Garmin G1000 NXi - Beechcraft Baron G58 Reference guide

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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
Copyright © 2017-2018 Garmin Ltd. or its subsidiaries. All rights reserved.
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
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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Garmin G1000 NXi - Beechcraft Baron G58 Reference guide

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