICENSE AGREEMENT
vi
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.
190-02452-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA40NG
vii
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-02452-00 A 06/7/18 All Initial Release for GDU 20.80
Garmin G1000 NXi Pilot’s Guide for the Diamond DA40NG
190-02452-00 Rev. Aviii
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................... 1
Line Replaceable Units (LRU) ......................................... 1
1.2 System Controls ........................................................ 4
PFD/MFD Controls ........................................................ 4
Secure Digital Cards ...................................................... 7
1.3 System Operation ..................................................... 8
System Power-up .......................................................... 8
Normal Operation ......................................................... 8
Reversionary Mode ....................................................... 9
System Annunciations ................................................. 10
System Status ............................................................. 11
AHRS Operation ......................................................... 12
GPS Receiver Operation .............................................. 14
1.4 Accessing System Functionality ............................ 19
Softkey Function ......................................................... 19
Menus ....................................................................... 23
MFD Page Groups ....................................................... 24
Split Screen Functionality ............................................ 28
System Settings .......................................................... 30
System Utilities ........................................................... 40
1.5 Display Backlighting ............................................... 44
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................... 48
Attitude Indicator ....................................................... 48
Airspeed Indicator ...................................................... 49
Altimeter ................................................................... 50
Vertical Speed Indicator (VSI) ....................................... 54
Vertical Deviation ....................................................... 54
Horizontal Situation Indicator (HSI) .............................. 56
Course Deviation Indicator (CDI) .................................. 60
2.2 Supplemental Flight Data ...................................... 67
Generic Timer ............................................................. 67
Temperature Displays .................................................. 67
Wind Data ................................................................. 68
Vertical Navigation (VNV) Indications ........................... 69
2.3 PFD Annunciations and Alerting Functions .......... 70
Marker Beacon Annunciations...................................... 70
Altitude Alerting ......................................................... 70
Low Altitude Annunciation .......................................... 71
Minimum Descent Altitude/Decision Height Alerting ...... 71
2.4 Garmin Synthetic Vision Technology (SVT) ........... 73
SVT Operation ............................................................ 74
SVT Features .............................................................. 75
Field of View .............................................................. 84
2.5 Abnormal Operations ............................................. 86
Abnormal GPS Conditions ........................................... 86
SVT Troubleshooting ................................................... 87
Unusual Attitudes ....................................................... 87
SVT Unusual Attitudes ................................................. 88
SECTION 3 ENGINE INDICATION SYSTEM (EIS)
3.1 Engine Display ......................................................... 90
3.2 Engine Page ............................................................. 92
Fuel Calculations ........................................................ 94
3.3 Reversionary Mode ................................................. 95
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview .................................................................. 97
PFD Controls and Frequency Display ............................. 98
Audio Panel Controls ................................................ 100
4.2 COM Operation...................................................... 103
COM TUNING BOXES ................................................ 103
COM Transceiver Manual Tuning ................................ 104
Auto-Tuning the COM Frequency ................................ 104
Frequency Spacing ................................................... 107
4.3 NAV Operation....................................................... 108
NAV Tuning Boxes..................................................... 108
NAV Radio Selection and Activation ........................... 109
NAV Receiver Manual Tuning ..................................... 109
Auto-Tuning a NAV Frequency from the MFD............... 110
Marker Beacon Receiver ............................................ 112
ADF/DME ................................................................. 113
ADF Tuning .............................................................. 114
DME Tuning ............................................................. 116
4.4 Mode S Transponder ............................................. 117
Transponder Controls ................................................ 117
Transponder Mode Selection ...................................... 118
Entering a Transponder Code ..................................... 120
IDENT Function ........................................................ 120
4.5 Additional Audio Panel Functions ....................... 122
Power-Up ................................................................. 122
Mono/Stereo Headsets .............................................. 122
Speaker ................................................................... 122
190-02452-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA40NG
ix
TABLE OF CONTENTS
Intercom .................................................................. 122
Blue-Select Mode (Telephone/Entertainment Distribution) ..
125
3D Audio ................................................................. 126
Bluetooth
®
.................................................................................................................127
Clearance Recorder and Player ................................... 128
Entertainment Inputs ................................................ 129
4.6 Audio Panel Preflight Procedure ......................... 130
4.7 Abnormal Operation ............................................. 131
Stuck Microphone ..................................................... 131
COM Tuning Failure ................................................... 131
Audio Panel Fail-Safe Operation ................................. 131
Reversionary Mode ................................................... 131
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ........................................................... 133
Navigation Status Box and Data Bar ........................... 135
5.2 Using Map Displays .............................................. 136
Map Orientation ....................................................... 136
Map Range .............................................................. 138
Map Panning ............................................................ 140
Measuring Bearing and Distance ................................ 142
Topography .............................................................. 142
Map Symbols ........................................................... 145
Airways ................................................................... 149
Additional Navigation Map Items ............................... 151
5.3 Waypoints .............................................................. 154
Airports ................................................................... 155
Non-Airport Waypoints .............................................. 160
5.4 Airspaces ................................................................ 169
Nearest Airspace ...................................................... 170
Smart Airspace ......................................................... 172
5.5 Direct-to-Navigation ........................................... 173
5.6 Flight Planning ...................................................... 178
Flight Plan Views ...................................................... 181
Creating a Flight Plan ............................................... 184
Flight Plan Waypoint and Airway Modifications ........... 185
Flight Plan Operations ............................................... 193
Closest Point of FPL .................................................. 196
User-Defined Holding Patterns ................................... 197
Managing Flight Plans .............................................. 201
5.7 Vertical Navigation ............................................... 210
Altitude Constraints .................................................. 212
Vertical Situation Display (VSD) .................................. 214
5.8 Procedures ............................................................. 218
Departures ............................................................... 220
Arrivals ................................................................... 223
Approaches ............................................................. 226
5.9 Trip Planning .......................................................... 234
Trip Planning ............................................................ 234
5.10 Abnormal Operation ............................................. 238
SECTION 6 HAZARD AVOIDANCE
6.1 Data Link Weather ................................................ 242
Activating Data Link Weather Services ........................ 243
Weather Product Age ................................................ 246
Displaying Data Link Weather Products ....................... 251
Connext Data Requests ............................................. 260
Weather Product Overview ........................................ 264
FIS-B Weather Status................................................. 300
Abnormal Operations for Garmin Connext Weather ..... 301
6.2 Stormscope Lightning Detection System ........... 303
Using the Stormscope Page ....................................... 303
Setting Up Stormscope on the Navigation Map ........... 305
6.3 Terrain Displays ..................................................... 307
Relative Terrain Symbology ........................................ 308
Terrain-SVT Alerting Displays ..................................... 313
Forward Looking Terrain Avoidance ............................ 315
System Status ........................................................... 316
6.4 Traffic Information Service (TIS) .......................... 318
Displaying Traffic Data .............................................. 319
Traffic Map Page ....................................................... 320
TIS Alerts ................................................................. 321
System Status ........................................................... 323
6.5 Avidyne TAS600 Traffic ......................................... 325
TAS Theory of Operation ............................................ 325
TAS Alerts ................................................................ 327
System Test .............................................................. 328
Operation ................................................................ 329
6.6 ADS-B Traffic .......................................................... 335
ADS-B System Overview ............................................ 335
Conflict Situational Awareness & Alerting (CSA) .......... 337
Garmin G1000 NXi Pilot’s Guide for the Diamond DA40NG
190-02452-00 Rev. Ax
TABLE OF CONTENTS
Airborne and Surface Applications .............................. 339
Traffic Description ..................................................... 341
Operation ................................................................ 342
ADS-B System Status ................................................ 347
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Overview ...................................................... 351
Additional AFCS Controls .......................................... 353
7.2 Flight Director Operation ..................................... 354
Activating the Flight Director ..................................... 354
AFCS Status Box ....................................................... 355
Flight Director Modes ................................................ 355
Command Bars ......................................................... 356
7.3 AFCS MODES .......................................................... 357
Vertical Modes ......................................................... 357
Lateral Modes .......................................................... 363
7.4 Autopilot Operation ............................................. 379
Flight Control ........................................................... 379
Engagement ............................................................. 380
Control Wheel Steering ............................................. 380
Disengagement ........................................................ 381
7.5 AFCS Annunciations and Alerts ........................... 382
Overspeed Protection ................................................ 382
7.6 Abnormal Operation ............................................. 384
Suspected Autopilot Malfunction ............................... 384
Overpowering Autopilot Servos .................................. 384
SECTION 8 ADDITIONAL FEATURES
8.1 SafeTaxi .................................................................. 386
8.2 Charts ..................................................................... 389
ChartView ................................................................ 390
FliteCharts ............................................................... 398
IFR/VFR Charts ......................................................... 403
8.3 AIrport Directory ................................................... 406
8.4 Database Cycle Number and Revisions .............. 407
Cycle Number and Revision ....................................... 407
8.5 SiriusXM Radio Entertainment ............................ 409
Activating SiriusXM Satellite Radio Services ................ 409
Using SiriusXM Radio ................................................ 410
8.6 Flight Data Logging .............................................. 413
8.7 Satellite Telephone and SMS Messaging ........... 415
Registering with Garmin Connext .............................. 415
Disabling/Enabling Iridium Transceiver ........................ 415
Telephone Communication ........................................ 416
8.8 Connext Setup ....................................................... 436
8.9 Electronic Stability and Protection (ESP) ........... 438
Roll Engagement ...................................................... 439
Pitch Engagement..................................................... 441
Angle of Attack Protection ......................................... 442
High Airspeed Protection ........................................... 442
8.10 Electronic Checklists ............................................. 443
8.11 Abnormal Operation ............................................. 445
SiriusXM Data Link Receiver Troubleshooting .............. 445
APPENDICES
Annunciations and Alerts ............................................... 447
CAS Message Prioritization ........................................ 448
CAS Annunciations ................................................... 449
Audio Alerting System Test ........................................ 451
System Message Advisories ....................................... 451
Database Management .................................................. 461
Loading Updated Databases ...................................... 461
Database Deletion Feature ....................................... 473
Magnetic Field Variation Database Update .................. 474
Aviation Terms and Acronyms ........................................ 475
Frequently Asked Questions .......................................... 485
Miscellaneous
Map Symbols ......................................... 489
INDEX
Index .................................................................................. I-1
190-02452-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA40NG
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
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 Diamond
DA40NG. The system presents flight instrumentation, position, navigation, communication, and identification
information to the pilot through large-format displays.
NOTE: Refer to the Automatic Flight Control System (AFCS) Section for details on the Garmin AFCS.
LINE REPLACEABLE UNITS (LRU)
The system consists of the following Line Replaceable Units (LRUs):
GDU 1050
(1) – The GDU 1050 is configured as a Primary Flight Display (PFD). The display communicates
with the Multi Function Display (MFD) and with the #1 Integrated Avionics Unit (IAU) through a High-Speed
Data Bus (HSDB) Ethernet connection.
GDU 1055
(1) – The GDU 1055 is configured as a Multi Function Display (MFD. The display communicates
with the PFD and with the #2 Integrated Avionics Unit (IAU) through an HSDB Ethernet connection.
GIA 63W / GIA 64W
(2) – The GIA Integrated Avionics Units (IAU) function as the main communication
hub, linking all LRUs with the PFD and MFD. Each IAU contains a GPS SBAS receiver, VHF COM/NAV/GS
receivers, a flight director (FD) and system integration microprocessors. Each IAU is paired with the PFD
and MFD via HSDB connection. The IAUs are not paired together and do not communicate with each other
directly.
GRS 79
(1) – The GRS Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading
information via ARINC 429 to both displays and both IAUs. The AHRS contains advanced sensors (including
accelerometers and rate sensors) and interfaces with the Magnetometer to obtain magnetic field information,
and with the Air Data Computer to obtain air data. The AHRS communicates with both IAUs to obtain GPS
information.
GMU 44
(1) – The GMU Magnetometer measures local magnetic field. Data is sent to the AHRS unit for
processing to determine aircraft magnetic heading. The Magnetometer receives communicates with and
receives power directly from the AHRS using an RS-485 digital interface.
GDC 72
(1) – The GDC Air Data Computer (ADC) processes data from the pitot/static system as well as the
Outside Air Temperature (OAT) probe. This unit provides pressure altitude, airspeed, vertical speed and
OAT information to the system, and it communicates with the IAUs, PFD, MFD, and the AHRS, using an
ARINC 429 digital interface (it also interfaces directly with the Air Temperature Probe).
GEA 71 / GEA 71B
(1) – The GEA Engine Airframe Unit receives and processes signals from the engine and
airframe sensors. This unit communicates with both IAUs using an RS-485 digital interface.
GMA 1347 / GMA 1360
(1) – The GMA Audio Panel integrates NAV/COM digital audio, intercom system
and marker beacon controls. This unit also enables the manual control of the display reversionary mode (red
DISPLAY BACKUP
button) and communicates with the #1 IAU, using an HSDB connection. The GMA 1360
offers Bluetooth® capability.
190-02452-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA40NG
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
2
SYSTEM OVERVIEW
GTX 335R (Standard) / GTX345R (Alternate)(1) – Solid-state transponder that provides Mode A, C, S capability.
The GTX 345R also provides ADS-B In/Out. The transponder can be controlled from the PFD. The transponder
communicates with the both IAUs through an RS-232 digital interface.
GSA 81
(3), and
GSM 86/85
(3) – The GSA Servos are used for the automatic control of roll, pitch, yaw, and
pitch trim. These units interface with each IAU.
The GSM 86/85 servo gearbox is responsible for transferring the output torque of the GSA 81 servo actuator
to the mechanical flight-control surface linkage.
GDL 69A SXM
(1) (Optional) – The GDL SiriusXM Datalink Receiver provides data link weather information
to the MFD (and, indirectly, to PFD map) as well as digital audio entertainment. The unit communicates
with the MFD via HSDB connection. Subscriptions to the SiriusXM Weather or SiriusXM Satellite Radio are
required to enable services.
GSR 56
(1) (Optional) – The GSR Iridium Transceiver operation for voice communication is by means of
pilot and copilot headsets in the cockpit. The transceiver can provide Garmin Connext Weather and SMS
functions.
Flight Stream 510
(1) (Optional) – The Flight Stream Bluetooth Transceiver provides wireless connectivity
between a compatible tablet/mobile device and the avionics system. GPS, AHRS, ADC, 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.
Figure 1-1 shows interactions between the LRUs. Additional optional equipment are also shown in Figure
1-1. The system is also capable of interfacing with the following optional equipment:
KN 63 DME
RA 3502 ADF Receiver
TAS 600 Traffic Advisory System
WX-500 Stormscope Lightning Sensor
NOTE: For information on the additional equipment shown in Figure 1-1, consult the applicable optional
interface user’s guide. This document assumes that the reader is already familiar with the operation of this
additional equipment.
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.
190-02452-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA40NG
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
3
SYSTEM OVERVIEW
GTX 335R /
GTX 345R
(Transponder)
#1
GDU 1050
(PFD)
GDL 69A SXM
(Datalink Receiver)
#1 GIA 64W
/ GIA 63W
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
Flight
Director
AFCS Mode
Logic
Servo Logic
#2 GIA 64W
/ GIA 63W
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
Flight
Director
AFCS Mode
Logic
Servo Logic
#2
GDU 1055
(MFD)
Non-Garmin Equipment
GEA 71 / GEA 71B
(Engine &
Airframe Unit)
GRS 79
(AHRS)
Optional
Garmin Equipment
Optional
Non-Garmin Equipment
GDC 72
(Air Data Computer)
Garmin Equipment
GMU 44
(Magnetometer)
GSA 81
(Servos)
WX-500 Stormscope
(Lightning Sensor)
GSR 56
(Iridium Transceiver)
TAS 600
(Traffic Advisory)
GMA 1347 / GMA 1360
(Audio Panel)
RA 3502 (ADF)
KN-63 (DME)
FS 510
(SD Card
Bluetooth Link)
Figure 1-1 System (LRU Configuration)
190-02452-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA40NG
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
4
SYSTEM OVERVIEW
1.2 SYSTEM CONTROLS
NOTE: The Audio Panel controls are described in the CNS & Audio Panel Section.
The system controls are located on the PFD and MFD bezels and audio panel. The controls for the PFD and
MFD are discussed within the following pages of this section.
PFD/MFD CONTROLS
Figure 1-2 PFD/MFD Controls
4
2
1
6
5
7
9
8
3
12
16
11
10
15
14
13
20
21
19
18
26
25
24
22
23
29
28
*MFD Only
17
27
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Garmin G1000 NXi: Diamond DA40NG User guide

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