Garmin G3000 Owner’s Manual

Name: Garmin G3000
Brand: Garmin
SKU: 17899655
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4 (1)

Integrated Avionics System

G3000

Pilot’s Guide

Daher TBM 930

System Software Version 2234.05 or later

This manual reﬂects the operation of System Software version 2234.05 or later for the Daher TBM 930. 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.

Garmin AT, Inc.

2345 Turner Road SE Salem, OR 97302, U.S.A.

Garmin (Europe) Ltd.

Liberty House, Hounsdown Business Park Southampton, Hampshire SO40 9LR U.K.

Garmin Corporation

No. 68, Zhangshu 2nd Road Xizhi District, New Taipei City, Taiwan

Contact Garmin Product Support or view warranty information at ﬂygarmin.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® and G3000®, WATCH®, FliteCharts®, Connext® and SafeTaxi® are registered trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin.

NavData® is a registered trademark of Jeppesen, Inc.; Stormscope® is a registered trademark of L-3 Communications. SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, Inc.

AC-U-KWIK® is a registered trademark of Penton Business Media Inc. NavData® is a registered trademark of Jeppesen, Inc.; Wi-Fi® is a registered trademark of the Wi-Fi Alliance. The Bluetooth® word mark and logos are owned by the Bluetooth SIG, Inc. and any use of such marks by Garmin is under license.

AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively “AOPA”) expressly disclaim all warranties, with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties of merchantability and ﬁtness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to you.

AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”) expressly disclaim all warranties with respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of merchantability and ﬁtness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to licensee.

Printed in the U.S.A

190-02046-02 Rev. A

Garmin G3000 Pilot’s Guide for the Daher TBM 930

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Garmin G3000 Pilot’s Guide for the Daher TBM 930

190-02046-02 Rev. A

WARNINGS, CAUTIONS, AND NOTES

WARNING: Do not operate this equipment without ﬁrst obtaining qualiﬁed instruction.

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: 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: Do not rely on the displayed minimum safe altitude (MSAs) as the sole source of obstacle

and terrain avoidance information. Always refer to current aeronautical charts for appropriate minimum clearance altitudes.

WARNING: Do not use GPS to navigate to any active waypoint identiﬁed as a ‘NON WGS84 WPT’ by a

system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned in error as displayed.

190-02046-02 Rev. A

Garmin G3000 Pilot’s Guide for the Daher TBM 930

WARNINGS, CAUTIONS, AND NOTES

WARNING: Do not rely on the autopilot to level the aircraft at the MDA/DH when ﬂying 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 on the accuracy of attitude and heading indications in the following geographic

areas (due to variations in the earth’s magnetic ﬁeld): 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: 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: Do not use the Garmin SVT runway depiction as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing.

WARNING: Do not operate the weather radar in a transmitting mode when personnel or objects are within

the MPEL boundary.

WARNING: Always position the weather radar gain setting to Calibrated for viewing the actual intensity of

precipitation. Changing the gain in weather mode causes precipitation intensity to be displayed as a color not representative of the true intensity.

WARNING: Do not consider the overﬂight of thunderstorms to be safe, as extreme turbulence may exist

signiﬁcantly above observed returns.

WARNING: Do not assume weather radar transmission is disabled unless all display panes displaying

weather radar are set to Standby Mode, and are displaying ‘STANDBY’ in the center of each weather radar display. Transmission is also disabled by touching the Radar On Button or pressing the Radar On Softkey to set the weather radar system to Off Mode, as indicated by a gray annunciator.

WARNING: Do not rely only on the Turbulence Detection function for hazardous weather avoidance, or to

maneuver in, near, or around areas of hazardous weather.

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.

Garmin G3000 Pilot’s Guide for the Daher TBM 930

190-02046-02 Rev. A

WARNINGS, CAUTIONS, AND NOTES

WARNING: Do not use TAWS information for primary terrain or obstacle avoidance. TAWS is intended only

to enhance situational awareness.

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: Do not use a QFE altimeter setting with this system. System functions will not operate properly

with a QFE altimeter setting. Use only a QNH altimeter setting for height above mean sea level, or the standard pressure setting, as applicable.

WARNING: Do not use 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: Do not allow repairs to be made by anyone other than an authorized Garmin service center. Unauthorized repairs or modiﬁcations could void both the warranty and affect the airworthiness of the aircraft.

CAUTION: Never disconnect power to the system when loading a database. Power interruption during the

database loading process could result in maintenance being required to reboot the system.

CAUTION: Avoid areas on the radar display that appear “shadowed” (gray). The accuracy of the intensity

of returns in the shaded areas should be treated as suspect. Exercise extreme caution, making maneuvering decisions with this information in mind.

CAUTION: When all display panes displaying weather radar are set to Standby Mode, the antenna is parked

at the center line. It is always a good idea to put the radar in Standby Mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly.

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: 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.

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Garmin G3000 Pilot’s Guide for the Daher TBM 930

WARNINGS, CAUTIONS, AND NOTES

NOTE: The United States government operates the Global Positioning System and is solely responsible for

its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or misinterpreted and, therefore, become unsafe.

NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) this device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation.

NOTE: 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 ﬂygarmin.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 pertinent aircraft documents and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment.

Garmin G3000 Pilot’s Guide for the Daher TBM 930

190-02046-02 Rev. A

WARNINGS, CAUTIONS, AND NOTES

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 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 ﬂygarmin.com by selecting ‘Aviation Database Alerts.’

NOTE: If the pilot/operator wants or needs to adjust the database, contact Garmin Product Support.

NOTE: Garmin requests the ﬂight crew report any observed discrepancies related to database information.

These discrepancies could come in the form of an incorrect procedure; incorrectly identiﬁed terrain, obstacles and ﬁxes; or any other displayed item used for navigation or communication in the air or on the ground. Go to ﬂygarmin.com and select ‘Aviation Data Error Report’.

NOTE: Electronic aeronautical charts displayed on this system have been shown to meet the guidance in AC

120-76D as a Type B Electronic Flight Bag (EFB) for FliteCharts and ChartView. The accuracy of the charts is subject to the chart data provider. Own-ship position on airport surface charts cannot be guaranteed to meet the accuracy speciﬁed in AC 120-76D. Possible additional requirements may make a secondary source of aeronautical charts, such as traditional paper charts or an additional electronic display, necessary on the aircraft and available to the pilot. If the secondary source of aeronautical charts is a Portable Electronic Device (PED), its use must be consistent with the guidance in AC 120-76D.

NOTE: The navigation databases used in Garmin navigation systems contain Special Procedures. Prior

to ﬂying these procedures, pilots must have speciﬁc FAA authorization, training, and possession of the corresponding current, and legitimately-sourced chart (approach plate, etc.). Inclusion of the Special Procedure in the navigation database DOES NOT imply speciﬁc FAA authorization to ﬂy the procedure.

NOTE: Terrain and obstacle alerting is not available north of 89º North latitude and south of 89º South latitude. This is due to limitations present within the Terrain database and the system’s ability to process the data representing the affected areas.

NOTE: The nose of the ‘own ship’ symbol represents the location of the aircraft. The center of any trafﬁc

symbol represents the location of that trafﬁc. The trafﬁc and own ship symbols are an abstract representation and do not reﬂect the physical extent of the aircraft/trafﬁc, and should not replace other methods for identifying trafﬁc.

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.

190-02046-02 Rev. A

Garmin G3000 Pilot’s Guide for the Daher TBM 930

WARNINGS, CAUTIONS, AND NOTES

NOTE: Intruder aircraft at or below 500 ft. AGL may not appear on the Garmin SVT display or may appear

as a partial symbol.

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: Operate G3000 system power through at least one cycle in a period of four days of continuous

operation to avoid an autonomous system reboot.

Garmin G3000 Pilot’s Guide for the Daher TBM 930

190-02046-02 Rev. A

RECORD OF REVISIONS

Record of Revisions

Part Number Revision Date Page Range Description

190-02046-00 A

2/16

All

Production release.

190-02046-01 A 5/25 All Added support for HF Radio

190-02046-02 A 5/29/20 All Updated to GDU 20.92

3/16

All

Removed references to Baro-VNAV Removed reference to takeoff conﬁguration of landing gear and ﬂaps from the Negative Climb Rate TAWS discussion Removed references to GDL 59 Removed references to Wi-Fi Removed APR Advisory System Message Added Animated NEXRAD for SiriusXM Weather

Added SELCAL Added other GDU 6.56 parameters Removed references to CCD VNAV functions.

190-02046-02 Rev. A

Garmin G3000 Pilot’s Guide for the Daher TBM 930

RECORD OF REVISIONS

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TABLE OF CONTENTS

SECTION 1 SYSTEM OVERVIEW

1.1 System Description ..............................................1

1.2 System Controls ...................................................4

PFD Controls .......................................................................4

Touchscreen Controller ......................................................10

Secure Digital Cards .......................................................... 30

1.3 System Operation ..............................................32

System Power-On .............................................................. 32

Normal Operation .............................................................33

Reversionary Display Operation ........................................34

Touchscreen Controller Failure ..........................................35

AHRS Operation ................................................................ 35

GPS Receiver Operation ....................................................37

Annunciations ................................................................... 40

1.4 Initialization ....................................................... 41

1.5 System Management .........................................43

Avionics Settings ............................................................... 43

Avionics Status..................................................................53

SiriusXM Information ........................................................ 54

1.6 Utilities...............................................................55

Timer .................................................................................55

Trip Statistics ..................................................................... 56

Scheduled Messages ......................................................... 60

Screen Cleaning ................................................................61

Crew Proﬁles ..................................................................... 61

1.7 Display Backlighting ..........................................64

2.4 PFD Annunciations and Alerting Functions ...... 108

Marker Beacon Annunciations ........................................108

Altitude Alerting .............................................................. 108

Low Altitude Annunciation .............................................. 109

Minimum Altitude Alerting .............................................. 109

Radio Altimeter (RA) ....................................................... 110

2.5 Abnormal Operations .......................................112

Abnormal GPS Conditions ............................................... 112

Comparator Annunciations .............................................113

Reversionary Sensor Annunciations ................................114

Garmin SVT Troubleshooting ...........................................115

Unusual Attitudes ...........................................................115

SVT Unusual Attitudes ....................................................116

SECTION 3 ENGINE INDICATION & CREW ALERTING

SYSTEMS

3.1 Engine Indication System (EIS) ........................118

3.2 Synoptics .......................................................... 124

Electrical System .............................................................125

Fuel System ..................................................................... 128

General Systems .............................................................129

3.3 Landing Field Elevation ...................................131

3.4 Crew Alerting System (CAS) ............................. 132

CAS Messages and Prioritization ....................................133

3.5 Reversionary Mode ..........................................134

SECTION 4 AUDIO AND CNS

SECTION 2 FLIGHT INSTRUMENTS

2.1 Flight Instruments .............................................. 68

Airspeed Indicator ............................................................. 68

Attitude Indicator .............................................................. 70

Altimeter ........................................................................... 71

Vertical Speed Indicator (VSI) ............................................74

Vertical Deviation Indicator (VDI) ......................................75

Horizontal Situation Indicator (HSI) ................................... 78

2.2 Garmin SVT (Synthetic Vision Technology) ......... 92

SVT Operation ................................................................... 93

SVT Features .....................................................................95

Field of View ...................................................................103

2.3 Supplemental Flight Data ................................104

Temperature Displays ...................................................... 104

Generic Timer ..................................................................104

Wind Data ....................................................................... 105

Angle of Attack (AOA) Indicator ...................................... 106

Vertical Navigation (VNV) Indications .............................107

4.1 Overview .......................................................... 135

Touchscreen Controller Audio and CNS Controls .............136

PFD COM/NAV display ....................................................138

MFD COM display ........................................................... 139

COM Transceiver Selection and Activation ......................140

COM Frequency Tuning ...................................................143

Frequency Spacing ..........................................................151

Automatic Squelch .......................................................... 152

Volume ............................................................................153

HF COM Transceiver ........................................................155

SELCAL ............................................................................ 156

4.2 NAV Operation ................................................. 159

NAV Radio Selection and Activation................................159

NAV Receiver Tuning ....................................................... 160

Marker Beacon Receiver .................................................168

ADF/DME Tuning ............................................................. 170

4.3 Transponder(s) .................................................176

Transponder Controls ...................................................... 176

Transponder Selection ..................................................... 177

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Transponder Mode Selection ........................................... 177

Entering a Transponder Code ..........................................180

IDENT Function ...............................................................181

4.4 Additional Audio Functions ..............................182

Mono/Stereo Headsets .................................................... 182

Speaker ...........................................................................182

Intercom ..........................................................................182

Passenger Address (PA) System .......................................186

Clearance Recorder and Player .......................................186

3D Audio ......................................................................... 188

Simultaneous COM Operation ........................................189

Auxiliary Audio ...............................................................190

Audio Feedback (Clicks) ..................................................192

Telephone (TEL) ...............................................................193

4.5 Abnormal Operation ........................................194

Stuck Microphone ........................................................... 194

COM Failure ....................................................................194

COM Tuning Failure .........................................................195

Audio Controller Fail-Safe Operation ..............................195

Touchscreen Controller Failure ........................................195

SECTION 5 FLIGHT MANAGEMENT

5.1 Introduction .....................................................197

Navigation Status Box / MFD Navigation Data Bar ......... 199

5.2 Using Map Displays .......................................... 201

Map Settings Synchronization ......................................... 201

Map Orientation .............................................................202

Map Range .....................................................................204

Map Panning ...................................................................206

Measuring Bearing and Distance ....................................210

Absolute Terrain .............................................................. 212

Map Symbols ..................................................................215

Airways ...........................................................................221

Additional Navigation Map Items ................................... 222

5.3 Waypoints ........................................................227

Airports ........................................................................... 227

Non-Airport and User Created Waypoints ....................... 233

5.4 Airspaces ..........................................................242

Nearest Airspace ............................................................. 243

Smart Airspace ................................................................ 246

5.5 Direct-to Navigation .......................................247

5.6 Flight Planning ................................................. 252

Introduction ....................................................................252

Creating a Flight Plan .....................................................257

Flight Plan Waypoint and Airway Modiﬁcations ..............259

Flight Plan Operations ....................................................271

Managing Flight Plans ....................................................287

5.7 Vertical Navigation ..........................................295

Constraints ...................................................................... 296

Vertical Situation Display ................................................300

5.8 Procedures .......................................................307

Preview Only Procedures ................................................309

Departures ......................................................................310

Arrivals ...........................................................................313

Approaches ..................................................................... 315

5.9 Trip Planning ....................................................328

Trip Statistics ................................................................... 329

Fuel Statistics .................................................................. 330

Other Statistics ................................................................ 330

5.10 Weight and Fuel Planning ................................332

Weight Caution And Warning Conditions ........................336

5.11 Abnormal Operation ........................................337

Dead Reckoning Navigation ............................................337

SECTION 6 HAZARD AVOIDANCE

6.1 Data Link Weather............................................340

Activating Data Link Weather Services ............................ 341

Registering the system for Garmin Connext Services ...... 342

Accessing FIS-B Weather Information .............................342

Weather Product Age ...................................................... 344

Displaying Data Link Weather Products ..........................348

Connext Weather Data Requests .....................................355

Weather Product Overview .............................................359

Data Link Weather Products ............................................ 371

FIS-B Weather Abnormal Operations ............................... 394

Garmin Connext Abnormal Operations ...........................395

6.2 Stormscope Lightning Detection System ......... 396

Using the Stormscope Pane .............................................396

Stormscope Information on Navigation Maps ................. 399

Abnormal Operations ...................................................... 402

System Status..................................................................402

6.3 Airborne Color Weather Radar ......................... 403

System Description .......................................................... 403

Principles of Airborne Weather Radar..............................403

NEXRAD and Airborne Weather Radar ............................ 404

Antenna Beam Illumination ............................................405

Safe Operating Distance .................................................410

Basic Antenna Tilt and Range Setup ................................411

Weather Display And Interpretation ................................ 414

Ground Mapping and Interpretation ............................... 428

Additional Radar Displays ............................................... 429

System Status..................................................................435

6.4 Vertical Situation Display Terrain .....................437

VSD Inset Window...........................................................439

Track Mode Boundary ..................................................... 440

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TABLE OF CONTENTS

6.5 Terrain Displays ................................................ 442

Relative Terrain Symbology .............................................443

Displaying Relative Terrain Information ..........................445

Terrain Pane ....................................................................445

Terrain-SVT and TAWS-B Terrain And Obstacle alerts ......449

Forward Looking Terrain Avoidance ................................451

Additional TAWS-B Alerting ............................................454

System Status..................................................................456

TAWS-B Abnormal operations ......................................... 458

6.6 Trafﬁc Information Service (TIS) ......................460

Trafﬁc Map Pane .............................................................461

Displaying Trafﬁc Data on Navigation Maps ...................462

TIS Alerts ......................................................................... 464

Additional Trafﬁc Displays ............................................... 466

System Status..................................................................467

6.7 Trafﬁc Advisory System (TAS) ...........................469

Theory of Operation ........................................................469

Trafﬁc Alerts .................................................................... 473

Operations ......................................................................476

Additional Trafﬁc Displays ............................................... 477

6.8 ADS-B Trafﬁc ....................................................481

ADS-B System Overview .................................................481

ADS-B Trafﬁc Advisory System (ATAS) .............................484

Airborne and Surface Applications ..................................485

Operation ........................................................................ 486

System Status..................................................................491

SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM

7.1 Overview .......................................................... 495

Basic Autopilot Operation ............................................... 496

AFCS Preﬂight Test (PFT) .................................................496

7.2 AFCS Controls ..................................................497

AFCS Controller ............................................................... 497

Additional AFCS Controls ................................................ 498

7.3 Flight Director Operation .................................499

Activating the Flight Director ..........................................499

AFCS Status Box..............................................................500

Flight Director Modes......................................................500

Flight Director Selection .................................................. 501

Command Bars ...............................................................501

LEVEL MODE ................................................................... 502

7.4 AFCS Modes .....................................................503

Vertical Modes ................................................................503

Lateral Modes ................................................................. 509

Combination Modes ........................................................ 514

7.5 Autopilot and Yaw Damper Operation .............525

Flight Control .................................................................. 525

Engaging the Autopilot and Yaw Damper .......................526

Control Wheel Steering (CWS) ........................................526

Disengaging the Autopilot and Yaw Damper ...................526

7.6 AFCS Annunciations and Alerts ........................ 528

AFCS Status Alerts...........................................................528

7.7 Abnormal Operation ........................................529

Suspected Autopilot Malfunction .................................... 529

Overpowering Autopilot Servos ......................................529

Overspeed Protection ...................................................... 529

Underspeed Protection .................................................... 530

Emergency Descent Mode ............................................... 532

SECTION 8 ADDITIONAL FEATURES

8.1 Overview .......................................................... 533

8.2 SafeTaxi (Optional) ...........................................534

8.3 SurfaceWatch (Optional) ..................................537

Information Display ......................................................... 538

Alerts ..............................................................................538

SurfaceWatch Setup ........................................................540

8.4 Electronic Charts ..............................................542

ChartView (Optional) ......................................................543

FliteCharts ....................................................................... 549

8.5 Satellite Telephone and Datalink Services (Optional) 556

Registering the System with Garmin Connext ................. 556

Contacts .......................................................................... 557

Telephone Communication (Optional) .............................560

Text Messaging (SMS) ..................................................... 567

8.6 Connext Setup (Optional) ................................577

8.7 SiriusXM Satellite Radio (Optional) .................581

Activating SiriusXM Satellite Services .............................581

Using SiriusXM Radio ...................................................... 582

8.8 Data Logging ...................................................586

Flight Data Logging.........................................................586

CMC Data Logging (Optional) ......................................... 587

8.9 Electronic Checklists (Optional) .......................588

Checklist features............................................................588

Operation ........................................................................ 589

8.10 Electronic Documents (Optional) ..................... 593

Installed Documents .......................................................593

User Documents .............................................................. 593

Viewing Electronic Documents ........................................593

190-02046-02 Rev. A iii

Garmin G3000 Pilot’s Guide for the Daher TBM 930

TABLE OF CONTENTS

8.11 Electronic Stability & Protection (ESP) (Optional) 601

Roll Engagement ............................................................. 601

Pitch Engagement ........................................................... 603

Angle of Attack Protection ..............................................604

High Airspeed Protection ................................................605

8.12 Database Cycle Number and Revisions ............606

Cycle Number and Revision ............................................606

8.13 Abnormal Operation ........................................609

Datalink Troubleshooting ................................................609

APPENDICES

Annunciations and Alerts .........................................611

CAS (Crew Alerting System) Messages............................611

VOICE Alerts ....................................................................613

System Message Annunciations ...................................... 614

System Messages ............................................................ 615

Database Management ............................................631

Loading Updated Databases ...........................................632

Database Updates Using a Supplemental Data Card ......633

Database Updates Using The Wireless Transceiver .......... 636

Database Synchronization Feature ................................641

Database Deletion Feature ............................................642

Magnetic Field Variation Database Update .....................643

Aviation Terms and Acronyms...................................647

Frequently Asked Questions ..................................... 659

INDEX

Index ......................................................................... I-1

Garmin G3000 Pilot’s Guide for the Daher TBM 930

190-02046-02 Rev. Aiv

SYSTEM OVERVIEW

SECTION 1 SYSTEM OVERVIEW

1.1 SYSTEM DESCRIPTION

This section provides an overview of the Garmin G3000 as installed in the Daher TBM 930 aircraft. It is integrated ﬂight control system that presents ﬂight instrumentation, position, navigation, communication, and identiﬁcation information to the ﬂight crew using ﬂat-panel color displays and Touchscreen Controllers. The system consists of the following Line Replaceable Units (LRUs):

• GDU 1200W (3) – Each GDU is conﬁgured as one of two Primary Flight Displays (PFDs) or one Multi-

function Display (MFD). The GDU 1200W features a 12-inch light emitting diode (LED) backlit widescreen

display with a 1280 x 800 resolution. The unit installed on the left/pilot side is designated as PFD1, and the

one installed on the right/copilot side is designated as PFD2. The unit installed in the center is designated as

the MFD. The displays communicate with each other and the Touchscreen Controllers through a High-Speed

Data Bus (HSDB) Ethernet connection

• GTC 580 (2)

to FMS functions, data entry capability, and communications control to the system. The unit installed on the

left/pilot side is designated as GTC1, and the one installed on the right/copilot side is designated as GTC2. Each

touchscreen controller communicates with the on-side PFD, the MFD. GTC1 communicates with the GMA 36

using an HDSB connection.

• GMA 36 (1)

intercom, and marker beacon audio. The GMA 36 is connected to GTC1 using an HSDB interface and to the

each IAU using an RS-232 and digital audio connections.

• GIA 63W

LRUs with each on-side GDU 1200W. Each IAU contains a GPS Satellite-Based Augmentation System (SBAS)

receiver, a very high frequency (VHF) communication/navigation/glideslope (COM/NAV/GS) receiver, a Flight

Director (FD) and system integration microprocessors. The IAUs communicate with each other through using

usign HSDB and additional backup paths.

• GDC 74B – Processes data from the pitot/static system as well as the OAT probe. This unit provides pressure

altitude, airspeed, vertical speed and OAT information to the G3000 system, and it communicates with the on-

side GIA 63W, on-side GDU 1200W and on-side GRS 77, using an ARINC 429 digital interface (it also interfaces

directly with the OAT). The GDC 74B is designed to operate in Reduced Vertical Separation Minimum (RVSM)

airspace.

• GEA 71 (2)

This unit communicate with both IAUs using an RS-485 digital interface.

• GTX 33 with ES

with ES

ﬁgure). These solid-state transponders provide Modes A/C/S and ADS-B Out capability. The GTX 345R also

provides ADS-B In capability. The GTX 33 with ES and GTX 33D with ES feature extended squitter capabilities.

The GTX 33D also features diversity. The transponder(s) communicate with the onside IAU(s).

• GRS 77

information via ARINC 429 protocol to the on-side and cross-side IAU, and to the on-side GDU 1200W. An

RS-232 backup path connects each AHRS to each 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 System Operation, later in this section.

– The Touchscreen Controller provides MFD control, Display Pane control on the PFD, in addition

– The Remote Audio Unit integrates navigation/communication radio (NAV/COM) digital audio,

(2) – The Integrated Avionics Units (IAU) function as the main communications hub, linking several

– The Engine Airframe Unit receives and processes signals from the engine and airframe sensors.

(1) (standard) GTX 345R (1) (standard)

(1) (optional) or GTX 345R (1) (optional) – One or two transponders are installed (see the following

(2) – The Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading

or GTX 33D with ES

(1) (standard) and

GTX 33

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Garmin G3000 Pilot’s Guide for the Daher TBM 930

SYSTEM OVERVIEW

• GMU 44 to determine aircraft magnetic heading. The magnetometer receives power directly from the AHRS and communicates with it via an RS-485 and RS-232 digital interface.

• GDL 69A SXM (1 optional) digital audio entertainment. The Data Link Receiver communicates with the MFD via a HSDB connection. A subscription to SiriusXM Weather and/or SiriusXM Satellite Radio service is required to enable the GDL 69A capability.

• GMC 710 to PFD1 and PFD2.

• GRA 55 (1 optional) of radar altitude information.

• GTA 82 – The GTA 82 Trim Adapter is a remote mounted device that is used to allow the AFCS to drive the yaw trim actuator.

• GTS 820 – The GTS 820 Trafﬁc Advisory System (TAS) uses active interrogations of Mode S and Mode C transponders to provide Trafﬁc Advisories to the pilot independent of the air trafﬁc control system.

• GSA 81 units interface with each GIA 63W.

• GWX 70 (1 optional) – The GWX 70 provides airborne real-time weather and ground mapped radar data to the displays. The unit is connected to the MFD with an HSDB connection.

• GSR 56 (1 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.

The Daher TBM 930 is also equipped with a Garmin Automated Flight Control System (AFCS), which includes

the Flight Director (FD), Autopilot (AP), manual electric trim, and control wheel steering (CWS) functions of the G3000 system.

(2) – The Magnetometer measures local magnetic ﬁeld and sends data to the AHRS for processing

– The Satellite Data Link Radio Receiver receives weather information, as well as

– The AFCS Controller provides AFCS control through an RS-232 digital interface. The unit connects

– The Radar Altimeter provides altitude above the ground information and rate of change

(4) – The GSA 81 servos are used for the automatic control of roll, yaw, pitch, and pitch trim. These

NOTE: Refer to the Automatic Flight Control System (AFCS) Section for details on the Garmin AFCS.

Figure 1-1 shows interconnection of the LRUs.

NOTE: For information on optional equipment not shown in Figure 1-1, consult the applicable optional

interface user’s guide. This document assumes the reader is already familiar with the operation of this additional equipment

Garmin G3000 Pilot’s Guide for the Daher TBM 930

190-02046-02 Rev. A2

SYSTEM OVERVIEW

BARO Set

GDU 1200W

(PFD1)

#1 GIA 63W

(Integrated

Avionics

Unit)

VHF COM

GPS/SBAS

VOR/LOC

G/S

AFCS Mode

Logic

Flight

Director

Servo

Management

#2 GIA 63W

(Integrated

Avionics

Unit)

VHF COM

GPS/SBAS

VOR/LOC

G/S

AFCS Mode

Logic

Flight

Director

Servo

Management

GDU 1200W

(PFD2)

Non-Garmin Equipment

RA-3502

(ADF)

ELT

FDR

WX-500 (Lightning Detection)

#1 GTX 33 w/ES

(Transponder)

GDU 1200W

(MFD)

#1 GDC 74B

(Air Data

Computer)

#2 GDC 74B

(Air Data

Computer)

#1 GRS 77

(Attitude &

Heading)

#2 GRS 77

(Attitude &

Heading)

Optional

Garmin Equipment

Optional

Non-Garmin Equipment

AOA Computer

KN-63 (DME)

#1 GMU 44

(Magnetometer)

#2 GMU 44

(Magnetometer)

Garmin Equipment

#1 GTC 580

(Touchscreen

Controller)

#2 GTC 580

(Touchscreen

Controller)

GMA 36

(Audio

Processor)

CVR

HF Radio

GDL 69A SXM

(XM Weather/

Audio Datalink)

GWX 70

(Weather

Radar)

GMC 710

(AFCS Mode

Controller)

GRA 55

(Radar

Altimeter)

GSA 81 (4)

Pitch/Roll/Yaw/Pitch

Trim Servos

#1 GEA 71

(Engine & Airframe I/F)

GTA 82

Yaw Trim

GTS 820

(TAS)

#2 GEA 71

(Engine & Airframe I/F)

BARO Set

#1 GTX 33D w/ES

(Transponder)

Flight Stream

510

(SD Card

Wireless

Transceiver)

#1 GTX 345R

(Transponder)

GSR 56

(Iridium)

#2 GTX 33 w/ES

(Transponder)

#2 GTX 345R

(Transponder)

GASC (Global

Air System Controller)

Figure 1-1 Basic System Block Diagram

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Garmin G3000 Pilot’s Guide for the Daher TBM 930

SYSTEM OVERVIEW

1.2 SYSTEM CONTROLS

The system controls simplify operation, minimize crew workload, and reduce the time required to access sophisticated functionality. Controls are located on the PFD bezels, Touchscreen Controllers and on the Automatic Flight Control System (AFCS) Controller. The PFD bezels and Touchscreen Controllers are discussed in this section. AFCS controls are described in the AFCS section. See the Audio and Communication/Navigation/ Surveillance (CNS) Section for detailed information about NAV/COM controls.

AFCS Controller

PFD1 MFD

PFD CONTROLS

GTC1

Figure 1-2 Garmin System Controls

GTC2

PFD2

PFD Softkeys

Figure 1-3 PFD Controls

Garmin G3000 Pilot’s Guide for the Daher TBM 930

190-02046-02 Rev. A4

SYSTEM OVERVIEW

Selection softkeys are located along the bottom of PFD1. The softkeys shown depend on the softkey level previously selected. The bezel keys below the softkey labels can be used to select the appropriate softkey. There are three types of softkeys. One selects a simple on/off state, indicated by an annunciator on the softkey label displayed as green (on) or gray (off). The next type of softkey selects among several options, indicated by the softkey label changing (with the exception of the Map Range keys) to reﬂect the name of the chosen option. The last type of softkey, when pressed displays another set of softkeys available for the selected function. Also, these softkeys revert to the previous level after 45 seconds of inactivity. When a softkey function is disabled, the softkey label is subdued. When the PFD is in split mode, an alternate softkey conﬁguration is shown with a reduced number of softkeys displayed on the left pane.

Selected Function

Softkey Names

(FMS selected for

the CDI)

Bezel-Mounted

Softkeys (Press)

Subdued Softkey

(function

unavailable)

Full Mode

Split or Reversionary Mode

Figure 1-4 Top Level PFD Softkeys

Each softkey sublevel has a BACK Softkey which can be selected to return to the previous level.

Level 1 Level 2 Level 3 Level 4

Map

Description

Decreases the PFD Map display range

Range -

Map

Increases the PFD Map display range

Range +

PFD Map

Displays the PFD Map display settings softkeys

Settings

Map

Displays softkeys used to select map layouts

Layout

Map Off

Inset Map

HSI Map

Removes the PFD Map from the display

• Displays the Inset Map

• Displays the HSI Map

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Garmin G3000 Pilot’s Guide for the Daher TBM 930

SYSTEM OVERVIEW

Level 1 Level 2 Level 3 Level 4

Inset Trafﬁc

HSI Trafﬁc

Detail

Weather

Legend

Trafﬁc

Storm-

scope

Terrain • Off: Removes terrain information from the PFD Map.

Data Link

Settings

Description

Overlays a dedicated trafﬁc display on the Inset Map. Overlays a dedicated trafﬁc display on the HSI.

Selects desired amount of map detail; cycles through declutter levels:

• All (No Declutter): All map features visible

• DCLTR 1: Declutters land data

• DCLTR 2: Declutters land and SUA data

• Least: Removes everything except for the active ﬂight plan Displays/removes the name of the selected data link weather

provider (SiriusXM, Connext, FIS-B) and the weather product icon and age box (for enabled weather products).

Adds or removes the display of trafﬁc on the PFD Map. The softkey annunciator is green when the trafﬁc function is on. When the trafﬁc function is off, the annunciator is gray.

Adds or removes the display of Stormscope information on the PFD Map. The softkey annunciator is green when the function is on. When the function is off, the annunciator is gray.

• Absolute: Displays Absolute terrain information on the PFD Map.

• Relative: Displays relative terrain information on the PFD Map.

• Displays Data Link settings softkeys.

Data Link Selects the data link source for the PFD Map:

• Connext: Selects Garmin Connext (optional) as the weather

source for the display of weather data on the PFD Map.

• SiriusXM: Selects SiriusXM (optional) as the weather source for the display of weather data on the PFD Map.

• FIS-B: Selects FIS-B (optional) as the weather source for the display of weather data on the PFD Map.

NEXRAD Selects type of NEXRAD coverage:

• CONUS: Selects NEXRAD coverage for continental U.S.

• Regional: Selects NEXRAD coverage for a region which

provides a higher resolution.

• Combined: Combines CONUS and Regional coverages.

Source Selects USA or Canada as the source when SiriusXM is enabled as

the datalink setting.

Storm Cell Movement

NEXRAD

Animation

Adds or removes the display of storm cell movement. Available when SiriusXM is selected as the weather source.

Animates NEXRAD Data. Available when SiriusXM is selected as the weather source.

Garmin G3000 Pilot’s Guide for the Daher TBM 930

190-02046-02 Rev. A6

SYSTEM OVERVIEW

Level 1 Level 2 Level 3 Level 4

Overlay

SiriusXM

Lightning

Description

Selects the display of weather information on the PFD Map:

• SiriusXM: Selects SiriusXM as the weather source for the display of weather data when SiriusXM is selected as the weather source using the Data Link softkey.

• Connext: Selects Connext as the weather source for the display of weather data when Connext is selected as the weather source using the Data Link softkey.

• WX Radar: Displays airborne weather radar map overlay on the Inset or HSI Map.

• FIS-B: Selects FIS-B as the weather source for the display of weather data when FIS-B is selected as the weather source using the Data Link softkey.

• Off: Removes weather data from HSI Map.

Softkey is available when SiriusXM is selected as the weather source under Data Link Settings. Adds/removes the display of SiriusXM information on the PFD Map. The softkey annunciator is green when the lightning function is on. When the lightning function is off, the annunciator is gray.

Trafﬁc

Map

PFD

Settings

Connext

Lightning

METAR

Attitude

Overlays

Pathways Synthetic

Terrain

Horizon

Heading

Airport

Signs

Softkey is available when Connext is selected as the weather source Data Link Settings. Adds/removes the display of Connext information on the PFD Map. The softkey annunciator is green when the lightning function is on. When the lightning function is off, the annunciator is gray.

Adds or removes the display of SiriusXM, Connext, or FIS-B sourced METAR data on the PFD Map. The softkey annunciator is green when the METAR data is enabled. When the METAR data is off, the annunciator is gray.

Replaces the PFD Map with a dedicated trafﬁc display. The softkey annunciator is green when the dedicated trafﬁc display on. When the PFD Map is on, the softkey annunciator is gray.

Displays the PFD settings softkeys.

Displays the softkeys for enabling or disabling Synthetic Vision features.

Displays Pathway Boxes on the Synthetic Vision Display. Enables synthetic terrain depiction.

Displays compass heading along the Zero-Pitch line.

Displays position markers for airports within approximately 15 nm of the current aircraft position. Airport identiﬁers are displayed when the airport is within approximately 9 nm.

190-02046-02 Rev. A

Garmin G3000 Pilot’s Guide for the Daher TBM 930

SYSTEM OVERVIEW

Level 1 Level 2 Level 3 Level 4

PFD Mode

Bearing 1

Bearing 2

Other PFD

Settings

Wind

Option 1

Option 2

Description

Enables or disables a multi-function Display Pane to the right or left (depending on pilot-side or copilot-side) on the PFD.

• FULL: Display Pane is disabled. The PFD display occupies the full screen.

• Split: Display Pane is enabled. The PFD screen is split between the PFD display and the Display Pane.

Cycles the Bearing 1 Information Window through NAV1, NAV2, FMS/waypoint identiﬁer and GPS-derived distance information, ADF1/frequency, and Off.

Cycles the Bearing 2 Information Window through NAV1, NAV2, FMS/ waypoint identiﬁer and GPS-derived distance information, ADF1/ frequency, and Off.

Displays additional PFD settings softkeys.

Displays the wind option softkeys

Headwind/tailwind and crosswind arrows with numeric speed components.

Total wind direction arrow with numeric speed.

OBS

Active

NAV

Sensors

ADC

Settings

AOA

Altitude

Units

COM1

121.5

ADC 1

Option 3

Off

Meters

HPA

Total wind direction arrow with digital numeric direction and speed.

Information not displayed.

Selects the display mode for the Angle of Attack (AOA) indicator on the PFD

• On: Displays AOA indicator on the PFD

• Off: Removes AOA indicator from the PFD

Displays softkeys to select altitude unit parameters.

When enabled, adds altimeter meters overlay.

Press to display the BARO setting as inches of mercury

Press to display the BARO setting as hectopascals.

Sets COM1 to 121.50 MHz.

Selects OBS mode on the CDI when navigating by FMS (only available with active leg). When OBS is on, the softkey annunciator is green.

Cycles through FMS, VOR1, and VOR2 navigation modes on the CDI.

Displays the sensor selection softkeys. Displays the ADC selection softkeys.

Selects the number 1 ADC. The softkey annunciator is green when selected.

Garmin G3000 Pilot’s Guide for the Daher TBM 930

190-02046-02 Rev. A8

SYSTEM OVERVIEW

Level 1 Level 2 Level 3 Level 4

ADC 2

AHRS

Settings

AHRS 1

AHRS 2

WX Radar

Controls

Mode

Display

Description

Selects the number 2 ADC. The softkey annunciator is green when selected.

Displays the AHRS selection softkeys.

Selects the number 1 AHRS. The softkey annunciator is green when selected.

Selects the number 2 AHRS. The softkey annunciator is green when selected.

Displays the WX Radar softkeys.

Selects the display mode for the display of weather radar on the HSI map:

• Standby: Sets the weather radar displayed on the HSI map to Standby when airborne.

• On: Enables display of weather radar on the HSI Map.

If enabled (Mode Softkey On), selects the mode of weather radar displayed. If not enabled, this softkey is subdued.

• Ground: Allows ground mapping returns to be displayed on the HSI map.

•

Weather:

map.

Allows weather returns to be displayed on the HSI

Tilt Down

Tilt Up

Gain -

Gain +

GND Clutter Suppression

Features

WX WATCH

Altitude

COMP Tilt

Turbulence

Detection

Pressing the softkey once adjusts the antenna tilt angle down in

0.25º increments. Pressing and holding the softkey continues

adjustment.

Pressing the softkey once adjusts the antenna tilt angle up in

0.25º increments. Pressing and holding the softkey continues

adjustment.

Pressing the softkey once decreases the gain in increments of 0.5. Pressing and holding the softkey continues adjustment. A manual setting of ‘0.0’ is equivalent to the calibrated gain setting.

Pressing the softkey once increases the gain in increments of 0.5. Pressing and holding the softkey continues adjustment. A manual setting of ‘0.0’ is equivalent to the calibrated gain setting. NEXRAD

(Optional) Toggles ground clutter suppression.

Displays softkeys for enabling/disabling Altitude Compensated Tilt and Antenna Stabilization.

Toggles the Weather Attenuated Color Highlight feature. Toggles the Altitude Compensated Tilt (ACT) feature. Used to

automatically adjust tilt as aircraft climbs or descends. (Optional) Toggles Turbulence Detection.

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Garmin G3000 Pilot’s Guide for the Daher TBM 930

SYSTEM OVERVIEW

TOUCHSCREEN CONTROLLER

The two Touchscreen Controllers, designated from left to right as GTC1 and GTC2 are a pedestal-mounted user interface allowing for ease of data entry, as well as operation of the PFD, Display Panes, and NAV/COM system. Many procedures in this Pilot’s Guide are performed using the Touchscreen Controllers.

3 4

Figure 1-5 GTC 580 Touchscreen Controller

Screen Title Displays the title of the current screen

Screen Displays set of context sensitive controls and data

Button Bar Displays System level buttons (e.g. MFD Home, MSG, Full/Half/Split, Scroll Up/Down,

Back, Enter, Cancel)

Label Bar Displays labels to show status and current functions of knobs and softkeys, when functions

are available.

Small Upper Knob Provides functions as labeled on the Label Bar (e.g. Display Pane selection, COM Freq/

switching/Hold, Data Entry/map panning)

Large Upper Knob Provides functions as labeled on the Label Bar (e.g. Display Pane selection, COM Freq/

switching, Data Entry/map panning)

Softkeys Provides functions as labeled on the Label Bar (e.g. PFD/MFD/NAV Com Control Mode

selection)

Lower Knob Provides functions as labeled on the screen (e.g. COM volume/squelch/map range

adjustment/checklist item control)

The Touchscreen Controller uses a grid of infrared beams and sensors to detect the location of touch input, even when the operator is wearing gloves. Objects or debris on the glass surface can interfere with these infrared beams and cause unintended activation of buttons. A screen cleaning procedure, described later in this section, is available to temporarily disable the touch recognition capability to facilitate screen cleaning.

In normal operations, both Touchscreen Controllers can control the PFD, MFD and NAV/COM system. The pilot selects a control mode for a given controller (i.e. PFD, MFD, NAV/COM) by pressing context-sensitive softkeys located on the right portion of each controller bezel. These softkeys are aligned with labels for each control mode currently available on a given controller. A box appears around the selected control mode, and a green arrow points to the currently selected softkey.

Garmin G3000 Pilot’s Guide for the Daher TBM 930

190-02046-02 Rev. A10

SYSTEM OVERVIEW

The Touchscreen Controller’s functions are arranged by screen. Each screen has a title which appears at the top of the screen area. The contents of each screen change dynamically in response to the selected control mode, and to pilot or system input. At the top level of each mode is a corresponding MFD Home containing mode-speciﬁc controls. PFD Home is MFD Home for PFD control mode. MFD Home is MFD Home for MFD (i.e. Display Pane) control mode. ‘NAV/COM’ Home is MFD Home for NAV/COM control mode.

The Touchscreen Controller’s available functions for the selected control mode are accessible from MFD Home. The MFD Home may be accessed any time it is not currently displayed by touching the Home Button in the Button Bar below the screen area. Procedures in this Pilot’s Guide generally begin from MFD Home as a reference point; however it is not necessary to return to MFD Home before performing each procedure if the appropriate screen is already displayed.

As the Touchscreen Controller is used, certain selections will cause another screen to be displayed. To return to the previous screen, touch the Back or Cancel Button (as applicable) in the Button Bar, or touch the Home Button to return to MFD Home. If MFD Home was the previous screen, pressing either the Back or Home Button will also return to MFD Home.

The Button Bar is also where the Home, Cancel, and Back buttons are displayed. If the system issues a message, the MSG Button is shown. Touching this button will display the ‘Messages’ Screen. The Button Bar also contains buttons for controlling the size of MFD Display Panes (Full or Half Mode), and PFD Display Panes (Full or Split Mode), discussed later in this section. The following buttons may be displayed on the Button Bar, depending on current availability and/or settings.

Returns to MFD Home Selects split display mode on the PFD.

Returns to the previous screen Selects half-display mode on the MFD.

Displays the System Messages Window on Touchscreen Controller. Flashes when a new system message is issued.

Displays the Telephone Window on Touchscreen Controller. Flashes when a new telephone call is received.

Displays the ‘Initialization’ Screen on Touchscreen Controller. Button appears on MFD Home if initialization tasks have not been completed.

Displays the SMS Text Inbox Window on Touchscreen Controller. Flashes when a new SMS message is received.

Scrolls up in a list

Scrolls down in a list

Cancels data entry and returns to the previous screen

Accepts entered data into the system.

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Garmin G3000 Pilot’s Guide for the Daher TBM 930

SYSTEM OVERVIEW

Selects full-display mode when controlling the MFD. Selects full display mode when controlling the PFD.

Table 1-1 Button Bar Buttons with Functions

Displays the Connext Notiﬁcations Window on the Touchscreen Controller. Flashes when a new Connext message is received.

The Label Bar, on the right side of the Touchscreen Controller, displays the current function of each control as a reference. These functions include Map Range adjustment, Display Pane selection, radio volume/squelch adjustment, COM radio tuning, and alphanumeric data entry, which are controlled using the Touchscreen Controller knob.

The labels change based on the context of the options being performed. If a Touchscreen Controller knob cannot be used because of a failure in a system component (COM, NAV, Audio, etc.), the Label Bar also indicates this status; refer to the Audio and CNS section for more information about radio failures.

The Touchscreen Controller recognizes input based on a touch, a gesture (such as sliding a ﬁnger), or by pressing or turning the knobs or softkeys.

On-screen buttons are selected by momentarily touching them with a ﬁnger and then releasing. It is not necessary to apply pressure, as the infrared touchscreen surface detects only the presence and movement of the ﬁnger, not pressure. When touched, the button background is highlighted in blue until the ﬁnger is released. If enabled, an aural ‘click’ sound is also issued to conﬁrm the button has been touched. When releasing the ﬁnger, make sure it released within the boundary of the button, otherwise the input is considered invalid. If enabled, an aural ‘doink’ is heard to indicate the touch input was not accepted.

Some adjustments are made using horizontal or vertical sliders. To use, simply touch within the slider box and slide the ﬁnger in the desired slider bar direction, then release the ﬁnger. The ﬁnger may move outside of the slider box during adjustment; slider movement stops when either the ﬁnger is released or the slider has reached its maximum travel. In some cases, the slider can also be adjusted by touching a + or - Button if it accompanies the slider, such as in the Map Detail Adjustment Slider. In addition, a slider adjustment may also be accomplished using knobs on the Touchscreen Controller if the Label Bar indicates the selected slider supports this additional control.

Volume Adjustment Slider

Figure 1-6 Sliders on the Touchscreen Controller

Map Detail Adjustment Slider

Garmin G3000 Pilot’s Guide for the Daher TBM 930

190-02046-02 Rev. A12

SYSTEM OVERVIEW

When a Touchscreen Controller screen window contains more information than the window can currently show, a scroll bar and scroll buttons appear. To scroll inside of a window, touch the controller while moving the ﬁnger up or down accordingly or touch and drag the ﬁnger up or down. To scroll more quickly, move the ﬁnger up or down rapidly in a ﬂicking motion. Scrolling can also be performed by pressing the Up or Down scroll buttons, each touch of the scroll button will display one ‘page’ of information. Press and hold the Up or

Down scroll buttons for a continuous scroll.

Some screens provide tabs as a means to group multiple categories of information or buttons. Touch the desired tab to display its contents and manage settings or information. The selected tab is highlighted.

Selected Tab Highlighted

Scroll Bar

Other Available Tabs

Scroll Arrows

Figure 1-7 Touchscreen Controller with Tabs and Scroll Arrows

Elements on the Touchscreen Controller screens (such as buttons and sliders) may appear subdued to indicate their functions are currently not available. Generally, pilot-selectable ﬁelds appear in cyan. In some cases, the system may highlight the expected button in cyan which completes a data entry process or function.

Touch the highlighted button to activate the Direct-To function

Buttons subdued until Direct-To is activated

Figure 1-8 Subdued Buttons on Touchscreen Controller

BUTTON TYPES

Annunciator Buttons operate in an on/off state. An ‘on’ or enabled button displays a green annunciator; an

‘off’ or disabled button displays a gray annunciator. Touch the annunciator button to change its state.

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On or Enabled Off or Disabled

Figure 1-9 Touchscreen Controller Annunciator Buttons

Garmin G3000 Pilot’s Guide for the Daher TBM 930

SYSTEM OVERVIEW

Dataﬁeld Buttons can be modiﬁed based on information the pilot can enter or change, and often contain

cyan alphanumeric text. Touching dataﬁeld buttons will either display a pop-up window from which a selection can be made, or display a keypad to supply the data. See the Data Entry discussion in this section for more information.

Selected Dataﬁeld Button

Dataﬁeld Buttons

Figure 1-10 Touchscreen Controller Dataﬁeld Buttons

Options for Selected Dataﬁeld Button

If a system failure causes a button’s function to be inaccessible, an amber ‘X’ appears over the button. These

buttons will not respond if touched.

SCREEN OVERVIEW

The following is a brief overview of the major screens used to access Touchscreen Controller functions.

Additional speciﬁc screens used to perform functions are shown and discussed in detail throughout this Pilot’s Guide.

NOTE: Screen appearance varies based on the installed options.

MFD HoMe

Shows ‘Navigation Map’ Pane in the selected display Pane. Touch the button again to access the ‘Map Settings’ Screen on the Touchscreen Controller.

Garmin G3000 Pilot’s Guide for the Daher TBM 930

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