Garmin G1000 NXi - Beechcraft Bonanza A36/G36 Reference guide

Type
Reference guide
190-02179-01
Revision B
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
Contact Garmin Product Support at: www.flygarmin.com
For warranty information refer to: www.flygarmin.com
Beechcraft G36
Beechcraft G36 Series
System Software Version 3185.04 or later
Pilot’s Guide
®
G1000
®
Pilot’s Guide
SYSTEM OVERVIEW
FLIGHT INSTRUMENTS
EIS
AUDIO PANEL & CNS
FLIGHT MANAGEMENT
HAZARD AVOIDANCE
AFCS
ADDITIONAL FEATURES
APPENDICES
INDEX
190-02179-01 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Beechcraft G36
Copyright © 2017-2019 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 3185.04 or later for the G1000 NXi Beechcraft G36 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
Contact Garmin Product Support or view warranty information at www.flygarmin.com.
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or
stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission
to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium
to be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete
text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision
hereto is strictly prohibited.
Garmin
®
G1000
®
NXi, FliteCharts
®
, and SafeTaxi
®
are registered trademarks of Garmin International, Inc. or its subsidiaries.
Garmin ESP
, Garmin SVT
, SurfaceWatch
, Connext
, and WireAware
are trademarks of Garmin International, Inc. or its
subsidiaries. These trademarks may not be used without the express permission of Garmin.
Skywatch
®
and Stormscope
®
are registered trademarks of L-3 Communications. Ryan
®
, TCAD
®
and Avidyne
®
are registered
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®
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®
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
®
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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 G36
190-02179-01 Rev. B
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.
190-02179-01 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Beechcraft G36
v
WARNINGS, CAUTIONS, AND NOTES
WARNING: Do not use terrain avoidance displays as the sole source of information for maintaining
separation from terrain and obstacles. Garmin obtains terrain and obstacle data from third party sources
and cannot independently verify the accuracy of the information.
WARNING: Always refer to current aeronautical charts and NOTAMs for verification of displayed aeronautical
information. Displayed aeronautical data may not incorporate the latest NOTAM information.
WARNING: Do not use geometric altitude for compliance with air traffic control altitude requirements. The
primary barometric altimeter must be used for compliance with all air traffic control altitude regulations,
requirements, instructions, and clearances.
WARNING: Do not use basemap information (land and water data) as the sole means of navigation.
Basemap data is intended only to supplement other approved navigation data sources and should be
considered only an aid to enhance situational awareness.
WARNING: Do not rely solely upon the display of traffic information to accurately depict all of the traffic
within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information
from aircraft or ground stations, traffic may be present that is not represented on the display.
WARNING: Do not use data link weather information for maneuvering in, near, or around areas of
hazardous weather. Information contained within data link weather products may not accurately depict
current weather conditions.
WARNING: Do not use the indicated data link weather product age to determine the age of the weather
information shown by the data link weather product. Due to time delays inherent in gathering and processing
weather data for data link transmission, the weather information shown by the data link weather product
may be older than the indicated weather product age.
WARNING: Do not rely on the displayed minimum safe altitude (MSAs) as the sole source of obstacle
and terrain avoidance information. Always refer to current aeronautical charts for appropriate minimum
clearance altitudes.
WARNING: Do not operate this equipment without first obtaining qualified instruction.
WARNING
:
Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a
system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that
may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned
in error as displayed.
Garmin G1000 NXi Pilot’s Guide for the Beechcraft G36
190-02179-01 Rev. Bvi
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 solely upon the display of traffic information for collision avoidance maneuvering.
The traffic display does not provide collision avoidance resolution advisories and does not under any
circumstances or conditions relieve the pilot’s responsibility to see and avoid other aircraft.
WARNING
:
Do not rely 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 rely on information from a lightning detection system display as the sole basis for
hazardous weather avoidance. Range limitations and interference may cause the system to display inaccurate
or incomplete information. Refer to documentation from the lightning detection system manufacturer for
detailed information about the system.
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 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: Do not use QFE altimeter setting outside of the terminal environment for the corresponding
issuing airport to ensure adequate obstacle clearance.
190-02179-01 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Beechcraft G36
vii
WARNINGS, CAUTIONS, AND NOTES
WARNING: Do not fly QFE procedures above the Transition Altitude or when navigating to a waypoint that
contains a QNE (flight level) altitude constraint.
WARNING: Always fly a procedure that provides terrain and obstacle clearance from the reference airfield
when operating in IMC while conducting QFE procedures.
CAUTION: Do not clean display surfaces with abrasive cloths or cleaners containing ammonia. They will
harm the anti-reflective coating.
CAUTION
:
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.
CAUTION: Never disconnect power to the system when loading a database. Power interruption during the
database loading process could result in maintenance being required to reboot the system.
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: The navigation databases used in Garmin navigation systems contain Special Procedures. Prior
to flying these procedures, pilots must have specific FAA authorization, training, and possession of the
corresponding current, and legitimately-sourced chart (approach plate, etc.). Inclusion of the Special
Procedure in the navigation database DOES NOT imply specific FAA authorization to fly the procedure.
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: The nose of the ‘own ship’ symbol represents the location of the aircraft. The center of any traffic
symbol represents the location of that traffic. The traffic and own ship symbols are an abstract representation
and do not reflect the physical extent of the aircraft/traffic, and should not replace other methods for
identifying traffic.
NOTE: ESP is designed to discourage exceeding the normal flight envelope. It is not designed or capable
of performing the necessary recovery procedures due to encounters with adverse flight conditions and
environments.
Garmin G1000 NXi Pilot’s Guide for the Beechcraft G36
190-02179-01 Rev. Bviii
WARNINGS, CAUTIONS, AND NOTES
NOTE: All visual depictions contained within this document, including screen images of the system panel
and displays, are subject to change and may not reflect the most current system and aviation databases.
Depictions of equipment may differ slightly from the actual equipment.
NOTE: The United States government operates the Global Positioning System and is solely responsible for
its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and
performance of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation
AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or
misinterpreted and, therefore, become unsafe.
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.
190-02179-01 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Beechcraft G36
ix
WARNINGS, CAUTIONS, AND NOTES
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.
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: Operate G1000NXi system power through at least one cycle in a period of four days of continuous
operation to avoid an autonomous system reboot.
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.
Garmin G1000 NXi Pilot’s Guide for the Beechcraft G36
190-02179-01 Rev. Bx
WARNINGS, CAUTIONS, AND NOTES
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: Intruder aircraft at or below 500 ft. AGL may not appear on the Garmin SVT display or may appear
as a partial symbol.
NOTE: The navigation databases used in Garmin navigation systems contain Special Procedures. Prior
to flying these procedures, pilots must have specific FAA authorization, training, and possession of the
corresponding current, and legitimately-sourced chart (approach plate, etc.). Inclusion of the Special
Procedure in the navigation database DOES NOT imply specific FAA authorization to fly the procedure.
190-02179-01 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Beechcraft G36
SOFTWARE LICENSE AGREEMENT
xi
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 G36
190-02179-01 Rev. B
SOFTWARE LICENSE AGREEMENT
xii
Blank Page
190-02179-01 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Beechcraft G36
xiii
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-02179-00 A
B
1/5/17
5/18/17
i – I-6
i – I-6
Initial Release for GDU 20.05
Updated SurfaceWatch Information
Clerical
190-02179-01 A 6/1/18 i – I-6 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
B 10/29/19 i – I-6 Production release for the following updates:
Fixed clerical errors
Added QFE Constraints description
Revised Approaches description
Added Transition to Approach description
Revised Temperature Compensation description
Clarified Enhanced AFCS, ESP, and USP
Added CAS Messages
Garmin G1000 NXi Pilot’s Guide for the Beechcraft G36
190-02179-01 Rev. Bxiv
REVISION INFORMATION
Blank Page
190-02179-01 Rev. B
Garmin G1000 NXi Pilot’s Guide for the Beechcraft G36
xv
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 Application ................................................... 8
Normal Operation ...............................................................9
Reversionary Mode .............................................................9
System Annunciations .......................................................10
System Status....................................................................12
AHRS Operation ................................................................13
GPS Receiver Operation ....................................................14
1.4 Accessing System Functionality .........................19
Softkey Function ...............................................................19
Menus ............................................................................... 23
MFD Page Groups .............................................................24
Split Screen Functionality .................................................. 26
System Settings .................................................................27
System Utilities .................................................................35
1.5 Display Backlighting ..........................................39
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ..............................................44
Attitude Indicator ..............................................................44
Airspeed Indicator ............................................................. 45
Altimeter ........................................................................... 47
Vertical Speed Indicator (VSI) ............................................ 51
Vertical Deviation ..............................................................51
Horizontal Situation Indicator (HSI) ...................................54
Course Deviation Indicator (CDI) .......................................58
2.2 Supplemental Flight Data ..................................65
Generic Timer ....................................................................65
Temperature Displays ........................................................ 65
Wind Data ......................................................................... 66
2.3 Synthetic Vision Technology (SVT) .....................67
SVT Operation ................................................................... 68
SVT Features .....................................................................69
Field of View .....................................................................77
2.4 PFD Annunciations and Alerting Functions ........79
Altitude Alerting ................................................................79
Baro Transition Alerts ........................................................79
BARO QFE Indications .......................................................80
Low Altitude Annunciation ................................................ 80
Marker Beacon Annunciations ..........................................81
Minimum Altitude Alerting ................................................81
2.5 Abnormal Operations .........................................83
Abnormal GPS Conditions .................................................83
Unusual Attitudes .............................................................84
SVT Unusual Attitudes ......................................................85
SECTION 3 ENGINE INDICATION SYSTEM
3.1 Engine Display ...................................................88
Engine Softkeys ................................................................. 90
Exhaust Gas Temperature ..................................................90
Cylinder Head Temperature ...............................................90
Lean Engine Display .......................................................... 91
Fuel Calculations ...............................................................92
3.2 EIS Display (Reversionary Mode) .........................93
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview ............................................................ 95
PFD Controls and Frequency Display .................................96
Audio Panel Controls ........................................................98
4.2 COM Operation ................................................102
COM Tuning Boxes .......................................................... 102
COM Transceiver Manual Tuning ..................................... 103
Auto-Tuning the COM Frequency ....................................103
Frequency Spacing .........................................................106
4.3 NAV Operation .................................................107
NAV Tuning Boxes ...........................................................107
NAV Radio Selection and Activation................................108
NAV Receiver Manual Tuning .......................................... 108
Auto-Tuning a NAV Frequency from the MFD .................108
Marker Beacon Receiver .................................................111
DME Tuning .....................................................................112
4.4 Mode S Transponder ........................................113
Transponder Controls ......................................................113
Transponder Mode Selection ........................................... 114
Entering a Transponder Code ..........................................116
IDENT Function ...............................................................116
Flight ID Reporting .......................................................... 117
4.5 Additional Audio Panel Functions ....................118
Power Application ...........................................................118
Mono/Stereo Headsets .................................................... 118
Speaker (GMA 1347) .......................................................118
Speaker (GMA 1360) .......................................................118
Intercom (GMA 1347) .....................................................118
Intercom (GMA 1360) .....................................................120
Split-Com Mode (GMA 1360) .........................................122
Blue-Select Mode (GMA 1360) .......................................122
3D Audio (GMA 1360).....................................................123
Bluetooth
®
(GMA 1360) ..................................................124
Clearance Recorder and Player .......................................125
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TABLE OF CONTENTS
Telephone and Entertainment Inputs ..............................125
4.6 Audio Panels Preflight Procedure ....................127
4.7 Abnormal Operation ........................................128
Stuck Microphone ...........................................................128
COM Tuning Failure ......................................................... 128
Audio Panel Fail-Safe Operation ......................................128
Reversionary Mode .........................................................128
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction .....................................................129
Navigation Status Box and Data Bar ............................... 131
5.2 Using Map Displays ..........................................133
Map Orientation .............................................................133
Map Range .....................................................................135
Map Panning ...................................................................137
Measuring Bearing and Distance ....................................139
Topography .....................................................................140
Map Symbols ..................................................................142
Airways ...........................................................................146
Additional Navigation Map Items ...................................148
5.3 Waypoints ........................................................151
Airports ...........................................................................152
Non-Airport Waypoints ...................................................158
5.4 Airspaces .......................................................... 166
Nearest Airspace .............................................................167
Smart Airspace ................................................................169
5.5 Direct-to Navigation ........................................170
5.6 Flight Planning .................................................174
Flight Plan Views ............................................................. 177
Creating a Flight Plan .....................................................179
Flight Plan Waypoint and Airway Modifications ..............181
Flight Plan Operations ....................................................188
Closest Point of FPL.........................................................192
User-Defined Holding Patterns ........................................193
Managing Flight Plans ....................................................196
5.7 Vertical Navigation ..........................................205
Constraints ......................................................................206
Vertical Navigation Direct To ........................................... 210
Vertical Situation Display (VSD) ......................................211
5.8 Procedures .......................................................215
Departures ......................................................................216
Arrivals ............................................................................219
Approaches .....................................................................222
5.9 Trip Planning ....................................................233
Trip Planning ...................................................................233
5.10 Abnormal Operation ........................................237
Dead Reckoning Mode ....................................................237
SECTION 6 HAZARD AVOIDANCE
6.1 Data Link Weather............................................240
Activating Data Link Weather Services ............................ 241
Weather Product Age ......................................................244
Displaying Data Link Weather Products ..........................248
Connext Data Requests ...................................................257
Weather Product Overview .............................................260
FIS-B Weather Status .......................................................293
Abnormal Operations for Garmin Connext Weather .......294
6.2 Stormscope Lightning Detection System ......... 296
Using the Stormscope Page .............................................296
Setting Up Stormscope on the Navigation Map ..............298
6.3 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 ................................313
Additional TAWS-B Alerting ............................................313
Inhibiting Alerting ...........................................................316
System Status..................................................................316
6.4 Traffic Information Service (TIS) ......................319
Displaying Traffic Data ....................................................320
‘Map - Traffic Map’ Page .................................................321
TIS Alerts ......................................................................... 322
System Status..................................................................324
6.5 TAS Traffic .........................................................326
TAS Theory of Operation .................................................326
TAS Alerts ........................................................................330
System Test .....................................................................331
Operation ........................................................................ 332
6.6 ADS-B Traffic ....................................................338
ADS-B System Overview .................................................338
Conflict Situational Awareness & Alerting (CSA) ............. 340
Airborne and Surface Applications .................................. 341
Traffic Description ...........................................................342
Operation ........................................................................ 342
ADS-B System Status.......................................................348
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Overview .................................................351
AFCS Controls on the MFD ..............................................352
Additional AFCS Controls ................................................353
Basic Autopilot Operation ...............................................354
7.2 Flight Director Operation ................................. 355
Activating the Flight Director ..........................................355
AFCS Status Box..............................................................356
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TABLE OF CONTENTS
Flight Director Modes......................................................357
Command Bars ...............................................................357
7.3 AFCS Modes .....................................................358
Vertical Modes ................................................................358
Lateral Modes .................................................................364
7.4 Autopilot and Yaw Damper Operation .............380
Flight Control ..................................................................380
Engagement ....................................................................380
Control Wheel Steering ...................................................381
Disengagement ............................................................... 381
7.5 AFCS Annunciations and Alerts ........................ 383
AFCS CAS Messages .......................................................383
Overspeed Protection ...................................................... 384
Underspeed Protection ....................................................384
7.6 Abnormal Operation ........................................387
Suspected Autopilot Malfunction ....................................387
Level Mode .....................................................................387
Reversionary Mode ........................................................388
SECTION 8 ADDITIONAL FEATURES
8.1 SafeTaxi ............................................................ 390
8.2 Charts ............................................................... 392
ChartView .......................................................................393
FliteCharts .......................................................................401
IFR/VFR Charts ................................................................405
8.3 Airport Directory .............................................. 408
8.4 SurfaceWatch ...................................................409
Information Box ..............................................................409
Alerts ..............................................................................410
Surfacewatch Setup ........................................................412
8.5 Database Cycle Number And Revisions ...........415
Cycle Number and Revision ............................................415
8.6 SiriusXM Radio Entertainment .........................417
Activating SiriusXM Satellite Radio Services ...................417
Using SiriusXM Radio ......................................................418
8.7 Satellite Telephone and SMS Messaging .........421
Registering with Garmin Connext ..................................421
Disable/Enable Iridium Transceiver .................................. 421
Telephone Communication..............................................422
Text Messaging (SMS) ..................................................... 429
8.8 Flight Data Logging .........................................441
8.9 Connext Setup..................................................443
8.10 Electronic Checklists ........................................445
8.11 Electronic Stability & Protection (ESP
) ..........447
Roll Engagement .............................................................448
Pitch Engagement ........................................................... 450
High Airspeed Protection ................................................451
Low AirSpeed Protection ................................................451
8.12 Abnormal Operation ........................................452
SiriusXM Data Link Receiver Troubleshooting .................452
Annunciations and Alerts .........................................453
CAS Message Prioritization ............................................. 454
CAS Annunciations ..........................................................455
Audio Alerting System Test ..............................................457
System Message Advisories ............................................457
Database Management ............................................469
Loading Updated Databases ...........................................469
Database Deletion Feature ............................................ 481
Magnetic Field Variation Database Update .....................482
Aviation Terms and Acronyms...................................483
Frequently Asked Questions .....................................493
Map Symbols ............................................................497
Garmin G1000 NXi Pilot’s Guide for the Beechcraft G36
190-02179-01 Rev. Bxviii
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Garmin G1000 NXi - Beechcraft Bonanza A36/G36 Reference guide

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Reference guide

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