Garmin G1000 NXi - Piper PA-44-180 Seminole Reference guide

Type
Reference guide

This manual is also suitable for

Piper PA-44-180 Seminole
G1000
®
Integrated Flight Deck
Pilot’s Guide
G1000
®
Pilot’s Guide
Piper PA-44-180
Seminole
190-02198-00
Revision B
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
190-02198-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
Copyright © 2016 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 2694.01 or later for the PA-44-180. 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 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.
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®
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.
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.
November 2016 Printed in the U.S.A
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
190-02198-00 Rev. B
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190-02198-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
i
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.
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
190-02198-00 Rev. Bii
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
:
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 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: Do not use TAWS information for primary terrain or obstacle avoidance. TAWS is intended only
to enhance situational awareness.
CAUTION: Do not clean display surfaces with abrasive cloths or cleaners containing ammonia. They will
harm the anti-reflective coating.
190-02198-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
iii
WARNINGS, CAUTIONS, AND NOTES
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.
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.
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
190-02198-00 Rev. Biv
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: 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: Operate G1000 system power through at least one cycle in a period of four days of continuous
operation to avoid an autonomous system reboot.
190-02198-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
v
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-02198-00 A
B
11/22/16
11/29/16
i – I-6
i – I-6
Initial Release
Clerical Revision
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
190-02198-00 Rev. Bvi
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................. 1
Line Replaceable Units (LRU) ......................................... 2
1.2 System Controls....................................................... 4
PFD/MFD Controls ........................................................ 4
Secure Digital Cards ...................................................... 7
Softkey Function ........................................................... 8
1.3 System Power-up ................................................... 16
1.4 System Operation .................................................. 17
Normal Operation ....................................................... 17
Reversionary Mode ..................................................... 18
AHRS Operation ......................................................... 19
System Annunciations ................................................. 20
System Status ............................................................. 21
GPS Receiver Operation .............................................. 22
1.5 Accessing System Functionality .......................... 27
Menus ....................................................................... 27
MFD Page Groups ....................................................... 28
System Settings .......................................................... 31
System Utilities ........................................................... 39
1.6 Display Backlighting ............................................. 44
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 48
Airspeed Indicator ...................................................... 48
Attitude Indicator ....................................................... 50
Altimeter ................................................................... 52
Vertical Speed Indicator (VSI) ....................................... 55
Vertical Deviation ....................................................... 55
Horizontal Situation Indicator (HSI) .............................. 56
Course Deviation Indicator (CDI) .................................. 60
2.2 Supplemental Flight Data .................................... 67
Temperature Displays .................................................. 67
Wind Data ................................................................. 67
Vertical Navigation (VNV) Indications ........................... 68
2.3 PFD Annunciations and Alerting Functions ........ 70
System Annunciations ................................................. 70
Marker Beacon Annunciations...................................... 71
Altitude Alerting ......................................................... 71
Low Altitude Annunciation .......................................... 72
Minimum Descent Altitude/Decision Height Alerting ...... 72
2.4 Abnormal Operations ........................................... 74
Abnormal GPS Conditions ........................................... 74
Unusual Attitudes ....................................................... 75
SECTION 3 ENGINE INDICATION SYSTEM (EIS)
3.1 Engine Display ....................................................... 78
3.2 Engine Page............................................................ 80
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview ................................................................ 87
PFD Controls and Frequency Display ............................. 88
GMA 1347 Audio Panel Controls .................................. 90
4.2 COM Operation ...................................................... 92
COM Transceiver Selection and Activation ..................... 92
COM Transceiver Manual Tuning .................................. 93
Quick-tuning and Activating 121.500 MHz .................... 94
Auto-tuning the COM Frequency .................................. 95
Auto-tuning from the MFD .......................................... 96
Frequency Spacing ...................................................... 99
Automatic Squelch .................................................... 100
Volume .................................................................... 100
4.3 NAV Operation ..................................................... 101
NAV Radio Selection and Activation ........................... 101
NAV Receiver Manual Tuning ..................................... 102
Auto-tuning a NAV Frequency from the MFD ............... 104
Auto-tuning NAV Frequencies on Approach Activation . 108
Marker Beacon Receiver ............................................ 109
ADF/DME Tuning ...................................................... 110
4.4 GTX 335 or GTX 345 Mode S Transponder ....... 114
Transponder Controls ................................................ 114
Transponder Mode Selection ...................................... 115
Entering a Transponder Code ..................................... 117
IDENT Function ........................................................ 118
Flight ID Reporting.................................................... 118
4.5 Additional Audio Panel Functions ..................... 120
Power-Up ................................................................. 120
Mono/Stereo Headsets .............................................. 120
Speaker ................................................................... 120
Intercom .................................................................. 120
Passenger Address (PA) System .................................. 123
Clearance Recorder and Player ................................... 123
Split COM Operation ................................................. 124
Entertainment Inputs ................................................ 125
190-02198-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
vii
TABLE OF CONTENTS
4.6 Audio Panel Preflight Procedure ....................... 126
4.7 Abnormal Operation ........................................... 127
Stuck Microphone ..................................................... 127
COM Tuning Failure ................................................... 127
Audio Panel Fail-safe Operation ................................. 127
PFD Failure (Reversionary Mode) ............................... 127
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 129
Navigation Status Box ............................................... 130
5.2 Using Map Displays ............................................. 132
Map Orientation ....................................................... 132
Map Range .............................................................. 134
Map Panning ............................................................ 137
Measuring Bearing and Distance ................................ 142
Topography .............................................................. 143
Map Symbols ........................................................... 146
Airways ................................................................... 152
Track Vector ............................................................. 154
Wind Vector ............................................................. 155
Fuel Range Ring ....................................................... 156
Field of View (SVT) .................................................... 157
Selected Altitude Intercept Arc ................................... 158
5.3 Waypoints ............................................................. 159
Airports ................................................................... 160
Intersections ............................................................ 167
NDBs ....................................................................... 169
VORs ....................................................................... 171
VRPs ....................................................................... 173
User Waypoints ........................................................ 175
5.4 Airspaces .............................................................. 181
5.5 Direct-to-Navigation .......................................... 185
5.6 Flight Planning ..................................................... 191
Flight Plan Creation .................................................. 192
Adding Waypoints to an Existing Flight Plan ................ 202
Adding Airways to a Flight Plan ................................. 204
Adding Procedures to a Stored Flight Plan .................. 207
Flight Plan Storage ................................................... 214
Flight Plan Editing .................................................... 216
Along Track Offsets ................................................... 220
Parallel Track ............................................................ 221
Activating a Flight Plan Leg ....................................... 224
Inverting a Flight Plan ............................................... 226
Flight Plan Views ......................................................226
Closest Point of FPL .................................................. 229
User-Defined Holding Patterns ................................... 229
5.7 Vertical Navigation ............................................. 235
Altitude Constraints .................................................. 237
5.8 Procedures ...........................................................241
Departures ............................................................... 242
Arrivals ................................................................... 245
Approaches ............................................................. 248
5.9 Trip Planning ........................................................ 256
Trip Planning ............................................................ 256
Weight Planning ....................................................... 260
Weight Caution And Warning Conditions .................... 262
5.10 Navigating a Flight Plan ..................................... 263
5.11 Abnormal Operation ........................................... 290
SECTION 6 HAZARD AVOIDANCE
6.1 SiriusXM Weather ................................................ 294
Activating Services .................................................... 294
Using SiriusXM Weather Products .............................. 296
6.2 FIS-B Weather ...................................................... 334
Using FIS-B Weather Products .................................... 334
FIS-B Weather Status................................................. 358
6.3 Terrain Proximity ................................................. 359
Displaying Terrain Proximity Data ............................... 359
6.4 Vertical Situation Display (VSD) Terrain ........... 364
VSD Display ............................................................. 364
Track Mode Boundary ............................................... 366
6.5 Terrain-SVT ........................................................... 368
Displaying Terrain-SVT Data ....................................... 369
Terrain-SVT Page ...................................................... 372
Terrain-SVT Alerts ..................................................... 372
Forward Looking Terrain Avoidance ............................ 374
System Status ........................................................... 376
6.6 TAWS-B ................................................................. 377
Relative Terrain Symbology ........................................ 378
TAWS-B Page ........................................................... 382
TAWS-B Alerts .......................................................... 383
System Status ........................................................... 388
6.7 Traffic Information Service (TIS) ........................ 390
Displaying Traffic Data .............................................. 391
Traffic Map Page ....................................................... 393
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
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TABLE OF CONTENTS
TIS Alerts ................................................................. 394
System Status ........................................................... 395
6.8 GTS 800 Traffic ..................................................... 397
Theory of Operation .................................................. 397
TAS Alerts ................................................................ 401
System Test .............................................................. 402
Operation ................................................................ 403
6.9 ADS-B Traffic ........................................................ 410
ADS-B System Overview ............................................ 410
ADS-B with TAS ........................................................ 411
Conflict Situational Awareness & Alerting ................... 412
Airborne and Surface Applications .............................. 414
Traffic Description ..................................................... 415
Operation ................................................................ 415
ADS-B System Status ................................................ 421
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 Basic Autopilot Operation .................................. 426
7.2 AFCS Controls ...................................................... 427
7.3 Flight Director Operation ................................... 429
Activating the Flight Director ..................................... 429
AFCS Status Box ....................................................... 430
Flight Director Modes ................................................ 431
Command Bars ......................................................... 431
7.4 AFCS Modes ......................................................... 432
Vertical Modes ......................................................... 432
Lateral Modes .......................................................... 438
Combination modes (VNV, APR, NAV, BC, GA) ............. 442
7.5 Autopilot Operation ............................................ 453
Flight Control ........................................................... 453
Engagement ............................................................. 453
Control Wheel Steering ............................................. 454
Disengagement ........................................................ 454
Level Mode .............................................................. 455
Underspeed Protection .............................................. 456
7.6 Example Flight Plan ............................................ 458
Departure ................................................................ 458
Intercepting a VOR Radial .......................................... 460
Flying a Flight Plan/FMS Course ................................. 461
Descent ................................................................... 462
Approach ................................................................. 466
Go Around/Missed Approach ..................................... 470
7.7 AFCS Annunciations and Alerts ......................... 472
AFCS Status Alerts .................................................... 472
Overspeed Protection ................................................ 473
7.8 Abnormal Operation ........................................... 474
Suspected Autopilot Malfunction ............................... 474
Overpowering Autopilot Servos .................................. 474
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision Technology (SVT) ..................... 476
SVT Operation .......................................................... 477
SVT Features ............................................................ 479
Field of View ............................................................488
8.2 SafeTaxi ................................................................ 490
SafeTaxi Cycle Number and Revision .......................... 493
8.3 FliteCharts ............................................................ 496
FliteCharts Softkeys .................................................. 497
Terminal Procedures Charts ....................................... 498
Chart Options ........................................................... 501
Day/Night View ........................................................ 501
FliteCharts Cycle Number and Expiration Date ............. 502
8.4 Airport Directory ................................................. 505
Airport Directory Database Cycle Number and Revision 505
8.5 WIFI Connections ................................................. 508
8.6 SiriusXM Radio Entertainment .......................... 511
Activating SiriusXM Satellite Radio Services ................ 511
Using SiriusXM Radio ................................................ 512
8.7 Scheduler .............................................................. 516
8.8 Flight Data Logging ............................................ 518
8.9 Abnormal Operation ........................................... 520
SVT Troubleshooting ................................................. 520
Reversionary Mode ................................................... 520
Unusual Attitudes ..................................................... 520
GDL 59/69/69A SXM Troubleshooting ......................... 520
APPENDICES
Annunciations and Alerts ............................................. 523
CAS Message Prioritization ........................................ 524
CAS Annunciations ................................................... 526
System Annunciations ............................................... 528
System Message Advisories ....................................... 530
Aural Alerts .............................................................. 540
Flight Plan Import/Export Messages ........................... 541
190-02198-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
ix
TABLE OF CONTENTS
Pilot Profile Import/Export Messages .......................... 541
ADS-B Status Page Messages ..................................... 542
Terrain-SVS Alerts ..................................................... 543
Terrain-SVS System Status Annunciations .................... 543
TAWS-B Alerts .......................................................... 544
TIS Annunciations ..................................................... 545
TAS Annunciations .................................................... 546
ADS-B Alerts and Annunciations ................................. 547
GDL 69 SXM Data Link Receiver Messages .................. 549
Database Management ................................................ 551
Loading Updated Databases ...................................... 551
Magnetic Field Variation Database Update .................. 560
Garmin Aviation Glossary ............................................ 561
Frequently Asked Questions ........................................ 571
Map Symbols ................................................................. 575
INDEX
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
190-02198-00 Rev. Bx
TABLE OF CONTENTS
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190-02198-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
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-44-
180 Seminole. 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, AHRS, 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 1050/1054
Multi Function Display (MFD)
GIA 63W
Integrated Avionics Unit
GMU 44
Magnetometer
GRS 79
Attitude and Heading Reference System
(AHRS)
GDC 72
Air Data Computer (ADC)
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 system 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
GSA 80/81
AFCS Servos
GSM 86
Servo Gearboxes
KN 63 DME
KR 87 ADF
S-TEC 55X Autopilot
190-02198-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
2
SYSTEM OVERVIEW
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.
GMU 44
(1) – The Magnetometer measures local magnetic field and sends data to the AHRS for processing to
determine aircraft magnetic heading. This unit receives power directly from the AHRS and communicates with
it via an RS-485 digital interface.
GRS 79 (1)
– The Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading
information via ARINC 429 to both GDUs and both IAUs. The AHRS contains advanced sensors (including
accelerometers and rate sensors) and interfaces with the Magnetometer to obtain magnetic field information,
with the ADC to obtain air data, and with both IAUs to obtain GPS information.
GDC 72 (1)
– The Air Data Computer (ADC) processes data from the pitot/static system and outside air
temperature (OAT) sensor. The ADC provides pressure altitude, airspeed, vertical speed, and OAT information
to the system. It communicates with the IAUs, displays, and AHRS using an ARINC 429 digital interface.
GEA 71
(1) – Receives and processes signals from the engine and airframe sensors. This unit communicates
with both GIA 63Ws 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, 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.
GTP 59
(1) – Provides Outside Air Temperature (OAT) data.
GDL 59
(1) (Optional) – The GDL 59 is connected to the PFD via HSDB and provides wireless data transfer.
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.
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.
GSA 80
(1)
/ GSA 81
(2) (only with Garmin AFCS option) – The GSA 80 servo is used for the automatic control
of pitch trim. The GSA 81 servos are used for the automatic control of pitch and roll. These units interface with
each GIA 63W.
The GSM 86 servo gearboxes are responsible for transferring the output torque of the GSA 80/81 servo actuators
to the mechanical flight-control surface linkage.
190-02198-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
3
SYSTEM OVERVIEW
#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)
or
GDU 1054
(MFD)
Non-Garmin Equipment
KR-87
(ADF)
GTX 335R/345R
(Transponder)
GEA 71 (Engine &
Airframe I/F)
GDC 72
(Air Data
Computer)
GRS 79
(Attitude &
Heading)
Optional
Garmin Equipment
Optional
Non-Garmin Equipment
GMU 44
(Magnetometer)
GTS 800
(TAS)
Garmin Equipment
GSA 80/81 (3)
(Garmin AFCS
Servos)
Figure 1-1 System (LRU Configuration)
NOTE: For information on optional equipment not shown in Figure 1-1, it may be necessary consult an
additional user’s guide. This document assumes that the reader is already familiar with the operation of this
additional equipment.
190-02198-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
4
SYSTEM OVERVIEW
1.2 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/MFD CONTROLS
Figure 1-2 PFD/MFD Controls
4
2
1
6
5
7
9
8
3
12
16
11
10
15
14
13
20
21
19
18
25
24
22
23
28
27
MFD Only
17
26
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Garmin G1000 NXi - Piper PA-44-180 Seminole Reference guide

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