Garmin G1000 NXi - Diamond DA62 User guide

Type
User guide
190-02100-00
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
Diamond DA62
Diamond DA62
Pilot’s Guide
®
G1000
®
Pilot’s Guide
190-01904-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA62
SYSTEM OVERVIEW
FLIGHT INSTRUMENTS
ENGINE INDICATION SYSTEM
AUDIO PANEL & CNS
FLIGHT MANAGEMENT
HAZARD AVOIDANCE
AUTOMATIC FLIGHT CONTROL SYSTEM
ADDITIONAL FEATURES
APPENDICES
INDEX
Garmin G1000 NXi Pilot’s Guide for the Diamond DA62
190-01904-00 Rev. A
Copyright © 2017 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 1373.02 or later for the G1000 NXi Diamond DA62. 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,
WATCH
®
, FliteCharts
®
, and SafeTaxi
®
are registered trademarks of Garmin International, Inc. or its subsidiaries.
Garmin ESP
, Garmin SVT
, SurfaceWatch
, and Connext
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. AC-U-KWIK
®
is a registered trademark of Penton Business
Media Inc. NavData
®
is a registered trademark of Jeppesen, Inc. Wi-Fi
®
is a registered trademark of the Wi-Fi Alliance. SiriusXM Weather
and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, Inc.
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.
190-01904-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA62
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.
Garmin G1000 NXi Pilot’s Guide for the Diamond DA62
190-01904-00 Rev. Aiv
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.
190-01904-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA62
v
WARNINGS, CAUTIONS, AND NOTES
WARNING: When using the autopilot to fly an approach with vertical guidance, the autopilot will not level
the aircraft at the MDA/DH even if the MDA/DH is set in the altitude preselect.
WARNING: Do not rely solely upon the display of traffic information for collision avoidance maneuvering.
The traffic display does not provide collision avoidance resolution advisories and does not under any
circumstances or conditions relieve the pilot’s responsibility to see and avoid other aircraft.
WARNING
:
Because of variation in the earth’s magnetic field, do not rely on the accuracy of attitude and
heading indications in the following geographic areas: North of 72° North latitude at all longitudes; South
of 70° South latitude at all longitudes; North of 65° North latitude between longitude 75° W and 120° W.
(Northern Canada); North of 70° North latitude between longitude 70° W and 128° W. (Northern Canada);
North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia); South of 55° South
latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand).
WARNING: Do not rely on information from a lightning detection system display as the sole basis for hazardous
weather avoidance. Range limitations and interference may cause the system to display inaccurate or
incomplete information. Refer to documentation from the lightning detection system manufacturer for
detailed information about the system.
WARNING:
Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance.
Garmin SVT is intended as an aid to situational awareness only and may not provide either the accuracy or
reliability upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic.
WARNING:
Intruder aircraft at or below 500 ft. AGL may not appear on the Garmin SVT display or may
appear as a partial symbol.
WARNING:
Do not use the Garmin SVT runway depiction as the sole means for determining the proximity of
the aircraft to the runway or for maintaining the proper approach path angle during landing.
WARNING: Do not operate the weather radar in a transmitting mode when personnel or objects are within
the MPEL boundary.
WARNING: Always position the weather radar gain setting to Calibrated for viewing the actual intensity of
precipitation. Changing the gain in weather mode causes precipitation intensity to be displayed as a color
not representative of the true intensity.
WARNING: Do not use TAWS information for primary terrain or obstacle avoidance. TAWS is intended only
to enhance situational awareness.
Garmin G1000 NXi Pilot’s Guide for the Diamond DA62
190-01904-00 Rev. Avi
WARNINGS, CAUTIONS, AND NOTES
CAUTION: Do not clean display surfaces with abrasive cloths or cleaners containing ammonia. They will
harm the anti-reflective coating.
CAUTION:
Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or
modifications could void both the warranty and affect the airworthiness of the aircraft.
NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information.
Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control.
NOTE: All visual depictions contained within this document, including screen images of the system panel
and displays, are subject to change and may not reflect the most current system and aviation databases.
Depictions of equipment may differ slightly from the actual equipment.
NOTE: The United States government operates the Global Positioning System and is solely responsible for
its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and
performance of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation
AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or
misinterpreted and, therefore, become unsafe.
NOTE
: This device complies with part 15 of the FCC Rules. Operation is subject to the following two
conditions: (1) this device may not cause harmful interference, and (2) this device must accept any
interference received, including interference that may cause undesired operation.
NOTE
: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of
attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards
away from the source of the interference should alleviate the condition.
NOTE
: Use of polarized eyewear may cause the flight displays to appear dim or blank.
NOTE
: This product, its packaging, and its components contain chemicals known to the State of California
to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with
California’s Proposition 65. If you have any questions or would like additional information, please refer to
our web site at www.garmin.com/prop65.
NOTE: Operating the system in the vicinity of metal buildings, metal structures, or electromagnetic fields
can cause sensor differences that may result in nuisance miscompare annunciations during start up, shut
down, or while taxiing. If one or more of the sensed values are unavailable, the annunciation indicates no
comparison is possible.
NOTE: The system responds to a terminal procedure based on data coded within that procedure in the
Navigation Database. Differences in system operation may be observed among similar types of procedures
due to differences in the Navigation Database coding specific to each procedure.
190-01904-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA62
vii
WARNINGS, CAUTIONS, AND NOTES
NOTE
: The FAA has asked Garmin to remind pilots who fly with Garmin database-dependent avionics of the
following:
It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory guidance and information
related to the use of databases in the National Airspace System.
• Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen. Databases
obtained from Garmin or Jeppesen that have a Type 2 Letter of Authorization (LOA) from the FAA are assured
compliance with all data quality requirements (DQRs). A copy of the Type 2 LOA is available for each applicable
database and can be viewed at http://fly.garmin.com by selecting Aviation Database Declarations.
Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with
established FAA regulatory guidance, but does not constitute authorization to fly any and all terminal procedures
that may be presented by the system. It is the pilot’s responsibility to operate in accordance with established
AFM(S) and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment.
NOTE
: The pilot/operator must review and be familiar with Garmin’s database exclusion list as discussed in
SAIB CE-14-04 to determine what data may be incomplete. The database exclusion list can be viewed at
www.flygarmin.com by selecting ‘Database Exclusions List.
NOTE
: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their
impact on the intended aircraft operation. The database alerts can be viewed at www.flygarmin.com by
selecting ‘Aviation Database Alerts.
NOTE
: If the pilot/operator wants or needs to adjust the database, contact Garmin Product Support.
NOTE: Garmin requests the flight crew report any observed discrepancies related to database information.
These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles
and fixes; or any other displayed item used for navigation or communication in the air or on the ground. Go
to FlyGarmin.com and select Aviation Data Error Report’.
NOTE: The system supports approval of AC 120-76C Hardware Class 3, Software Type B Electronic Flight Bag
(EFB) electronic aeronautical chart applications. Possible additional requirements may make a secondary
source (traditional paper or additional electronic display) necessary onboard the aircraft. If the secondary
source is a Portable Electronic Device (PED), its use must be consistent with guidance in AC 120-76C.
NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms
that can cause isolated discharge points in the strike display mode. However, clusters of two or more
discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after
the screen has been cleared.
NOTE: Operate G1000 NXi system power through at least one cycle in a period of four days of continuous
operation to avoid an autonomous system reboot.
Garmin G1000 NXi Pilot’s Guide for the Diamond DA62
190-01904-00 Rev. Aviii
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-01904-00 A 3/10/17 i – I-6 Initial Release for GDU 20.05
190-01904-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA62
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 .......................................................... 29
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 Garmin Synthetic Vision Technology (SVT) ........... 68
SVT Operation ............................................................ 69
SVT Features .............................................................. 71
Field of View ..............................................................80
2.3 Supplemental Flight Data ...................................... 82
Temperature Displays .................................................. 82
Wind Data ................................................................. 82
Vertical Navigation (VNV) Indications ........................... 83
2.4 PFD Annunciations and Alerting Functions .......... 85
Marker Beacon Annunciations...................................... 85
Altitude Alerting ......................................................... 85
Low Altitude Annunciation .......................................... 86
Minimum Descent Altitude/Decision Height Alerting ...... 86
2.5 Abnormal Operations ............................................. 88
Abnormal GPS Conditions ........................................... 88
SVT Troubleshooting ................................................... 89
Unusual Attitudes ....................................................... 89
SVT Unusual Attitudes ................................................. 90
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 ........................................................ 122
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 DA62
190-01904-00 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 ............................................................ 137
Measuring Bearing and Distance ................................ 139
Topography .............................................................. 140
Map Symbols ........................................................... 143
Airways ................................................................... 148
Additional Navigation Map Items ............................... 150
IFR/VFR Charts ......................................................... 153
5.3 Waypoints .............................................................. 156
Airports ................................................................... 158
Intersections ............................................................ 165
NDBs ....................................................................... 167
VORs ....................................................................... 169
VRPs ....................................................................... 171
User Waypoints ........................................................ 173
5.4 Airspaces ................................................................ 178
5.5 Direct-to-Navigation ........................................... 182
5.6 Flight Planning ...................................................... 187
Flight Plan Creation .................................................. 188
Flight Plan Import/Export........................................... 191
Adding Waypoints to an Existing Flight Plan ................ 195
Adding Airways to a Flight Plan ................................. 197
Adding Procedures to a Stored Flight Plan .................. 199
Flight Plan Storage ................................................... 204
Flight Plan Editing .................................................... 206
Along Track Offsets ................................................... 210
Parallel Track ............................................................ 211
Activating a Flight Plan Leg ....................................... 212
Inverting a Flight Plan ............................................... 213
Flight Plan Views ......................................................213
Closest Point of FPL .................................................. 214
User-Defined Holding Patterns ................................... 215
5.7 Vertical Navigation ............................................... 219
Altitude Constraints .................................................. 221
5.8 Procedures ............................................................. 227
Departures ............................................................... 229
Arrivals ................................................................... 231
Approaches ............................................................. 233
5.9 Trip Planning .......................................................... 241
Trip Planning ............................................................ 241
5.10 Abnormal Operation ............................................. 245
SECTION 6 HAZARD AVOIDANCE
6.1 Data Link Weather ................................................ 248
Activating Data Link Weather Services ........................ 248
Weather Product Age ................................................ 251
Displaying Data Link Weather Products ....................... 254
Connext Data Requests ............................................. 263
Weather Product Overview ........................................ 266
Abnormal Operations for Garmin Connext Weather ..... 295
6.2 Stormscope Lightning Detection System ........... 297
Using the Stormscope Page ....................................... 297
Setting Up Stormscope on the Navigation Map ........... 299
6.3 Airborne Color Weather Radar ............................ 301
System Description ................................................... 301
Principles of Pulsed Airborne Weather Radar ............... 301
Safe Operating Distance ............................................ 305
Basic Antenna Tilt Setup ............................................ 306
Weather Mapping and Interpretation ......................... 307
Ground Mapping and Interpretation ........................... 318
Additional Weather Radar Displays ............................. 319
System Status ........................................................... 321
6.4 Terrain Displays ..................................................... 322
Relative Terrain Symbology ........................................ 323
Terrain-SVT Alerting Displays ..................................... 328
Forward Looking Terrain Avoidance ............................ 330
System Status ........................................................... 331
6.5 Traffic Information Service (TIS) .......................... 333
Displaying Traffic Data .............................................. 334
Traffic Map Page ....................................................... 335
TIS Alerts ................................................................. 336
System Status ........................................................... 338
190-01904-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA62
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TABLE OF CONTENTS
6.6 Avidyne TAS600 Traffic ......................................... 340
TAS Theory of Operation ............................................ 340
TAS Alerts ................................................................ 342
System Test .............................................................. 343
Operation ................................................................ 344
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 ................................................ 356
Command Bars ......................................................... 356
7.3 AFCS Modes .............................................................. 357
Vertical Modes ......................................................... 357
Lateral Modes .......................................................... 363
Combination modes (VNV, APR, NAV, BC, GA) ............. 367
7.4 Autopilot and Yaw Damper Operation ............... 379
Flight Control ........................................................... 379
Engagement ............................................................. 380
Control Wheel Steering ............................................. 380
Disengagement ........................................................ 381
Underspeed Protection .............................................. 382
7.5 AFCS Annunciations and Alerts ........................... 384
Overspeed Protection ................................................ 384
7.6 Abnormal Operation ............................................. 385
Suspected Autopilot malfunction ................................ 385
Overpowering Autopilot Servos .................................. 385
SECTION 8 ADDITIONAL FEATURES
8.1 SafeTaxi .................................................................. 388
8.2 Database Cycle number and revisions ............... 390
Cycle Number and Revision ....................................... 390
8.3 FliteCharts .............................................................. 392
FliteCharts Softkeys .................................................. 393
Terminal Procedures Charts ....................................... 393
Chart Options ........................................................... 395
Day/Night View ........................................................ 396
8.4 Airport Directory ................................................... 397
8.5 SiriusXM Radio Entertainment ............................ 398
Activating SiriusXM Satellite Radio Services ................ 398
Using SiriusXM Radio ................................................ 399
8.6 Scheduler ............................................................... 402
8.7 Flight Data Logging .............................................. 405
8.8 Electronic Stability and Protection (ESP) ........... 407
Roll Engagement ...................................................... 408
Pitch Engagement..................................................... 409
High Airspeed Protection ........................................... 410
8.9 Satellite Telephone ............................................... 411
Registering with Garmin Connext
®
............................ 411
Disable/Enable Iridium Transceiver.............................. 411
Telephone Communication ........................................ 412
Text Messaging (SMS) ............................................... 417
8.10 Abnormal Operation ............................................. 428
GDL 69A SXM Troubleshooting .................................. 428
APPENDICES
Annunciations and Alerts ............................................... 429
Alert Level Definitions ............................................... 430
System Message Advisory Annunciations .................... 431
System Message Advisories ....................................... 432
Database Management .................................................. 443
Loading Updated Databases ...................................... 443
Magnetic Field Variation Database Update .................. 447
Garmin Aviation Glossary .............................................. 449
Frequently Asked Questions .......................................... 459
Map Symbols ................................................................... 463
Garmin G1000 NXi Pilot’s Guide for the Diamond DA62
190-01904-00 Rev. Axii
TABLE OF CONTENTS
Blank Page
190-01904-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA62
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). 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) – The GDU 1055 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 GIA 63Ws. 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 GIA 63Ws to obtain GPS information.
GEA 71
(1) – Receives and processes signals from the engine and airframe sensors. This unit communicates
with both GIA 63Ws 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 the #1 GIA 63W or both GIA 63Ws, using an RS-232 digital interface.
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.
190-01904-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA62
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
2
SYSTEM OVERVIEW
GSA 80, GSA 81 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 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).
GCU 476
(1) (Optional) – Provides the Flight Management System (FMS) controls for the MFD through an
RS-232 digital interface.
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.
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:
GCU 476 Control Unit
GDL 69A SXM
Data Link Receiver
GRA 5500 Radar Altimeter
GSR 56 Satellite Radio
GWX 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.
190-01904-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA62
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)
GMA 1347
(Audio
Panel)
#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 81/80
(Servos)
GRA 5500
(Radar Altimeter)
RA 3502 (ADF)
GCU 476
(Control Unit)
KN-63 (DME)
WX-500 Stormscope
(Lightning Sensor)
GSR 56
(Satellite Radio)
GWX 70
(Weather Radar)
TAS 6xx
(Traffic Advisory)
Figure 1-1 System (LRU Configuration)
190-01904-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA62
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
190-01904-00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Diamond DA62
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
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Garmin G1000 NXi - Diamond DA62 User guide

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