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Piper PA-28-181 Archer
G1000
®
Integrated Flight Deck
Pilot’s Guide
G1000
®
Pilot’s Guide
Piper PA-28-181
Archer
190-02130-00
Revision A
Garmin International, Inc.
1200 East 151st Street
Olathe, Kansas 66062, U.S.A.
Tel: 913.397.8200
Fax: 913.397.8282
Aircraft On Ground (AOG)
Hotline: 913.397.0836
Aviation Dealer Technical
Support: 888.606.5482
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Tel: 503.581.8101
Fax 503.364.2138
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
Tel: +44 (0) 238 052 4000
Fax: +44 (0) 238 052 4004
Aviation Support: +44 (0) 370 850 1243
Garmin Corporation
No. 68, Zhangshu 2nd Road
Xizhi District,
New Taipei City, Taiwan
Tel: 34-93-357-2608
Fax: 34-93-429-4484
www.garmin.com
SYSTEM OVERVIEW
FLIGHT INSTRUMENTS
ENGINE INDICATION SYSTEM
AUDIO PANEL & CNS
FLIGHT MANAGEMENT
HAZARD AVOIDANCE
AUTOMATIC FLIGHT CONTROL SYSTEM
ADDITIONAL FEATURES
APPENDICES
INDEX
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
190-02130-00 Rev. C
Copyright © 2016 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 2698.00 or later for the 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.
Garmin International, Inc.
1200 East 151st Street
Olathe, Kansas 66062, U.S.A.
Tel: 913.397.8200
Fax: 913.397.8282
Aircraft On Ground (AOG) Hotline: 913.397.0836
Aviation Dealer Technical Support: 888.606.5482
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
Tel: +44 (0) 238 052 4000
Fax: +44 (0) 238 052 4004
Aviation Support: +44 (0) 370 850 1243
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Tel: 503.581.8101
Fax 503.364.2138
Garmin Corporation
No. 68, Zhangshu 2nd Road
Xizhi District, New Taipei City, Taiwan
Tel: 34-93-357-2608
Fax: 34-93-429-4484
Website Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored
in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download
a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for
personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice
and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin
®
, G1000
®
, FliteCharts
®
, and SafeTaxi
®
are registered trademarks of Garmin International, Inc. or its subsidiaries. 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.
AC-U-KWIK
®
is a registered trademark of Penton Business Media Inc. Bendix/King
®
and Honeywell
®
are registered trademarks of Honeywell
International, Inc. Becker
®
is a registered trademark of Becker Flugfunkwerk GmbH. NavData
®
is a registered trademark of Jeppesen, Inc.
Wi-Fi
®
is a registered trademark of the Wi-Fi Alliance. SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite
Radio, Inc.
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.
190-02130-00 Rev. C
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
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.
October 2016 Printed in the U.S.A.
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
190-02130-00 Rev. Civ
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: 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 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.
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.
190-02130-00 Rev. C
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
v
WARNINGS, CAUTIONS, AND NOTES
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: 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 use TAWS information for primary terrain or obstacle avoidance. TAWS is intended only
to enhance situational awareness.
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).
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.
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
190-02130-00 Rev. Cvi
WARNINGS, CAUTIONS, AND NOTES
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.
190-02130-00 Rev. C
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
vii
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 G1000 system power through at least one cycle in a period of four days of continuous
operation to avoid an autonomous system reboot.
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.
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
190-02130-00 Rev. Cviii
REVISION INFORMATION
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
i – I-6
i – I-6
i – I-6
Initial Release for GDU 20.02
Updated to fix clerical errors
Updated to fix clerical errors
190-02130-00 Rev. C
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
ix
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................... 1
1.2 Line Replaceable Units (LRU) ................................... 2
1.3 System Controls ........................................................ 4
PFD Controls ................................................................ 4
1.4 Secure Digital Cards ................................................. 6
1.5 System Power-up ....................................................... 7
1.6 System Operation ..................................................... 8
Normal Operation ......................................................... 8
Reversionary Mode ....................................................... 8
ADAHRS Operation ....................................................... 9
System Annunciations ................................................. 11
Softkey Function ......................................................... 11
GPS Receiver Operation .............................................. 18
1.7 Accessing System Functionality ............................ 23
Menus ....................................................................... 23
MFD Page Groups ....................................................... 24
MFD System Pages...................................................... 28
1.8 Display Backlighting ............................................... 42
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................... 46
Airspeed Indicator ...................................................... 46
Attitude Indicator ....................................................... 48
Altimeter ................................................................... 49
Vertical Speed Indicator (VSI) ....................................... 52
Vertical Deviation ....................................................... 52
Horizontal Situation Indicator (HSI) .............................. 54
Course Deviation Indicator (CDI) .................................. 58
2.2 Supplemental Flight Data ...................................... 65
Temperature Displays .................................................. 65
Wind Data ................................................................. 66
Vertical Navigation (VNV) Indications ........................... 67
2.3 PFD Annunciations and Alerting Functions .......... 68
System Annunciations ................................................. 68
Marker Beacon Annunciations...................................... 69
Altitude Alerting ......................................................... 69
Low Altitude Annunciation .......................................... 70
Minimum Descent Altitude/Decision Height Alerting ...... 70
2.4 Abnormal Operations ............................................. 72
Abnormal GPS Conditions ........................................... 72
Unusual Attitudes ....................................................... 73
SECTION 3 ENGINE INDICATION SYSTEM
3.1 Engine Display ......................................................... 76
Engine Page ............................................................... 78
Oil Pressure and Temperature Gauges ........................... 82
Fuel Quantity ............................................................. 82
EIS Display (Reversionary Mode) .................................. 83
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview .................................................................. 85
PFD Controls and Frequency Display ............................. 86
GMA 1347 Audio Panel Controls .................................. 88
4.2 COM Operation........................................................ 90
COM Transceiver Selection and Activation ..................... 90
COM Transceiver Manual Tuning .................................. 91
Quick-tuning and Activating 121.500 MHz .................... 92
Auto-tuning the COM Frequency .................................. 93
Auto-tuning from the MFD .......................................... 94
Frequency Spacing ...................................................... 97
Automatic Squelch ...................................................... 98
Volume ...................................................................... 98
4.3 NAV Operation......................................................... 99
NAV Radio Selection and Activation ............................. 99
NAV Receiver Manual Tuning ..................................... 100
Auto-tuning a NAV Frequency from the MFD ............... 102
Auto-tuning NAV Frequencies on Approach Activation .106
Marker Beacon Receiver ............................................ 107
ADF/DME Tuning ...................................................... 108
4.4 GTX 345 Mode S Transponder ............................. 112
Transponder Controls ................................................ 112
Transponder Mode Selection ...................................... 113
Entering a Transponder Code ..................................... 115
IDENT Function ........................................................ 116
4.5 Additional Audio Panel Functions ....................... 117
Power-Up ................................................................. 117
Mono/Stereo Headsets .............................................. 117
Speaker ................................................................... 117
Intercom .................................................................. 117
Passenger Address (PA) System .................................. 120
Clearance Recorder and Player ................................... 120
Split COM Operation ................................................. 121
Entertainment Inputs ................................................ 122
4.6 Audio Panel Preflight Procedure ......................... 123
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
190-02130-00 Rev. Cx
TABLE OF CONTENTS
4.7 Abnormal Operation ............................................. 124
Stuck Microphone ..................................................... 124
COM Tuning Failure ................................................... 124
Audio Panel Fail-safe Operation ................................. 124
PFD Failure, Dual System ...........................................124
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ........................................................... 127
Navigation Status Box ............................................... 128
5.2 Using Map Displays .............................................. 130
Map Orientation ....................................................... 130
Map Range .............................................................. 132
Map Panning ............................................................ 134
Measuring Bearing and Distance ................................ 138
Topography .............................................................. 139
Map Symbols ........................................................... 142
Airways ................................................................... 148
Track Vector ............................................................. 150
Wind Vector ............................................................. 151
Fuel Range Ring ....................................................... 152
Field of View (SVt) .................................................... 153
Selected Altitude Intercept Arc ................................... 154
5.3 Waypoints .............................................................. 155
Airports ................................................................... 157
Intersections ............................................................ 163
NDBs ....................................................................... 165
VORs ....................................................................... 167
VRPs ....................................................................... 169
User Waypoints ........................................................ 171
5.4 Airspaces ................................................................ 177
5.5 Direct-to-Navigation ........................................... 181
5.6 Flight Planning ...................................................... 187
Flight Plan Creation .................................................. 188
Adding Waypoints to an Existing Flight Plan ................ 197
Adding Airways to a Flight Plan ................................. 199
Adding Procedures to a Stored Flight Plan .................. 201
Flight Plan Storage ................................................... 208
Flight Plan Editing .................................................... 210
Along Track Offsets ................................................... 214
Parallel Track ............................................................ 215
Activating a Flight Plan Leg ....................................... 218
Inverting a Flight Plan ............................................... 219
Flight Plan Views ...................................................... 220
Closest Point of FPL .................................................. 222
User-Defined Holding Patterns ................................... 222
5.7 Vertical Navigation ............................................... 228
Altitude Constraints .................................................. 230
5.8 Procedures ............................................................. 234
Departures ............................................................... 235
Arrivals ................................................................... 238
Approaches ............................................................. 240
5.9 Trip Planning .......................................................... 249
Trip Planning ............................................................ 249
Weight Planning ....................................................... 253
Weight Caution And Warning Conditions .................... 255
5.10 RAIM Prediction .................................................... 256
5.11 Navigating a Flight Plan ....................................... 259
5.12 Abnormal Operation ............................................. 286
SECTION 6 HAZARD AVOIDANCE
6.1 SiriusXM Weather .................................................. 290
Activating Services .................................................... 290
Using SiriusXM Weather Products .............................. 292
6.2 FIS-B Weather ........................................................ 328
Using FIS-B Weather Products .................................... 328
FIS-B Weather Status................................................. 352
6.3 Terrain Proximity ................................................... 353
Displaying Terrain Proximity Data ............................... 353
6.4 Vertical Situation Display (VSD) Terrain ............. 358
VSD Display ............................................................. 358
Track Mode Boundary ............................................... 360
6.5 Terrain-SVT ............................................................. 362
Displaying Terrain-SVT Data ....................................... 363
Terrain-SVT Page ...................................................... 366
Terrain-SVT Alerts ..................................................... 367
Forward Looking Terrain Avoidance ............................ 368
System Status ........................................................... 370
6.6 TAWS-B ................................................................... 371
Relative Terrain Symbology ........................................ 372
TAWS-B Page ........................................................... 376
TAWS-B Alerts .......................................................... 377
System Status ........................................................... 382
190-02130-00 Rev. C
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
xi
TABLE OF CONTENTS
6.7 Traffic Information Service (TIS) .......................... 384
Displaying TRAFFIC Data ........................................... 385
Traffic Map Page ....................................................... 387
TIS Alerts ................................................................. 388
System Status ........................................................... 389
6.8 GTS 800 Traffic ....................................................... 392
Theory of operation .................................................. 392
TAS Alerts ................................................................ 396
System Test .............................................................. 397
Operation ................................................................ 398
6.9 ADS-B Traffic .......................................................... 405
ADS-B System Overview ............................................ 405
ADS-B with TAS ........................................................ 406
Conflict Situational Awareness & Alerting ................... 407
Airborne and Surface Applications .............................. 409
Traffic Description ..................................................... 410
Operation ................................................................ 410
ADS-B System Status ................................................ 416
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
Automatic Flight Control System .................................. 419
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision Technology (SVT) ...................... 422
SVT Operation .......................................................... 423
SVT Features ............................................................ 425
Field of View ............................................................434
8.2 SafeTaxi .................................................................. 436
SafeTaxi Cycle Number and Revision .......................... 439
8.3 FliteCharts .............................................................. 442
FliteCharts Softkeys .................................................. 443
Terminal Procedures Charts ....................................... 444
Chart Options ........................................................... 447
Day/Night View ........................................................ 447
FliteCharts Cycle Number and Expiration Date ............. 448
8.4 Airport Directory ................................................... 451
Airport Directory Database Cycle Number and Revision 451
8.5 WIFI Connections .................................................. 454
8.6 SiriusXM Radio Entertainment ............................ 457
Activating SiriusXM Satellite Radio Services ................ 457
Using SiriusXM Radio ................................................ 458
8.7 Scheduler ............................................................... 462
8.8 Flight Data Logging .............................................. 464
8.9 Connext Setup ....................................................... 466
8.10 Abnormal Operation ............................................. 468
SVT Troubleshooting ................................................. 468
Reversionary Mode ................................................... 468
Unusual Attitudes ..................................................... 468
GDL 59/69/69A SXM Troubleshooting ......................... 469
APPENDICES
Annunciations and Alerts ............................................... 471
CAS Message Prioritization ........................................ 473
CAS Annunciations ................................................... 475
System Annunciations ............................................... 476
System Message Advisories ....................................... 478
Flight Plan Import/Export Messages ........................... 489
Pilot Profile Import/Export Messages .......................... 490
ADS-B Status Page Messages ..................................... 491
Terrain-SVT Alerts And Annunciations ......................... 492
TAWS-B Alerts And Annunciations .............................. 493
TIS Annunciations ..................................................... 495
TAS Annunciations .................................................... 496
ADS-B Alerts and Annunciations ................................. 497
GDL 69/69A SXM Data Link Receiver Messages ........... 498
Database Management .................................................. 499
Loading Updated Databases ...................................... 499
Magnetic Field Variation Database Update .................. 508
Garmin Aviation Glossary .............................................. 509
Frequently Asked Questions .......................................... 519
General TIS Information ................................................. 523
Map Symbols ................................................................... 525
INDEX
Index .................................................................................. I-1
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
190-02130-00 Rev. Cxii
TABLE OF CONTENTS
Blank Page
190-02130-00 Rev. C
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
1
SYSTEM OVERVIEW
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section provides an overview of the G1000 Integrated Avionics System as installed in the Piper PA-
28-181 Archer. The system is an integrated system that presents flight instrumentation, position, navigation,
communication, and identification information to the pilot through large-format displays.
The optional Flight Stream 510 device provides a Bluetooth
®
connection between the system and a mobile
device. GPS, ADAHRS, ADS-B, traffic, Sirius XM audio, and FIS-B weather data can then be shared with the
mobile device, and flight plans can be transferred to or from the mobile device. Also, database updates may also
be performed using the Flight Stream 510 WiFi link.
The system consists of the following Line Replaceable Units (LRUs):
•
GDU 1050
Primary Flight Display (PFD)
•
GDU 1050
Multi Function Display (MFD)
•
GIA 63W
Integrated Avionics Unit
•
GMU 44
Magnetometer
•
GSU 75
Air Data, Attitude and Heading
Reference System (ADAHRS)
•
GEA 71
Engine/Airframe Unit
•
GMA 1347
Dual Audio System with Integrated
Marker Beacon Receiver
•
GTX 335R/345R
Extended Squitter Mode S
Transponder
•
GTP 59
Outside Air Temperature (OAT) Probe
Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are also shown in Figure 1-1.
The G1000 is capable of interfacing with the following optional equipment:
•
GDL 69A SXM
Data Link Receiver
•
GTS 800
Traffic Advisory System
•
GDL 59
WiFi Data Link
• KN 63 DME
• KR 87 ADF or ADF 3504
• S-TEC 55X Autopilot
190-02130-00 Rev. C
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
2
SYSTEM OVERVIEW
1.2 LINE REPLACEABLE UNITS (LRU)
•
GDU 1050
(2) – The GDUs are configured as a Primary Flight Display (PFD) and a Multi Function Display
(MFD). Both feature 10.4-inch LCD screens with 1024 x 768 resolution. The displays communicate with
each other through a High-Speed Data Bus (HSDB) Ethernet connection. Each display is also paired with an
Ethernet connection to an IAU.
•
GIA 63W
(2) – Functions as the main communication hub, linking all LRUs with the PFD and MFD. Each
GIA 63W contains a GPS SBAS receiver, VHF COM/NAV/GS receivers, a flight director (FD) and system
integration microprocessors. Each GIA 63W is paired with the PFD and MFD via HSDB connection. The GIA
63Ws are not paired together and do not communicate with each other directly.
•
GSU 75
(1) – Processes data from the pitot/static system as well as the OAT probe to provide pressure altitude,
airspeed, vertical speed and OAT information to the system. This unit also provides aircraft attitude and
heading information via ARINC 429 to the PFD, MFD, and GIA 63W. The GSU 75B contains advanced
sensors (including accelerometers and rate sensors) and interfaces with the GMU 44 to obtain magnetic field
information, and with the GIA 63W to obtain GPS information. ADAHRS modes of operation are discussed
later in this document.
•
GTP 59
(1) – Provides Outside Air Temperature (OAT) data to the GSU 75B.
•
GEA 71
(2) – Receives and processes signals from the engine and airframe sensors. This unit communicates
with both GIA 63Ws using an RS-485 digital interface.
•
GMU 44
(1) – Measures local magnetic field. Data is sent to the GSU 75B for processing to determine aircraft
magnetic heading. This unit receives power directly from the GSU 75B and communicates with the GSU 75B,
using an RS-485 digital interface.
•
GMA 1347
(1) – The Audio Panel integrates navigation/communication radio (NAV/COM) digital audio,
intercom, and marker beacon controls, and is installed between the displays. This unit also provides manual
control of display reversionary mode (red
DISPLAY BACKUP
Button; see Section 1.5, System Operation) and
communicates with both IAUs using an RS-232 digital interface.
•
GTX 335R/345R
(1) – Solid-state transponders that provide Modes A, C, S and ADS-B capability. The optional
GTX 345R also provides ADS-B In/Out. The transponder can be controlled from the PFD. The transponder
communicates with the both GIA 63Ws through an RS-232 digital interface.
•
GDL 69A SXM
(1) (Optional) – A satellite radio receiver that provides data link weather information to the
MFD (and, indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL 69A
SXM communicates with the MFD via HSDB connection. Subscriptions to the SiriusXM Weather or SiriusXM
Satellite Radio services are required to enable the GDL 69A SXM capability.
•
GDL 59
(1) (Optional) – GDL 59 operation is performed with the PFD through HSDB.
•
GTS 800
(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.
190-02130-00 Rev. C
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
3
SYSTEM OVERVIEW
GTX 345R
Or
#1
GDU 1050
(PFD)
GDL 69A SXM
(XM Weather/
Audio Datalink)
GMA 1347
(Audio
Panel)
KN-63
(DME)
#1 GIA 63W
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
Flight
Director
AFCS Mode
Logic
Servo Logic
#2 GIA 63W
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
Flight
Director
AFCS Mode
Logic
Servo Logic
#2
GDU 1050
(MFD)
Non-Garmin Equipment
KR-87 or ADF 3504
(ADF)
GEA 71 (Engine &
Airframe I/F)
GTX 335R
(Transponder)
GSU 75
(ADAHRS)
Optional
Garmin Equipment
Optional
Non-Garmin Equipment
GMA 44
(Magnetometer)
GTS 800
(TAS)
Garmin Equipment
GDL 59
(Data Link)
STEC 55X
(AFCS)
Figure 1-1 System (LRU Configuration)
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.
190-02130-00 Rev. C
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
4
SYSTEM OVERVIEW
1.3 SYSTEM CONTROLS
NOTE: The Audio Panel (GMA 1347) is described in the CNS & Audio Panel section.
The system controls are located on the PFD and MFD bezels and audio panel. The controls for the PFD and
MFD are discussed within the following pages of this section.
PFD CONTROLS
Figure 1-2 PFD/MFD Controls
21 5
4
6
8
7
3
11
12
10
9
15
14
13
The following list provides an overview of the controls located on the PFD/MFD bezels (see Figure 1-2).
190-02130-00 Rev. C
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
5
SYSTEM OVERVIEW
1
NAV VOL/ID Knob
– Controls NAV audio volume level. Press to toggle the Morse code identifier audio ON
and OFF. Volume level is shown in the NAV frequency field as a percentage.
2
NAV Frequency Transfer Key
– Toggles the standby and active NAV frequencies.
3
Dual
NAV Knob
– Tunes the standby frequencies for the NAV receiver (large knob for MHz; small knob for
kHz). Press to switch the tuning box (cyan box) between NAV1 and NAV2.
4
Joystick
– Changes the map range when rotated. Activates the map pointer when pressed.
5
BARO Knob
– Sets the altimeter barometric pressure. Press to enter standard pressure (29.92).
6
Dual COM Knob
– Tunes the standby frequencies for the COM transceiver (large knob for MHz; small
knob for kHz). Press to switch the tuning box (cyan box) between COM1 and COM2.
7
COM Frequency Transfer Key
– Toggles the standby and active COM frequencies. Press and hold this
key for two seconds to tune the emergency frequency (121.5 MHz) automatically into the active frequency
field.
8
COM
VOL/SQ Knob
– Controls COM audio volume level. Volume level is shown in the COM frequency
field as a percentage. Press to turn the COM automatic squelch ON and OFF.
9
Direct-to Key ( )
– Allows the user to enter a destination waypoint and establish a direct course to the
selected destination (the destination is either specified by the identifier, chosen from the active route, or
taken from the map pointer position).
10
FPL Key
– Displays the active Flight Plan Page for creating and editing the active flight plan.
11
CLR
Key
– Erases information, cancels entries, or removes page menus.
12
Dual FMS Knob
– Flight Management System Knob. Press the
FMS
Knob to turn the selection cursor
ON and OFF. When the cursor is ON, data may be entered in the applicable window by turning the small
and large
knobs. The large
knob moves the cursor on the page, while the small
knob selects individual
characters for the highlighted cursor location.
13
MENU Key
– Displays a context-sensitive list of options. This list allows the user to access additional
features or make setting changes that relate to particular pages.
14
PROC Key
– Gives access to IFR departure procedures (DPs), arrival procedures (STARs) and approach
procedures (IAPs) for a flight plan. If a flight plan is used, available procedures for the departure and/or
arrival airport are automatically suggested. These procedures can then be loaded into the active flight plan.
If a flight plan is not used, both the desired airport and the desired procedure may be selected.
15
ENT Key
– Validates or confirms a menu selection or data entry.
190-02130-00 Rev. C
Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
6
SYSTEM OVERVIEW
1.4 SECURE DIGITAL CARDS
NOTE:
Refer to the Appendices for instructions on updating the aviation databases.
NOTE:
Ensure that the system is powered off before inserting the SD card.
The GDU 1050 data card slots use Secure Digital (SD) cards and are located on the top right portion of the
display bezels. Each display bezel is equipped with two SD card slots. SD cards are used for aviation database
and system software updates as well as terrain database storage. Also, flight plans may be imported or exported
from an SD card in the MFD.
Install an SD card
Insert the SD card in the SD card slot, pushing the card in until the spring latch engages. The front of the card
should remain flush with the face of the display bezel.
Remove an SD card
Gently press on the SD card to release the spring latch and eject the card.
Figure 1-3 PFD/MFD Display Bezel SD Card Slots
SD Card Slots
/
