Garmin G1000 NXi - Socata TBM 910 Reference guide

®

Pilot’s Guide

Daher TBM 910

System software Version 2883.00 or later

190-02218-00 Rev. C

Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910

This manual reﬂects the operation of System Software version 2883.00 or later for the G1000 NXi Daher TBM 910. 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 (Europe) Ltd.

Liberty House, Hounsdown Business Park

Southampton, Hampshire SO40 9LR U.K.

Garmin AT, Inc.

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Salem, OR 97302, U.S.A.

Garmin Corporation

No. 68, Zhangshu 2nd Road

Xizhi District, New Taipei City, Taiwan

Contact Garmin Product Support or view warranty information at www.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

®

, G1000

®

NXi,

WATCH

®

, FliteCharts

®

, and SafeTaxi

®

are registered trademarks of Garmin International, Inc. or its subsidiaries.

Garmin ESP

™

, Garmin SVT

™

, SurfaceWatch

™

, and Connext

™

are trademarks of Garmin International, Inc. or its subsidiaries. These

trademarks may not be used without the express permission of Garmin.

Skywatch

®

and Stormscope

®

are registered trademarks of L-3 Communications. Ryan

®

, TCAD

®

and Avidyne

®

are registered trademarks of

Avidyne Corporation. AC-U-KWIK

®

is a registered trademark of Penton Business Media Inc. Bendix/King

®

and Honeywell

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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. 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.

190-02218-00 Rev. C

Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910

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.

190-02218-00 Rev. C

Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910

iii

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

WARNING

:

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

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

standard pressure setting, as applicable.

WARNING

:

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

system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that

may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned

in error as displayed.

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Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910

iv

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 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 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: 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:

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:

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 operate the weather radar in a transmitting mode when personnel or objects are within

the MPEL boundary.

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

precipitation. Changing the gain in weather mode causes precipitation intensity to be displayed as a color

not representative of the true intensity.

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

to enhance situational awareness.

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Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910

v

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:

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.

NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information.

Always conﬁrm TFR information through ofﬁcial sources such as Flight Service Stations or Air Trafﬁc Control.

NOTE: All visual depictions contained within this document, including screen images of the system panel

and displays, are subject to change and may not reﬂect the most current system and aviation databases.

Depictions of equipment may differ slightly from the actual equipment.

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

its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and

performance of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation

AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or

misinterpreted and, therefore, become unsafe.

NOTE

: This device complies with part 15 of the FCC Rules. Operation is subject to the following two

conditions: (1) this device may not cause harmful interference, and (2) this device must accept any

interference received, including interference that may cause undesired operation.

NOTE

: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of

attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards

away from the source of the interference should alleviate the condition.

NOTE

: Use of polarized eyewear may cause the ﬂight displays to appear dim or blank.

NOTE

: This product, its packaging, and its components contain chemicals known to the State of California

to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with

California’s Proposition 65. If you have any questions or would like additional information, please refer to

our web site at www.garmin.com/prop65.

190-02218-00 Rev. C

Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910

vi

WARNINGS, CAUTIONS, AND NOTES

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.’

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’.

190-02218-00 Rev. C

Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910

vii

WARNINGS, CAUTIONS, AND NOTES

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

a partial symbol.

NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms

that can cause isolated discharge points in the strike display mode. However, clusters of two or more

discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after

the screen has been cleared.

NOTE: Operate G1000 NXi system power through at least one cycle in a period of four days of continuous

operation to avoid an autonomous system reboot.

190-02218-00 Rev. C

Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910

viii

WARNINGS, CAUTIONS, AND NOTES

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190-02218-00 Rev. C

Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910

SOFTWARE LICENSE AGREEMENT

ix

SOFTWARE LICENSE AGREEMENT

BY USING THE DEVICE, COMPONENT OR SYSTEM MANUFACTURED OR SOLD BY GARMIN (“THE GARMIN PRODUCT”), YOU AGREE TO

BE BOUND BY THE TERMS AND CONDITIONS OF THE FOLLOWING SOFTWARE LICENSE AGREEMENT. PLEASE READ THIS AGREEMENT

CAREFULLY. Garmin Ltd. and its subsidiaries (“Garmin”) grants you a limited license to use the software embedded in the Garmin Product

(the “Software”) in binary executable form in the normal operation of the Garmin Product. Title, ownership rights, and intellectual property

rights in and to the Software remain with Garmin and/or its third-party providers. You acknowledge that the Software is the property of

Garmin and/or its third-party providers and is protected under the United States of America copyright laws and international copyright

treaties. You further acknowledge that the structure, organization, and code of the Software are valuable trade secrets of Garmin and/or its

third-party providers and that the Software in source code form remains a valuable trade secret of Garmin and/or its third-party providers.

You agree not to reproduce, decompile, disassemble, modify, reverse assemble, reverse engineer, or reduce to human readable form the

Software or any part thereof or create any derivative works based on the Software. You agree not to export or re-export the Software to

any country in violation of the export control laws of the United States of America.

190-02218-00 Rev. C

Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910

SOFTWARE LICENSE AGREEMENT

x

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190-02218-00 Rev. C

Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910

xi

REVISION INFORMATION

Record of Revisions

Part Number Revision Date Page Range Description

190-02218-00 A 3/27/17 i – I-6 Initial Release for GDU 20.51

B 4/10/17 i – I-6 Revision

Added support for Split Screen Mode

Updated CAS Messages

Added Voice Message Alerts

Updated ESP Information

Added support for Electronic Checklists

C 9/5/19 All Revision

Added support for Baro-VNAV

Clerical changes

190-02218-00 Rev. C

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xii

REVISION INFORMATION

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Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910

xiii

TABLE OF CONTENTS

SECTION 1 SYSTEM OVERVIEW

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

Line Replaceable Units (LRU)..............................................1

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

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

Controls Associated With the MFD .....................................6

Secure Digital Cards ...........................................................8

1.3 System Operation ................................................ 9

System Power-up ................................................................ 9

Normal Operation ............................................................10

Reversionary Mode...........................................................11

System Annunciations ......................................................12

System Status ................................................................... 14

AHRS Operation ...............................................................15

GPS Receiver Operation ...................................................16

1.4 Accessing System Functionality ........................21

Softkey Function ...............................................................21

Menus ..............................................................................27

MFD Page Groups.............................................................28

Split Screen Functionality .................................................31

System Settings ................................................................32

System Utilities .................................................................41

1.5 Display Backlighting ..........................................46

SECTION 2 FLIGHT INSTRUMENTS

2.1 Flight Instruments .............................................50

Airspeed Indicator ............................................................50

Attitude Indicator .............................................................53

Altimeter ..........................................................................54

Vertical Speed Indicator (VSI) ...........................................57

Vertical Deviation .............................................................57

Horizontal Situation Indicator (HSI) .................................. 60

Course Deviation Indicator (CDI) ......................................64

Angle of Attack (AOA) Indicator .......................................72

Radar Altimeter ................................................................73

2.2 Supplemental Flight Data..................................75

Temperature Displays .......................................................75

Wind Data ........................................................................76

Vertical Navigation (VNV) Indications ..............................77

2.3 PFD Annunciations and Alerting Functions .......78

Marker Beacon Annunciations ..........................................78

Altitude Alerting ...............................................................78

Low Altitude Annunciation ...............................................79

Minimum Descent Altitude/Decision Height Alerting ........ 79

2.4 Garmin SVT (Synthetic Vision Technology) ........81

SVT Operation ..................................................................82

SVT Features .....................................................................84

Field of View ..................................................................... 92

2.5 Abnormal Operations ........................................93

Abnormal GPS Conditions ................................................93

Comparator Annunciations ...............................................94

Reversionary Sensor Annunciations ..................................95

Unusual Attitudes ............................................................. 96

SECTION 3 ENGINE INDICATION SYSTEM

3.1 Engine Display ................................................... 98

3.2 Landing Field Elevation ...................................101

3.3 Synoptics ........................................................102

Electrical (ELEC) ..............................................................102

Fuel (FUEL) .....................................................................105

General System (GEN) ....................................................106

3.4 EIS Display (Reversionary Mode).....................108

SECTION 4 AUDIO PANEL AND CNS

4.1 Overview .........................................................109

Audio Panel Volume Control ........................................... 109

PFD Controls and Frequency Display ..............................110

Audio Panel Controls ...................................................... 112

4.2 COM Operation ................................................114

COM Transceiver Manual Tuning ....................................115

Auto-Tuning the COM Frequency ...................................115

Frequency Spacing .........................................................118

4.3 NAV Operation ................................................119

NAV Tuning Boxes ..........................................................119

NAV Radio Selection and Activation ...............................120

NAV Receiver Manual Tuning .........................................120

Auto-Tuning a NAV Frequency from the MFD ................. 121

Marker Beacon Receiver ................................................. 123

ADF/DME Tuning ............................................................124

4.4 Mode S Transponders ......................................127

Transponder Controls .....................................................127

Transponder Mode Selection ..........................................128

Entering a Transponder Code .........................................130

IDENT Function...............................................................131

4.5 Additional Audio Panel Functions ...................132

Power-Up........................................................................132

Mono/Stereo Headsets ...................................................132

Speaker ..........................................................................132

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TABLE OF CONTENTS

Intercom ......................................................................... 132

Passenger Address (PA) System ......................................133

Simultaneous COM Operation ........................................ 133

Clearance Recorder and Player .......................................133

Entertainment Inputs ......................................................134

4.6 Audio Panels Preﬂight Procedure .................... 135

4.7 Abnormal Operation ........................................137

Stuck Microphone ..........................................................137

COM Tuning Failure ........................................................137

PFD Failure, Dual System ................................................137

Audio Panel Fail-Safe Operation ..................................... 138

Reversionary Mode.........................................................138

SECTION 5 FLIGHT MANAGEMENT

5.1 Introduction .....................................................139

Navigation Status Box and Data Bar ..............................141

5.2 Using Map Displays .........................................143

Map Orientation ............................................................. 143

Map Range .....................................................................145

Map Panning ..................................................................147

Measuring Bearing and Distance ....................................149

Topography ....................................................................150

Map Symbols ..................................................................153

Airways ..........................................................................158

Additional Navigation Map Items ..................................160

IFR/VFR Charts ...............................................................163

5.3 Waypoints ........................................................ 166

Airports ..........................................................................167

Intersections ................................................................... 174

NDBs ..............................................................................176

VORs ..............................................................................178

VRPs ............................................................................... 180

User Waypoints ..............................................................182

5.4 Airspaces .........................................................188

5.5 Direct-to-Navigation ......................................192

5.6 Flight Planning ................................................197

Flight Plan Creation ........................................................198

Flight Plan Import/Export ...............................................201

Adding Waypoints to an Existing Flight Plan ..................206

Adding Airways to a Flight Plan .....................................210

Adding Procedures to a Stored Flight Plan .....................212

Flight Plan Storage .........................................................217

Flight Plan Editing ..........................................................219

Along Track Offsets.........................................................222

Parallel Track ..................................................................223

Activating a Flight Plan Leg ............................................ 226

Inverting a Flight Plan ....................................................226

Flight Plan Views ............................................................226

Closest Point of FPL ........................................................ 229

Collapsing Airways .........................................................230

User-Deﬁned Holding Patterns .......................................231

5.7 Vertical Navigation ..........................................235

Altitude Constraints .......................................................236

5.8 Procedures ....................................................... 243

Departures ......................................................................245

Arrivals ..........................................................................247

Approaches ...................................................................249

5.9 Weight Planning ..............................................256

Weight Caution And Warning Conditions .......................258

5.10 Trip Planning ....................................................259

Trip Planning ..................................................................259

5.11 Abnormal Operation ........................................263

SECTION 6 HAZARD AVOIDANCE

6.1 Data Link Weather ...........................................266

Activating Data Link Weather Services ...........................267

Weather Product Age .....................................................270

Displaying Data Link Weather Products .......................... 275

Connext Data Requests ..................................................284

Weather Product Overview .............................................288

FIS-B Weather Status ...................................................... 323

Abnormal Operations for Garmin Connext Weather ....... 325

6.2 Stormscope Lightning Detection System ........327

Using the Stormscope Page ............................................327

Setting Up Stormscope on the Navigation Map .............329

6.3 Airborne Color Weather Radar ........................333

System Description .........................................................333

Principles of Pulsed Airborne Weather Radar..................333

Safe Operating Distance ................................................. 337

Basic Antenna Tilt Setup .................................................338

Practical Application Using the Basic Tilt Setup ..............338

Weather Mapping and Interpretation ............................. 340

Ground Mapping and Interpretation ..............................351

Additional Weather Radar Displays ................................351

System Status ................................................................. 354

6.4 Terrain Displays ...............................................355

Relative Terrain Symbology.............................................356

Terrain Page ....................................................................359

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TABLE OF CONTENTS

Vertical Situation Display (VSD) Terrain ..........................360

Terrain-SVT and TAWS-B Alerting Displays .....................363

Forward Looking Terrain Avoidance ................................367

Additional TAWS-B Alerting ............................................ 369

System Status ................................................................. 371

6.5 Trafﬁc Information Service (TIS) ...................... 373

Displaying Trafﬁc Data ....................................................374

Trafﬁc Map Page .............................................................375

TIS Alerts ........................................................................376

System Status ................................................................. 378

6.6 TAS Trafﬁc ........................................................380

TAS Theory of Operation ................................................. 380

TAS Alerts .......................................................................384

System Test .....................................................................385

Operation .......................................................................386

6.7 ADS-B Trafﬁc .................................................... 393

ADS-B System Overview ................................................. 393

Conﬂict Situational Awareness & Alerting (CSA) ............395

Airborne and Surface Applications .................................396

Trafﬁc Description...........................................................397

Operation .......................................................................398

ADS-B System Status ...................................................... 404

SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM

7.1 AFCS Overview ................................................407

Additional AFCS Controls ...............................................409

Basic Autopilot Operation ..............................................410

7.2 Flight Director Operation ................................411

Activating the Flight Director .........................................411

AFCS Status Box ............................................................. 412

Flight Director Modes ..................................................... 413

Switching Flight Directors...............................................413

Command Bars ............................................................... 414

7.3 AFCS Modes .....................................................415

Vertical Modes ...............................................................415

Lateral Modes ................................................................422

Combination modes (VNV, APR, NAV, BC, GA) ................427

7.4 Autopilot and Yaw Damper Operation ............438

Flight Control .................................................................438

Engagement ...................................................................439

Control Wheel Steering...................................................439

Disengagement ..............................................................440

7.5 AFCS Annunciations and Alerts .......................441

Overspeed Protection .....................................................442

Underspeed Protection ................................................... 442

Level Mode .....................................................................444

Emergency Descent Mode ..............................................445

7.6 Abnormal Operation ........................................446

Suspected Autopilot malfunction....................................446

Overpowering Autopilot Servos ......................................446

SECTION 8 ADDITIONAL FEATURES

8.1 SafeTaxi ...........................................................448

8.2 Charts ..............................................................451

Split view........................................................................452

ChartView ......................................................................453

FliteCharts ......................................................................462

IFR/VFR Charts ...............................................................467

Airport Directory .............................................................468

8.3 Database Cycle number and revisions ............469

Cycle Number and Revision ............................................469

8.4 SiriusXM Radio Entertainment ........................471

Activating SiriusXM Satellite Radio Services...................471

Using SiriusXM Radio ..................................................... 472

8.5 Flight Data Logging ......................................... 475

8.6 Satellite Telephone and sms messaging ..........477

Registering with Garmin Connext

®

...............................477

Disable/Enable Iridium Transceiver .................................477

Telephone Communication ............................................. 478

Text Messaging (SMS) ....................................................485

8.7 Connext Setup .................................................497

8.8 Maintenance Logs ...........................................499

8.9 Electronic Stability and Protection (ESP

™

) ......500

Roll Engagement ............................................................501

Pitch Engagement ..........................................................502

Angle of Attack Protection .............................................504

High Airspeed Protection ................................................ 504

8.10 Electronic Checklists........................................505

8.11 Abnormal Operation ........................................507

SiriusXM Data Link Receiver Troubleshooting .................507

APPENDICES

Annunciations and Alerts .........................................509

CAS Message Prioritization ............................................510

CAS Messages ................................................................ 512

Audio Alerts ....................................................................514

System Message Advisories ............................................515

190-02218-00 Rev. C

Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910

xvi

TABLE OF CONTENTS

Database Management ............................................529

Loading Updated Databases ..........................................529

Magnetic Field Variation Database Update ....................536

Garmin Aviation Glossary ......................................... 539

Frequently Asked Questions .....................................549

Map Symbols ............................................................553

INDEX

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

190-02218-00 Rev. C

Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910

1

SYSTEM OVERVIEW

SECTION 1 SYSTEM OVERVIEW

1.1 SYSTEM DESCRIPTION

This section provides an overview of the G1000 NXi Integrated Avionics System as installed in the Daher TBM

910. The system is an integrated avionics system that presents ﬂight instrumentation, position, navigation,

communication, and identiﬁcation information to the pilot through large-format displays.

The system is comprised of several Line Replaceable Units along with an optional Flight Stream 510 device.

The Flight Stream 510 provides a Bluetooth

®

connection between the system and a mobile device. GPS, AHRS,

ADS-B, trafﬁc, SiriusXM audio, and weather data can then be shared with the mobile device, and ﬂight plans can

be transferred to or from the mobile device. Also, database updates may be performed using the Flight Stream

510 WiFi link.

LINE REPLACEABLE UNITS (LRU)

•

GDU 1050A

(2) – Each unit is conﬁgured as a PFD that features a 10.5-inch LCD display. 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. These units communicate with each other, the MFD, and with the on-side GIA 63W Integrated

Avionics Unit through a High-Speed Data Bus (HSDB) connection.

•

GDU 1550

(1) – This unit features a 15-inch LCD display and is conﬁgured as an MFD. This unit is linked

to both PFDs via HSDB connection.

•

GIA 63W

(2) – Functions as the main communication hub, linking all LRUs with the PFD and MFD. Each

GIA 63W contains a GPS SBAS receiver, VHF COM/NAV/GS receivers, a ﬂight director (FD) and system

integration microprocessors. Each GIA 63W is paired with the PFD and MFD via High Speed Database

connection. The GIA 63Ws are not paired together and do not communicate with each other directly.

•

GDC 72B

(2) – Processes data from the pitot/static system as well as the OAT probe. This unit provides

pressure altitude, airspeed, vertical speed and OAT information to the system, and it communicates with the

GIA 63Ws, the displays, and the GRS 79, using an ARINC 429 digital interface. The GDC 72B is designed to

operate in Reduced Vertical Separation Minimum (RVSM) airspace.

•

GRS 79

(2) – Provides aircraft attitude and heading information via ARINC 429 to both displays and both

GIA 63Ws. The GRS 79 contains advanced sensors (including accelerometers and rate sensors) and interfaces

with the GMU 44 to obtain magnetic ﬁeld information, with the GDC 72B to obtain air data, and with both

GIA 63Ws to obtain GPS information. AHRS modes of operation are discussed later in this document.

•

GMU 44

(2) – Measures local magnetic ﬁeld. Data is sent to the GRS 79 unit for processing to determine

aircraft magnetic heading. The GMU 44 receives power directly from the GRS unit, and communicates with

the GRS 79 unit using an RS-485 digital interface.

•

GMA 1347D

(2) – Integrates NAV/COM digital audio, intercom system and marker beacon controls, and is

installed in dual conﬁguration on the outboard side of PFD1 and PFD2. This unit also enables the manual

control of the display reversionary mode (red

DISPLAY BACKUP

button) and communicates with the on-side

GIA 63W, using an RS-232 digital interface.

•

GMC 710

(1) – Provides the controls for the Garmin AFCS through an RS-232 digital interface allowing

communication with both PFDs.

190-02218-00 Rev. C

Garmin G1000 NXi Pilot’s Guide for the Daher TBM 910

2

SYSTEM OVERVIEW

•

GCU 475

– Provides the Flight Management System (FMS) controls for the MFD through an RS-232 digital

interface.

• GTX 33D ES (1), or the GTX 345R (optional) (1 or 2) – Solid state transponders that provide Mode A,

C, S capability. The standard GTX 33D includes Mode S with diversity and Extended Squitter Automatic

Dependent Surveillance (ADS-B out) transmission, and is indicated as ‘XPDR1’. The optional GTX 345R

provides ADS-B In/Out. The optional GTX 345R may be installed in addition to the GTX 33D, in which

case, it is indicated as ‘XPDR2’. The system may instead accommodate an optional dual set of GTX 345R

transponders as well, occupying ‘XPDR1’ and ‘XPDR2’. Only one transponder can be active at a time. Each

transponder communicates with the on-side GIA 63W through an RS-232 digital interface. If installed, the

(#1) GTX 345R communicates with the PFD via High Speed Database connection.

•

GEA 71

(2) – Receives and processes signals from the engine and airframe sensors. This unit communicates

with both GIA 63Ws using an RS-485 digital interface.

•

GSA 81 (4)

, and

GSM 86

(1) – The GSA 81 servos are used for the automatic control of roll, yaw, pitch, and

pitch trim. These units interface with each GIA 63W.

The GSM 86 servo gearbox is responsible for transferring the output torque of the GSA 81 servo actuator to

the mechanical ﬂight-control surface linkage.

•

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.

•

GDL 69A SXM

(1) (Optional) – A satellite radio receiver that provides data link weather information to the

MFD (and, indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL 69A

SXM communicates with the MFD via HSDB connection. Subscriptions to the SiriusXM Weather or SiriusXM

Satellite Radio services are required to enable the GDL 69A SXM capability.

•

GTS 820

(Optional) – The GTS 820 Trafﬁc Advisory System (TAS) uses active interrogations of Mode S and

Mode C transponders to provide trafﬁc information to the pilot independent of the air trafﬁc control system.

•

GWX 70

(1) (Optional) – Provides airborne weather and ground mapped radar data to the MFD via HSDB

connection.

•

GRA 55

(1) (Optional) – The optional Radar Altimeter provides altitude above the ground information and

rate of change of radar altitude information.

•

GSR 56

(1) (Optional) - The Iridium Transceiver provides voice communications by means of a telephone

handset in the cabin and pilot and copilot headsets in the cockpit. The transceiver can also send and receive

short message service (SMS) text messages. The GSR 56 also receives data link weather products from the

Garmin Connext weather service through the Iridium satellite network.

Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are also shown in Figure

1-1. The system is capable of interfacing with the following optional equipment:

•

GDL 69A SXM

Data Link Receiver

•

GTS 820

Trafﬁc Advisory System

•

FS 510

Flight Stream (SD Card)

•

GRA 55

Radio Altimeter

•

GSR 56

Iridium Transceiver

•

WX 500

Stormscope Lightning Sensor

• KN 63 DME

• Becker ADF 3502

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