Garmin G1000: Socata TBM 850 Reference guide

G1000

®

Integrated Flight Deck

Pilot’s Guide

TBM 850 & TBM 900

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

This manual reﬂects the operation of System Software version 0719.16 or later for the Socata TBM 850/900. Some differences in operation may

be observed when comparing the information in this manual to earlier or later software versions.

Garmin International, Inc.

1200 East 151st Street

Olathe, Kansas 66062, U.S.A.

Tel: 913.397.8200

Fax: 913.397.8282

Aircraft On Ground (AOG) Hotline: 913.397.0836

Aviation Dealer Technical Support: 888.606.5482

Garmin (Europe) Ltd.

Liberty House, Hounsdown Business Park

Southampton, Hampshire SO40 9LR U.K.

Tel: 44.(0).23.8052.4000

Fax: 44.(0).23.8052.4004

Aviation Support: 44.(0).37.0850.1243

Garmin AT, Inc.

2345 Turner Road SE

Salem, OR 97302, U.S.A.

Tel: 503.581.8101

Fax 503.364.2138

Garmin Corporation

No. 68, Zhangshu 2nd Road

Xizhi District, New Taipei City, Taiwan

Tel: 34.93.357.2608

Fax: 34.93.429.4484

Web Site Address: www.garmin.com

Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any

storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download a single copy

of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use, provided

that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that

any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.

Garmin

®

and G1000

®

, WATCH

®

, FliteCharts

®

, and SafeTaxi

®

are registered trademarks of Garmin Ltd. or its subsidiaries. Connext

™

and Garmin

ESP

™

is a trademark 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.

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.

April, 2016 190-00709-07 Rev. B Printed in the U.S.A

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

Blank Page

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

i

WARNINGS, CAUTIONS, AND NOTES

WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance

feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance

and does not relieve the pilot from the responsibility of being aware of surroundings during ﬂight. The

terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from

third party sources. Garmin is not able to independently verify the accuracy of the terrain data.

WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be

relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current

aeronautical charts for appropriate minimum clearance altitudes.

WARNING: Do not use outdated database information. Databases used in the system must be updated

regularly in order to ensure that the information remains current. Pilots using any outdated database do so

entirely at their own risk.

WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data

is intended only to supplement other approved navigation data sources and should be considered as an aid

to enhance situational awareness.

WARNING: 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 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 signiﬁcantly older than the indicated weather product age.

WARNING: Do not rely on information from the lightning detection system display as the sole basis for

hazard weather avoidance. Range limitations and interference may cause the system to display inaccurate

or incomplete information. Refer to the documentation from the lightning detection system manufacturer

for detailed information about the system.

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

ii

WARNINGS, CAUTIONS, AND NOTES

WARNING:

The system, as installed in the Socata TBM 850/900 aircraft, has a very high degree of functional

integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all

conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation

to occur without a fault indication shown by the system. It is thus the responsibility of the pilot to detect

such an occurrence by means of cross-checking with all redundant or correlated information available in the

cockpit.

WARNING:

For safety reasons, system operational procedures must be learned on the ground.

WARNING:

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

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

performance of all GPS equipment. Portions of the 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.

WARNING

:

Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of

according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/

aboutGarmin/environment/disposal.jsp.

WARNING:

To reduce the risk of unsafe operation, carefully review and understand all aspects of the Pilot’s

Guide documentation and the Socata TBM 850/900 Airplane Flight Manual. Thoroughly practice basic

operation prior to actual use. During ﬂight operations, carefully compare indications from the system to all

available navigation sources, including the information from other NAVAIDs, visual sightings, charts, etc. For

safety purposes, always resolve any discrepancies before continuing navigation.

WARNING

: The illustrations in this guide are only examples. Never use the system to attempt to penetrate

a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information

Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identiﬁed as severe or giving an

intense radar echo.”

WARNING

:

Because of variation in the earth’s magnetic ﬁeld, operating the system within the following

areas could result in loss of reliable attitude and heading indications. North of 72° North latitude at all

longitudes. South of 70° South latitude at all longitudes. North of 65° North latitude between longitude

75° W and 120° W. (Northern Canada). North of 70° North latitude between longitude 70° W and 128° W.

(Northern Canada). North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia).

South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New

Zealand).

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.

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

iii

WARNINGS, CAUTIONS, AND NOTES

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

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

standard pressure setting, as applicable.

CAUTION: The PFD and MFD displays use a lens coated with a special anti-reﬂective coating that is very

sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE

ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an

eyeglass lens cleaner that is speciﬁed as safe for anti-reﬂective coatings.

CAUTION:

The system does not contain any user-serviceable parts. Repairs should only be made by an

authorized Garmin service center. Unauthorized repairs or modiﬁcations could void both the warranty and

the pilot’s authority to operate this device under FAA/FCC regulations.

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

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

equipment may differ slightly from the actual equipment.

NOTE

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

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

interference received, including interference that may cause undesired operation.

NOTE: The data contained in the terrain and obstacle databases comes from government agencies. Garmin

accurately processes and cross-validates the data, but cannot guarantee the accuracy and completeness of

the data.

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

: 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.

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

iv

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 both of the sensed values are unavailable, it will be annunciated as a ‘NO COMP’

(no compare).

NOTE

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

NOTE

: The FAA has asked Garmin to remind pilots who ﬂy with Garmin database-dependent avionics of the

following:

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

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

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

obtained from Garmin or Jeppesen are assured compliance with all data quality requirements (DQRs) by virtue of a

Type 2 Letter of Authorization (LOA) from the FAA. A copy of the Type 2 LOA is available for each database and can

be viewed at http://ﬂy.garmin.com by selecting ‘Type 2 LOA Status.’

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

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

be presented by the system. It is the pilot’s responsibility to operate in accordance with established AFM(S) and

regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment.

NOTE

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

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

ﬂygarmin.com by selecting ‘Database Exclusions List.’

NOTE

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

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

‘Aviation Database Alerts.’

NOTE

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

the revised DQRs.

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

discrepancies could come in the form of an incorrect procedure; incorrectly identiﬁed terrain, obstacles and ﬁxes;

or any other displayed item used for navigation or communication in the air or on the ground. Go to FlyGarmin.

com and select ‘Report An Aviation Data Error Report.’

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

v

REVISION INFORMATION

Record of Revisions

Part Number Revision Date Page Range Description

190-00709-01 A 7/7/08 All Added Synthetic Vision System and other GDU 9.02 parameters

190-00709-02 A

B

5/5/09

7/30/09

All

53

Added new page selection presentation

Added import/export ﬂight plans

Added ﬂight data logging

Added other GDU 9.14 parameters.

Corrected discussion of setting Selected Altitude

190-00709-03 A

B

4/10

6/10

All

Page 7

Pages 411-413

Pages 106, 558

Page 579

Added GDU 11.01 parameters.

Added GTS 820

Added AOPA Airport Directory

Added dual navigation database capability

Added database synchronization

Updated System Conﬁguration Diagram

Added Flight ID discussion for GTS 820 Trafﬁc Page

Added NG HI CAS message

Added “Airspeed, Airspeed” and GTS 820 aural alerts

190-00709-04 A 10/11 All Added Proﬁle View

Added Standby Navigation Database

Added new database update procedures

Added Iridium Satellite Telephone & SMS messaging

Added GFDS Worldwide Weather

Added WX LGND, LEGEND, and METAR softkeys

Updated system messages

Added other GDU 12.01 parameters

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

vi

REVISION INFORMATION

Record of Revisions

Part Number Revision Date Page Range Description

190-00709-05 A

B

C

D

1/14

2/14

1/15

All

Added Maintenance Log feature

Added Auxiliary Video

Added CPDLC

Added AC-U-KWIK Airport Directory

Added User Deﬁned Holding Patterns

Added temperature compensated altitude

Changed GFDS Weather to Connext

™

Weather

Changed XM to SiriusXM

Changed Synthetic Vision System (SVS) to Synthetic Vision

Technology (SVT)

Added other GDU 14.01 parameters

Clerical

Added database use notes

Changed vacuum low pressure CAS message description

Changed oil pressure CAS message description

Added import/export of Pilot Proﬁles

Added discussion regarding system behavior when

automatically switching from GPS to LOC

Updated weather radar precipitation intensity table

Added QFE altimeter setting warning

Clerical

190-00709-06 A 11/15 All Updated Warnings, Cautions, and Notes

Added Flight Stream 210

Added Radar Altimeter

Added Nexrad C/Nexrad B

Added ADS-B Out

Added Smart Airspace

Added GDU 15.00 parameters

Updated CAS Messages

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

vii

REVISION INFORMATION

Record of Revisions

Part Number Revision Date Page Range Description

190-00709-07 A

B

4/16

All

Added GDU 15.11 parameters

Added support for AOA indicator

Updated AFCS information

Added Electronic Stability and Protection (ESP

™

)

Added Emergency Descent Mode (EDM)

Added Underspeed Protection (USP)

Updated Nexrad information

Updated CAS Messages

Updated Softkey Maps

Added Altitude Compensated Tilt information

Updated Database Procedures

Added Datalink Receiver Messages

Clerical

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

viii

REVISION INFORMATION

Blank Page

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

ix

TABLE OF CONTENTS

SECTION 1 SYSTEM OVERVIEW

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

1.2 Line Replaceable Units (LRU) ................................. 2

1.3 G1000 Controls ........................................................ 8

PFD Controls ................................................................ 8

Controls Associated With the MFD ............................... 10

AFCS Controls ............................................................ 11

Audio Panel Controls .................................................. 13

1.4 Secure Digital Cards.............................................. 15

1.5 System Power-up ................................................... 16

1.6 System Operation .................................................. 17

Normal Operation ....................................................... 17

Reversionary Mode ..................................................... 18

G1000 System Annunciations ...................................... 21

Softkey Function ......................................................... 22

GPS Receiver Operation .............................................. 30

1.7 Accessing G1000 Functionality............................ 35

Menus ....................................................................... 35

MFD Page Groups ....................................................... 35

MFD System Pages...................................................... 41

1.8 Display Backlighting ............................................. 53

Automatic Adjustment ................................................ 53

Manual Adjustment .................................................... 53

SECTION 2 FLIGHT INSTRUMENTS

2.1 Flight Instruments ................................................. 58

Airspeed Indicator ...................................................... 58

Attitude Indicator ....................................................... 60

Altimeter ................................................................... 61

Vertical Speed Indicator (VSI) ....................................... 65

Vertical Deviation ....................................................... 65

Horizontal Situation Indicator (HSI) .............................. 66

Course Deviation Indicator (CDI) .................................. 71

Angle of Attack (AOA) Indicator ................................... 79

2.2 Supplemental Flight Data .................................... 80

Temperature Displays .................................................. 80

Wind Data ................................................................. 82

Vertical Navigation (VNV) Indications ........................... 83

2.3 PFD Annunciations and Alerting Functions ........ 84

System Alerting .......................................................... 84

Marker Beacon Annunciations...................................... 85

Trafﬁc Annunciation .................................................... 85

Terrain Annunciations ................................................. 86

Altitude Alerting ......................................................... 87

Low Altitude Annunciation .......................................... 87

Minimum Descent Altitude/Decision Height Alerting ...... 88

Radar Altimeter .......................................................... 89

2.4 Abnormal Operations ........................................... 91

Abnormal GPS Conditions ........................................... 91

Heading Failure Modes................................................ 92

Unusual Attitudes ....................................................... 92

SECTION 3 ENGINE AND AIRFRAME SYSTEMS

3.1 Engine Indication System (EIS) ............................ 97

Engine Parameters ...................................................... 98

Cabin Pressurization ................................................. 100

Fuel Information ....................................................... 102

Electrical Information ................................................ 102

Trim and Flap Indicators ............................................ 103

3.2 Synoptics .............................................................. 104

Electrical System ....................................................... 106

Fuel System .............................................................. 109

General Systems ....................................................... 111

3.3 Crew Alerting System (CAS) ............................... 112

CAS Messages and Prioritization ................................ 113

SECTION 4 AUDIO PANEL AND CNS

4.1 Overview .............................................................. 115

Audio Panel Volume Control ...................................... 115

PFD Controls and Frequency Display ........................... 116

Audio Panel Controls ................................................ 118

4.2 COM Operation .................................................... 120

COM Transceiver Selection and Activation ................... 120

COM Transceiver Manual Tuning ................................ 121

Quick-Tuning and Activating 121.500 MHz .................. 122

Auto-Tuning the COM Frequency ................................ 123

Frequency Spacing .................................................... 128

Automatic Squelch .................................................... 129

Volume .................................................................... 129

4.3 Controller Pilot Data Link Communications

(CPDLC) ................................................................. 130

CPDLC Session Overview ........................................... 130

CPDLC System Status ................................................ 130

CPDLC Message Status Icons ..................................... 131

Connecting to the CPDLC System ............................... 132

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

x

TABLE OF CONTENTS

Creating a Message .................................................. 135

Responding to an ATC Message ................................. 137

Viewing an ATC Message .......................................... 138

Viewing CPDLC Message Dialogs ............................... 138

Deleting Message Dialogs ......................................... 139

Disconnecting from the CPDLC System ....................... 140

Enabling/Disabling Data Mode ................................... 140

CPDLC System Failure ............................................... 140

4.4 NAV Operation ..................................................... 141

NAV Radio Selection and Activation ........................... 141

NAV Receiver Manual Tuning ..................................... 142

Auto-Tuning a NAV Frequency from the MFD............... 144

Marker Beacon Receiver ............................................ 149

ADF/DME Tuning ...................................................... 150

4.5 Mode S Transponders .......................................... 154

Transponder Controls ................................................ 155

Transponder Mode Selection ...................................... 156

Entering a Transponder Code ..................................... 158

IDENT Function ........................................................ 159

Flight ID Reporting.................................................... 160

4.6 Additional Audio Panel Functions ..................... 161

Power-Up ................................................................. 161

Mono/Stereo Headsets .............................................. 161

Speaker ................................................................... 161

Intercom .................................................................. 162

Passenger Address (PA) System .................................. 163

Simultaneous COM Operation .................................... 163

Clearance Recorder and Player ................................... 164

Entertainment Inputs ................................................ 165

4.7 Audio Panels Preﬂight Procedure ...................... 166

4.8 Abnormal Operation ........................................... 168

Stuck Microphone ..................................................... 168

COM Tuning Failure ................................................... 168

PFD Failure ............................................................... 169

Audio Panel Fail-Safe Operation ................................. 170

Reversionary Mode ................................................... 170

SECTION 5 FLIGHT MANAGEMENT

5.1 Introduction ......................................................... 171

Navigation Status Box ............................................... 172

5.2 Using Map Displays ............................................. 174

Map Orientation ....................................................... 174

Map Range .............................................................. 176

Map Panning ............................................................ 178

Measuring Bearing and Distance ................................ 184

Topography .............................................................. 185

Map Symbols ........................................................... 188

Airways ................................................................... 194

Track Vector ............................................................. 196

Wind Vector ............................................................. 197

Nav Range Ring........................................................ 198

Fuel Range Ring ....................................................... 199

Field of View (SVT) .................................................... 200

Selected Altitude Intercept Arc ................................... 201

5.3 Waypoints ............................................................. 202

Airports ................................................................... 203

Intersections ............................................................ 210

NDBs ....................................................................... 212

VORs ....................................................................... 214

VRPs ....................................................................... 216

User Waypoints ........................................................ 218

5.4 Airspaces .............................................................. 224

5.5 Direct-to-Navigation .......................................... 229

5.6 Flight Planning ..................................................... 235

Flight Plan Creation .................................................. 236

Adding Waypoints to an Existing Flight Plan ................ 244

Adding Airways to a Flight Plan ................................. 246

Adding Procedures to a Stored Flight Plan .................. 249

Flight Plan Storage ................................................... 256

Flight Plan Editing .................................................... 258

Along Track Offsets ................................................... 262

Parallel Track ............................................................ 263

Activating a Flight Plan Leg ....................................... 266

Inverting a Flight Plan ............................................... 267

Flight Plan Views ...................................................... 268

Closest Point of FPL .................................................. 270

User-Deﬁned Holding Patterns ................................... 271

5.7 Vertical Navigation ............................................. 276

Altitude Constraints .................................................. 278

5.8 Procedures ...........................................................282

Departures ............................................................... 283

Arrivals ................................................................... 286

Approaches ............................................................. 289

5.9 Trip Planning ........................................................ 297

Trip Planning ............................................................ 297

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

xi

TABLE OF CONTENTS

Weight Planning ....................................................... 301

Weight Caution And Warning Conditions .................... 303

5.10 RAIM Prediction................................................... 304

5.11 Navigating a Flight Plan ..................................... 308

5.12 Abnormal Operation ........................................... 337

SECTION 6 HAZARD AVOIDANCE

6.1 SiriusXM Weather ................................................ 340

Activating Services .................................................... 340

Using SiriusXM Weather Products .............................. 342

Weather Softkeys on the Weather Data Link (XM) Page 346

SiriusXM Weather Abnormal Operations ..................... 376

6.2 Garmin Connext Weather ................................... 378

Registering the Iridium Satellite System ...................... 378

Registering Garmin Connext Weather ......................... 379

Accessing Garmin Connext Weather Products .............. 380

Connext Data Requests ............................................. 388

Garmin Connext Weather Products ............................. 392

Abnormal Operations ................................................ 408

6.3 Airborne Color Weather Radar .......................... 410

System Description ................................................... 410

Principles of Pulsed Airborne Weather Radar ............... 410

Safe Operating Distance ............................................ 414

Basic Antenna Tilt Setup ............................................ 415

Weather Mapping and Interpretation ......................... 417

Weather Radar Overlay on the Navigation Map Page ... 429

System Status ........................................................... 430

6.4 Stormscope .......................................................... 432

Setting Up Stormscope on the Navigation Map ........... 432

Selecting the Stormscope Page .................................. 436

6.5 Terrain Proximity ................................................. 438

Displaying Terrain Proximity Data ............................... 438

Terrain Proximity Page ............................................... 441

6.6 Terrain-SVS ........................................................... 443

Displaying Terrain-SVS Data ....................................... 444

Terrain-SVS Page ...................................................... 446

Terrain-SVS Alerts ..................................................... 448

System Status ........................................................... 451

6.7 TAWS-B ................................................................. 453

Displaying TAWS-B Data ............................................ 454

TAWS-B Alerts .......................................................... 458

System Status ........................................................... 465

6.8 Proﬁle View Terrain ............................................. 467

Proﬁle View Display .................................................. 468

6.9 Trafﬁc Information Service (TIS) ........................ 471

Displaying TRAFFIC Data ........................................... 472

Trafﬁc Map Page ....................................................... 474

TIS Alerts ................................................................. 475

System Status ........................................................... 477

6.10 GTS 820 Trafﬁc ..................................................... 479

Theory of operation .................................................. 479

TAS Alerts ................................................................ 482

System Test .............................................................. 483

Operation ................................................................ 484

6.11 KTA 870 Trafﬁc ..................................................... 492

TAS Symbology ......................................................... 492

Operation ................................................................ 493

Altitude Display ........................................................ 496

Trafﬁc Map Page Display Range ................................. 496

TAS Alerts ................................................................ 498

System Status ........................................................... 498

SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM

Basic Autopilot Operation .......................................... 502

7.1 AFCS Controls ...................................................... 503

7.2 Flight Director Operation ................................... 505

Activating the Flight Director ..................................... 505

AFCS Status Box ....................................................... 506

Flight Director Modes ................................................ 507

Switching Flight Directors .......................................... 507

Command Bars ......................................................... 508

Level Mode .............................................................. 508

7.3 Vertical Modes ..................................................... 509

Pitch Hold Mode (PIT) ............................................... 510

Selected Altitude Capture Mode (ALTS) ....................... 511

Altitude Hold Mode (ALT) .......................................... 512

Vertical Speed Mode (VS) .......................................... 513

Flight Level Change Mode (FLC) ................................. 514

Vertical Navigation Modes (VPTH, ALTV) ..................... 516

Glidepath Mode (GP) ................................................ 520

Glideslope Mode (GS) ............................................... 522

Takeoff (TO) and Go Around (GA) Modes .................... 523

7.4 Lateral Modes ...................................................... 524

Roll Hold Mode (ROL) ............................................... 525

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

xii

TABLE OF CONTENTS

Low Bank Mode ....................................................... 525

Heading Select Mode (HDG) ...................................... 526

Navigation Modes (GPS, VOR, LOC) ............................ 526

Approach Modes (GPS, VAPP, LOC) ............................. 528

Backcourse Mode (BC) .............................................. 530

Intercepting and Flying a DME Arc ............................. 530

7.5 Autopilot and Yaw Damper Operation ............. 531

Flight Control ........................................................... 531

Engagement ............................................................. 532

Control Wheel Steering ............................................. 532

Disengagement ........................................................ 533

7.6 Example Flight Plan ............................................ 534

Departure ................................................................ 534

Intercepting a VOR Radial .......................................... 536

Flying a Flight Plan/GPS Course ................................. 537

Descent ................................................................... 538

Approach ................................................................. 541

Go Around/Missed Approach ..................................... 544

7.7 AFCS Annunciations and Alerts ......................... 546

AFCS Status Alerts .................................................... 546

7.8 Abnormal Operation ........................................... 547

Suspected Autopilot malfunction ................................ 547

Overpowering Autopilot Servos .................................. 547

Overspeed Protection ................................................ 548

Underspeed Protection .............................................. 548

Emergency Descent Mode ......................................... 550

SECTION 8 ADDITIONAL FEATURES

8.1 Synthetic Vision Technology (SVT) ..................... 554

SVT Operation .......................................................... 555

SVT Features ............................................................ 557

Field of View ............................................................ 566

8.2 SafeTaxi

®

............................................................. 568

SafeTaxi Cycle Number and Revision .......................... 571

8.3 ChartView ............................................................. 574

ChartView Softkeys ................................................... 575

Terminal Procedures Charts ....................................... 576

Chart Options ........................................................... 584

Day/Night View ........................................................ 590

ChartView Cycle Number and Expiration Date ............. 592

8.4 FliteCharts

®

......................................................... 594

FliteCharts Softkeys .................................................. 596

Terminal Procedures Charts ....................................... 597

Chart Options ........................................................... 604

Day/Night View ........................................................ 607

FliteCharts Cycle Number and Expiration Date ............. 609

8.5 Airport Directory ................................................. 612

Airport Directory Database Cycle Number and Revision 613

8.6 SiriusXM Radio Entertainment .......................... 614

Activating SiriusXM Satellite Radio Services ................ 615

Using SiriusXM Radio ................................................ 616

8.7 Scheduler .............................................................. 620

8.8 Electronic Checklists ........................................... 622

8.9 Flight Data Logging ............................................ 626

8.10 Satellite Telephone and SMS Messaging .......... 628

Registering the Iridium Satellite System ...................... 628

Disable/Enable Iridium Transceiver.............................. 629

Telephone Communication ........................................ 630

Text Messaging (SMS) ............................................... 643

8.11 Maintenance Logs ............................................... 655

8.12 Auxiliary Video (Optional) .................................. 656

Video Setup .............................................................657

Display Selection ...................................................... 657

Input Selection ......................................................... 658

Zoom/Range ............................................................ 659

8.13 Electronic Stability & Protection (ESP

™

) ........... 660

Roll Engagement ...................................................... 661

Pitch Engagement..................................................... 662

Angle of Attack Protection ......................................... 664

High Airspeed Protection ........................................... 664

8.14 Bluetooth

®

Management ................................... 665

8.15 Abnormal Operation ........................................... 667

SVT Troubleshooting ................................................. 667

Reversionary Mode ................................................... 667

Unusual Attitudes ..................................................... 668

APPENDICES

Annunciations and Alerts ............................................. 671

CAS Messages .......................................................... 671

Comparator Annunciations ........................................ 674

Reversionary Sensor Annunciations ............................ 675

System Annunciations ............................................... 676

Message Advisories .................................................. 679

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

xiii

TABLE OF CONTENTS

AFCS Alerts .............................................................. 693

Terrain-SVT Alerts ..................................................... 694

TAWS-B ALERTS ........................................................695

Other G1000 Aural Alerts .......................................... 696

Flight Plan Import/Export Messages ........................... 697

GDL 69/GDL 69A/GDL 69A SXM Data Link

Receiver Messages ................................................... 698

Database Management ................................................ 699

Navigation Databases ............................................... 699

Jeppesen Chartview Database Update ........................ 703

Garmin Databases .................................................... 704

Garmin Aviation Glossary ............................................ 711

Frequently Asked Questions ........................................ 721

Map Symbols ................................................................. 725

INDEX

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

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

xiv

TABLE OF CONTENTS

Blank Page

190-00709-07 Rev. B

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

1

SYSTEM OVERVIEW

SECTION 1 SYSTEM OVERVIEW

1.1 SYSTEM DESCRIPTION

This section is designed to provide an overview of the G1000 Integrated Flight Deck. The G1000 system is an

integrated ﬂight control system that presents ﬂight instrumentation, position, navigation, communication, and

identiﬁcation information to the pilot through large-format displays. The system consists of the following Line

Replaceable Units (LRUs):

•

GDU 1040A

Primary Flight Display (PFD)

•

GDU 1500

Multi Function Display (MFD)

•

GIA 63W

Integrated Avionics Unit

•

GDC 74B

Air Data Computer (ADC)

•

GEA 71

Engine/Airframe Unit

•

GRS 77

Attitude and Heading Reference System

(AHRS)

•

GMU 44

Magnetometer

•

GMA 1347D Cabin

Dual Audio System with

Integrated Marker Beacon Receiver

•

GTX 33/33D w/ES

Mode S Transponder

•

GDL 69A

or

GDL 69SXM

Data Link (optional)

•

GWX 68

or

GWX 70

Weather Radar (optional)

• GDR 66 VHF Data Link Transceiver (optional)

•

GSR 56

Iridium Transceiver (optional)

•

GCU 475

MFD Control Unit

•

GMC 710

AFCS Control Unit

•

GTS 820

Trafﬁc Avoidance System (optional)

•

GA 58

Directional Antenna

•

GA 36

and

GA 37

GPS/SBAS Antennas

•

GSA 81

AFCS Servos

•

GSM 85/86

Servo Gearboxes

•

GTA 82

Trim Adapter

•

GRA 55

– Provides altitude above the ground to the

PFD, through the GIA 63W, via HSDB connection.

•

Flight Stream 210

Wireless Bluetooth

®

Gateway

A top-level G1000 system block diagram is shown in Figure 1-1 (it does not include the GA 36, GA 37, GA 58,

or GSM 85/86).

NOTE: Refer to the AFCS section for details on the Garmin AFCS.

In the aircraft, the Garmin Automated Flight Control System (AFCS) provides the Flight Director (FD), Autopilot

(AP), and Yaw Damper (YD) functions of the G1000 system.

Garmin G1000 Pilot’s Guide for the Socata TBM 850/900

190-00709-07 Rev. B2

SYSTEM OVERVIEW

1.2 LINE REPLACEABLE UNITS (LRU)

•

GDU 1040A

– Each unit is conﬁgured as a PFD that features a 10.4-inch LCD with 1024 x 768 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. 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 1500

– Features a 15-inch LCD with 1024 x 768 resolution and is conﬁgured as an MFD. This unit is

linked to both PFDs via HSDB connection.

•

GIA 63W

– Functions as the main communication hub, linking all LRUs with the on-side PFD. 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 on-side PFD via HSDB connection. The GIA 63Ws are not

paired together and do not communicate with each other directly.

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