Garmin G1000 NXi: Piper PA-46 M500 Meridian Reference guide

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Copyright © 2017 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 2785.02 or later for the G1000 NXi
Piper M500. 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®, 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.
Stormscope® is a registered trademark of L-3 Communications. 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
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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
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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
190–02380–00 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Piper M500
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
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AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”) expressly
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or make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue
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jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or
consequential damages so the above limitations or exclusions may not apply to licensee.
Printed in the U.S.A.
Garmin G1000 NXi Pilot’s Guide for the Piper M500
190–02380–00 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
190–02380–00 Rev. A Garmin G1000 NXi Pilot’s Guide for the Piper M500 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:
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:
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 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 precipitation. Changing the gain in weather mode causes precipitation
intensity to be displayed as a color not representative of the true intensity.
WARNING, CAUTIONS, AND NOTES
ii Garmin G1000 NXi Pilot’s Guide for the Piper M500 190–02380–00 Rev. A
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 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.
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.
WARNING, CAUTIONS, AND NOTES
190–02380–00 Rev. A Garmin G1000 NXi Pilot’s Guide for the Piper M500 iii
NOTE: Interference from GPS repeaters operating inside nearby hangars can cause an
intermittent loss of attitude and heading displays while the aircraft is on the ground. Moving
the aircraft more than 100 yards away from the source of the interference should alleviate
the condition.
NOTE: Use of polarized eyewear may cause the flight displays to appear dim or blank.
NOTE: This product, its packaging, and its components contain chemicals known to the
State of California to cause cancer, birth defects, or reproductive harm. This notice is being
provided in accordance with California’s Proposition 65. If you have any questions or would
like additional information, please refer to our web site at www.garmin.com/prop65.
NOTE: Operating the system in the vicinity of metal buildings, metal structures, or
electromagnetic fields can cause sensor differences that may result in nuisance miscompare
annunciations during start up, shut down, or while taxiing. If one or more of the sensed
values are unavailable, the annunciation indicates no comparison is possible.
NOTE:
The system responds to a terminal procedure based on data coded within that
procedure in the Navigation Database. Differences in system operation may be observed
among similar types of procedures due to differences in the Navigation Database coding
specific to each procedure.
NOTE:
The FAA has asked Garmin to remind pilots who fly with Garmin database-dependent
avionics of the following:
It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory
guidance and information related to the use of databases in the National Airspace System.
Garmin equipment will only recognize and use databases that are obtained from Garmin or
Jeppesen. Databases obtained from Garmin or Jeppesen that have a Type 2 Letter of
Authorization (LOA) from the FAA are assured compliance with all data quality
requirements (DQRs). A copy of the Type 2 LOA is available for each applicable database
and can be viewed at http://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.’
WARNING, CAUTIONS, AND NOTES
iv Garmin G1000 NXi Pilot’s Guide for the Piper M500 190–02380–00 Rev. A
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:
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:
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 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
190–02380–00 Rev. A Garmin G1000 NXi Pilot’s Guide for the Piper M500 v
WARNING, CAUTIONS, AND NOTES
vi Garmin G1000 NXi Pilot’s Guide for the Piper M500 190–02380–00 Rev. A
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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
190–02380–00 Rev. A Garmin G1000 NXi Pilot’s Guide for the Piper M500 vii
SOFTWARE LICENSE AGREEMENT
viii Garmin G1000 NXi Pilot’s Guide for the Piper M500 190–02380–00 Rev. A
BLANK PAGE
Record of Revisions
Part Number Revision Date Page
Range
Description
190–02380-00 A 12/15/17 All Production Release with GDU Software
20.80
RECORD OF REVISIONS
190–02380–00 Rev. A Garmin G1000 NXi Pilot’s Guide for the Piper M500 ix
RECORD OF REVISIONS
x Garmin G1000 NXi Pilot’s Guide for the Piper M500 190–02380–00 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 ................................... 4
PFD/MFD Control Unit.............................. 6
Secure Digital Cards.................................. 8
1.3
System Operation.............................. 10
System Power-up...................................... 10
Normal Operation..................................... 11
Reversionary Mode................................... 11
System Annunciations............................... 12
System Status........................................... 14
AHRS Operation....................................... 15
GPS Receiver Operation............................ 17
1.4
Accessing System Functionality........ 23
Softkey Function....................................... 23
Menus...................................................... 31
MFD Page Groups..................................... 32
Split Screen Functionality.......................... 35
System Settings........................................ 37
System Utilities......................................... 47
1.5
Display Backlighting.......................... 52
SECTION 2 FLIGHT INSTRUMENTS
2.1
Overview
............................................ 55
2.2
Flight Instruments.............................. 58
Attitude Indicator..................................... 58
Airspeed Indicator..................................... 60
Altimeter.................................................. 61
Vertical Speed Indicator (VSI)..................... 65
Vertical Deviation...................................... 66
Vertical Navigation (VNV) Indications......... 68
Horizontal Situation Indicator (HSI)............ 69
Course Deviation Indicator (CDI)............... 73
GPS CDI Scaling (FMS Navigation Source). 75
OBS Mode................................................ 78
Turn Rate Indicator .................................. 79
Bearing Pointers and Information
Windows.................................................. 80
DME Information Window........................ 81
2.3
Supplemental Flight Data.................. 82
Generic Timer........................................... 82
Temperature Displays................................ 82
Wind Data................................................ 83
2.4
PFD Annunciations and Alerting
Functions............................................ 84
Altitude Alerting....................................... 84
Low Altitude Annunciation....................... 84
Marker Beacon Annunciations.................. 84
Minimum Descent Altitude/Decision
Height Alerting......................................... 85
2.5
Garmin Synthetic Vision Technology
(SVT).................................................... 87
Garmin SVT (Synthetic Vision Technology). 87
SVT Operation.......................................... 88
SVT Features............................................. 90
2.6
Abnormal Operations........................101
Abnormal GPS Conditions........................ 101
Comparator Annunciations....................... 102
Reversionary Sensor Annunciations........... 103
SVT Troubleshooting................................. 104
SVT in Reversionary Mode......................... 104
Unusual Attitudes..................................... 104
SVT Unusual Attitudes.............................. 105
SECTION 3 ENGINE INDICATION SYSTEM
3.1
Engine Display
....................................108
3.2
EIS Display (Reversionary Mode)......112
SECTION 4 AUDIO PANEL AND CNS
4.1
Overview
............................................113
Overview.................................................. 113
MFD/PFD Control Unit.............................. 117
4.2
COM Operation..................................119
COM Tuning Boxes................................... 119
COM Transceiver Manual Tuning............... 120
Auto-Tuning the COM Frequency.............. 120
Auto-tuning from the MFD....................... 121
Frequency Spacing.................................... 123
4.3
NAV Operation...................................125
NAV Tuning Boxes..................................... 125
NAV Radio Selection and Activation.......... 126
NAV Receiver Manual Tuning.................... 126
Auto-Tuning a NAV Frequency from the
MFD......................................................... 127
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190–02380–00 Rev. A Garmin G1000 NXi Pilot’s Guide for the Piper M500 xi
Auto-Tuning NAV Frequencies on
Approach Activation................................. 129
Marker Beacon Receiver (Optional)........... 130
ADF/DME Tuning...................................... 131
ADF Tuning............................................... 131
Selecting ADF Receiver Mode.................... 133
DME Tuning.............................................. 134
4.4
Mode S Transponder..........................135
Transponder Controls................................ 135
Transponder Mode Selection..................... 136
Entering a Transponder Code.................... 138
Ident Function.......................................... 139
4.5
Additional Audio Panel Functions....141
Power-Up................................................. 141
Mono/Stereo Headsets.............................. 141
Speaker.................................................... 141
Intercom................................................... 141
Clearance Recorder and Player.................. 144
Split-COM Operation................................ 145
Entertainment Inputs................................ 145
Bluetooth®............................................... 146
4.6
Audio Panel Preflight Procedure.......148
4.7
Abnormal Operation..........................149
Stuck Microphone.................................... 149
COM Tuning Failure.................................. 149
Audio Panel Fail-Safe Operation................ 149
Reversionary Mode................................... 149
SECTION 5 FLIGHT MANAGEMENT SYSTEM
5.1
Introduction
........................................151
Navigation Status Box and Data Bar.......... 153
5.2
Using Map Displays............................156
Map Orientation....................................... 156
Map Range............................................... 159
Map Panning............................................ 161
Measuring Bearing and Distance............... 164
Topography.............................................. 165
Map Symbols............................................ 168
Airways.................................................... 173
Additional Navigation Map Items.............. 175
5.3
Waypoints...........................................179
Airports.................................................... 180
Intersections............................................. 188
NDB.......................................................... 190
VOR.......................................................... 192
VRP.......................................................... 195
User Waypoints......................................... 197
5.4
Airspaces.............................................204
5.5
Direct-To Navigation..........................210
5.6
Flight Planning...................................216
Flight Plan Creation.................................. 217
Flight Plan Import/Export........................... 221
Adding Airways to a Flight Plan................ 231
Adding Procedures to a Stored Flight Plan. 233
Active Flight Plan...................................... 244
Along Track Offsets................................... 247
Parallel Track............................................. 248
Flight Plan Views....................................... 251
Closest Point of FPL.................................. 254
User-Defined Holding Patterns.................. 255
5.7
Vertical Navigation............................261
Altitude Constraints.................................. 263
Vertical Situation Display (VSD)................. 267
5.8
Procedures..........................................272
Departures................................................ 274
Arrivals .................................................... 277
Approaches.............................................. 279
5.9
Weight and Fuel Planning.................291
Weight Warning Conditions...................... 291
5.10
Trip Planning.......................................294
Trip Planning............................................. 294
5.11
Abnormal Operation..........................298
SECTION 6 HAZARD AVOIDANCE
6.1
Overview
............................................301
6.2
Data Link Weather.............................302
Activating Data Link Weather Services....... 303
Weather Product Age............................... 307
Displaying Data Link Weather Products..... 310
Weather Data Link (XM) Page Softkeys .... 311
Weather Data Link (CNXT) Page Softkeys . 314
CONNEXT DATA REQUESTS...................... 321
Weather Product Overview....................... 324
FIS-B Weather Status................................ 363
Abnormal Operations for Garmin Connext
Weather................................................... 365
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xii Garmin G1000 NXi Pilot’s Guide for the Piper M500 190–02380–00 Rev. A
6.3
Stormscope.........................................367
Using The Stormscope Page...................... 367
Setting Up Stormscope On The Navigation
Map......................................................... 369
Cell And Strike On The Navigation Map.... 370
6.4
Airborne Weather Radar...................372
System Description................................... 372
Principles of Pulsed Airborne Weather
Radar........................................................ 372
NEXRAD and Airborne Weather Radar...... 373
Antenna Beam Illumination....................... 373
Safe Operating Distance........................... 376
Basic Antenna Tilt Setup........................... 377
Weather Mapping and Interpretation........ 378
Ground Mapping and Interpretation......... 388
Weather Radar Overlay on the Navigation
Map Page................................................. 389
System Status........................................... 391
6.5
Terrain Displays..................................393
Relative Terrain Symbology........................ 394
Wire Obstacle Information and Alerting.... 399
Terrain Page.............................................. 399
Vertical Situation Display (VSD) Terrain...... 400
Terrain-SVT and TAWS-B Alerting Displays. 403
Forward Looking Terrain Avoidance........... 406
Inhibiting FLTA Alerting............................. 407
Additional TAWS-B Alerting...................... 408
System Status........................................... 411
6.6
TIS........................................................414
Traffic Information Service (TIS)................. 414
Displaying Traffic Data.............................. 415
Traffic Map Page....................................... 417
TIS Alerts.................................................. 418
System Status........................................... 420
6.7
TAS/TCAS I Traffic...............................423
Theory of Operation................................. 423
System Test............................................... 427
Operation................................................. 428
Traffic Map Page....................................... 429
System Status........................................... 432
6.8
ADS-B Traffic.......................................434
ADS-B System Overview............................ 434
ADS-B with TAS/TCAS I............................. 436
Conflict Situational Awareness and
Alerting.................................................... 436
Airborne and Surface Applications............ 439
Traffic Description..................................... 440
Operation................................................. 441
ADS-B System Status................................ 447
SECTION 7 AUTOMATIC FLIGHT CONTROL
SYSTEM
7.1
AFCS Overview...................................451
AFCS Control Unit.................................... 451
Additional AFCS Controls......................... 452
Basic Autopilot Operation......................... 453
7.2
Flight Director Operation..................455
AFCS Status Box....................................... 455
Flight Director Modes............................... 456
Command Bars......................................... 457
7.3
AFCS Modes........................................459
Vertical Modes.......................................... 459
Pitch Hold Mode....................................... 459
Selected Altitude Capture Mode (ALTS)..... 460
Altitude Hold Mode.................................. 461
Vertical Speed Mode................................. 463
Flight Level Change Mode........................ 464
Lateral Modes........................................... 466
Roll Hold Mode (ROL)............................... 466
Low Bank Mode....................................... 467
Heading Select Mode (HDG)..................... 468
Navigation Modes (FMS, VOR, LOC).......... 469
Combination Modes (VNV, APR, NAV, BC,
GA).......................................................... 471
Vertical Navigation Modes (VPTH, ALTV).... 473
Vertical Path Tracking Mode...................... 473
VNV Target Altitude Capture Mode (ALTV) 477
Glidepath Mode (GP)................................ 478
Glideslope Mode (GS)............................... 480
Approach Modes (FMS, VAPP, LOC).......... 482
Backcourse Mode (BC).............................. 483
Takeoff (TO) and Go Around (GA) Modes.. 485
7.4
Autopilot and Yaw Damper
Operation...........................................487
Pitch Axis and Trim.................................... 487
Roll Axis.................................................... 487
Yaw Axis................................................... 487
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190–02380–00 Rev. A Garmin G1000 NXi Pilot’s Guide for the Piper M500 xiii
Flight Control........................................... 487
Engagement............................................. 488
Control Wheel Steering............................ 488
Disengagement........................................ 488
7.5
AFCS Annunciations and Alerts........490
AFCS Alerts.............................................. 490
Overspeed Protection................................ 491
Underspeed Protection............................. 492
Altitude Critical Modes (ALT, GS, GP, TO,
GA, FLC)................................................... 492
Non Altitude Critical Modes (VS, VNAV,
IAS).......................................................... 493
Level Mode............................................... 494
7.6
Abnormal Operation..........................495
SECTION 8 ADDITIONAL FEATURES
8.1
Overview............................................497
8.2
SafeTaxi...............................................499
8.3
Charts..................................................501
Charts...................................................... 501
ChartView................................................ 501
Chart Options........................................... 507
FliteCharts................................................ 512
Airport Directory....................................... 513
IFR/VFR Charts.......................................... 514
8.4
Database Cycle Number and
Revisions.............................................516
8.5
SiriusXM Radio Entertainment..........518
Using SiriusXM Radio................................ 519
Active Channel and Channel List............... 519
Category.................................................. 520
Presets...................................................... 520
8.6
Satellite Telephone and SMS
Messaging..........................................522
Disable/Enable Iridium Transceiver............. 522
Telephone Communication....................... 523
Contacts................................................... 524
Incoming Calls.......................................... 525
Outgoing Calls.......................................... 526
Placing The Cockpit Phone on Hold.......... 529
Text Messaging (SMS)............................... 529
Viewing a Text Message When Received... 530
Reply to a Text Message............................ 532
Sending a Text Message............................ 532
Predefined Text Messages......................... 534
Text Message Boxes.................................. 536
Managing Text Messages.......................... 538
8.7
Flight Data Logging...........................541
8.8
Connext Setup....................................544
8.9
SurfaceWatch.....................................546
SurfaceWatch........................................... 546
Information Box........................................ 546
Alerts........................................................ 547
Takeoff Alerts........................................... 548
Landing Alerts.......................................... 549
SurfaceWatch Setup................................. 550
8.10
Electronic Stability and Protection
(ESP)....................................................554
Roll Engagement...................................... 555
Pitch Engagement..................................... 556
Angle of Attack Protection........................ 557
High Airspeed Protection.......................... 558
8.11
Electronic Checklists...........................559
8.12
Abnormal Operation..........................561
Unusual Attitudes..................................... 561
GDL 69A / GDL 69A SiriusXM Data Link
Receiver Troubleshooting.......................... 561
APPENDICES
Annunciations and Alerts
........................ 563
CAS Message Prioritization....................... 563
CAS Messages.......................................... 567
System Message Annunciations................ 570
System Messages...................................... 571
Database Management............................597
Loading Updated Databases..................... 597
Magnetic Field Variation Database Update 606
Aviation Terms and Acronyms
................. 609
Frequently Asked Questions....................629
Map Symbols............................................ 633
INDEX
Index
......................................................... I-1
TABLE OF CONTENTS
xiv Garmin G1000 NXi Pilot’s Guide for the Piper M500 190–02380–00 Rev. A
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section provides an overview of the G1000 NXi Integrated Avionics System as installed in the
Piper M500. 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
(2) – Each unit is configured as a PFD that features a 10 inch backlit LED screens with
high resolution. The unit installed on the left/pilot side is designated as PFD1, and the one installed
on the right/copilot side is designated as PFD2. These units communicate with each other and the
MFD through a High-Speed Data Bus (HSDB) connection.
GDU 1250A
(1) – Features a 12-inch backlit LED screen with high resolution and is configured as
an MFD. This unit is linked to both PFDs and GIAs via HSDB connection.
GIA 64W
(2) – Functions as the main communication hub, linking LRUs to the PFD and MFD.
Each GIA contains a GPS SBAS receiver, VHF COM/NAV/GS receivers, a flight director (FD) and
system integration microprocessors. Each GIA is paired with the PFD and MFD via an HSDB
connection. The GIAs are not paired together and do not communicate with each other directly.
GTP 59
(2) – Provides Outside Air Temperature (OAT) data to the on-side GDC.
GDC 72
(2) – Processes data from the pitot/static system as well as the OAT probe. This unit
provides pressure altitude, airspeed, vertical speed and OAT information to the system, and
communicates with both GIAs, the on-side PFD, the MFD (GDC#2 only), and the on-side GRS,
using an ARINC 429 digital interface. The GDC is designed to operate in Reduced Vertical
Separation Minimum (RVSM) airspace.
GRS 79
(2) – Provides aircraft attitude and heading information via ARINC 429 to both the on-side
PFD, the MFD (GRS#2 only), and both GIAs. The GRS contains advanced sensors (including
accelerometers and rate sensors) and interfaces with the on-side GMU to obtain magnetic field
information, with the GDC to obtain air data, and with both GIAs to obtain GPS information. AHRS
modes of operation are discussed later in this document.
GEA 71B
(1) – Receives and processes signals from the engine and airframe sensors. This unit
communicates with both GIAs using an RS-485 digital interface.
GMU 44
(2) – Measures local magnetic field. Data is sent to the GSU 75 for processing to determine
aircraft magnetic heading. This unit receives power directly from the GSU 75 and communicates
with the GSU 75 using an RS-485 digital interface.
GMA 350C
(1) – Integrates NAV/COM digital audio, intercom system and marker beacon controls.
This unit features an all-digital audio panel with Bluetooth® capability, and communicates with both
GIAs, using an RS-232 digital interface.
GCU 476
(1) – The Control Unit provides MFD/PFD and radio tuning control through an RS-232
digital interface.
SYSTEM OVERVIEW
190–02380–00 Rev. A Garmin G1000 NXi Pilot’s Guide for the Piper M500 1
GMC 710 (1) – Provides the controls for the Garmin AFCS through an RS-232 digital interface
allowing communication with PFD1 and the MFD.
GTX 335R (1)/ GTX 345R (Alternate) (1)/ GTX 33D w/ES (Optional as #2) – The GTX 335R solid-
state transponder provides Modes A, C, S and ADS-B Out capability. As an alternative, the GTX
345R provides the same capabilities, plus an ADS-B In/Out capability. The optional GTX 33
Diversity with Extended Squitter may be installed in addition to the GTX 335R/GTX 345R. The
transponder can be controlled from the PFD, and it communicates with the both GIAs through an
RS-232 digital interface.
GSR 56
(1) (Optional) – The Iridium Transceiver provides voice communication by means of pilot
and copilot headsets. The unit can also send and receive data over the Iridium satellite network. The
GSR is connected to the #2 GIA with an RS-232 digital interface.
Flight Stream 510
(1) (Optional) – Provides wireless Bluetooth® connectivity between a compatible
tablet/mobile device and the avionics system.
GWX 68
(1) (Optional) – Provides airborne weather and ground mapped radar data to the MFD via
HSDB connection.
GDL 69A SXM
(1) (Optional) – A satellite radio receiver that provides data link weather
information to the MFD and PFD map as well as digital audio entertainment. The GDL 69A SXM
communicates with the MFD via an HSDB connection. Subscriptions to the SiriusXM Weather or
SiriusXM Satellite Radio services are required to enable the GDL 69A SXM capability.
GTS 800
(1) (Optional) – The GTS 800 Traffic Advisory System (TAS) uses active interrogations of
Mode S and Mode C transponders to provide traffic information to the pilot independent of the air
traffic control system.
The Garmin Automated Flight Control System (AFCS) provides the flight director (FD), autopilot
(AP), and yaw damper (YD) functions of the system. See the AFCS Section for more information.
Figure 1-1 shows interactions between the LRUs and optional equipment. The system is capable of
interfacing with the following optional equipment:
GTS 800
Traffic Advisory System
Flight Stream 510
Wireless Bluetooth® Gateway
GSR 56
Iridium Transceiver
GDL 69A SXM
Data Link Receiver
KN 63
DME
RA 3504
ADF
WX-500
Lightning Detection
NOTE: For information on non-Garmin equipment, consult the applicable optional interface
user’s guide. This document assumes that the reader is already familiar with the operation of
this additional equipment.
SYSTEM OVERVIEW
2 Garmin G1000 NXi Pilot’s Guide for the Piper M500 190–02380–00 Rev. A
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Garmin G1000 NXi: Piper PA-46 M500 Meridian Reference guide

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