Garmin G1000: Diamond DA62 User guide

Type
User guide

This manual is also suitable for

®
G1000
®
Pilot’s Guide
G1000
®
Integrated Avionics System
Pilot’s Guide
Diamond DA62
Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p:913.397.8200
f:913.397.8282
www.garmin.com
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
p:503.391.3411
f:503.364.2138
Garmin (Europe) Ltd.
Liberty House,Houndsdown Business Park
Southampton, Hampshire, SO40 9LR, U.K.
p:44 (0) 23 8052 4000
f:44 (0) 23 8052 4004
Aviation Support: 44 (0) 87 0850 1243
Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p:886/02.2642.9199
f:886/02.2642.9099
Diamond DA62
190-01895-00
Revision A
SYSTEM OVERVIEW
FLIGHT INSTRUMENTS
EIS
AUDIO PANEL & CNS
FLIGHT MANAGEMENT
HAZARD AVOIDANCE
AFCS
ADDITIONAL FEATURES
APPENDICES
INDEX
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-00 Rev. A
Copyright © 2015 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 1373.00 or later for the 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
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: 503/391.3411 Fax: 503/364.2138
Garmin (Europe) Ltd., Liberty House, Hounsdown Business Park, Southampton, SO40 9LR, U.K.
Tel: 44 (0) 23 8052 4000 Fax: 44 (0) 23 8052 4004
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: 886/02.2642.9199 Fax: 886/02.2642.9099
For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please
contact Garmin’s AOG Hotline at 913.397.0836.
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
®
is a registered trademark of Garmin Ltd. or its subsidiaries, and G1000
®
is a trademark of Garmin Ltd. or its subsidiaries. These
trademarks may not be used without the express permission of Garmin.
Honeywell
®
is a registered trademark of Honeywell International, Inc. 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. 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.
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.
March 2015 Printed in the U.S.A
190-01895-00 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA62
i
WARNINGS, CAUTIONS, AND NOTES
WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance
feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance
and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The
terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from
third party sources. Garmin is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (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: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and
could vary significantly from the altitude displayed by pressure altimeters, such as the Air Data Computer, or
other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always use pressure
altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in the G1000 system must be updated
regularly in order to ensure that the information remains current. Pilots using any outdated database do so
entirely at their own risk.
WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is
intended only to supplement other approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING: Traffic information shown on the G1000 is provided as an aid in visually acquiring traffic. Pilots
must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting
traffic.
WARNING: Use of the Lightning Detection System is not intended for hazardous weather penetration
(thunderstorm penetration). Lightning Detection System information, as displayed on the G1000, is to be
used only for weather avoidance, not penetration.
WARNING: XM Weather should not be used for hazardous weather penetration. Weather information
provided by the GDL 69A is approved only for weather avoidance, not penetration.
WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent
delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for
short-range weather avoidance.
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-00 Rev. Aii
WARNINGS, CAUTIONS, AND NOTES
WARNING: The Garmin G1000, as installed in this aircraft, has a very high degree of functional integrity.
However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable
system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur
without a fault indication shown by the G1000. It is thus the responsibility of the pilot to detect such an
occurrence by means of cross-checking with all redundant or correlated information available in the cockpit.
WARNING: For safety reasons, G1000 operational procedures must be learned on the ground.
WARNING: 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 Garmin G1000 utilize GPS as a precision electronic
NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be
misused or misinterpreted and, therefore, become unsafe.
WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000
Pilot’s Guide documentation and the Airplane Flight Manual. Thoroughly practice basic operation prior to
actual use. During flight operations, carefully compare indications from the G1000 to all available navigation
sources, including the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes,
always resolve any discrepancies before continuing navigation.
WARNING: The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate
a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information
Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an
intense radar echo.
WARNING: Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of
according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/
aboutGarmin/environment/disposal.jsp.
WARNING
:
Because of variation in the earth’s magnetic field, operating the G1000 within the following
areas could result in loss of reliable attitude and heading indications. 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)
190-01895-00 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA62
iii
WARNINGS, CAUTIONS, AND NOTES
WARNING:
Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a
system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that
may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned
in error as displayed.
WARNING:
Do not 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.
CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very
sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE
ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an
eyeglass lens cleaner that is specified as safe for anti-reflective coatings.
CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by
an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty
and the pilot’s authority to operate this device under FAA/FCC regulations.
NOTE: When using the on-board Lightning Detection System, 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: All visual depictions contained within this document, including screen images of the G1000 panel
and displays, are subject to change and may not reflect the most current G1000 system. Depictions of
equipment may differ slightly from the actual equipment.
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 feet
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.
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-00 Rev. Aiv
WARNINGS, CAUTIONS, AND NOTES
NOTE: This product, its packaging, and its components contain chemicals known to the State of California
to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with
California’s Proposition 65. If you have any questions or would like additional information, please refer to
our web site at www.garmin.com/prop65.
NOTE
: 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 are assured compliance with all data quality requirements (DQRs) by virtue
of a Type 2 Letter of Authorization (LOA) from the FAA. A copy of the Type 2 LOA is available for each database
and can be viewed at http://fly.garmin.com by selecting ‘Type 2 LOA Status.
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 to
coordinate the revised DQRs.
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 ‘Report An Aviation Data Error Report.’
190-01895-00 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA62
v
REVISION INFORMATION
Record of Revision
Part Number Revision Date Page Range Description
190-01895-00 A i – I-6 Initial release with GDU SW Version 14.04
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-00 Rev. Avi
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 Line Replaceable Units ........................................... 2
1.2 Secure Digital (SD) Cards .......................................6
1.3 System Power-up ..................................................... 7
1.4 System Operation .................................................... 8
Display Operation ......................................................... 8
G1000 System Annunciations ........................................ 9
System Status ............................................................. 10
AHRS Operation ......................................................... 12
GPS Receiver Operation .............................................. 13
1.5 G1000 Controls ...................................................... 17
PFD/MFD Controls ...................................................... 17
Softkey Function ......................................................... 19
1.6 Accessing G1000 Functionality............................ 26
Menus ....................................................................... 26
Data Entry.................................................................. 26
Page Groups .............................................................. 28
System Settings .......................................................... 32
Timers ....................................................................... 38
Electronic Checklists ................................................... 41
1.7 Display Backlighting ............................................. 43
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 48
Airspeed Indicator ...................................................... 48
Attitude Indicator ....................................................... 50
Altimeter ................................................................... 51
Vertical Speed Indicator (VSI) ....................................... 53
Vertical Deviation ....................................................... 54
Horizontal Situation Indicator (HSI) .............................. 55
Course Deviation Indicator (CDI) .................................. 60
2.2 Supplemental Flight Data .................................... 67
Outside Air Temperature .............................................. 67
Wind Data ................................................................. 69
Vertical Navigation (VNV) Indications ........................... 70
2.3 PFD Annunciations and Alerting Functions ........ 71
System Alerting .......................................................... 71
Marker Beacon Annunciations...................................... 72
Traffic Annunciation .................................................... 72
Altitude Alerting ......................................................... 73
Low Altitude Annunciation .......................................... 73
Minimum Descent Altitude/Decision Height Alerting ...... 74
Radar Altimeter .......................................................... 75
2.4 Abnormal Operations ........................................... 77
Abnormal GPS Conditions ........................................... 77
Unusual Attitudes ....................................................... 78
SECTION 3 ENGINE INDICATION SYSTEM (EIS)
3.1 Engine Display ....................................................... 82
3.2 System Display ...................................................... 84
3.3 Fuel Display ............................................................ 86
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview ................................................................ 89
MFD/PFD Controls and Frequency Display ..................... 90
Audio Panel Controls .................................................. 92
4.2 COM Operation ...................................................... 94
COM Transceiver Selection and Activation ..................... 94
COM Transceiver Manual Tuning .................................. 95
Quick-tuning and Activating 121.500 MHz .................... 96
Auto-tuning the COM Frequency .................................. 97
Frequency Spacing .................................................... 101
Automatic Squelch .................................................... 102
Volume .................................................................... 102
4.3 NAV Operation ..................................................... 103
NAV Radio Selection and Activation ........................... 103
NAV Receiver Manual Tuning ..................................... 104
Auto-tuning a NAV Frequency from the MFD ............... 106
Marker Beacon Receiver ............................................ 111
ADF/DME Tuning ...................................................... 112
4.4 GTX 33/GTX 33 ES Mode S Transponder ........... 116
Transponder Controls ................................................ 116
Transponder Mode Selection ...................................... 117
ADS-B TX (Optional) .................................................. 120
Entering a Transponder Code ..................................... 120
IDENT Function ........................................................ 122
Flight ID Reporting.................................................... 123
4.5 Additional Audio Panel Functions ..................... 124
Power-up ................................................................. 124
Mono/Stereo Headsets .............................................. 124
Intercom .................................................................. 124
Clearance Recorder and Player ................................... 126
Split COM ................................................................ 127
Entertainment Inputs ................................................ 127
4.6 Audio Panel Preflight Procedure ....................... 128
4.7 Abnormal Operation ........................................... 129
190-01895-00 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA62
vii
TABLE OF CONTENTS
Stuck Microphone ..................................................... 129
COM Tuning Failure ................................................... 129
Audio Panel Fail-safe Operation ................................. 129
Reversionary Mode ................................................... 129
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 131
Navigation Status Box ............................................... 132
5.2 Using Map Displays ............................................. 134
Map Orientation ....................................................... 134
Map Range .............................................................. 136
Map Panning ............................................................ 138
Measuring Bearing and Distance ................................ 143
Topography .............................................................. 144
Map Symbols ........................................................... 147
Airways ................................................................... 153
Track Vector ............................................................. 155
Wind Vector ............................................................. 156
Nav Range Ring........................................................ 157
Fuel Range Ring ....................................................... 158
Field of View (SVT) .................................................... 159
Selected Altitude Intercept Arc ................................... 160
5.3 Waypoints ............................................................. 161
Airports ................................................................... 162
Intersections ............................................................ 169
NDBs ....................................................................... 171
VORs ....................................................................... 173
User Waypoints ........................................................ 175
5.4 Airspaces .............................................................. 181
5.5 Direct-to-Navigation .......................................... 185
5.6 Flight Planning ..................................................... 190
Flight Plan Creation .................................................. 191
Adding Waypoints to an Existing Flight Plan ................196
Adding Airways to a Flight Plan ................................. 198
Adding Procedures to a Stored Flight Plan .................. 200
Flight Plan Storage ................................................... 207
Flight Plan Editing .................................................... 209
Along Track Offsets ................................................... 212
Parallel Track ............................................................ 214
Activating a Flight Plan Leg ....................................... 217
Inverting a Flight Plan ............................................... 218
Flight Plan Views ...................................................... 219
Closest Point of FPL .................................................. 221
User-Defined Holding Patterns ................................... 221
5.7 Vertical Navigation ............................................. 226
Altitude Constraints .................................................. 228
5.8 Procedures ...........................................................232
Departures ............................................................... 233
Arrivals ................................................................... 236
Approaches ............................................................. 239
5.9 Trip Planning ........................................................ 247
Trip Planning ............................................................ 247
5.10 RAIM Prediction................................................... 251
5.11 Navigating a Flight Plan ..................................... 254
5.12 Abnormal Operation ........................................... 282
SECTION 6 HAZARD AVOIDANCE
6.1 SiriusXM Weather ................................................ 286
Activating Services .................................................... 286
Using SiriusXM Weather Products .............................. 287
6.2 Garmin Connext Weather ................................... 320
Registering the Iridium Satellite System ...................... 320
Registering Garmin Connext Weather ......................... 321
Accessing Garmin Connext Weather Products .............. 323
Connext Data Requests ............................................. 330
Garmin Connext Weather Products ............................. 334
Abnormal Operations ................................................ 349
6.3 Airborne Color Weather Radar .......................... 351
System Description ................................................... 351
Principles of Pulsed Airborne Weather Radar ............... 351
Safe Operating Distance ............................................ 355
Basic Antenna Tilt Setup ............................................ 356
Weather Mapping and Interpretation ......................... 357
Ground Mapping and Interpretation ........................... 369
Weather Radar Overlay on the Navigation Map Page ... 370
System Status ........................................................... 371
6.4 Lightning Detection System ............................... 373
Setting Up Lightning Detection Information on the
Navigation Map ....................................................... 373
Selecting the Stormscope Page .................................. 377
6.5 Terrain Proximity ................................................. 379
Displaying Terrain Proximity Data ............................... 379
Terrain Proximity Page ............................................... 382
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-00 Rev. Aviii
TABLE OF CONTENTS
6.6 Profile View Terrain ............................................. 384
Profile View Display .................................................. 385
6.7 Terrain-SVS ........................................................... 388
Displaying Terrain-SVS Data ....................................... 389
Terrain-SVS Page ...................................................... 391
Terrain-SVS Alerts ..................................................... 393
System Status ........................................................... 396
6.8 Traffic Information Service (TIS) ........................ 397
Displaying Traffic Data .............................................. 398
Traffic Map Page ....................................................... 400
TIS Alerts ................................................................. 401
System Status ........................................................... 403
6.9 Avidyne TAS600 Traffic ........................................ 405
TAS Symbology ......................................................... 405
Displaying Traffic Data .............................................. 406
Altitude Display ........................................................ 408
Traffic Map Page Display Range ................................. 408
TAS Alerts ................................................................ 410
System Status ........................................................... 411
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Controls ...................................................... 414
7.2 Flight Director Operation ................................... 416
Activating the Flight Director ..................................... 416
AFCS Status Box ....................................................... 417
Command Bars ......................................................... 418
Flight Director Modes ................................................ 418
7.3 Vertical Modes ..................................................... 419
Pitch Hold Mode (PIT) ............................................... 420
Selected Altitude Capture Mode (ALTS) ....................... 421
Altitude Hold Mode (ALT) .......................................... 422
Vertical Speed Mode (VS) .......................................... 423
Flight Level Change Mode (FLC) ................................. 424
Vertical Navigation Modes (VPTH, ALTV) ..................... 425
Glidepath Mode (GP) (SBAS only) ............................... 430
Glideslope Mode (GS) ............................................... 432
Takeoff (TO) and Go Around (GA) Modes .................... 433
7.4 Lateral Modes ...................................................... 434
Roll Hold Mode (ROL) ............................................... 435
Heading Select Mode (HDG) ...................................... 436
Navigation Modes (GPS, VOR, LOC, BC) ...................... 437
Approach Modes (GPS, VAPP, LOC) ............................. 439
7.5 Autopilot and Yaw Damper Operation ............. 441
Flight Control ........................................................... 441
Engaging the Autopilot and Yaw Damper .................... 442
Control Wheel Steering ............................................. 442
Disengaging the Autopilot and Yaw Damper ................ 443
Underspeed Protection .............................................. 444
7.6 Example Flight Plan ............................................ 446
Departure ................................................................ 446
Intercepting a VOR Radial .......................................... 448
Flying a Flight Plan/GPS Course ................................. 449
Descent ................................................................... 450
Approach ................................................................. 454
Go Around/Missed Approach ..................................... 456
7.7 AFCS Annunciations and Alerts ......................... 458
AFCS Status Alerts .................................................... 458
Overspeed Protection ................................................ 459
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision Technology (SVT)
(Optional) ............................................................. 462
SVT Operation .......................................................... 463
SVT Features ............................................................ 465
Field of View ............................................................ 473
8.2 SafeTaxi ................................................................ 475
8.3 ChartView (Optional) .......................................... 480
ChartView Softkeys ................................................... 481
Terminal Procedures Charts ....................................... 482
Chart Options ........................................................... 490
Day/Night View ........................................................ 496
ChartView Cycle Number and Expiration Date ............. 498
8.4 FliteCharts ............................................................ 501
FliteCharts Softkeys .................................................. 502
Terminal Procedures Charts ....................................... 503
Chart Options ........................................................... 510
Day/Night View ........................................................ 514
FliteCharts Cycle Number and Expiration Date ............. 516
8.5 Airport Directory ................................................. 519
Airport Directory Database Cycle Number and Revision 520
8.6 SiriusXM Satellite Radio Entertainment
(Optional) ............................................................. 522
Activating SiriusXM Satellite Radio Services ................ 522
190-01895-00 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA62
ix
TABLE OF CONTENTS
Using SiriusXM Radio ................................................ 524
8.7 Satellite Telephone Services (Optional) ............ 527
Telephone Communication ........................................ 527
Text Messaging (SMS) ............................................... 534
8.8 Electronic Stability and Protection
(Garmin ESP
) ...................................................... 545
Roll Engagement ...................................................... 546
Pitch Engagement..................................................... 547
High Airspeed Protection ........................................... 548
8.9 Scheduler .............................................................. 549
8.10 Electronic Checklists ........................................... 551
8.11 Flight Data Logging ............................................ 554
8.12 Auxiliary Video (Optional) .................................. 556
Video Setup .............................................................557
Display Selection ...................................................... 557
Zoom/Range ............................................................ 558
8.13 Abnormal Operation ........................................... 559
SVT Troubleshooting ................................................. 559
Reversionary Mode ................................................... 559
Unusual Attitudes ..................................................... 560
GDL 69/69A Data Link Receiver Troubleshooting .......... 561
APPENDICES
Annunciations and Alerts ............................................. 563
SVS Terrain Alerts ...................................................... 582
SVS Terrain Status Annunciations ............................... 583
Database Management ................................................ 584
Jeppesen Databases .................................................. 584
Garmin Databases .................................................... 586
Glossary .......................................................................... 593
Frequently Asked Questions ........................................ 599
General TIS Information ............................................... 603
Introduction ............................................................. 603
TIS VS. TAS/TCAS ....................................................... 603
TIS Limitations.......................................................... 603
Map Symbols ................................................................. 605
INDEX
Index ................................................................................ I-1
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-00 Rev. Ax
TABLE OF CONTENTS
Blank Page
190-01895-00 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA62
1
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
SECTION 1 SYSTEM OVERVIEW
NOTE: Refer to the Automatic Flight Control System (AFCS) Section for details on the Garmin AFCS.
The G1000 Integrated Avionics System presents flight instrumentation, position, navigation, communication,
and identification information using flat-panel color displays. The system is distributed across the following Line
Replaceable Units (LRUs):
GDU 1040
Primary Flight Display (PFD)
GDU 1045
Multi Function Display (MFD)
GMA 1347
Audio Panel with Integrated Marker
Beacon Receiver
GIA 63W
Integrated Avionics Units (IAU)
GDC 74A
Air Data Computer (ADC)
GEA 71
Engine/Airframe Unit
GTX 33
Mode S Transponder
GRS 77
Attitude and Heading Reference System
(AHRS)
GMU 44
Magnetometer
GDL 69/69A
Data Link Receiver
GSA 80
AFCS Yaw Damper Servo
GSA 81
AFCS Servos (3)
GSM 86
Servo Mounts (4)
GSR 56
Iridium Transceiver (optional)
GWX 70
Weather Radar
GRA 5500
Radar Altimeter (optional)
Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are shown in Figure 1-2.
The Diamond DA62 may be optionally equipped with a Garmin AFCS Automated Flight Control System,
providing flight director (FD), autopilot (AP), and manual electric trim (MET) functions of the G1000 System.
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-00 Rev. A2
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
1.1 LINE REPLACEABLE UNITS
GDU 1040/1045 (2) – A GDU 1040 is configured as the Primary Flight Display (PFD) and a GDU 1045 as
the Multi Function Display (MFD). Both displays feature 10.4-inch LCD screens with 1024 x 768 resolution.
The displays communicate with each other through a High-speed Data Bus (HSDB) Ethernet connection. Each
display is also paired with an Ethernet connection to an IAU.
GMA 1347
– The Audio Panel integrates navigation/communication radio (NAV/COM) digital audio, intercom,
and marker beacon controls, and is installed between the displays. This unit also provides manual control
of display Reversionary Mode (red
DISPLAY BACKUP
button; see Section 1.4, System Operation) and
communicates with both IAUs using an RS-232 digital interface.
GIA 63W
(2) – The Integrated Avionics Units (IAU) function as the main communications hub, linking all LRUs
with the PFD. Each GIA 63W contains a GPS SBAS receiver, VHF COM/NAV/GS receivers, a flight director (FD;
if Garmin AFCS is installed), and system integration microprocessors. Each GIA 63W is paired with the on-side
display via an HSDB connection. The IAUs are not paired together and do not communicate with each other
directly.
NOTE: Refer to the Airplane Flight Manual (AFM) to determine whether SBAS functionality is approved.
GDC 74A
– The Air Data Computer (ADC) processes data from the pitot/static system and outside air temperature
(OAT) sensor. The ADC provides pressure altitude, airspeed, vertical speed, and OAT information to the G1000
System, and it communicates with the primary IAU, displays, and AHRS using an ARINC 429 digital interface.
GEA 71
– The Engine Airframe Unit receives and processes signals from the engine and airframe sensors. This
unit communicates with both IAUs using an RS-485 digital interface.
GTX 33 or GTX 33 with Extended Squitter
– The GTX 33 solid-state Transponder provides Modes A, C, and
S capability. The GTX 33 with Extended Squitter will also provide 1090 MHz Extended Squitter (1090ES)
transmit capability. The transponder communicates with both IAUs through an RS-232 digital interface.
GRS 77
(2) – The Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading
information via ARINC 429 to both the PFD and the primary IAU. The AHRS contains advanced sensors
(including accelerometers and rate sensors) and interfaces with the Magnetometer to obtain magnetic field
information, with the ADC to obtain air data, and with both IAUs to obtain GPS information. AHRS operation
is discussed in Section 1.4, System Operation.
GMU 44
– The Magnetometer measures local magnetic field and sends data to the AHRS for processing to
determine aircraft magnetic heading. This unit receives power directly from the AHRS and communicates with
it via an RS-485 digital interface.
GDL 69/69A
– The Data Link Satellite Radio Receiver provides real-time weather information to MFD maps
and the PFD Inset Map. The GDL 69A model is also capable of providing digital audio entertainment. The
Data Link Receiver communicates with the MFD via an HSDB connection. A subscription to XM Satellite Radio
Service is required to enable Data Link Receiver capability.
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 IAU.
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).
190-01895-00 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA62
3
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
GRA 5500
– The optional Radar Altimeter provides altitude above the ground (AGL) to the MFD, through the
GIA 63W, using an RS-422 digital interface.
GWX 70
– Provides airborne weather and ground mapped radar data to the MFD, via HSDB ethernet connection.
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-00 Rev. A4
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
Figure 1-1 G1000 System Block Diagram
GMU 44
Magnetometer
Heading
Reversionary
Control
Reversionary
Control
GMA 1347
Audio Panel
GDU 1040
Primary Flight Display
GDU 1045
Multi Function Display
GDC 74A
Air Data
Computer
OAT
Airspeed
Altitude
Vertical Speed
GRS 77
AHRS
Attitude
Rate of Tu rn
Slip/Skid
GTX 33/33ES
Transponder
GEA 71
Engine/Airframe
Unit
GSA 81
Roll Servo
Autopilot Calculations
(optional)
GSA 81
Pitch Servo
Autopilot Calculations
(optional)
GSA 80
Ya w Damper Servo
Ya w Damper Calculations
(optional)
GSA 81
Pitch Tr im Servo
Autopilot Calculations
(optional)
No. 1 GIA 63W
Integrated Avionics Unit
System Inegration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/SBAS
Glideslope
Flight Director (with AFCS option)
GPS Output
No. 2 GIA 63W
Integrated Avionics Unit
System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/SBAS
Glideslope
GPS Output
190-01895-00 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA62
5
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
No. 2 GIA 63W
Integrated Avionics Unit
System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/SBAS
Glideslope
GDL 69/69A
Data Link Receiver
Real-time Weather
Digital Audio Entertainment
(optional subscription-
based service)
Avidyne
TAS600 Series
Traffic Advisory System
(optional)
Honeywell
KN 63
DME
(optional)
Avidyne
TWX 670
Lightning Strike and
Thunderstorm Detection
(optional)
Garmin
GRA 5500
Radar Altimeter
(optional)
Becker
RA 3502-(1)
ADF Receiver
(optional)
Free Flight
Radar Altimeter
(optional))
GWX 70
Weather Radar
Airborne Weather Radar
(optional)
Figure 1-2 G1000 With Optional/Additional Interfaces
NOTE: For information on additional equipment shown in Figure 1-2, consult the applicable optional interface
user’s guide. This document assumes that the reader is already familiar with the operation of this additional
equipment.
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-00 Rev. A6
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
1.2 SECURE DIGITAL (SD) CARDS
NOTE:
Ensure the G1000 System is powered off before inserting an SD card.
NOTE:
Refer to the Appendix for instructions on updating databases.
The PFD and MFD data card slots use Secure Digital (SD) cards and are located on the upper right side of the
display bezels. Each display bezel is equipped with two SD card slots. SD cards are used for aviation database
and system software updates as well as terrain database storage.
Installing an SD card:
1) Insert the SD card in the SD card slot, pushing the card in until the spring latch engages. The front of the card
should remain flush with the face of the display bezel.
2) To eject the card, gently press on the SD card to release the spring latch.
Figure 1-3 Display Bezel SD Card Slots
SD Card Slots
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Garmin G1000: Diamond DA62 User guide

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