Garmin G1000 NXi - Piper PA-44-180 Seminole Reference guide

190-02198-02

Revision A

Garmin International, Inc.

1200 East 151st Street

Olathe, Kansas 66062, U.S.A.

Garmin AT, Inc.

2345 Turner Road SE

Salem, OR 97302, U.S.A.

Garmin (Europe) Ltd.

Liberty House, Hounsdown Business Park

Southampton, Hampshire SO40 9LR U.K.

Garmin Corporation

No. 68, Zhangshu 2nd Road

Xizhi District,

New Taipei City, Taiwan

www.ﬂy.garmin.com

Piper PA-44-180 Seminole

Pilot’s Guide

®

G1000

®

Pilot’s Guide

SYSTEM OVERVIEW

FLIGHT INSTRUMENTS

EIS

AUDIO PANEL & CNS

FLIGHT MANAGEMENT

HAZARD AVOIDANCE

AFCS

ADDITIONAL FEATURES

APPENDICES

INDEX

190-02198-02 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Piper PA-44-180 Seminole

This manual reﬂects the operation of System Software version 3344.01 or later for the PA-44-180. Some differences in operation may be

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

Garmin International, Inc.

1200 East 151st Street

Olathe, Kansas 66062, U.S.A.

Garmin (Europe) Ltd.

Liberty House, Hounsdown Business Park

Southampton, Hampshire SO40 9LR U.K.

Garmin AT, Inc.

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

®

, SurfaceWatch

™

, and SafeTaxi

®

are registered trademarks of Garmin International, Inc. or its

subsidiaries. Garmin ESP

™

, Garmin SVT

™

, Connext

™

, and WireAware

™

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

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

AC-U-KWIK

®

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

®

and Honeywell

®

are registered trademarks of Honeywell

International, Inc. Becker

®

is a registered trademark of Becker Flugfunkwerk GmbH. NavData

®

is a registered trademark of Jeppesen, Inc.;

Wi-Fi

®

is a registered trademark of the Wi-Fi Alliance. SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite

Radio, Inc. The Bluetooth

®

word mark and logos are owned by the Bluetooth SIG, Inc. and any use of such marks by Garmin is under

license.

AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively “AOPA”) expressly disclaim all warranties,

with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties

of merchantability and ﬁtness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any

representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any

incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if

AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to

the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual

or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for

incidental or consequential damages so the above limitations or exclusions may not apply to you.

AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”) expressly disclaim all warranties with

respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of

merchantability and ﬁtness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or

make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the

maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related

to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some jurisdictions

do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations

or exclusions may not apply to licensee..

Printed in the U.S.A

Garmin G1000 NXi Pilot’s Guide for the Piper PA-44-180 Seminole

190-02198-02 Rev. A

Blank Page

190-02198-02 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Piper PA-44-180 Seminole

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

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

standard pressure setting, as applicable.

WARNING

:

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

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

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

in error as displayed.

Garmin G1000 NXi Pilot’s Guide for the Piper PA-44-180 Seminole

190-02198-02 Rev. Aii

WARNINGS, CAUTIONS, AND NOTES

WARNING: Do not rely on the autopilot to level the aircraft at the MDA/DH when ﬂying an approach with

vertical guidance. The autopilot will not level the aircraft at the MDA/DH even if the MDA/DH is set in the

altitude preselect.

WARNING: Do not rely on the accuracy of attitude and heading indications in the following geographic

areas (due to variations in the earth’s magnetic ﬁeld): North of 72° North latitude at all longitudes; South

of 70° South latitude at all longitudes; North of 65° North latitude between longitude 75° W and 120° W.

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

North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia); South of 55° South

latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand).

WARNING: 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.

190-02198-02 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Piper PA-44-180 Seminole

iii

WARNINGS, CAUTIONS, AND NOTES

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

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

performance of all GPS equipment. Portions of the system 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.

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://ﬂygarmin.com by selecting ‘Aviation Database Declarations.’

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

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

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

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

Garmin G1000 NXi Pilot’s Guide for the Piper PA-44-180 Seminole

190-02198-02 Rev. Aiv

WARNINGS, CAUTIONS, AND NOTES

NOTE

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

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

www.ygarmin.combyselecting‘DatabaseExclusionsList.’

NOTE

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

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

selecting ‘Aviation Database Alerts.’

NOTE

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

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

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

and ﬁxes; or any other displayed item used for navigation or communication in the air or on the ground. Go

to FlyGarmin.com and select ‘Aviation Data Error Report’.

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: Terrain and obstacle alerting is not available north of 89º North latitude and south of 89º South

latitude. This is due to limitations present within the Terrain database and the system’s ability to process

the data representing the affected areas.

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

avoid an autonomous system reboot.

190-02198-02 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Piper PA-44-180 Seminole

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 Piper PA-44-180 Seminole

190-02198-02 Rev. Avi

REVISION INFORMATION

Record of Revisions

Part Number Revision Date Page Range Description

190-02198-00 A

B

11/22/16

11/29/16

All Initial Release

Clerical Revision

190-02198-01 A 5/16/17 All Added HSI Map

Added Bluetooth functionality

Added other GDU 20.10 parameters

190-02198-02 A 10/08/18 All Production release at GDU 20.87

Added GMA 1360

Added SurfaceWatch

Added WireAware

Added visual approaches

190-02198-02 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Piper PA-44-180 Seminole

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 ....................................................... 9

System Annunciations ................................................. 10

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

AHRS Operation ......................................................... 12

GPS Receiver Operation .............................................. 14

1.4 Accessing System Functionality .......................... 19

Softkey Function ......................................................... 19

Menus ....................................................................... 24

MFD Page Groups ....................................................... 25

Split Screen Functionality ............................................ 28

System Settings .......................................................... 30

System Utilities ........................................................... 39

1.5 Display Backlighting ............................................. 43

SECTION 2 FLIGHT INSTRUMENTS

2.1 Flight Instruments ................................................. 48

Attitude Indicator ....................................................... 48

Airspeed Indicator ...................................................... 49

Altimeter ................................................................... 51

Vertical Speed Indicator (VSI) ....................................... 54

Vertical Deviation ....................................................... 54

Vertical Navigation (VNV) Indications ........................... 56

Horizontal Situation Indicator (HSI) .............................. 57

Course Deviation Indicator (CDI) .................................. 61

2.2 Supplemental Flight Data .................................... 70

Generic Timer ............................................................. 70

Temperature Displays .................................................. 70

Wind Data ................................................................. 71

2.3 PFD Annunciations and Alerting Functions ........ 72

Altitude Alerting ......................................................... 72

LowAltitudeAnnunciation .......................................... 72

Marker Beacon Annunciations...................................... 73

Minimum Descent Altitude/Decision Height Alerting ...... 73

2.4 Garmin SVT (Synthetic Vision Technology) ......... 75

SVT Operation ............................................................ 76

SVT Features .............................................................. 77

Field of View .............................................................. 87

2.5 Abnormal Operations ........................................... 88

Abnormal GPS Conditions ........................................... 88

SVT Troubleshooting ................................................... 89

SVT in Reversionary Mode ........................................... 89

Unusual Attitudes ....................................................... 89

SVT Unusual Attitudes ................................................. 90

SECTION 3 ENGINE INDICATION SYSTEM (EIS)

3.1 EIS Display .............................................................. 92

3.2 Engine Page............................................................ 94

Fuel Calculations ....................................................... 96

CO Detector ............................................................... 97

3.3 EIS Display (Reversionary Mode) ........................ 98

SECTION 4 AUDIO PANEL AND CNS

4.1 Overview ................................................................ 99

PFD Controls and Frequency Display ........................... 100

Audio Panel Controls ................................................ 102

4.2 COM Operation .................................................... 105

COM TUNING BOXES ................................................ 105

COM Transceiver Manual Tuning ................................ 106

Auto-tuning the COM Frequency ................................ 106

Auto-tuning from the MFD ........................................ 108

Frequency Spacing .................................................... 110

4.3 NAV Operation ..................................................... 111

NAV Tuning Boxes..................................................... 111

NAV Radio Selection and Activation ........................... 112

NAV Receiver Manual Tuning ..................................... 112

Auto-tuning a NAV Frequency from the MFD ............... 112

Auto-tuning NAV Frequencies on Approach Activation . 115

Marker Beacon Receiver ............................................ 115

DME Tuning ............................................................. 116

4.4 GTX 335 or GTX 345 Mode S Transponder ....... 117

Transponder Controls ................................................ 117

Transponder Mode Selection ...................................... 118

Entering a Transponder Code ..................................... 120

IDENT Function ........................................................ 121

Flight ID Reporting.................................................... 121

Garmin G1000 NXi Pilot’s Guide for the Piper PA-44-180 Seminole

190-02198-02 Rev. Aviii

TABLE OF CONTENTS

4.5 Additional Audio Panel Functions ..................... 122

Power-Up ................................................................. 122

Mono/Stereo Headsets .............................................. 122

Speaker ................................................................... 122

Intercom .................................................................. 123

Blue-Select Mode (Telephone/Entertainment Distribution) ..

125

Clearance Recorder and Player ................................... 126

Split COM Operation ................................................. 126

3D Audio ................................................................. 126

Bluetooth

®

.................................................................................................................127

Telephone/Entertainment Inputs ................................. 128

4.6 Audio Panel Preﬂight Procedure ....................... 129

4.7 Abnormal Operation ........................................... 130

Stuck Microphone ..................................................... 130

COM Tuning Failure ................................................... 130

Audio Panel Fail-Safe Operation ................................. 130

Reversionary Mode ................................................... 130

SECTION 5 FLIGHT MANAGEMENT

5.1 Introduction ......................................................... 131

Navigation Status Box and Data Bar ........................... 133

5.2 Using Map Displays ............................................. 135

Map Orientation ....................................................... 135

Map Range .............................................................. 137

Map Panning ............................................................ 139

Measuring Bearing and Distance ................................ 141

Topography .............................................................. 142

Map Symbols ........................................................... 144

Airways ................................................................... 148

Additional Navigation Map Items ............................... 150

IFR/VFR Charts ......................................................... 153

5.3 Waypoints ............................................................. 156

Airports ................................................................... 157

Intersections ............................................................ 162

NDBs ....................................................................... 164

VORs ....................................................................... 166

VRPs ....................................................................... 168

User Waypoints ........................................................ 169

5.4 Airspaces .............................................................. 174

Nearest Airspace ...................................................... 175

Smart Airspace ......................................................... 177

5.5 Direct-to-Navigation .......................................... 179

5.6 Flight Planning ..................................................... 183

Flight Plan Views ...................................................... 186

Creating a Flight Plan ............................................... 188

Flight Plan Waypoint and Airway Modiﬁcations ........... 190

Flight Plan Operations ............................................... 198

User-Deﬁned Holding Patterns ................................... 202

Managing Flight Plans .............................................. 206

5.7 Vertical Navigation ............................................. 215

Constraints .............................................................. 216

Vertical Situation Display (VSD) .................................. 218

5.8 Procedures ...........................................................224

Departures ............................................................... 225

Arrivals ................................................................... 228

Approaches ............................................................. 231

5.9 Trip and Weight Planning ................................... 242

Trip Planning ............................................................ 242

Weight Planning ....................................................... 246

5.10 Abnormal Operation ........................................... 249

SECTION 6 HAZARD AVOIDANCE

6.1 Data Link Weather ............................................... 252

ActivatingDataLinkWeatherServices ........................ 252

Weather Product Age ................................................ 254

DisplayingDataLinkWeatherProducts ....................... 256

Weather Product Overview ........................................ 265

FIS-B Weather Status................................................. 298

6.2 Terrain Displays ................................................... 300

Relative Terrain Symbology ........................................ 301

Terrain Page ............................................................. 306

Wire Obstacle Information and Alerting ...................... 307

Vertical Situation Display (VSD) Terrain ....................... 307

Terrain-SVT and TAWS-B Alerting Displays ................... 310

ForwardLookingTerrainAvoidance ............................ 314

Additional TAWS-B Alerting ....................................... 314

Inhibiting Alerting ..................................................... 317

System Status ........................................................... 317

6.3 Trafﬁc Information Service (TIS) ........................ 320

Displaying Trafﬁc Data .............................................. 321

Trafﬁc Map Page ....................................................... 322

TIS Alerts ................................................................. 323

System Status ........................................................... 325

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Garmin G1000 NXi Pilot’s Guide for the Piper PA-44-180 Seminole

ix

TABLE OF CONTENTS

6.4 GTS 800 Trafﬁc ..................................................... 327

Theory of Operation .................................................. 327

TAS Alerts ................................................................ 331

System Test .............................................................. 332

Operation ................................................................ 333

6.5 ADS-B Trafﬁc ........................................................ 339

ADS-B System Overview ............................................ 339

ADS-B with TAS ........................................................ 341

Conﬂict Situational Awareness & Alerting ................... 341

Airborne and Surface Applications .............................. 342

Trafﬁc Description ..................................................... 344

Operation ................................................................ 344

ADS-B System Status ................................................ 350

SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM

7.1 AFCS Overview .................................................... 353

Basic Autopilot Operation .......................................... 353

AFCS Controls ......................................................... 354

7.2 Flight Director Operation ................................... 356

Activating the Flight Director ..................................... 356

AFCS Status Box ....................................................... 356

Flight Director Modes ................................................ 357

Command Bars ......................................................... 358

7.3 AFCS Modes ......................................................... 360

Vertical Modes ......................................................... 360

LateralModes .......................................................... 366

Combination Modes (VNV, APR, NAV, BC, GA) ............. 370

7.4 Autopilot Operation ............................................ 381

Flight Control ........................................................... 381

Engagement ............................................................. 381

Control Wheel Steering ............................................. 382

Disengagement ........................................................ 382

LevelMode .............................................................. 382

Underspeed Protection .............................................. 383

7.5 AFCS Annunciations and Alerts ......................... 385

AFCS Status Alerts .................................................... 385

Overspeed Protection ................................................ 385

7.6 Abnormal Operation ........................................... 387

Suspected Autopilot Malfunction ............................... 387

Overpowering Autopilot Servos .................................. 387

SECTION 8 ADDITIONAL FEATURES

8.1 SafeTaxi ................................................................ 390

8.2 Charts .................................................................... 392

ChartView ................................................................ 393

FliteCharts ............................................................... 402

8.3 Airport Directory ................................................. 408

8.4 SurfaceWatch ....................................................... 409

Information Box ....................................................... 409

Alerts ...................................................................... 411

Surfacewatch Setup .................................................. 413

8.5 Database Cycle Numbers and Revisions .......... 416

Cycle Number and Revision ....................................... 416

8.6 WiFi Connections ................................................. 418

8.7 SiriusXM Radio Entertainment .......................... 421

Activating SiriusXM Satellite Radio Services ................ 421

Using SiriusXM Radio ................................................ 422

8.9 Flight Data Logging ............................................ 426

8.10 Electronic Stability & Protection (ESP

™

) ........... 428

Roll Engagement ...................................................... 429

Pitch Engagement..................................................... 430

High Airspeed Protection ........................................... 431

8.11 Connext Setup ..................................................... 432

8.12 Abnormal Operation ........................................... 435

GDL59/69/69ASXMTroubleshooting ......................... 435

APPENDICES

Annunciations and Alerts ............................................. 437

CAS Message Prioritization ........................................ 438

CAS Annunciations ................................................... 439

System Annunciations ............................................... 442

System Messages ..................................................... 442

Database Management ................................................ 453

LoadingUpdatedDatabases ...................................... 453

Database Deletion Feature ....................................... 464

Magnetic Field Variation Database Update .................. 465

Aviation Terms and Acronyms .................................... 467

Frequently Asked Questions ........................................ 477

Miscellaneous

Map Symbols ....................................... 481

Garmin G1000 NXi Pilot’s Guide for the Piper PA-44-180 Seminole

190-02198-02 Rev. Ax

TABLE OF CONTENTS

Blank Page

190-02198-02 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Piper PA-44-180 Seminole

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 Piper

PA-44-180 Seminole. The system presents ﬂight instrumentation, position, navigation, communication, and

identiﬁcation information to the pilot through large-format displays.

LINE REPLACEABLE UNITS (LRU)

•

GDU 1050/1054

(2) – The system features two 10 inch, high resolution LED backlit display units. The left

display is a GDU 1050 is conﬁgured as a Primary Flight Display (PFD). The right display may be either a GDU

1050 or a GDU 1054, and is conﬁgured as an Multi Function Display (MFD). The displays communicate

with each other through a High-Speed Data Bus (HSDB) Ethernet connection. Each display is also paired

with an Ethernet connection to the GIA 64W.

•

GIA 64W

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

GIA 64W contains a GPS SBAS receiver, VHF COM/NAV/GS receivers, a ﬂight director (FD) and system

integration microprocessors. Each GIA 64W is paired with the PFD and MFD via HSDB connection. The

GIA 64Ws are not paired together and do not communicate with each other directly.

•

GMU 44B

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

to determine aircraft magnetic heading. This unit receives power directly from the AHRS and communicates

with it via an RS-485 digital interface.

•

GRS 79 (1)

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

information via ARINC 429 to both GDUs and both GIAs. The AHRS contains advanced sensors (including

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

with the ADC to obtain air data, and with both GIAs to obtain GPS information.

•

GDC 72 (1)

– The Air Data Computer (ADC) processes data from the pitot/static system and outside air

temperature (OAT) sensor. The ADC provides pressure altitude, airspeed, vertical speed, and OAT information

to the system. It communicates with the GIAs, displays, and AHRS using an ARINC 429 digital interface.

•

GEA 71B

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

with both GIA 64Ws using an RS-485 digital interface.

•

GMA 1360

(1) – The Audio Panel integrates navigation/communication radio (NAV/COM) digital audio,

intercom, and marker beacon controls, and is installed between the displays. This unit also provides manual

control of display reversionary mode (red

DISPLAY BACKUP

Button, and communicates with both GIAs

using an RS-232 digital interface.

•

GTX 335R/345R

(1) – Solid-state transponders that provide Modes A, C, S and ADS-B 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 GIA 64Ws through an RS-232 digital interface.

•

GDL 59

(1) (Optional) – The GDL 59 is connected to the PFD via HSDB and provides wireless data transfer.

190-02198-02 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Piper PA-44-180 Seminole

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

2

SYSTEM OVERVIEW

•

GDL 69A SXM

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

the MFD (and, indirectly, to the PFD Map) as well as digital audio entertainment. The GDL 69A SXM

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

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

•

GTS 800

(1) (Optional) – The GTS 800 Trafﬁc Advisory System (TAS) uses active interrogations of Mode

S and Mode C transponders to provide trafﬁc information to the pilot independent of the air trafﬁc control

system.

•

GSA 80

(1)

/GSA 81

(2) (only with Garmin AFCS option) – The GSA 80 servo is used for the automatic

control of pitch trim. The GSA 81 servos are used for the automatic control of pitch and roll. These units

interface with each GIA 64W.

The GSM 86 servo gearboxes are responsible for transferring the output torque of the GSA 80/81 servo actuators

to the mechanical ﬂight-control surface linkage.

The Piper PA44 has the option to be equipped with a Garmin Automated Flight Control System (AFCS),

which includes the Flight Director (FD), Autopilot (AP), manual electric trim, and control wheel steering (CWS)

functions of the 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 59

WiFi Data Link

•

GDL 69A SXM

Sirius XM Data Link Receiver

•

GTS 800

Trafﬁc Advisory System

•

Flight Stream 510 Wireless Transceiver

•KN 63 DME

•KR-87 ADF

The optional Flight Stream 510 device (SD Card) provides a Bluetooth

®

connection between the system and a

mobile device. GPS, AHRS, ADS-B, trafﬁc, Sirius XM audio, and FIS-B 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 also

be performed using the Flight Stream 510 WiFi link.

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.

190-02198-02 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Piper PA-44-180 Seminole

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

3

SYSTEM OVERVIEW

#1

GDU 1050

(PFD)

GDL 69A SXM

(XM Weather/

Audio Datalink)

GMA 1360

(Audio

Panel)

KN-63

(DME)

#1 GIA 64W

(Integrated

Avionics

Unit)

VHF COM

GPS/SBAS

VOR/LOC

G/S

Flight

Director

AFCS Mode

Logic

Servo Logic

#2 GIA 64W

(Integrated

Avionics

Unit)

VHF COM

GPS/SBAS

VOR/LOC

G/S

Flight

Director

AFCS Mode

Logic

Servo Logic

#2

GDU 1050

(MFD)

or

GDU 1054

(MFD)

Non-Garmin Equipment

KR-87

(ADF)

GTX 335R

(Transponder)

or

GEA 71B (Engine &

Airframe I/F)

GDC 72

(Air Data

Computer)

GRS 79

(Attitude &

Heading)

Optional

Garmin Equipment

Optional

Non-Garmin Equipment

GMU 44B

(Magnetometer)

GTS 800

(TAS)

Garmin Equipment

GSA 80/81 (3)

(Garmin AFCS

Servos)

FS 510

(SD Card

Bluetooth

Link)

GDL 59

(WiFi Data Link)

GTX 345R

(Alternate)

Figure 1-1 System (LRU Conﬁguration)

190-02198-02 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Piper PA-44-180 Seminole

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 is described in the Audio Panel & CNS 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

*GDU 1054 MFD Only

26

17

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Garmin G1000 NXi - Piper PA-44-180 Seminole, G1000 NXi: Piper PA-44-180 Seminole Reference guide

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