Garmin G1000 NXi - Diamond DA42NG User guide

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User guide

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Pilot’s Guide
190-02237-00
Revision A
Garmin International, Inc.
1200 East 151st Street
Olathe, Kansas 66062, U.S.A.
Tel: 913.397.8200
Fax: 913.397.8282
Aircraft On Ground (AOG)
Hotline: 913.397.0836
Aviation Dealer Technical
Support: 888.606.5482
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Tel: 503.581.8101
Fax 503.364.2138
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
Tel: +44 (0) 238 052 4000
Fax: +44 (0) 238 052 4004
Aviation Support: +44 (0) 370 850 1243
Garmin Corporation
No. 68, Zhangshu 2nd Road
Xizhi District,
New Taipei City, Taiwan
Tel: 34-93-357-2608
Fax: 34-93-429-4484
www.garmin.com
Cirrus SR2x
G1000
®
NXi Pilot’s Guide Diamond DA42NG
Diamond DA42NG
®
190-02237-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
Copyright © 2005-2017 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 20.05 or later for the Diamond DA42NG. Some differences in operation may
be observed when comparing the information in this manual to earlier or later software versions.
Garmin International, Inc.
1200 East 151st Street
Olathe, Kansas 66062, U.S.A.
Tel: 913.397.8200
Fax: 913.397.8282
Aircraft On Ground (AOG) Hotline: 913.397.0836
Aviation Dealer Technical Support: 888.606.5482
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
Tel: +44 (0) 238 052 4000
Fax: +44 (0) 238 052 4004
Aviation Support: +44 (0) 370 850 1243
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Tel: 503.581.8101
Fax 503.364.2138
Garmin Corporation
No. 68, Zhangshu 2nd Road
Xizhi District, New Taipei City, Taiwan
Tel: 34-93-357-2608
Fax: 34-93-429-4484
Website Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored
in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download
a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for
personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice
and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin
®
, G1000
®
NXi, FliteCharts
®
, and SafeTaxi
®
are registered trademarks of Garmin International, Inc. or its subsidiaries. Garmin ESP
,
Garmin SVT
, and Connext
are trademarks of Garmin International, Inc. or its subsidiaries. These trademarks may not be used without
the express permission of Garmin.
Stormscope
®
is a registered trademark of L-3 Communications. Avidyne
®
is a registered trademark of Avidyne Corporation. AC-U-KWIK
®
is
a registered trademark of Penton Business Media Inc. Bendix/King
®
and Honeywell
®
are registered trademarks of Honeywell International,
Inc. 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.
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
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
190-02237-00 Rev. A
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.
190-02237-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
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: 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 Diamond DA42NG
190-02237-00 Rev. Aiv
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: Steep approaches are not supported by Landing Data calculations.
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.
190-02237-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
v
WARNINGS, CAUTIONS, AND NOTES
WARNING: Do not rely on information from the reactive wind shear detection system display as the sole
basis for detecting wind shear conditions. The system cannot predict the conditions in which wind shear is
likely to develop.
WARNING: Do not use TAWS information for primary terrain or obstacle avoidance. TAWS is intended only
to enhance situational awareness.
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.
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
190-02237-00 Rev. Avi
WARNINGS, CAUTIONS, AND NOTES
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.
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’.
190-02237-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
vii
WARNINGS, CAUTIONS, AND NOTES
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.
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 G1000NXi system power through at least one cycle in a period of four days of continuous
operation to avoid an autonomous system reboot.
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
190-02237-00 Rev. Aviii
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-02237-00 A 04/2017 All Initial Release at GDU 20.05
190-02237-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
ix
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 ......................................................... 9
Reversionary Mode ..................................................... 10
System Annunciations ................................................. 11
System Status ............................................................. 13
AHRS Operation ......................................................... 14
GPS Receiver Operation .............................................. 16
1.4 Accessing System Functionality ............................ 21
Softkey Function ......................................................... 21
Menus ....................................................................... 26
MFD Page Groups ....................................................... 27
System Settings .......................................................... 30
System Utilities ........................................................... 38
1.5 Display Backlighting ............................................... 43
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................... 48
Airspeed Indicator ...................................................... 48
Attitude Indicator ....................................................... 50
Altimeter ................................................................... 51
Vertical Speed Indicator (VSI) ....................................... 54
Vertical Deviation ....................................................... 54
Horizontal Situation Indicator (HSI) .............................. 56
Course Deviation Indicator (CDI) .................................. 60
Radar Altimeter .......................................................... 66
2.2 Supplemental Flight Data ...................................... 68
Temperature Displays .................................................. 68
Wind Data ................................................................. 69
Vertical Navigation (VNV) Indications ........................... 70
2.3 PFD Annunciations and Alerting Functions .......... 71
Marker Beacon Annunciations...................................... 71
Altitude Alerting ......................................................... 71
Low Altitude Annunciation .......................................... 72
Minimum Descent Altitude/Decision Height Alerting ...... 72
2.4 Garmin Synthetic Vision Technology (SVT) ........... 74
SVT Operation ............................................................ 75
SVT Features .............................................................. 76
Field of View ..............................................................86
2.5 Abnormal Operations ............................................. 87
Abnormal GPS Conditions ........................................... 87
SVT Troubleshooting ................................................... 88
Unusual Attitudes ....................................................... 88
SVT Unusual Attitudes ................................................. 89
SECTION 3 ENGINE INDICATION SYSTEM (EIS)
3.1 Engine Display ......................................................... 93
3.2 Engine Page ............................................................. 95
Fuel Calculations ........................................................ 97
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview .................................................................. 99
PFD Controls and Frequency Display ........................... 100
Audio Panel Controls ................................................ 102
4.2 COM Operation...................................................... 104
COM TUNING BOXES ................................................ 104
COM Transceiver Manual Tuning ................................ 105
Auto-Tuning the COM Frequency ................................ 105
Frequency Spacing ................................................... 108
4.3 NAV Operation....................................................... 109
NAV Tuning Boxes..................................................... 109
NAV Radio Selection and Activation ........................... 110
NAV Receiver Manual Tuning ..................................... 110
Auto-Tuning a NAV Frequency from the MFD............... 111
Marker Beacon Receiver ............................................ 113
ADF/DME Tuning ...................................................... 114
DME Tuning ............................................................. 117
4.4 Mode S Transponder ............................................. 118
Transponder Controls ................................................ 118
Transponder Mode Selection ...................................... 119
IDENT Function ........................................................ 121
Flight ID Reporting.................................................... 122
4.5 Additional Audio Panel Functions ....................... 123
Power-Up ................................................................. 123
Mono/Stereo Headsets .............................................. 123
Speaker ................................................................... 123
Intercom .................................................................. 124
Split COM ................................................................ 126
Clearance Recorder and Player ................................... 126
Entertainment Inputs ................................................ 126
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
190-02237-00 Rev. Ax
TABLE OF CONTENTS
4.6 Audio Panels Preflight Procedure ....................... 127
4.7 Abnormal Operation ............................................. 128
Stuck Microphone ..................................................... 128
COM Tuning Failure ................................................... 128
Audio Panel Fail-Safe Operation ................................. 128
Reversionary Mode ................................................... 128
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ........................................................... 129
Navigation Status Box ............................................... 131
5.2 Using Map Displays .............................................. 133
Map Orientation ....................................................... 133
Map Range .............................................................. 135
Map Panning ............................................................ 138
Measuring Bearing and Distance ................................ 140
Topography .............................................................. 141
Map Symbols ........................................................... 144
Airways ................................................................... 149
Additional Navigation Map Items ............................... 151
IFR/VFR Charts ......................................................... 154
5.3 Waypoints .............................................................. 157
Airports ................................................................... 159
Intersections ............................................................ 166
NDBs ....................................................................... 168
VORs ....................................................................... 170
VRPs ....................................................................... 172
User Waypoints ........................................................ 174
5.4 Airspaces ................................................................ 179
5.5 Direct-to-Navigation ........................................... 183
5.6 Flight Planning ...................................................... 188
Flight Plan Creation .................................................. 189
Flight Plan Import/Export........................................... 192
Adding Waypoints to an Existing Flight Plan ................ 198
Adding Airways to a Flight Plan ................................. 199
Adding Procedures to a Stored Flight Plan .................. 202
Flight Plan Storage ................................................... 207
Flight Plan Editing .................................................... 210
Along Track Offsets ................................................... 214
Parallel Track ............................................................ 215
Activating a Flight Plan Leg ....................................... 217
Inverting a Flight Plan ............................................... 217
Flight Plan Views ......................................................217
Closest Point of FPL .................................................. 219
User-Defined Holding Patterns ................................... 220
5.7 Vertical Navigation ............................................... 224
Altitude Constraints .................................................. 226
5.8 Procedures ............................................................. 232
Departures ............................................................... 234
Arrivals .................................................................... 236
Approaches .............................................................. 238
5.9 Trip Planning .......................................................... 245
Trip Planning ............................................................ 245
5.10 Abnormal Operation ............................................. 249
SECTION 6 HAZARD AVOIDANCE
6.1 Data Link Weather ................................................ 252
Activating Data Link Weather Services ........................ 253
Weather Product Age ................................................ 256
Displaying Data Link Weather Products ....................... 260
Connext Data Requests ............................................. 270
Weather Product Overview ........................................ 274
FIS-B Weather Status................................................. 310
Abnormal Operations for Garmin Connext Weather ..... 311
6.2 Stormscope Lightning Detection System ........... 313
Using the Stormscope Page ....................................... 313
Setting Up Stormscope on the Navigation Map ........... 315
6.3 Airborne Color Weather Radar ............................ 317
System Description ................................................... 317
Principles of Pulsed Airborne Weather Radar ............... 317
Safe Operating Distance ............................................ 321
Basic Antenna Tilt Setup ............................................ 322
Weather Mapping and Interpretation ......................... 323
Ground Mapping and Interpretation ........................... 334
Additional Weather Radar Displays ............................. 335
System Status ........................................................... 338
6.4 Terrain Displays ..................................................... 340
Relative Terrain Symbology ........................................ 341
Terrain-SVT Alerting Displays ..................................... 346
Forward Looking Terrain Avoidance ............................ 348
System Status ........................................................... 349
6.5 Traffic Information Service (TIS) .......................... 351
Displaying Traffic Data .............................................. 352
Traffic Map Page ....................................................... 353
TIS Alerts ................................................................. 354
190-02237-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
xi
TABLE OF CONTENTS
System Status ........................................................... 356
6.6 Avidyne TAS600 Traffic ......................................... 358
TAS Theory of Operation ............................................ 358
TAS Alerts ................................................................ 360
System Test .............................................................. 360
Operation ................................................................ 362
6.7 ADS-B Traffic .......................................................... 368
ADS-B System Overview ............................................ 368
Conflict Situational Awareness & Alerting (CSA) .......... 370
Airborne and Surface Applications .............................. 372
Traffic Description ..................................................... 374
Operation ................................................................ 375
ADS-B System Status ................................................ 380
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Overview ...................................................... 385
Additional AFCS Controls .......................................... 387
7.2 Flight Director Operation ..................................... 388
Activating the Flight Director ..................................... 388
AFCS Status Box ....................................................... 389
Flight Director Modes ................................................ 390
Command Bars ......................................................... 390
7.3 AFCS MODES .......................................................... 391
Vertical Modes ......................................................... 391
Lateral Modes .......................................................... 397
Combination modes (VNV, APR, NAV, BC, GA) ............. 401
7.4 Autopilot and Yaw Damper Operation ............... 413
Flight Control ........................................................... 413
Engagement ............................................................. 414
Control Wheel Steering ............................................. 414
Disengagement ........................................................ 415
Underspeed Protection .............................................. 416
7.5 AFCS Annunciations and Alerts ........................... 418
Overspeed Protection ................................................ 419
7.6 Abnormal Operation ............................................. 420
Suspected Autopilot malfunction ................................ 420
Overpowering Autopilot Servos .................................. 420
SECTION 8 ADDITIONAL FEATURES
8.1 SafeTaxi .................................................................. 422
8.2 Charts ..................................................................... 425
ChartView ................................................................ 426
FliteCharts ............................................................... 434
IFR/VFR Charts ......................................................... 439
Airport Directory ....................................................... 440
8.3 Database Cycle number and revisions ............... 441
Cycle Number and Revision ....................................... 441
8.4 SiriusXM Radio Entertainment ............................ 443
Activating SiriusXM Satellite Radio Services ................ 443
Using SiriusXM Radio ................................................ 444
8.5 Flight Data Logging .............................................. 447
8.6 Satellite Telephone and sms messaging ............ 449
Registering with Garmin Connext
®
............................ 449
Disable/Enable Iridium Transceiver.............................. 449
Telephone Communication ........................................ 450
8.7 Connext Setup ....................................................... 469
8.8 WIFI Connections .................................................. 471
8.9 Electronic Stability and Protection (ESP
) ......... 474
Roll Engagement ...................................................... 475
Pitch Engagement..................................................... 476
Angle of Attack Protection ......................................... 478
High Airspeed Protection ........................................... 478
8.10 Auxiliary Video ...................................................... 479
Video Softkeys .......................................................... 479
Zoom/Range ............................................................ 480
8.11 Electronic Checklists ............................................. 481
8.12 Abnormal Operation ............................................. 483
SiriusXM Data Link Receiver Troubleshooting .............. 483
APPENDICES
Annunciations and Alerts ............................................... 485
Alert Level Definitions ............................................... 486
System Message Advisory Annunciations .................... 487
System Message Advisories ....................................... 488
Database Management .................................................. 499
Loading Updated Databases ...................................... 499
Magnetic Field Variation Database Update .................. 503
Garmin Aviation Glossary .............................................. 505
Frequently Asked Questions .......................................... 515
Map Symbols ................................................................... 519
INDEX
Index .................................................................................. I-1
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
190-02237-00 Rev. Axii
TABLE OF CONTENTS
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190-02237-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
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
DA62. 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) that features a 10-inch,
high resolution LED backlit display. The display communicates with the MFD and with the #1 GIA 63W
Integrated Avionics Unit through a High-Speed Data Bus (HSDB) Ethernet connection.
GDU 1055
(1) – Features a 10-inch, high resolution LED backlit display and is configured as an MFD. The
display communicates with the PFD and with the #2 GIA 63W Integrated Avionics Unit through a High-
Speed Data Bus (HSDB) Ethernet 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--if Garmin AFCS
is installed) system integration microprocessors. Each GIA 63W is paired with the PFD and MFD via HSDB
connection. The GIA 63Ws are not paired together and do not communicate with each other directly.
GDC 72
(1) – 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.
GRS 79
(1) – The Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading
information via ARINC 429 to both displays and both GIAs. The GRS 79 contains advanced sensors (including
accelerometers and rate sensors) and interfaces with the GMU 44 to obtain magnetic field information, the
GDC 72 to obtain air data, and both GIAs to obtain GPS information.
GEA 71
(1) – Receives and processes signals from the engine and airframe sensors. This unit communicates
with both GIAs using an RS-485 digital interface.
GMU 44
(1) – Measures local magnetic field. Data is sent to the GRS unit for processing to determine aircraft
magnetic heading. The GMU 44 receives power directly from the GRS unit and communicates with the
GRS unit using an RS-485 digital interface.
GMA 1347
(1) – 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 both GIA 63Ws, using an RS-232 digital interface.
190-02237-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
2
SYSTEM OVERVIEW
GTX 335R
(1) – Solid-state transponder that provides Mode A, C, S with an ADS-B Out capability. The
transponder can be controlled from the PFD. The transponder communicates with the both GIA 63Ws
through an RS-232 digital interface.
GSA 80, GSA 81, GSM 85 (Alternate), and GSM 86
– The GSA servos are used for the automatic control of
pitch, pitch trim, roll and yaw. These units interface with each GIA 63W.
The GSM 85 or 86 servo mounts are responsible for transferring the output torque of the servo actuators to
the mechanical flight-control surface linkages (not displayed in Figure 1-1).
Flight Stream 210
(1) (if installed) – Provides wireless Bluetooth® connectivity between a compatible tablet/
mobile device and the avionics system.
GDL 69A SXM
(1) (Optional) – A satellite radio receiver that provides data link weather information to the
MFD and PFD map as well as digital audio entertainment. The GDL 69A SXM communicates with the MFD
via an HSDB connection. Subscriptions to the SiriusXM Weather or SiriusXM Satellite Radio services are
required to enable the GDL 69A SXM capability.
GDL 59
(1) (if installed) – A data link transceiver that provides WiFi capability. Operation is performed on
the MFD.
GDL 88
(1) (if installed) – Provides ADS-B Traffic in and FIS-B Weather.
GRA 5500
(1) (Optional) – Provides altitude above the ground (AGL) to the MFD, through the GIA 63W, via
HSDB connection.
GSR 56
(1) (Optional) – The Iridium Transceiver operation for voice communication is by means of a
telephone handset in the cabin and pilot and copilot headsets in the cockpit.
GWX 70
(1) (Optional) – Provides airborne weather and ground mapped radar data to the MFD.
Figure 1-1 shows interactions between the LRUs and optional equipment. The system is capable of interfacing
with the following optional equipment:
Flight Stream 210
Wireless Bluetooth®
Gateway (if installed)
GDL 59
Data Link (if installed)
GDL 69A SXM
Data Link Receiver
GDL 88 ADS-B Transceiver (if installed)
GRA 5500 Radar Altimeter
GSM 85 Servo Mounts
GSR 56 Iridium Transceiver
GWX 68/70 Weather Radar
KN 63 DME
RA 3502 ADF Receiver
TAS 6xx 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.
190-02237-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
3
SYSTEM OVERVIEW
GTX 335R
(Transponder)
#1
GDU 1050
(PFD)
GDL 69A SXM
(Datalink Receiver)
#1 GIA 63W
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
Flight
Director
AFCS Mode
Logic
Servo Logic
#2 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
(Engine &
Airframe I/F)
GRS 79
(AHRS)
Optional
Garmin Equipment
Optional
Non-Garmin Equipment
GDC 72
(Air Data Computer)
Garmin Equipment
GMU 44
(Magnetometer)
GSA 80/81
(Servos)
GRA 5500
(Radar Altimeter)
RA 3502 (ADF)
KN-63 (DME)
WX-500 Stormscope
(Lightning Sensor)
GSR 56
(Satellite Radio)
GWX 70
(Weather Radar)
TAS 600
(Traffic Advisory)
GMA 1347 (Audio Panel)
GDL 59
(Data Link)
Flight Stream 210
(Bluetooth
Data Link)
GDL 88
(Data Link ADS-B
Traffic & Weather)
Figure 1-1 System (LRU Configuration)
190-02237-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
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 (GMA 1347) is 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
190-02237-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
5
SYSTEM OVERVIEW
1
NAV VOL/ID Knob
Turn to control NAV audio volume (shown in the NAV Frequency Box as a percentage)
Press to toggle Morse code identifier audio ON/OFF
2
NAV Frequency Trans-
fer Key
Transfers the standby and active NAV frequencies
3
NAV Knob
Turn to tune NAV receiver standby frequencies (large knob for MHz; small for kHz)
Press to toggle cyan tuning box between NAV1 and NAV2
4
*Heading Knob
Turn to manually select a heading. When operating in Heading Select mode, this knob pro-
vides the heading reference to the flight director.
Press to display a digital heading momentarily to the left of the HSI and synchronize the Se-
lected Heading to the current heading (MFD Only)
5
Joystick
Turn to change map range
Press to activate Map Pointer for map panning
6
CRS/BARO Knob
Turn large knob for altimeter barometric pressure setting
Turn the small knob to set the pilot-selected course on the HSI when the VOR1, VOR2, or
OBS/SUSP mode is selected. Pressing this knob centers the CDI on the currently selected
VOR. The pilot-selected course provides course reference to the pilot-side flight director
when operating in Navigation and Approach modes.
Press to re-center the CDI and return course pointer directly TO bearing of active waypoint/
station.
7
COM Knob
Turn to tune COM transceiver standby frequencies (large knob for MHz; small for kHz).
Press to toggle cyan tuning box between COM1 and COM2.
The selected COM (green) is controlled with the COM MIC Key (Audio Panel).
8
COM Frequency
Transfer Key (EMERG)
Transfers the standby and active COM frequencies.
Press and hold two seconds to tune the emergency frequency (121.5 MHz) automatically into
the active frequency field.
9
COM VOL/SQ Knob
Turn to control COM audio volume level (shown as a percentage in the COM Frequency
Box).
Press to turn the COM automatic squelch ON/OFF.
10
Direct-to Key ( )
Activates the direct-to function and allows the user to enter a destination waypoint and es-
tablish a direct course to the selected destination (specified by identifier, chosen from the
active route)
11
FPL Key
Displays flight plan information
12
CLR Key
(DFLT MAP)
Erases information, cancels entries, or removes menus.
Press and hold to display the MFD Navigation Map Page (MFD only).
13
MENU Key
Displays a context-sensitive list of options for accessing additional features or making setting
changes
14
PROC Key
Gives access to IFR departure procedures (DPs), arrival procedures (STARs), and approach
procedures (IAPs) for a flight plan or selected airport
15
ENT Key
Validates/confirms menu selection or data entry
190-02237-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA42NG
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
6
SYSTEM OVERVIEW
16
FMS Knob
(Flight Management
System Knob)
Press to turn the selection cursor ON/OFF.
Data Entry: With cursor ON, turn to enter data in the highlighted field (large knob moves
cursor location; small knob selects character for highlighted cursor location).
Scrolling: When a list of information is too long for the window/box, a scroll bar appears,
indicating more items to view. With cursor ON, turn large knob to scroll through the list.
Page Selection: Turn knob on MFD to select the page to view (large knob selects a page
group; small knob selects a specific page from the group).
17
*ALT SEL Knob
Sets the selected altitude in the Selected Altitude Box (the large knob selects the thousands,
the small knob selects the hundreds). In addition to providing the standard system altitude
alerter function, selected altitude provides an altitude setting for the Altitude Capture/Hold
mode of the AFCS (MFD only).
18
*AP Key
Engages/disengages the Autopilot and Flight Director in the default vertical and lateral
modes.
19
*FD Key Activates/deactivates the Flight Director only. Pressing the FD key turns on the Flight Direc-
tor in the default vertical and lateral modes. Pressing the FD key again deactivates the Flight
Director and removes the command bars, unless the Autopilot is engaged. If the Autopilot
is engaged, the FD key is disabled.
20
*NAV Key
Selects/deselects the Navigation mode.
21
*ALT Key
Selects/deselects the Altitude Hold mode.
22
*VS Key
Selects/deselects the Vertical Speed mode.
23
*FLC Key
Selects/deselects the Flight Level Change mode.
24
*YD Key
Engages/disengages the Yaw Damper.
25
*HDG Key
Selects/deselects the Heading Select mode.
26
*APR Key
Selects/deselects the Approach mode.
27
*VNV Key
(if equipped)
Selects/deselects Vertical Navigation mode
28
*NOSE UP Key
Controls the active pitch reference for the Pitch Hold, Vertical Speed, and Flight Level
Change modes.
29
*NOSE DN Key
Controls the active pitch reference for the Pitch Hold, Vertical Speed, and Flight Level
Change modes.
*This Key only appears on the MFD
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