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®
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.
Tel: 913.397.8200
Fax: 913.397.8282
AOG Hotline: 913.397.0836
Aviation Dealer
Technical Support:
888.606.5482
www.garmin.com
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,Houndsdown 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
Diamond DA62
190-01895-01
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
190-01895-01 Rev. B
Copyright © 2015, 2016 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 1373.01 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
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
®
, WATCH
®
, 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.
Skywatch
®
and Stormscope
®
are registered trademarks of L-3 Communications. Ryan
®
, TCAD
®
and Avidyne
®
are registered trademarks
of Avidyne Corporation. CO Guardian is a trademark of CO Guardian, Inc. AC-U-KWIK
®
is a registered trademark of Penton Business
Media Inc. Bendix/King
®
and Honeywell
®
are registered trademarks of Honeywell International, Inc. Becker
®
is a registered trademark of
Becker Flugfunkwerk GmbH. NavData
®
is a registered trademark of Jeppesen, Inc.; Wi-Fi
®
is a registered trademark of the Wi-Fi Alliance.
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.
October 2016 Printed in the U.S.A
190-01895-01 Rev. B
Garmin G1000 Pilot’s Guide for the Diamond DA62
i
WARNINGS, CAUTIONS, AND NOTES
WARNING: Do not use terrain avoidance displays as the sole source of information for maintaining separation
from terrain and obstacles. Garmin obtains terrain and obstacle data from third party sources and cannot
independently verify the accuracy of the information.
WARNING: Always refer to current aeronautical charts and NOTAMs for verification of displayed aeronautical
information. Displayed aeronautical data may not incorporate the latest NOTAM information.
WARNING: Do not use geometric altitude for compliance with air traffic control altitude requirements. The
primary barometric altimeter must be used for compliance with all air traffic control altitude regulations,
requirements, instructions, and clearances.
WARNING: Do not use basemap information (land and water data) as the sole means of navigation. Basemap
data is intended only to supplement other approved navigation data sources and should be considered only
an aid to enhance situational awareness.
WARNING: Do not rely solely upon the display of traffic information to accurately depict all of the traffic
within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information
from aircraft or ground stations, traffic may be present that is not represented on the display.
WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous
weather. Information contained within data link weather products may not accurately depict current
weather conditions.
WARNING: Do not use the indicated data link weather product age to determine the age of the weather
information shown by the data link weather product. Due to time delays inherent in gathering and processing
weather data for data link transmission, the weather information shown by the data link weather product
may be older than the indicated weather product age.
WARNING: The displayed minimum safe altitude (MSAs) are only advisory in nature and should not be relied
upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical
charts for appropriate minimum clearance altitudes.
WARNING: Always obtain qualified instruction prior to operational use of this equipment.
WARNING
:
Do not use a QFE altimeter setting with this system. System functions will not operate properly
with a QFE altimeter setting. Use only a QNH altimeter setting for height above mean sea level, or the
standard pressure setting, as applicable.
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-01 Rev. Bii
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: 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 (GRS 77 installations only) 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: 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.
190-01895-01 Rev. B
Garmin G1000 Pilot’s Guide for the Diamond DA62
iii
WARNINGS, CAUTIONS, AND NOTES
WARNING: Do not use SurfaceWatch
™
information as the primary method of flight guidance during airborne
or ground operations. SurfaceWatch does not have NOTAM or ATIS information regarding the current active
runway, condition, or information about the position of hold lines.
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: Lamp(s) inside this product 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
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: 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: Operate the G1000 system power through at least one cycle in a period of four days of continuous
operation to avoid an autonomous system reboot.
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.
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-01 Rev. Biv
WARNINGS, CAUTIONS, AND NOTES
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.
NOTE
: The FAA has asked Garmin to remind pilots who fly with Garmin database-dependent avionics of the
following:
•Itisthepilot’sresponsibilitytoremainfamiliarwithallFAAregulatoryandadvisoryguidanceandinformation
related to the use of databases in the National Airspace System.
•GarminequipmentwillonlyrecognizeandusedatabasesthatareobtainedfromGarminorJeppesen.Databases
obtainedfromGarminorJeppesenthathaveaType2LetterofAuthorization(LOA)fromtheFAAareassured
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
: Thepilot/operator must haveaccess to Garmin andJeppesen database alertsand consider their
impact on the intended aircraft operation. The database alerts can be viewed at www.flygarmin.com by
selecting ‘Aviation Database Alerts.’
190-01895-01 Rev. B
Garmin G1000 Pilot’s Guide for the Diamond DA62
v
WARNINGS, CAUTIONS, AND NOTES
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.
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-01 Rev. Bvi
WARNINGS, CAUTIONS, AND NOTES
Blank Page
190-01895-01 Rev. B
Garmin G1000 Pilot’s Guide for the Diamond DA62
vii
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
190-01895-01 A
B
9/20/16
10/5/16
i – I-6
i – I-6
Production release at GDU 15.12
Added ADS-B Traffic and Weather
Updated Weather Radar Information
Updated Sirius XM information
Updated Connext information
Added Bluetooth Management for Flight Stream 210
Updated CAS Messages
Updated Weather and Traffic Messages
Updated System Messages
Updated Softkey Maps
Updated Warnings/Cautions/Notes
Updated Garmin Contact Numbers
Clerical
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-01 Rev. Bviii
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
System Annunciations ................................................... 9
System Status ............................................................. 10
AHRS Operation ......................................................... 12
GPS Receiver Operation .............................................. 13
1.5 System Controls..................................................... 17
PFD/MFD Controls ...................................................... 17
MFD/PFD Control Unit ................................................. 20
Softkey Function ......................................................... 22
1.6 Accessing System Functionality .......................... 29
Menus ....................................................................... 29
Data Entry.................................................................. 29
Page Groups .............................................................. 31
System Settings .......................................................... 36
Timers ....................................................................... 49
Scheduler ................................................................... 51
Electronic Checklists ................................................... 53
1.7 Display Backlighting ............................................. 55
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 60
Airspeed Indicator ...................................................... 60
Attitude Indicator ....................................................... 62
Altimeter ................................................................... 63
Vertical Speed Indicator (VSI) ....................................... 65
Vertical Deviation ....................................................... 66
Horizontal Situation Indicator (HSI) .............................. 67
Course Deviation Indicator (CDI) .................................. 72
2.2 Supplemental Flight Data .................................... 79
Outside Air Temperature .............................................. 79
Wind Data ................................................................. 81
Vertical Navigation (VNV) Indications ........................... 82
2.3 PFD Annunciations and Alerting Functions ........ 83
System Alerting .......................................................... 83
Marker Beacon Annunciations...................................... 84
Altitude Alerting ......................................................... 84
Low Altitude Annunciation .......................................... 84
Minimum Descent Altitude/Decision Height Alerting ...... 85
Radar Altimeter .......................................................... 86
2.4 Abnormal Operations ........................................... 88
Abnormal GPS Conditions ........................................... 88
Unusual Attitudes ....................................................... 89
SECTION 3 ENGINE INDICATION SYSTEM (EIS)
3.1 Engine Display ....................................................... 93
3.2 System Display ...................................................... 95
3.3 Fuel Display ............................................................ 97
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview .............................................................. 101
MFD/PFD Controls and Frequency Display ................... 102
Audio Panel Controls ................................................ 104
MFD/PFD Control Unit ............................................... 106
4.2 COM Operation .................................................... 108
COM Transceiver Selection and Activation ................... 108
COM Transceiver Manual Tuning ................................ 109
Quick-tuning and Activating 121.500 MHz .................. 111
Auto-tuning the COM Frequency ................................ 112
Frequency Spacing .................................................... 116
Automatic Squelch .................................................... 117
Volume .................................................................... 117
4.3 NAV Operation ..................................................... 118
NAV Radio Selection and Activation ........................... 118
NAV Receiver Manual Tuning ..................................... 119
Auto-tuning a NAV Frequency from the MFD ............... 122
Marker Beacon Receiver ............................................ 125
ADF/DME Tuning ...................................................... 126
4.4 GTX 33 ES Mode S Transponder ........................ 131
Transponder Controls ................................................ 131
Transponder Mode Selection ...................................... 132
ADS-B TX (Optional) .................................................. 134
Entering a Transponder Code ..................................... 134
IDENT Function ........................................................ 136
Flight ID Reporting.................................................... 136
4.5 Additional Audio Panel Functions ..................... 138
Power-up ................................................................. 138
Mono/Stereo Headsets .............................................. 138
Intercom .................................................................. 138
Clearance Recorder and Player ................................... 140
SPlit COM ................................................................ 141
Entertainment Inputs ................................................ 141
4.6 Audio Panel Preflight Procedure ....................... 142
4.7 Abnormal Operation ........................................... 143
190-01895-01 Rev. B
Garmin G1000 Pilot’s Guide for the Diamond DA62
ix
TABLE OF CONTENTS
Stuck Microphone ..................................................... 143
COM Tuning Failure ................................................... 143
Audio Panel Fail-safe Operation ................................. 143
Reversionary Mode ................................................... 143
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 145
Navigation Status Box ............................................... 146
5.2 Using Map Displays ............................................. 148
Map Orientation ....................................................... 148
Map Range .............................................................. 150
Map Panning ............................................................ 152
Measuring Bearing and Distance ................................ 157
Topography .............................................................. 158
Map Symbols ........................................................... 161
Airways ................................................................... 167
Track Vector ............................................................. 169
Wind Vector ............................................................. 170
Nav Range Ring........................................................ 171
Fuel Range Ring ....................................................... 172
Field of View (SVT) .................................................... 173
Selected Altitude Intercept Arc ................................... 174
5.3 Waypoints ............................................................. 175
Airports ................................................................... 176
Intersections ............................................................ 183
NDBs ....................................................................... 185
VORs ....................................................................... 187
VRPs ....................................................................... 189
User Waypoints ........................................................ 191
5.4 Airspaces .............................................................. 197
5.5 Direct-to-Navigation .......................................... 201
5.6 Flight Planning ..................................................... 206
Flight Plan Creation .................................................. 207
Adding Waypoints to an Existing Flight Plan ................215
Adding Airways to a Flight Plan ................................. 217
Adding Procedures to a Stored Flight Plan .................. 219
Flight Plan Storage ................................................... 226
Flight Plan Editing .................................................... 228
Along Track Offsets ................................................... 231
Parallel Track ............................................................ 233
Activating a Flight Plan Leg ....................................... 236
Inverting a Flight Plan ............................................... 237
Flight Plan Views ...................................................... 238
Closest Point of FPL .................................................. 240
User-Defined Holding Patterns ................................... 240
5.7 Vertical Navigation ............................................. 245
Altitude Constraints .................................................. 247
5.8 Procedures ...........................................................251
Departures ............................................................... 252
Arrivals ................................................................... 255
Approaches ............................................................. 258
5.9 Trip Planning ........................................................ 266
Trip Planning ............................................................ 266
5.10 RAIM Prediction................................................... 270
5.11 Navigating a Flight Plan ..................................... 273
5.12 Abnormal Operation ........................................... 301
SECTION 6 HAZARD AVOIDANCE
6.1 SiriusXM Weather ................................................ 304
Activating Services .................................................... 304
Using SiriusXM Weather Products .............................. 305
6.2 Garmin Connext Weather ................................... 338
Registering the Iridium Satellite System ...................... 338
Registering Garmin Connext Weather ......................... 339
Accessing Garmin Connext Weather Products .............. 341
Connext Data Requests ............................................. 348
Garmin Connext Weather Products ............................. 352
Abnormal Operations ................................................ 367
6.3 FIS-B Weather ...................................................... 369
Using FIS-B Weather Products .................................... 369
FIS-B Weather Status................................................. 391
6.4 Airborne Color Weather Radar .......................... 392
System Description ................................................... 392
Principles of Pulsed Airborne Weather Radar ............... 392
Safe Operating Distance ............................................ 396
Basic Antenna Tilt Setup ............................................ 397
Weather Mapping and Interpretation ......................... 398
Ground Mapping and Interpretation ........................... 408
Weather Radar Overlay on the Navigation Map Page ... 409
System Status ........................................................... 411
6.5 Stormscope Lightning Detection System ......... 413
Setting Up Stormscope on the Navigation Map ........... 413
Selecting the Stormscope Page .................................. 417
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-01 Rev. Bx
TABLE OF CONTENTS
6.6 Terrain Proximity ................................................. 418
Displaying Terrain Proximity Data ............................... 418
Terrain Proximity Page ............................................... 421
6.7 Profile View Terrain ............................................. 423
Profile View Display .................................................. 424
6.8 Terrain-SVS ........................................................... 427
Displaying Terrain-SVS Data ....................................... 428
Terrain-SVS Page ...................................................... 430
Terrain-SVS Alerts ..................................................... 432
System Status ........................................................... 435
6.9 Traffic Information Service (TIS) ........................ 436
Displaying Traffic Data .............................................. 437
Traffic Map Page ....................................................... 439
TIS Alerts ................................................................. 440
System Status ........................................................... 441
6.10 Avidyne TAS600 Traffic ........................................ 444
TAS Symbology ......................................................... 444
Displaying Traffic Data .............................................. 445
Altitude Display ........................................................ 447
Traffic Map Page Display Range ................................. 447
TAS Alerts ................................................................ 449
System Status ........................................................... 450
6.11 Garmin GDL 88 ADS-B Traffic ............................. 451
ADS-B System Overview ............................................ 451
ADS-B with TAS ........................................................ 453
Conflict Situational Awareness & Alerting ................... 453
Airborne and Surface Applications .............................. 456
Traffic Description ..................................................... 457
Operation ................................................................ 457
System Status ........................................................... 466
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Controls ...................................................... 470
7.2 Flight Director Operation ................................... 472
Activating the Flight Director ..................................... 472
AFCS Status Box ....................................................... 473
Command Bars ......................................................... 474
Flight Director Modes ................................................ 474
7.3 Vertical Modes ..................................................... 475
Pitch Hold Mode (PIT) ............................................... 476
Selected Altitude Capture Mode (ALTS) ....................... 477
Altitude Hold Mode (ALT) .......................................... 478
Vertical Speed Mode (VS) .......................................... 479
Flight Level Change Mode (FLC) ................................. 480
Vertical Navigation Modes (VPTH, ALTV) ..................... 481
Glidepath Mode (GP) (SBAS only) ............................... 486
Glideslope Mode (GS) ............................................... 488
Takeoff (TO) and Go Around (GA) Modes .................... 489
7.4 Lateral Modes ...................................................... 490
Roll Hold Mode (ROL) ............................................... 491
Heading Select Mode (HDG) ...................................... 492
Navigation Modes (GPS, VOR, LOC, BC) ...................... 493
Approach Modes (GPS, VAPP, LOC) ............................. 495
7.5 Autopilot and Yaw Damper Operation ............. 497
Flight Control ........................................................... 497
Engaging the Autopilot and Yaw Damper .................... 498
Control Wheel Steering ............................................. 498
Disengaging the Autopilot and Yaw Damper ................ 499
Underspeed Protection .............................................. 500
7.6 Example Flight Plan ............................................ 502
Departure ................................................................ 502
Intercepting a VOR Radial .......................................... 504
Flying a Flight Plan/GPS Course ................................. 505
Descent ................................................................... 506
Approach ................................................................. 510
Go Around/Missed Approach ..................................... 512
7.7 AFCS Annunciations and Alerts ......................... 514
AFCS Status Alerts .................................................... 514
Overspeed Protection ................................................ 515
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision Technology (SVT) (Optional) .. 518
SVT Operation .......................................................... 519
SVT Features ............................................................ 521
Field of View ............................................................ 529
8.2 SafeTaxi ................................................................ 531
8.3 ChartView (Optional) .......................................... 536
ChartView Softkeys ................................................... 537
Terminal Procedures Charts ....................................... 538
Chart Options ........................................................... 546
Day/Night View ........................................................ 552
ChartView Cycle Number and Expiration Date ............. 554
8.4 FliteCharts ............................................................ 557
FliteCharts Softkeys .................................................. 558
190-01895-01 Rev. B
Garmin G1000 Pilot’s Guide for the Diamond DA62
xi
TABLE OF CONTENTS
Terminal Procedures Charts ....................................... 559
Chart Options ........................................................... 566
Day/Night View ........................................................ 570
FliteCharts Cycle Number and Expiration Date ............. 572
8.5 Airport Directory ................................................. 575
Airport Directory Database Cycle Number and Revision 576
8.6 SiriusXM Satellite Radio (Optional) .................. 578
Activating SiriusXM Satellite Radio Services ................ 578
Using SiriusXM Radio ................................................ 580
8.7 Satellite Telephone Services (Optional) ............ 583
Telephone Communication ........................................ 583
Text Messaging (SMS) ............................................... 590
8.8
Electronic Stability and Protection (Garmin ESP
™
)
601
Roll Engagement ...................................................... 602
Pitch Engagement..................................................... 603
High Airspeed Protection ........................................... 604
8.9 Scheduler .............................................................. 605
8.10 Electronic Checklists ........................................... 607
8.11 Flight Data Logging ............................................ 610
8.12 Auxiliary Video (Optional) .................................. 612
Video Setup .............................................................613
Display Selection ...................................................... 613
Zoom/Range ............................................................ 614
8.13 Bluetooth
®
Management ................................... 615
8.14 Abnormal Operation ........................................... 617
SVT Troubleshooting ................................................. 617
Reversionary Mode ................................................... 617
Unusual Attitudes ..................................................... 618
GDL 69A SXM Data Link Receiver Troubleshooting ....... 619
APPENDICES
Annunciations and Alerts ............................................. 621
Aircraft Alerts ........................................................... 624
Voice Alerts .............................................................. 626
G1000 System Annunciations .................................... 628
G1000 System Message Advisories ............................. 630
ADS-B Status Page Messages ..................................... 640
AFCS Status Annunciations ........................................ 641
SVS Terrain Alerts ...................................................... 642
SVS Terrain Status Annunciations ............................... 642
TIS Alerts and Annunciations...................................... 643
TAS Alerts and Annunciations .................................... 644
ADS-B Alerts and Annunciations ................................. 645
Weather Radar Alerts and Annunciations .................... 646
GDL 69A SXM Data Link Receiver Error Messages ....... 647
Database Management ................................................ 649
Navigation Databases ............................................... 649
GarminDatabases/JeppesenChartviewDatabase ........ 655
Magnetic Field Variation Database Update .................. 660
Garmin Aviation Glossary ............................................ 663
Frequently Asked Questions ........................................ 673
General TIS Information ............................................... 677
Introduction ............................................................. 677
TIS VS. TAS/TCAS ....................................................... 677
TIS Limitations.......................................................... 677
Map Symbols ................................................................. 679
Telephone/Text Messaging ........................................... 683
INDEX
Index ................................................................................ I-1
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-01 Rev. Bxii
TABLE OF CONTENTS
Blank Page
190-01895-01 Rev. B
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 69A SXM
Data Link Receiver
•
GSA 80
AFCS Yaw Damper Servo
•
GSA 81
AFCS Servos (3)
•
GSM 86
Servo Mounts (4)
•
GWX 70
Weather Radar
•
GSR 56
Iridium Transceiver (optional)
•
GCU 476
MFD/PFD Control Unit (optional)
•
GRA 5500
Radar Altimeter (optional)
•
GDL 88
ADS-B Transceiver (optional)
•
GDL 59
WiFi Data Link (optional)
•
Flight Stream 210
Wireless Bluetooth
®
Gateway
(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 system.
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-01 Rev. B2
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
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 69A SXM
– The Data Link Satellite Radio Receiver provides real-time weather information to MFD maps
and the PFD Inset Map. The GDL 69A SXM 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).
190-01895-01 Rev. B
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.
•
GCU 476
(1) (Optional) – The Control Unit provides MFD/PFD and radio tuning control through an RS-232
digital interface.
•
GDL 88
(1) (Optional) – Provides ADS-B Traffic in and FIS-B Weather.
•
GDL 59
(1) (Optional) – GDL 59 operation is performed with the MFD through HSDB.
•
Flight Stream 210
(Optional) – The Flight Stream 210 is optional and provides wireless Bluetooth connectivity
between a compatible tablet/mobile device and the avionics system.
•
GSR 56
(Optional)– The Iridium Transceiver operation for voice communication is by means of pilot and
copilot headsets in the cockpit. The system is also capable of SMS text messaging. Connection to the system is
through the RS-232 bus.
Garmin G1000 Pilot’s Guide for the Diamond DA62
190-01895-01 Rev. B4
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
Figure 1-1 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 Turn
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
Yaw Damper Servo
Yaw Damper Calculations
(optional)
GSA 81
Pitch Trim 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
/
