Garmin G1000 NXi - Piper PA-28-181 Archer Reference guide

Type
Reference guide

This manual is also suitable for

SYSTEM OVERVIEW
FLIGHT INSTRUMENTS
ENGINE INDICATION SYSTEM
AUDIO PANEL AND CNS
FLIGHT MANAGEMENT
HAZARD AVOIDANCE
AUTOMATIC FLIGHT CONTROL SYSTEM
ADDITIONAL FEATURES
APPENDICES
INDEX
Copyright © 2017 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 2698.04 or later for the G1000 NXi
Piper PA-28-181 Archer. Some differences in operation may be observed when comparing the
information in this manual to earlier or later software versions.
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Garmin (Europe) Ltd.
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Garmin AT, Inc.
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Salem, OR 97302, U.S.A.
Garmin Corporation
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New Taipei City, Taiwan
Contact Garmin Product Support at
www.flygarmin.com.
For warranty information refer to
www.flygarmin.com.
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted,
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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™, and Connext™ are trademarks of
Garmin International, Inc. or its subsidiaries. These trademarks may not be used without the express
permission of Garmin.
AC-U-KWIK® is a registered trademark of Penton Business Media Inc. 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
190-02130-02 Rev. A
Garmin G1000 NXi Pilot's Guide for the PA-28-181 Archer
representative has been advised of the possibility of such damages. User agrees not to sue AOPA and,
to the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action,
claims or losses related to any actual or alleged inaccuracies in the information. Some jurisdictions do
not allow the limitation or exclusion of implied warranties or liability for incidental or consequential
damages so the above limitations or exclusions may not apply to you.
AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”) expressly
disclaim all warranties with respect to the AC-U-KWIK information included in this data, express or
implied, including, but not limited to, the implied warranties of merchantability and fitness for a
particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant
or make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue
AC-U-KWIK Organizations and, to the maximum extent allowed by law, to release and hold harmless
AC-U-KWIK Organizations from any cause of action, claims or losses related to any actual or alleged
inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some
jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or
consequential damages so the above limitations or exclusions may not apply to licensee.
Printed in the U.S.A.
Garmin G1000 NXi Pilot's Guide for the PA-28-181 Archer 190-02130-02 Rev. A
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:
The displayed minimum safe altitude (MSAs) are only advisory in nature and
should not be relied upon as the sole source of obstacle and terrain avoidance information.
Always refer to current aeronautical charts for appropriate minimum clearance altitudes.
WARNING:
Always obtain qualified instruction prior to operational use of this equipment.
WARNING:
Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84
WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown
map reference datum that may be incompatible with the map reference datum used by GPS
(known as WGS84) and may be positioned in error as displayed.
WARNING, CAUTIONS, AND NOTES
190-02130-02 Rev. A Garmin G1000 NXi Pilot's Guide for the PA-28-181 Archer i
WARNING: When using the autopilot to fly 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: Because of variation in the earth’s magnetic field, do not rely on the accuracy of
attitude and heading indications in the following geographic areas: 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:
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:
Intruder aircraft at or below 500 ft. AGL may not appear on the Garmin SVT
display or may appear as a partial symbol.
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 a QFE altimeter setting with this system. System functions will not
operate properly with a QFE altimeter setting. Use only a QNH altimeter setting for height
above mean sea level, or the standard pressure setting, as applicable.
CAUTION:
Do not clean display surfaces with abrasive cloths or cleaners containing
ammonia. They will harm the anti-reflective coating.
CAUTION:
Repairs should only be made by an authorized Garmin service center.
Unauthorized repairs or modifications could void both the warranty and affect the
airworthiness of the aircraft.
WARNING, CAUTIONS, AND NOTES
ii Garmin G1000 NXi Pilot's Guide for the PA-28-181 Archer 190-02130-02 Rev. A
NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR)
information. Always confirm TFR information through official sources such as Flight Service
Stations or Air Traffic Control.
NOTE: All visual depictions contained within this document, including screen images of the
system panel and displays, are subject to change and may not reflect the most current system
and aviation databases. Depictions of equipment may differ slightly from the actual
equipment.
NOTE: The United States government operates the Global Positioning System and is solely
responsible for its accuracy and maintenance. The GPS system is subject to changes which
could affect the accuracy and performance of all GPS equipment. Portions of the system
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.
WARNING, CAUTIONS, AND NOTES
190-02130-02 Rev. A Garmin G1000 NXi Pilot's Guide for the PA-28-181 Archer iii
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:
The system supports approval of AC 120-76C Hardware Class 3, Software Type B
Electronic Flight Bag (EFB) electronic aeronautical chart applications. Possible additional
requirements may make a secondary source (traditional paper or additional electronic display)
necessary onboard the aircraft. If the secondary source is a Portable Electronic Device (PED),
its use must be consistent with guidance in AC 120-76C.
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.
WARNING, CAUTIONS, AND NOTES
iv Garmin G1000 NXi Pilot's Guide for the PA-28-181 Archer 190-02130-02 Rev. A
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: 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.
WARNING, CAUTIONS, AND NOTES
190-02130-02 Rev. A Garmin G1000 NXi Pilot's Guide for the PA-28-181 Archer v
WARNING, CAUTIONS, AND NOTES
vi Garmin G1000 NXi Pilot's Guide for the PA-28-181 Archer 190-02130-02 Rev. A
BLANK PAGE
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.
SOFTWARE LICENSE AGREEMENT
190-02130-02 Rev. A Garmin G1000 NXi Pilot's Guide for the PA-28-181 Archer vii
SOFTWARE LICENSE AGREEMENT
viii Garmin G1000 NXi Pilot's Guide for the PA-28-181 Archer 190-02130-02 Rev. A
BLANK PAGE
Record of Revisions
Part Number Revision Date Page
Range
Description
190–02130-00 A
B
C
10/11/16
10/12/16
10/31/16
All
All
All
Initial Release for GDU 20.02
Updated to fix clerical errors
Updated:
Bluetooth information
Connext information
SiriusXM information
SiriusXM Weather symbology
190–02130–01 A
B
4/20/17
4/24/17
All
All
Initial Release for GDU 20.10
Updated to fix clerical errors
190–02130-02 A 12/13/17 All Initial Release for GDU 20.80
RECORD OF REVISIONS
190-02130-02 Rev. A Garmin G1000 NXi Pilot's Guide for the PA-28-181 Archer ix
RECORD OF REVISIONS
x Garmin G1000 NXi Pilot's Guide for the PA-28-181 Archer 190-02130-02 Rev. A
BLANK PAGE
SECTION 1 SYSTEM OVERVIEW
1.1
System Description............................ 1
Line Replaceable Units (LRU)..................... 1
1.2
System Controls................................. 4
PFD/MFD Controls ................................... 5
Secure Digital Cards.................................. 7
1.3
System Operation.............................. 9
System Power-up...................................... 9
Normal Operation..................................... 10
Reversionary Mode................................... 10
System Annunciations............................... 11
System Status........................................... 13
ADAHRS Operation................................... 13
GPS Receiver Operation............................ 15
1.4
Accessing System Functionality........ 21
Softkey Function....................................... 21
Menus...................................................... 28
MFD Page Groups..................................... 29
Split Screen Functionality.......................... 32
System Settings........................................ 34
System Utilities......................................... 44
1.5
Display Backlighting.......................... 49
SECTION 2 FLIGHT INSTRUMENTS
2.1
Overview
............................................ 51
2.2
Flight Instruments.............................. 54
Attitude Indicator..................................... 54
Airspeed Indicator..................................... 56
Altimeter.................................................. 57
Vertical Speed Indicator (VSI)..................... 61
Vertical Deviation...................................... 61
Vertical Navigation (VNV) Indications......... 64
Horizontal Situation Indicator (HSI)............ 66
Course Deviation Indicator (CDI)............... 69
Turn Rate Indicator .................................. 70
GPS CDI Scaling (FMS Navigation Source). 72
OBS Mode................................................ 74
Bearing Pointers and Information
Windows.................................................. 75
DME Information Window........................ 77
2.3
Supplemental Flight Data.................. 78
Generic Timer........................................... 78
Temperature Displays................................ 78
Wind Data................................................ 79
2.4
PFD Annunciations and Alerting
Functions............................................ 80
Altitude Alerting....................................... 80
Low Altitude Annunciation....................... 80
Marker Beacon Annunciations.................. 80
Minimum Descent Altitude/Decision
Height Alerting......................................... 81
2.5
Garmin Synthetic Vision Technology
(SVT).................................................... 83
Garmin SVT (Synthetic Vision Technology). 83
SVT Operation.......................................... 84
SVT Features............................................. 86
2.6
Abnormal Operations........................ 96
Abnormal GPS Conditions........................ 96
SVT Troubleshooting................................. 97
SVT in Reversionary Mode......................... 97
Unusual Attitudes..................................... 97
SVT Unusual Attitudes.............................. 98
SECTION 3 ENGINE INDICATION SYSTEM
3.1
Engine Display
....................................100
3.2
Engine Page........................................102
Fuel Calculations....................................... 103
Carbon Monoxide Detector (Optional)...... 104
3.3
EIS Display (Reversionary Mode)......105
SECTION 4 AUDIO PANEL AND CNS
4.1
Overview
............................................107
Overview.................................................. 107
4.2
COM Operation..................................113
COM Tuning Boxes................................... 113
COM Transceiver Manual Tuning............... 114
Auto-Tuning the COM Frequency.............. 114
Auto-tuning from the MFD....................... 115
Frequency Spacing.................................... 118
4.3
NAV Operation...................................120
NAV Tuning Boxes..................................... 120
NAV Radio Selection and Activation.......... 121
NAV Receiver Manual Tuning.................... 121
Auto-Tuning a NAV Frequency from the
MFD......................................................... 122
Auto-Tuning NAV Frequencies on
Approach Activation................................. 124
TABLE OF CONTENTS
190-02130-02 Rev. A Garmin G1000 NXi Pilot's Guide for the PA-28-181 Archer xi
Marker Beacon Receiver (Optional)........... 125
ADF/DME Tuning...................................... 125
ADF Tuning............................................... 126
Selecting ADF Receiver Mode.................... 127
DME Tuning.............................................. 128
4.4
Mode S Transponder..........................130
Transponder Controls................................ 130
Transponder Mode Selection..................... 131
Entering a Transponder Code.................... 133
Ident Function.......................................... 134
4.5
Additional Audio Panel Functions....135
Power-Up................................................. 135
Mono/Stereo Headsets.............................. 135
Speaker.................................................... 135
Intercom................................................... 135
Clearance Recorder and Player.................. 140
Split-COM Operation................................ 140
3D Audio.................................................. 140
Entertainment Inputs................................ 142
Bluetooth®............................................... 143
4.6
Audio Panel Preflight Procedure.......144
4.7
Abnormal Operation..........................145
Stuck Microphone.................................... 145
COM Tuning Failure.................................. 145
Audio Panel Fail-Safe Operation................ 145
Reversionary Mode................................... 145
SECTION 5 FLIGHT MANAGEMENT
5.1
Introduction
........................................147
Navigation Status Box and Data Bar.......... 149
5.2
Using Map Displays............................151
Map Orientation....................................... 151
Map Range............................................... 153
Map Panning............................................ 155
Measuring Bearing and Distance............... 158
Topography.............................................. 159
Map Symbols............................................ 161
Airways.................................................... 166
Additional Navigation Map Items.............. 168
5.3
Waypoints...........................................172
Airports.................................................... 173
Intersections............................................. 180
NDB.......................................................... 182
VOR.......................................................... 184
VRP.......................................................... 187
User Waypoints......................................... 188
5.4
Airspaces.............................................195
5.5
Direct-To-Navigation..........................200
5.6
Flight Planning...................................206
Flight Plan Creation.................................. 207
Flight Plan Import/Export........................... 211
Adding Airways to a Flight Plan................ 221
Adding Procedures to a Stored Flight Plan. 223
Active Flight Plan...................................... 233
Along Track Offsets................................... 236
Parallel Track............................................. 237
Flight Plan Views....................................... 240
Closest Point of FPL.................................. 243
User-Defined Holding Patterns.................. 243
5.7
Vertical Navigation............................249
Altitude Constraints.................................. 251
Vertical Situation Display (VSD)................. 254
5.8
Procedures..........................................259
Departures................................................ 261
Arrivals .................................................... 263
Approaches.............................................. 265
5.9
Weight Planning.................................277
Weight Warning Conditions...................... 277
5.10
Trip Planning.......................................280
Trip Planning............................................. 280
5.11
Abnormal Operation..........................284
SECTION 6 HAZARD AVOIDANCE
6.1
Overview
............................................287
6.2
Data Link Weather.............................288
Activating Data Link Weather Services....... 288
Weather Product Age............................... 290
Displaying Data Link Weather Products..... 292
Weather Data Link (XM) Page Softkeys..... 294
Weather Product Overview....................... 303
FIS-B Weather Status................................ 338
6.3
Terrain Displays..................................340
Relative Terrain Symbology........................ 341
Terrain Page.............................................. 345
Wire Obstacle Information and Alerting.... 346
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xii Garmin G1000 NXi Pilot's Guide for the PA-28-181 Archer 190-02130-02 Rev. A
Vertical Situation Display (VSD) Terrain...... 347
Terrain-SVT and TAWS-B Alerting Displays. 350
Forward Looking Terrain Avoidance........... 352
Inhibiting FLTA Alerting............................. 353
Additional TAWS-B Alerting...................... 354
System Status........................................... 357
6.4
Traffic Information Service (TIS)........360
Traffic Information Service (TIS)................. 360
Displaying Traffic Data.............................. 361
Traffic Map Page....................................... 363
TIS Alerts.................................................. 364
System Status........................................... 366
6.5
TAS Traffic...........................................369
Theory of Operation................................. 369
Traffic Map Page....................................... 373
System Test............................................... 374
Operation................................................. 376
System Status........................................... 380
6.6
ADS-B Traffic.......................................382
ADS-B System Overview............................ 382
ADS-B with TAS/TCAS I............................. 384
Conflict Situational Awareness and
Alerting.................................................... 384
Airborne and Surface Applications............ 387
Traffic Description..................................... 388
Operation................................................. 389
ADS-B System Status................................ 394
SECTION 7 AUTOMATIC FLIGHT CONTROL
SYSTEM
7.1
Overview
............................................399
AFCS Control Unit.................................... 399
Additional AFCS Controls......................... 400
Basic Autopilot Operation......................... 401
7.2
Flight Director Operation..................402
AFCS Status Box....................................... 402
Flight Director Modes............................... 403
Command Bars......................................... 403
7.3
AFCS Modes........................................405
Vertical Modes.......................................... 405
Pitch Hold Mode....................................... 406
Selected Altitude Capture Mode (ALTS)..... 407
Altitude Hold Mode (ALT).......................... 408
Vertical Speed Mode (VS).......................... 409
Flight Level Change Mode (FLC)................ 411
Lateral Modes........................................... 412
Roll Hold Mode (ROL)............................... 413
Heading Select Mode (HDG)..................... 414
Navigation Modes (FMS, VOR, LOC).......... 415
Combination Modes (VNV, APR, NAV, GA) 416
Vertical Navigation Modes (VPTH, ALTV).... 418
Vertical Path Tracking Mode...................... 419
VNV Target Altitude Capture Mode (ALTV) 422
Glidepath Mode (GP)................................ 423
Glideslope Mode (GS)............................... 425
Approach Modes (FMS, VAPP, LOC).......... 427
Backcourse Mode (BC).............................. 428
Takeoff (TO) and Go Around (GA) Modes.. 429
7.4
Autopilot and Yaw Damper
Operation...........................................431
Pitch Axis and Trim.................................... 431
Roll Axis.................................................... 431
Flight Control........................................... 431
Engagement............................................. 431
Control Wheel Steering............................ 432
Disengagement........................................ 432
7.5
AFCS Annunciations and Alerts........433
AFCS Alerts.............................................. 433
Overspeed Protection................................ 434
Altitude Critical Modes (ALT, GS, GP, TO,
GA, FLC)................................................... 434
Non Altitude Critical Modes (VS, VNAV,
IAS).......................................................... 435
7.6
Abnormal Operation..........................437
SECTION 8 ADDITIONAL FEATURES
8.1
Overview
............................................439
8.2
SafeTaxi...............................................441
8.3
Charts..................................................443
Charts...................................................... 443
ChartView................................................ 444
Chart Options........................................... 451
FliteCharts................................................ 456
Airport Directory....................................... 457
IFR/VFR Charts.......................................... 458
TABLE OF CONTENTS
190-02130-02 Rev. A Garmin G1000 NXi Pilot's Guide for the PA-28-181 Archer xiii
8.4
Database Cycle Number and
Revisions.............................................460
8.5
SiriusXM Radio Entertainment..........462
Using SiriusXM Radio................................ 463
Active Channel and Channel List............... 463
Category.................................................. 464
Presets...................................................... 464
8.6
Flight Data Logging...........................466
8.7
Connext Setup....................................469
8.8
WiFi Connections................................471
8.9
Electronic Checklists...........................476
8.10
Electronic Stability and Protection
(ESP)....................................................478
Roll Engagement...................................... 479
Pitch Engagement..................................... 480
Angle of Attack Protection........................ 481
High Airspeed Protection.......................... 482
8.11
Abnormal Operation..........................483
Unusual Attitudes..................................... 483
GDL 69A / GDL 69A SiriusXM Data Link
Receiver Troubleshooting.......................... 483
APPENDICES
Annunciations and Alerts........................ 485
CAS Message Prioritization....................... 486
CAS Messages.......................................... 487
System Message Annunciations................ 489
System Messages...................................... 490
Database Management
............................513
Loading Updated Databases..................... 513
Magnetic Field Variation Database Update 519
Aviation Terms and Acronyms
................. 521
Frequently Asked Questions....................541
Map Symbols............................................ 545
INDEX
Index
......................................................... I-1
TABLE OF CONTENTS
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Garmin G1000 NXi - Piper PA-28-181 Archer Reference guide

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