Garmin G1000 NXi - Beechcraft Baron G58 Reference guide

190-02181-01

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.garmin.com

Beechcraft G58

Beechcraft G58 Series

Pilot’s Guide

®

G1000

®

Pilot’s Guide

SYSTEM OVERVIEW

FLIGHT INSTRUMENTS

EIS

AUDIO PANEL & CNS

FLIGHT MANAGEMENT

HAZARD AVOIDANCE

AFCS

ADDITIONAL FEATURES

APPENDICES

INDEX

190-02181-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Beechcraft G58

This manual reﬂects the operation of System Software version 3185.00 or later for the G1000 NXi Beechcraft G58 Series. 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

Website 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

®

, G1000

®

NXi,

WATCH

®

, FliteCharts

®

, and SafeTaxi

®

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

Garmin ESP

™

, Garmin SVT

™

, SurfaceWatch

™

, and Connext

™

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

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

Skywatch

®

and Stormscope

®

are registered trademarks of L-3 Communications. Ryan

®

, TCAD

®

and Avidyne

®

are registered trademarks of

Avidyne Corporation. AC-U-KWIK

®

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

®

and Honeywell

®

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.

Garmin G1000 NXi Pilot’s Guide for the Beechcraft G58

190-02181-01 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.

190-02181-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Beechcraft G58

iii

WARNINGS, CAUTIONS, AND NOTES

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

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

verify the accuracy of the information.

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

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

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

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

instructions, and clearances.

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

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

enhance situational awareness.

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

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

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

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

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

conditions.

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

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

for data link transmission, the weather information shown by the data link weather product may be older than the

indicated weather product age.

WARNING: 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 mes-

sage. ‘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.

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).

Garmin G1000 NXi Pilot’s Guide for the Beechcraft G58

190-02181-01 Rev. Aiv

WARNINGS, CAUTIONS, AND NOTES

WARNING: Do not use SurfaceWatch

™

information as the primary method of ﬂight guidance during airborne or

ground operations. SurfaceWatch does not have NOTAM or ATIS information regarding the current active runway,

condition, or information about the position of hold lines.

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.

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

MPEL boundary.

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

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

of the true intensity.

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. Unauthor-

ized 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 accu-

racy 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.

190-02181-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Beechcraft G58

v

WARNINGS, CAUTIONS, AND NOTES

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 taxi-

ing. If one or more of the sensed values are unavailable, the annunciation indicates no comparison is possible.

NOTE: The system responds to a terminal procedure based on data coded within that procedure in the Navigation

Database. Differences in system operation may be observed among similar types of procedures due to differences

in the Navigation Database coding speciﬁc to each procedure.

NOTE

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

following:

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

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

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

obtainedfromGarminorJeppesenthathaveaType2LetterofAuthorization(LOA)fromtheFAAareassured

compliance with all data quality requirements (DQRs). A copy of the Type 2 LOA is available for each applicable

database and can be viewed at http://ﬂy.garmin.com by selecting ‘Aviation Database Declarations.’

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

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

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

AFM(S) and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment.

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

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

com by selecting ‘Database Exclusions List.’

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

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

Database Alerts.’

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

Garmin G1000 NXi Pilot’s Guide for the Beechcraft G58

190-02181-01 Rev. Avi

WARNINGS, CAUTIONS, AND NOTES

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.-

190-02181-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Beechcraft G58

SOFTWARE LICENSE AGREEMENT

vii

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 Beechcraft G58

190-02181-01 Rev. A

SOFTWARE LICENSE AGREEMENT

viii

Blank Page

190-02181-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Beechcraft G58

ix

REVISION INFORMATION

Record of Revisions

Part Number Revision Date Page Range Description

190-02181-00 A

B

1/6/17

5/18/17

All

Production Release for GDU 20.05

Updated Surfacewatch information

Clerical

190-02181-01 A

6/1/18

All

Production release for GDU 20.83

Updated EIS information

Added WireAware

Added Visual Approaches

Added Baro QFE Altimeter settings

Added Connext Weather

Added Electronic Stability and Protection

Updated Audio Panel Information

Updated Weather Radar

Garmin G1000 NXi Pilot’s Guide for the Beechcraft G58

190-02181-01 Rev. Ax

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 ......................................................... 8

Reversionary Mode ....................................................... 9

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

System Status ............................................................. 11

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 ........................................................... 40

1.5 Display Backlighting ............................................... 44

SECTION 2 FLIGHT INSTRUMENTS

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

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

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

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

Vertical Speed Indicator (VSI) ....................................... 55

Vertical Deviation ....................................................... 55

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

Course Deviation Indicator (CDI) .................................. 60

2.2 Supplemental Flight Data ...................................... 69

Generic Timer ............................................................. 69

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

Wind Data ................................................................. 70

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

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

SVT Features .............................................................. 78

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

2.5 Abnormal Operations ............................................. 89

Abnormal GPS Conditions ........................................... 89

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

SVT Unusual Attitudes ................................................. 91

SECTION 3 ENGINE INDICATION SYSTEM

3.1 Engine Display ......................................................... 94

Engine Softkeys .......................................................... 96

Exhaust Gas Temperature ............................................ 97

Cylinder Head Temperature .......................................... 97

Lean Engine .............................................................. 97

Fuel Calculations ........................................................ 99

3.2 EIS Display (Reversionary Mode) ........................... 100

SECTION 4 AUDIO PANEL AND CNS

4.1 Overview ................................................................ 101

PFD Controls and Frequency Display ........................... 102

Audio Panel Controls ................................................ 104

4.2 COM Operation...................................................... 107

COM Tuning Boxes .................................................... 107

COM Transceiver Manual Tuning ................................ 108

Auto-Tuning the COM Frequency ................................ 108

Frequency Spacing ................................................... 111

4.3 NAV Operation....................................................... 112

NAV Tuning Boxes..................................................... 112

NAV Radio Selection and Activation ........................... 113

NAV Receiver Manual Tuning ..................................... 113

Auto-Tuning a NAV Frequency from the MFD............... 114

Marker Beacon Receiver ............................................ 116

DME Tuning ............................................................. 117

4.4 Mode S Transponder ............................................. 118

Transponder Controls ................................................ 118

Transponder Mode Selection ...................................... 119

Entering a Transponder Code ..................................... 121

IDENT Function ........................................................ 122

Flight ID Reporting.................................................... 122

4.5 Additional Audio Panel Functions ....................... 123

Power-Up ................................................................. 123

190-02181-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Beechcraft G58

xi

TABLE OF CONTENTS

Mono/Stereo Headsets .............................................. 123

Speaker (GMA 1347) ................................................. 123

Speaker (GMA 1360) ................................................. 123

Intercom (GMA 1347) ............................................... 124

Intercom (GMA 1360) ............................................... 125

Blue-Select Mode (Telephone/Entertainment Distribution)

(GMA 1360) ............................................................. 127

3D Audio (GMA 1360) ............................................... 128

Bluetooth

®

(GMA 1360 Only)..................................... 130

Clearance Recorder and Player ................................... 131

Entertainment Inputs ................................................ 132

4.6 Audio Panels Preﬂight Procedure ....................... 133

4.7 Abnormal Operation ............................................. 134

Stuck Microphone ..................................................... 134

COM Tuning Failure ................................................... 134

Audio Panel Fail-Safe Operation ................................. 134

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

SECTION 5 FLIGHT MANAGEMENT

5.1 Introduction ........................................................... 135

Navigation Status Box and Data Bar ........................... 137

5.2 Using Map Displays .............................................. 138

Map Orientation ....................................................... 138

Map Range .............................................................. 140

Map Panning ............................................................ 142

Measuring Bearing and Distance ................................ 144

Topography .............................................................. 144

Map Symbols ........................................................... 147

Airways ................................................................... 151

Additional Navigation Map Items ............................... 153

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

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

Non-Airport Waypoints .............................................. 163

5.4 Airspaces ................................................................ 171

Nearest Airspace ...................................................... 172

Smart Airspace ......................................................... 174

5.5 Direct-to-Navigation ........................................... 175

5.6 Flight Planning ...................................................... 180

Flight Plan Views ...................................................... 183

Creating a Flight Plan ............................................... 186

Flight Plan Waypoint and Airway Modiﬁcations ........... 187

Flight Plan Operations ............................................... 195

Closest Point of FPL .................................................. 198

User-Deﬁned Holding Patterns ................................... 199

Managing Flight Plans .............................................. 202

5.7 Vertical Navigation ............................................... 212

Altitude Constraints .................................................. 214

Vertical Situation Display (VSD) .................................. 216

5.8 Procedures ............................................................. 220

Departures ............................................................... 222

Arrivals ................................................................... 225

Approaches ............................................................. 228

5.9 Trip Planning .......................................................... 238

Trip Planning ............................................................ 238

5.10 Abnormal Operation ............................................. 242

SECTION 6 HAZARD AVOIDANCE

6.1 Data Link Weather ................................................ 246

Activating Data Link Weather Services ........................ 247

Weather Product Age ................................................ 250

Displaying Data Link Weather Products ....................... 254

Connext Data Requests ............................................. 263

Weather Product Overview ........................................ 266

FIS-B Weather Status................................................. 300

Abnormal Operations for Garmin Connext Weather ..... 301

6.2 Airborne Color Weather Radar ............................ 303

System Description ................................................... 303

Principles of Airborne Weather Radar .......................... 303

Safe Operating Distance ............................................ 308

Basic Antenna Tilt Setup ............................................ 309

Weather Mapping and Interpretation ......................... 311

Ground Mapping and Interpretation ........................... 324

Additional Weather Radar Displays ............................. 324

System Status ........................................................... 327

6.3 Stormscope Lightning Detection System ........... 329

Using the Stormscope Page ....................................... 329

Setting Up Stormscope on the Navigation Map ........... 331

6.4 Terrain Displays ..................................................... 333

Relative Terrain Symbology ........................................ 334

Terrain Page ............................................................. 339

Wire Obstacle Information and Alerting ...................... 340

Vertical Situation Display (VSD) Terrain ....................... 340

Garmin G1000 NXi Pilot’s Guide for the Beechcraft G58

190-02181-01 Rev. Axii

TABLE OF CONTENTS

Terrain-SVT and TAWS-B Alerting Displays ................... 343

Forward Looking Terrain Avoidance ............................ 346

Additional TAWS-B Alerting ....................................... 346

Inhibiting Alerting ..................................................... 349

System Status ........................................................... 349

6.5 Trafﬁc Information Service (TIS) .......................... 352

Displaying Trafﬁc Data .............................................. 353

Trafﬁc Map Page ....................................................... 354

TIS Alerts ................................................................. 355

System Status ........................................................... 357

6.6 TAS Trafﬁc ............................................................... 359

TAS Theory of Operation ............................................ 359

TAS Alerts ................................................................ 363

System Test .............................................................. 364

Operation ................................................................ 365

6.7 ADS-B Trafﬁc .......................................................... 371

ADS-B System Overview ............................................ 371

Conﬂict Situational Awareness & Alerting (CSA) .......... 373

Airborne and Surface Applications .............................. 374

Trafﬁc Description ..................................................... 375

Operation ................................................................ 375

ADS-B System Status ................................................ 381

SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM

7.1 AFCS Overview ...................................................... 385

AFCS Controls on the MFD ........................................ 386

Additional AFCS Controls .......................................... 387

Basic Autopilot Operation .......................................... 388

7.2 Flight Director Operation ..................................... 389

Activating the Flight Director ..................................... 389

AFCS Status Box ....................................................... 390

Flight Director Modes ................................................ 391

Command Bars ......................................................... 391

7.3 AFCS Modes ........................................................... 392

Vertical Modes ......................................................... 392

Lateral Modes .......................................................... 398

Combination Modes (VNV, APR, NAV, GA) ................... 402

7.4 Autopilot and Yaw Damper Operation ............... 414

Flight Control ........................................................... 414

Engagement ............................................................. 415

Control Wheel Steering ............................................. 415

Disengagement ........................................................ 416

7.5 AFCS Annunciations and Alerts ........................... 417

AFCS CAS Messages ................................................. 417

Overspeed Protection ................................................ 418

Underspeed Protection .............................................. 418

SECTION 8 ADDITIONAL FEATURES

8.1 SafeTaxi .................................................................. 422

8.2 Charts ..................................................................... 424

ChartView ................................................................ 425

FliteCharts ............................................................... 433

IFR/VFR Charts ......................................................... 438

8.3 Airport Directory ................................................... 441

8.4 SurfaceWatch ......................................................... 442

Information Box ....................................................... 442

Alerts ...................................................................... 443

Surfacewatch Setup .................................................. 446

8.5 Database Cycle Number and Revisions .............. 448

Cycle Number and Revision ....................................... 448

8.6 SiriusXM Radio Entertainment ............................ 450

Satellite Radio Services ............................................ 450

Using SiriusXM Radio ................................................ 451

8.7 Satellite Telephone and SMS Messaging ........... 454

Registering with Garmin Connext .............................. 454

Disable/Enable Iridium Transceiver.............................. 454

Telephone Communication ........................................ 455

Text Messaging (SMS) ............................................... 462

8.8 Connext Setup ....................................................... 474

8.9 Flight Data Logging .............................................. 476

8.10 Electronic Checklists ............................................. 478

8.11 Electronic Stability & Protection (ESP

™

) ............ 480

Roll Engagement ...................................................... 480

Pitch Engagement..................................................... 482

High Airspeed Protection ........................................... 483

Low AirSpeed Protection .......................................... 483

Stall Protection ......................................................... 484

8.12 Abnormal Operation ............................................. 485

SiriusXM Data Link Receiver Troubleshooting .............. 485

190-02181-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Beechcraft G58

xiii

TABLE OF CONTENTS

APPENDICES

Annunciations and Alerts ............................................... 487

CAS Message Prioritization ........................................ 488

CAS Annunciations ................................................... 489

Audio Alerting System Test ........................................ 490

System Message Advisories ....................................... 490

Loading Updated Databases ...................................... 501

Database Deletion Feature ....................................... 512

Magnetic Field Variation Database Update .................. 513

Aviation Terms and Acronyms ........................................ 515

Frequently Asked Questions .......................................... 525

Map Symbols ................................................................... 529

INDEX

Garmin G1000 NXi Pilot’s Guide for the Beechcraft G58

190-02181-01 Rev. Axiv

TABLE OF CONTENTS

Blank Page

190-02181-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Beechcraft G58

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 Beechcraft

G58 Baron. 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 1050

(1) – The GDU 1050 is conﬁgured as a Primary Flight Display (PFD). The display communicates

with the Multi Function Display (MFD) and with the #1 Integrated Avionics Unit (IAU) through a High-Speed

Data Bus (HSDB) Ethernet connection.

•

GDU 1055

(1) – The GDU 1055 is conﬁgured as a Multi Function Display (MFD. The display communicates

with the PFD and with the #2 Integrated Avionics Unit (IAU) through an HSDB Ethernet connection.

•

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. The IAUs are not paired together and do not communicate with each other

directly.

•

GRS 77 / 79

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

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

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

information, and with the Air Data Computer to obtain air data. The AHRS communicates with both IAUs to

obtain GPS information.

•

GMU 44

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

processing to determine aircraft magnetic heading. The Magnetometer receives communicates with and

receives power directly from the AHRS using an RS-485 digital interface.

•

GDC 72 / 74A

(1) – The GDC Air Data Computer (ADC) processes data from the pitot/static system as well

as the Outside Air Temperature (OAT) probe. This unit provides pressure altitude, airspeed, vertical speed

and OAT information to the system, and it communicates with the IAUs, PFD, MFD, and the AHRS, using an

ARINC 429 digital interface (it also interfaces directly with the Air Temperature Probe). The ADC is designed

to operate in Reduced Vertical Separation Minimum (RVSM) airspace.

•

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.

190-02181-01 Rev. A

Garmin G1000 NXi Pilot’s Guide for the Beechcraft G58

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

2

SYSTEM OVERVIEW

•

GTX 335R/345R/33ES

(1) – 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

(4), and

GSM 86/85

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

pitch trim. These units interface with each IAU.

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

to the mechanical ﬂight-control surface linkage.

•

GWX 68 / GWX 75

(1) – The GWX 68 Airborne Weather Radar provides airborne weather and ground

mapped radar data to the MFD, through the GDL 69A, via HSDB connection. The GWX 75 is capable of

providing this data to both the PFD and MFD.

•

GDL 69A / GDL 69A SXM

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

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

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

Satellite Radio are required to enable services.

•

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, AHRS, ADC, 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.

•

GTS 800/820

(Optional) – The GTS 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.

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 800/820

Trafﬁc Advisory System

•

WX 500

Stormscope Lightning Sensor

•KN63DME

•SkywatchTrafcAdvisorySystem

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