Garmin G1000 NXi - Cessna 182T/T182T/J182T Nav III Reference guide

Pilot’s Guide

190-02177-01

Revision A

Garmin International, Inc.

1200 East 151st Street

Olathe, Kansas 66062, U.S.A.

www.ﬂygarmin.com

Garmin AT, Inc.

2345 Turner Road SE

Salem, OR 97302, U.S.A.

Garmin (Europe) Ltd.

Liberty House, Hounsdown Business Park

Southampton, Hampshire SO40 9LR U.K.

Garmin Corporation

No. 68, Zhangshu 2nd Road

Xizhi District,

New Taipei City, Taiwan

Cirrus SR2x

G1000

®

NXi Pilot’s Guide Cessna Nav III

Cessna Nav III

®

SYSTEM OVERVIEW

FLIGHT INSTRUMENTS

EIS

AUDIO PANEL & CNS

FLIGHT MANAGEMENT

HAZARD AVOIDANCE

AFCS

ADDITIONAL FEATURES

APPENDICES

INDEX

190-02177-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III

This manual reﬂects the operation of System Software version 2501.03 or later for Cessna 172R, 172S, 182T, T182T, 206H, and T206H

aircraft. Some differences in operation may be observed when comparing the information in this manual to earlier or later software

versions.

NOTE: Cessna Nav III aircraft include the Cessna 172R, the Cessna 172S, the normally aspirated Cessna 182 (182),

the turbocharged Cessna 182 (T182), the normally aspirated Cessna 206 (206), and the turbocharged Cessna 206

(T206). Unless otherwise indicated, information in the G1000 Cockpit Reference Guide pertains to all Cessna Nav

III aircraft.

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.

2345 Turner Road SE

Salem, OR 97302, U.S.A.

Garmin Corporation

No. 68, Zhangshu 2nd Road

Xizhi District, New Taipei City, Taiwan

Contact Garmin Product Support at www.ﬂygarmin.com.

For warranty information refer to 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, FliteCharts

®

, and SafeTaxi

®

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

ESP

™

, Garmin SVT

™

, SurfaceWatch

™

, Connext

™

, and WireAware

™

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

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

Stormscope

®

is registered trademarks of L-3 Communications. CO Guardian is a trademark of CO Guardian, Inc. AC-U-KWIK

®

is a

registered trademark of Penton Business Media Inc. Bendix/King

®

and Honeywell

®

are registered trademarks of Honeywell International,

Inc. 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.

Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III

190-02177-01 Rev. A

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.

190-02177-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III

i

WARNINGS, CAUTIONS, AND NOTES

WARNING: Do not use terrain avoidance displays as the sole source of information for maintaining separation

from terrain and obstacles. Garmin obtains terrain and obstacle data from third party sources and cannot

independently verify the accuracy of the information.

WARNING: Always refer to current aeronautical charts and NOTAMs for veriﬁcation of displayed aeronautical

information. Displayed aeronautical data may not incorporate the latest NOTAM information.

WARNING: Do not use geometric altitude for compliance with air trafﬁc control altitude requirements. The

primary barometric altimeter must be used for compliance with all air trafﬁc control altitude regulations,

requirements, instructions, and clearances.

WARNING: Do not use basemap information (land and water data) as the sole means of navigation. Basemap

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

an aid to enhance situational awareness.

WARNING: Do not rely solely upon the display of trafﬁc information to accurately depict all of the trafﬁc

within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information

from aircraft or ground stations, trafﬁc may be present that is not represented on the display.

WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous

weather. Information contained within data link weather products may not accurately depict current

weather conditions.

WARNING: Do not use the indicated data link weather product age to determine the age of the weather

information shown by the data link weather product. Due to time delays inherent in gathering and processing

weather data for data link transmission, the weather information shown by the data link weather product

may be older than the indicated weather product age.

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

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

clearance altitudes.

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

WARNING

:

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

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

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

in error as displayed.

WARNING: 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.

Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III

190-02177-01 Rev. Aii

WARNINGS, CAUTIONS, AND NOTES

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 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.

WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and trafﬁc avoidance.

Garmin SVT is intended as an aid to situational awareness only and may not provide either the accuracy or

reliability upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or trafﬁc.

WARNING: Do not use the Garmin SVT runway depiction as the sole means for determining the proximity of

the aircraft to the runway or for maintaining the proper approach path angle during landing.

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

to enhance situational awareness.

CAUTION: Do not clean display surfaces with abrasive cloths or cleaners containing ammonia. They will

harm the anti-reﬂective coating.

C

AUTION: 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.

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 use 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.

190-02177-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III

iii

WARNINGS, CAUTIONS, AND NOTES

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.

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

POHs 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.’

Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III

190-02177-01 Rev. Aiv

WARNINGS, CAUTIONS, AND NOTES

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’.

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: 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.

190-02177-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III

SOFTWARE LICENSE AGREEMENT

v

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.

Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III

190-02177-01 Rev. Avi

REVISION INFORMATION

Record of Revisions

Part Number Revision Date Page Range Description

190-02177-00 A January 2017 All Production release with GDU software version 20.05.

190-02177-00 B May 2017 All HSI Map information added

SurfaceWatch information added

VSD information added

Updated to ﬁx clerical errors

190-02177-01 A May 2018 All Production release at GDU 20.83

Updated EIS information

Added charts split screen description

Added WireAware

Added visual approaches

Added Baro QFE Altimeter settings

Added Connext Weather

Updated Audio Panel Information

Added Underspeed Protection

Added Electronic Stability and Protection

190-02177-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III

vii

TABLE OF CONTENTS

SECTION 1 SYSTEM OVERVIEW

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

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

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

PFD/MFD Controls ........................................................ 4

Secure Digital Cards ...................................................... 7

1.3 System Operation .................................................... 8

System Power-up .......................................................... 8

Normal Operation ......................................................... 9

Reversionary Mode ..................................................... 10

System Annunciations ................................................. 11

System Status ............................................................. 12

ADAHRS Operation ..................................................... 13

AHRS Operation ......................................................... 14

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

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

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

Menus ....................................................................... 26

MFD Page Groups ....................................................... 27

Split Screen Functionality ............................................ 30

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

System Utilities ........................................................... 38

1.5 Display Backlighting ............................................. 42

SECTION 2 FLIGHT INSTRUMENTS

2.1 Flight Instruments ................................................. 46

Attitude Indicator ....................................................... 46

Airspeed Indicator ...................................................... 47

Altimeter ................................................................... 49

Vertical Speed Indicator (VSI) ....................................... 52

Vertical Deviation ....................................................... 53

Horizontal Situation Indicator (HSI) .............................. 54

Course Deviation Indicator (CDI) .................................. 59

2.2 Supplemental Flight Data .................................... 66

Generic Timer ............................................................. 66

Temperature Display ................................................... 66

Wind Data ................................................................. 67

2.3 PFD Annunciations and Alerting Functions ........ 68

Altitude Alerting ......................................................... 68

Low Altitude Annunciation .......................................... 68

Marker Beacon Annunciations...................................... 68

Minimum Descent Altitude/Decision Height Alerting ...... 69

2.4 Synthetic Vision Technology (SVT) ....................... 71

SVT Operation ............................................................ 72

SVT Features .............................................................. 74

Field of View .............................................................. 83

2.5 Abnormal Operations ........................................... 85

Abnormal GPS Conditions ........................................... 85

SVT Troubleshooting ................................................... 86

SVT in Reversionary Mode ........................................... 86

Unusual Attitudes ....................................................... 86

SVT Unusual Attitudes ................................................. 88

SECTION 3 ENGINE INDICATION SYSTEM

3.1 Engine Display ....................................................... 90

Engine Display.......................................................... 102

3.2 EIS Display (Reversionary Mode) ...................... 107

SECTION 4 AUDIO PANEL AND CNS

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

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

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

4.2 COM Operation .................................................... 115

COM Tuning Boxes .................................................... 115

COM Transceiver Manual Tuning ................................ 116

Auto-Tuning the COM Frequency ................................ 116

Frequency Spacing .................................................... 119

4.3 NAV Operation ..................................................... 120

NAV Tuning Boxes..................................................... 120

NAV Radio Selection and Activation ........................... 121

NAV Receiver Manual Tuning ..................................... 121

Auto-Tuning a NAV Frequency from the MFD............... 122

Marker Beacon Receiver ............................................ 124

DME Tuning ............................................................. 125

4.4 Mode S Transponder ........................................... 126

Transponder Controls ................................................ 126

Transponder Mode Selection ...................................... 127

Entering a Transponder Code ..................................... 129

IDENT Function ........................................................ 130

Flight ID Reporting.................................................... 130

4.5 Additional Audio Panel Functions ..................... 131

Power-Up ................................................................. 131

Mono/Stereo Headsets .............................................. 131

Speaker (GMA 1347) ................................................. 131

Speaker (GMA 1360) ................................................. 131

Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III

190-02177-01 Rev. Aviii

TABLE OF CONTENTS

Intercom (GMA 1347) ............................................... 132

Intercom (GMA 1360) ............................................... 133

Blue-Select Mode (Telephone/Entertainment Distribution)

(GMA 1360) ............................................................. 135

3D Audio (GMA 1360) ............................................... 136

Bluetooth

®

(GMA 1360 Only)..................................... 137

Clearance Recorder and Player ................................... 138

Entertainment Inputs ................................................ 139

4.6 Audio Panels Preﬂight Procedure ...................... 140

4.7 Abnormal Operation ........................................... 141

Stuck Microphone ..................................................... 141

COM Tuning Failure ................................................... 141

Audio Panel Fail-Safe Operation ................................. 141

Reversionary Mode ................................................... 141

SECTION 5 FLIGHT MANAGEMENT

5.1 Introduction ......................................................... 143

Navigation Status Box and Data Bar ........................... 145

5.2 Using Map Displays ............................................. 147

Map Orientation ....................................................... 147

Map Range .............................................................. 149

Map Panning ............................................................ 151

Measuring Bearing and Distance ................................ 153

Topography .............................................................. 154

Map Symbols ........................................................... 156

Airways ................................................................... 160

Additional Navigation Map Items ............................... 163

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

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

Non-Airport Waypoints .............................................. 172

5.4 Airspaces .............................................................. 181

Nearest Airspace ...................................................... 182

Smart Airspace ......................................................... 184

5.5 Direct-to-Navigation .......................................... 185

5.6 Flight Planning ..................................................... 190

Flight Plan Views ...................................................... 193

Creating a Flight Plan ............................................... 196

Flight Plan Waypoint and Airway Modiﬁcations ........... 197

Flight Plan Operations ............................................... 205

Closest Point of FPL .................................................. 208

User-Deﬁned Holding Patterns ................................... 209

Managing Flight Plans .............................................. 212

5.7 Vertical Navigation ............................................. 221

Altitude Constraints .................................................. 223

Vertical Situation Display (VSD) .................................. 226

5.8 Procedures ...........................................................229

Departures ............................................................... 231

Arrivals ................................................................... 234

Approaches ............................................................. 237

5.9 Trip Planning ........................................................ 247

Trip Planning ............................................................ 247

5.10 Abnormal Operation ........................................... 251

SECTION 6 HAZARD AVOIDANCE

6.1 Data Link Weather ............................................... 254

Activating Data Link Weather Services ........................ 255

Weather Product Age ................................................ 258

Displaying Data Link Weather Products ....................... 262

Connext Data Requests ............................................. 271

Weather Product Overview ........................................ 274

FIS-B Weather Status................................................. 307

Abnormal Operations for Garmin Connext Weather ..... 308

6.2 Stormscope Lightning Detection System ......... 310

Using the Stormscope Page ....................................... 310

Setting Up Stormscope on the Navigation Map ........... 312

6.3 Terrain Displays ................................................... 314

Relative Terrain Symbology ........................................ 315

Terrain Page ............................................................. 320

Wire Obstacle Information and Alerting ...................... 321

Vertical Situation Display (VSD) Terrain ....................... 321

Terrain-SVT and TAWS-B Alerting Displays ................... 324

Forward Looking Terrain Avoidance ............................ 327

Additional TAWS-B Alerting ....................................... 327

Inhibiting Alerting ..................................................... 330

System Status ........................................................... 330

6.4 Trafﬁc Information Service (TIS) ........................ 333

Displaying Trafﬁc Data .............................................. 334

Trafﬁc Map Page ....................................................... 335

TIS Alerts ................................................................. 336

System Status ........................................................... 338

6.5 TAS Trafﬁc ............................................................. 340

TAS Theory of Operation ............................................ 340

TAS Alerts ................................................................ 344

System Test .............................................................. 345

Operation ................................................................ 346

6.6 ADS-B Trafﬁc ........................................................ 352

190-02177-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III

ix

TABLE OF CONTENTS

ADS-B System Overview ............................................ 352

Conﬂict Situational Awareness & Alerting (CSA) .......... 354

Airborne and Surface Applications .............................. 355

Trafﬁc Description ..................................................... 356

Operation ................................................................ 356

ADS-B System Status ................................................ 362

SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM

7.1 AFCS Overview .................................................... 365

7.2 Flight Director Operation ................................... 369

Activating the Flight Director ..................................... 369

AFCS Status Box ....................................................... 370

Flight Director Modes ................................................ 371

Command Bars ......................................................... 371

7.3 AFCS MODES ........................................................ 372

Vertical Modes ......................................................... 372

Lateral Modes .......................................................... 378

Combination Modes (VNV, APR, NAV, BC, GA) ............. 382

7.4 Autopilot .............................................................. 394

Flight Control ........................................................... 394

Engagement ............................................................. 395

Control Wheel Steering ............................................. 395

Disengagement ........................................................ 396

7.5 AFCS Annunciations and Alerts ......................... 397

Overspeed Protection ................................................ 398

Underspeed Protection .............................................. 398

SECTION 8 ADDITIONAL FEATURES

8.1 SafeTaxi ................................................................ 402

8.2 Charts .................................................................... 404

ChartView ................................................................ 405

FliteCharts ............................................................... 413

IFR/VFR Charts ......................................................... 417

8.3 Airport Directory ................................................. 420

8.4 SurfaceWatch ....................................................... 421

Information Box ....................................................... 421

Alerts ...................................................................... 422

Surfacewatch Setup .................................................. 425

8.5 Database Cycle Number and Revisions ............ 427

Cycle Number and Revision ....................................... 427

8.6 SiriusXM Radio Entertainment .......................... 429

Activating SiriusXM Satellite Radio Services ................ 429

Using SiriusXM Radio ................................................ 430

8.7 Satellite Telephone and SMS Messaging .......... 433

Registering with Garmin Connext .............................. 433

Disable/Enable Iridium Transceiver.............................. 433

Telephone Communication ........................................ 434

Text Messaging (SMS) ............................................... 441

8.8 Flight Data Logging ............................................ 453

8.9 Connext Setup ..................................................... 455

8.10 Auxiliary Video (Optional) .................................. 457

Video Setup .............................................................457

Display Selection ...................................................... 457

Zoom/Range ............................................................ 459

8.11 Electronic Stability & Protection (ESP

™

) ........... 460

Roll Engagement ...................................................... 461

Pitch Engagement..................................................... 462

High Airspeed Protection ........................................... 463

Angle of Attack Protection ......................................... 463

8.12 Electronic Checklists ........................................... 465

8.13 Abnormal Operation ........................................... 467

SiriusXm Data Link Receiver Troubleshooting............... 467

APPENDICES

Annunciations and Alerts ............................................. 469

Alert Level Deﬁnitions ............................................... 470

Audio Alerting System Test ........................................ 471

System Message Advisories ....................................... 471

Database Management ................................................ 481

Loading Updated Databases ...................................... 481

Database Deletion Feature ....................................... 492

Magnetic Field Variation Database Update .................. 493

Aviation Terms and Acronyms ...................................... 495

Frequently Asked Questions ........................................ 505

Map Symbols ................................................................. 509

INDEX

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

Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III

190-02177-01 Rev. Ax

TABLE OF CONTENTS

Blank Page

190-02177-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

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 Cessna

Nav III. The system presents ﬂight instrumentation, position, navigation, communication, and identiﬁcation

information to the pilot through large-format displays.

LINE REPLACEABLE UNITS (LRU)

The system consists of the following Line Replaceable Units (LRUs):

•

GDU 1054B/1050

(2) – The system features two 10.4-inch backlit LED display units with high resolution.

The left display is conﬁgured as a Primary Flight Display (PFD) and the right display is conﬁgured as an Multi

Function Display (MFD). The displays communicate with each other through a High-Speed Data Bus (HSDB)

connection. Each display is also connected to the onside Integrated Avionics Unit (IAU). Systems conﬁgured

with the Garmin Automatic Flight Control System (AFCS) use the GDU 1054B. Systems without the Garmin

AFCS use the GDU 1050.

•

GIA 63W / GIA 64W

(2) – The GIA Integrated Avionics Units (IAU) function as the main communication

hub, linking all LRUs with the PFD and MFD. Each IAU contains a GPS SBAS receiver, VHF COM/NAV/GS

receivers, a ﬂight director (FD) and system integration microprocessors. Each IAU is paired with the PFD and

MFD via HSDB connection.

•

GSU 75

(1) – The GSU Air Data and Attitude Reference System (ADAHRS) processes data from the pitot/

static system as well as the Outside Air Temperature (OAT) probe to provide pressure altitude, airspeed,

vertical speed and OAT information to the system. This unit also provides aircraft attitude and heading

information via ARINC 429 to the PFD, MFD, and IAU. The ADAHRS contains advanced sensors (including

accelerometers and rate sensors) and interfaces with the Magnetometer to obtain magnetic ﬁeld information,

and with the IAUs to obtain GPS information. ADAHRS/AHRS modes of operation are discussed later in this

document.

•

GMU 44

(1) – The GMU Magnetometer measures local magnetic ﬁeld. Data is sent to the ADAHRS for

processing to determine aircraft magnetic heading. The unit receives power directly from the ADAHRS and

communicates with the GRS unit using an RS-485 digital interface.

•

GDC 74A

(1) (Optional) – The GDC Air Data Computer (ADC) 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 IAUs, the PFD, MFD, and the Attitude and Heading Reference

System (AHRS), using an ARINC 429 digital interface (it also interfaces directly with the Air Temperature

Probe. The unit is designed to operate in Reduced Vertical Separation Minimum (RVSM) airspace.

•

GRS 77

(1) (Optional) – The Attitude and Heading Reference System (AHRS) provides aircraft attitude and

heading information via ARINC 429 to both displays and both IAUs. The unit contains advanced sensors

(including accelerometers and rate sensors) and interfaces with the Magnetometer to obtain magnetic ﬁeld

information, with the GDC 74A to obtain air data, and with both IAUs to obtain GPS information.

190-02177-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

2

SYSTEM OVERVIEW

•

GEA 71 / GEA 71B

(1) – The GEA Engine Airframe Unit receives and processes signals from the engine and

airframe sensors. This unit communicates with both IAUs using an RS-485 digital interface.

•

GMA 1347 / GMA 1360

(1) – The GMA Audio Panel integrates NAV/COM digital audio, intercom system

and marker beacon controls. This unit also enables the manual control of the display reversionary mode (red

DISPLAY BACKUP

button) and communicates with the #1 IAU, using an HSDB connection. The optional

GMA 1360 offers Bluetooth® capability.

•

GTX 335R/345R/33ES

(1) – The GTX 335R Transponder is a solid-state transponder that provides Mode A,

C, S capability. The optional GTX 345R also provides ADS-B In/Out. The transponder can be controlled

from the PFD. The transponder communicates with the both IAUs through an RS-232 digital interface.

•

GSA 81

(3), and

GSM 86/85/85A

(3) – The GSA Servos are used for the automatic control of roll, pitch, and

pitch trim. These units interface with each IAU.

The GSM 86/85/85A servo gearbox is responsible for transferring the output torque of the GSA 81 servo

actuator to the mechanical ﬂight-control surface linkage.

•

GSR 56

(1) (Optional) – The GSR Iridium Transceiver operation for voice communication is by means of

pilot and copilot headsets in the cockpit. The transceiver can provide Garmin Connext Weather and SMS

functions.

•

Flight Stream 510

(1) (Optional) – The Flight Stream Bluetooth Transceiver provides wireless connectivity

between a compatible tablet/mobile device and the avionics system. GPS, ADAHRS, 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.

•

GDL 69A / GDL 69A SXM

(1) (Optional) – The GDL SiriusXM Datalink Receiver provides data link weather

information to the MFD and, indirectly, to the PFD map as well as digital audio entertainment. The unit

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

Radio are required to enable services.

•

GTS 800

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

C transponders to provide Trafﬁc Advisories to the pilot independent of the air trafﬁc control system.

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 / GDL 69A SXM

Data Link Receiver

•

GTS 800

Trafﬁc Advisory System

•

L3 Stormscope Lightning Strike and Thunderstorm

Detection

• KN 63 DME

• KR 87 ADF Receiver

• KTA 870 Trafﬁc Avoidance System

• CO Guardian Carbon Monoxide Detection

190-02177-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

3

SYSTEM OVERVIEW

Non-Garmin Equipment

Optional

Garmin Equipment

Optional

Non-Garmin Equipment

Garmin Equipment

GTX 345R

Or

#1 GDU

1054B/1050

(PFD)

GDL 69A/

69A SXM

(SiriusXM

Datalink Receiver)

GMA

1347/1360

(Audio Panel)

#1 GIA

63W/64W

(Integrated

Avionics

Unit)

VHF COM

GPS/SBAS

VOR/LOC

G/S

Flight

Director

AFCS Mode

Logic

Servo Logic

#2 GIA

63W/64W

(Integrated

Avionics

Unit)

VHF COM

GPS/SBAS

VOR/LOC

G/S

Flight

Director

AFCS Mode

Logic

Servo Logic

#2 GDU

1054B/1050

(MFD)

GEA 71/71B

(Engine &

Airframe I/F)

GTX 335R/33

(Transponder)

GSA 81 (3)

(Servos)

GMU 44

(Magnetometer)

GSU 75

(ADAHRS)

GRS 77

(AHRS)

GDC 74A

(Air Data

Computer)

KTA 870

(Traffic

Avoidance)

GTS 800

(TAS)

CO Guardian

(Carbon Monoxide

Detection)

L-3

Stormscope

KN-63

(DME)

KR-87

(ADF Reciever)

ELT

(Emergency Locator

Transmitter)

FS 510

(SD Card

Bluetooth

Transceiver)

GSR 56

(Iridium Transceiver)

Figure 1-1 System (LRU Conﬁguration)

NOTE: For information on non-Garmin equipment, consult the applicable optional interface user’s guide.

This document assumes that the reader is already familiar with the operation of this additional equipment.

190-02177-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Cessna Nav III

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

4

SYSTEM OVERVIEW

1.2 SYSTEM CONTROLS

NOTE: The Audio Panel (GMA 1347) is described in the CNS & Audio Panel section.

The system controls are located on the PFD and MFD bezels and audio panel. The controls for the PFD and

MFD are discussed within the following pages of this section.

PFD/MFD CONTROLS

Figure 1-2 PFD/MFD Controls

4

2

1

6

5

7

9

8

3

12

16

11

10

15

14

13

20

21

19

18

25

24

22

23

28

27

*Only with Garmin AFCS

17

26

29

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