Garmin G1000 - Diamond DA62 User guide

®

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

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:

•Itisthepilot’sresponsibilitytoremainfamiliarwithallFAAregulatoryandadvisoryguidanceandinformation

related to the use of databases in the National Airspace System.

•GarminequipmentwillonlyrecognizeandusedatabasesthatareobtainedfromGarminorJeppesen.Databases

obtainedfromGarminorJeppesenthathaveaType2LetterofAuthorization(LOA)fromtheFAAareassured

compliance with all data quality requirements (DQRs). A copy of the Type 2 LOA is available for each applicable

database and can be viewed at http://ﬂy.garmin.com by selecting ‘Aviation Database Declarations.’

•Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with

established FAA regulatory guidance, but does not constitute authorization to ﬂy any and all terminal procedures

that may be presented by the system. It is the pilot’s responsibility to operate in accordance with established

AFM(S) and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment.

NOTE

: The pilot/operator must review and be familiar with Garmin’s database exclusion list as discussed in

SAIB CE-14-04 to determine what data may be incomplete. The database exclusion list can be viewed at

www.ﬂygarmin.com by selecting ‘Database Exclusions List.’

NOTE

: Thepilot/operator must haveaccess to Garmin andJeppesen database alertsand consider their

impact on the intended aircraft operation. The database alerts can be viewed at www.ﬂygarmin.com by

selecting ‘Aviation Database Alerts.’

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

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

GarminDatabases/JeppesenChartviewDatabase ........ 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

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Garmin G1000 - Diamond DA62 User guide

Garmin G1000 - Diamond DA62 User guide

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