Garmin G1000: Piper PA-46 M350 Mirage Reference guide

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Reference guide

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Garmin International, Inc.
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Piper PA-46 Mirage
G1000
®
Integrated Avionics System
Pilot’s Guide
G1000
®
Pilot’s Guide
Piper PA-46
Mirage
190-01889-00
Revision A
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-46 Mirage
190-01889-00 Rev. B
Copyright © 2015 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 2164.00 or later for the Piper Mirage. 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
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: 503/391.3411 Fax: 503/364.2138
Garmin (Europe) Ltd., Liberty House, Hounsdown Business Park, Southampton, SO40 9LR, U.K
Tel: 44 (0) 23 8052 4000 Fax: 44 (0) 23 8052 4004 Aviation Support:44 (0) 87 0850 1243
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: 886/02.2642.9199 Fax: 886/02.2642.9099
For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please
contact Garmin’s AOG Hotline at 913.397.0836.
Website Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored
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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
®
, WATCH
®
, 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.
Stormscope
®
is a registered trademark of L-3 Communications. AC-U-KWIK
®
is a registered trademark of Penton Business Media Inc.
Bendix/King
®
and Honeywell
®
are registered trademarks of Honeywell International, Inc. Becker
®
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®
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.
April 2015 Printed in the U.S.A.
190-01889-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
i
WARNINGS, CAUTIONS, AND NOTES
WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance
feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance
and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The
terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from
third party sources. Garmin is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (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: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and
could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74A Air Data
Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always
use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in the G1000 system must be updated
regularly in order to ensure that the information remains current. Pilots using any outdated database do so
entirely at their own risk.
WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is
intended only to supplement other approved navigation data sources and should be considered as an aid to
enhance situational awareness.
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 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 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: 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.
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
190-01889-00 Rev. Bii
WARNINGS, CAUTIONS, AND NOTES
WARNING:
For safety reasons, G1000 operational procedures must be learned on the ground.
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 significantly older than the indicated weather product age.
WARNING:
The Garmin G1000, as installed in this aircraft, has a very high degree of functional integrity.
However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable
system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur
without a fault indication shown by the G1000. It is thus the responsibility of the pilot to detect such an
occurrence by means of cross-checking with all redundant or correlated information available in the cockpit.
WARNING:
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 Garmin G1000 utilize GPS as a precision electronic
NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be
misused or misinterpreted and, therefore, become unsafe.
WARNING:
To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000
Pilot’s Guide documentation and the G1000 Integrated Avionics System in the Airplane Flight Manual.
Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications
from the G1000 to all available navigation sources, including the information from other NAVAIDs, visual
sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation.
WARNING
: The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate
a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information
Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an
intense radar echo.
WARNING
:
Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of
according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/
aboutGarmin/environment/disposal.jsp.
WARNING
:
Because of variation in the earth’s magnetic field, operating within the following areas could
result in loss of reliable attitude and heading indications. 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)
190-01889-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
iii
WARNINGS, CAUTIONS, AND NOTES
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.
CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very
sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE
ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an
eyeglass lens cleaner that is specified as safe for anti-reflective coatings.
CAUTION:
The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by
an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty
and the pilot’s authority to operate this device under FAA/FCC regulations.
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: 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 G1000 panel and
displays, are subject to change and may not reflect the most current G1000 system and aviation databases.
Depictions of equipment may differ slightly from the actual equipment.
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.
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
190-01889-00 Rev. Biv
WARNINGS, CAUTIONS, AND NOTES
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
: 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 are assured compliance with all data quality requirements (DQRs) by virtue
of a Type 2 Letter of Authorization (LOA) from the FAA. A copy of the Type 2 LOA is available for each database
and can be viewed at http://fly.garmin.com by selecting ‘Type 2 LOA Status.’
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 to
coordinate the revised DQRs.
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 ‘Report An Aviation Data Error Report.’
190-01889-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
v
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-01889-00 A 3/9/15 - Initial Release with GDU SW Version 15.00
190-01889-00 B 4/7/15 All
Revised to add Emergency Descent Mode and Hypoxia Prevention
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
190-01889-00 Rev. Bvi
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................. 1
1.2 Line Replaceable Units (LRU) ................................. 2
1.3 G1000 Controls ........................................................ 5
PFD/MFD Controls ........................................................ 5
MFD/PFD Control Unit ................................................... 7
AFCS Controls .............................................................. 9
Audio Panel Controls .................................................. 11
1.4 Secure Digital Cards.............................................. 13
1.5 System Power-up ................................................... 14
1.6 System Operation .................................................. 15
Normal Operation ....................................................... 15
Reversionary Mode ..................................................... 16
AHRS Operation ......................................................... 17
G1000 System Annunciations ...................................... 18
Softkey Function ......................................................... 19
GPS Receiver Operation .............................................. 26
1.7 Accessing G1000 Functionality............................ 31
Menus ....................................................................... 31
MFD Page Groups ....................................................... 32
MFD System Pages...................................................... 36
1.8 Display Backlighting ............................................. 53
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 58
Airspeed Indicator ...................................................... 58
Attitude Indicator ....................................................... 60
Altimeter ................................................................... 61
Vertical Speed Indicator (VSI) ....................................... 63
Vertical Deviation ....................................................... 64
Horizontal Situation Indicator (HSI) .............................. 65
Course Deviation Indicator (CDI) .................................. 71
2.2 Supplemental Flight Data .................................... 79
Temperature Displays .................................................. 79
Wind Data ................................................................. 80
Vertical Navigation (VNV) Indications ........................... 81
2.3 PFD Annunciations and Alerting Functions ........ 82
Marker Beacon Annunciations...................................... 82
Altitude Alerting ......................................................... 82
Low Altitude Annunciation .......................................... 83
Minimum Descent Altitude/Decision Height Alerting ...... 83
2.4 Abnormal Operations ........................................... 85
Abnormal GPS Conditions ........................................... 85
Heading Failure Modes................................................ 86
Unusual Attitudes ....................................................... 86
SECTION 3 ENGINE INDICATION SYSTEM
3.1 Engine Indication System (EIS) ............................ 91
Manifold Pressure Gauge ............................................ 92
Propeller RPM Gauge .................................................. 92
Turbine Inlet Temperature Gauge .................................. 92
Fuel Flow ................................................................... 93
Cylinder Head Temperature .......................................... 93
Oil Pressure and Temperature Gauges ........................... 93
Cabin Pressurization ................................................... 94
Pulse Oximeter ........................................................... 94
Fuel Quantity ............................................................. 95
Electrical .................................................................... 95
Flap Indicator ............................................................. 95
Landing Gear Indicator ................................................ 96
3.2 Engine Page............................................................ 97
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview ................................................................ 99
PFD Controls and Frequency Display ........................... 100
Audio Panel Controls ................................................ 102
MFD/PFD Control Unit ............................................... 104
4.2 COM Operation .................................................... 106
COM Transceiver Selection and Activation ................... 106
COM Transceiver Manual Tuning ................................ 107
Quick-tuning and Activating 121.500 MHz .................. 109
Auto-tuning the COM Frequency ................................ 110
Frequency Spacing .................................................... 115
Automatic Squelch .................................................... 116
Volume .................................................................... 116
4.3 NAV Operation ..................................................... 117
NAV Radio Selection and Activation ........................... 117
NAV Receiver Manual Tuning ..................................... 118
Auto-tuning a NAV Frequency from the MFD ............... 120
Auto-tuning NAV Frequencies on Approach Activation . 124
Marker Beacon Receiver ............................................ 124
ADF/DME Tuning ...................................................... 125
190-01889-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
vii
TABLE OF CONTENTS
4.4 GTX 33 ES Mode S Transponder(s) .................... 130
Transponder Controls ................................................ 130
Transponder Mode Selection ...................................... 131
Entering a Transponder Code ..................................... 133
IDENT Function ........................................................ 135
ADS-B TX ................................................................. 135
4.5 Additional Audio Panel Functions ..................... 136
Power-Up ................................................................. 136
Mono/Stereo Headsets .............................................. 136
Speaker ................................................................... 136
Passenger Address Mode (PA Mode) ........................... 136
Clearance Recorder and Player ................................... 136
Intercom System (ICS) .............................................. 137
Split COM Mode ....................................................... 142
Entertainment Inputs ................................................ 143
4.6 Audio Panels Preflight Procedure ...................... 144
Audio Panel Preflight ................................................ 144
4.7 Abnormal Operation ........................................... 145
Audio Panel Fail-safe Operation ................................. 145
Stuck Microphone ..................................................... 145
COM Tuning Failure ................................................... 145
PFD Failure, Dual System ........................................... 145
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 147
Navigation Status Box ............................................... 148
5.2 Using Map Displays ............................................. 150
Map Orientation ....................................................... 150
Map Range .............................................................. 152
Map Panning ............................................................ 154
Measuring Bearing and Distance ................................ 160
Topography .............................................................. 161
Map Symbols ........................................................... 164
Airways ................................................................... 170
Track Vector ............................................................. 172
Wind Vector ............................................................. 173
Nav Range Ring........................................................ 174
Fuel Range Ring ....................................................... 175
Field of View (SVT) .................................................... 176
Selected Altitude Intercept Arc ................................... 177
5.3 Waypoints ............................................................. 178
Airports ................................................................... 179
Intersections ............................................................ 186
NDBs ....................................................................... 188
VORs ....................................................................... 190
User Waypoints ........................................................ 192
5.4 Airspaces .............................................................. 198
5.5 Direct-to-Navigation .......................................... 203
5.6 Flight Planning ..................................................... 209
Flight Plan Creation .................................................. 210
Adding Waypoints to an Existing Flight Plan ................ 215
Adding Airways to a Flight Plan ................................. 218
Adding Procedures to a Stored Flight Plan .................. 221
Flight Plan Storage ................................................... 228
Flight Plan Editing .................................................... 230
Along Track Offsets ................................................... 234
Parallel Track ............................................................ 235
Activating a Flight Plan Leg ....................................... 238
Inverting a Flight Plan ............................................... 239
Flight Plan Views ...................................................... 240
Closest Point of FPL .................................................. 242
User-Defined Holding Patterns ................................... 243
5.7 Vertical Navigation ............................................. 248
Altitude Constraints .................................................. 250
5.8 Procedures ...........................................................254
Departures ............................................................... 255
Arrivals ................................................................... 258
Approaches ............................................................. 261
5.9 Trip Planning ........................................................ 269
Trip Planning ............................................................ 269
Weight Planning ....................................................... 273
Weight Caution And Warning Conditions .................... 275
5.10 RAIM Prediction................................................... 276
5.11 Navigating a Flight Plan ..................................... 280
5.12 Abnormal Operation ........................................... 308
SECTION 6 HAZARD AVOIDANCE
6.1 SiriusXM Weather ................................................ 312
Activating Services ................................................... 312
Using SiriusXM Weather Products .............................. 313
6.2 Garmin Connext Weather ................................... 347
Registering the system for Garmin Connext Weather .... 347
Accessing Garmin Connext Weather Products .............. 349
Connext Weather Data Requests ................................ 355
Garmin Connext Weather Products ............................. 359
Abnormal Operations ................................................ 371
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
190-01889-00 Rev. Bviii
TABLE OF CONTENTS
6.3 Airborne Color Weather Radar .......................... 373
System Description ................................................... 373
Principles of Pulsed Airborne Weather Radar ............... 373
NEXRAD and Airborne Weather Radar ....................... 374
Antenna Beam Illumination ....................................... 374
Safe Operating Distance ............................................ 377
Basic Antenna Tilt Setup ............................................ 378
Weather Mapping and Interpretation ......................... 380
Ground Mapping and Interpretation ........................... 392
Weather Radar Overlay on the Navigation Map Page ... 393
System Status ........................................................... 394
6.4 Stormscope Lightning ......................................... 396
Setting Up Stormscope on the Navigation Map ........... 396
Selecting the Stormscope Page .................................. 400
6.5 Terrain Proximity ................................................. 402
Displaying Terrain Proximity Data ............................... 402
Terrain Proximity Page ............................................... 406
6.6 Terrain-SVS ........................................................... 408
Displaying Terrain-SVS Data ....................................... 409
Terrain-SVS Page ...................................................... 411
Terrain-SVS Alerts ..................................................... 413
System Status ........................................................... 415
6.7 TAWS-B ................................................................. 417
Displaying TAWS-B Data ............................................ 418
TAWS-B Page ........................................................... 421
TAWS-B Alerts .......................................................... 423
System Status ........................................................... 429
6.8 Profile View Terrain ............................................. 431
Profile View Display .................................................. 431
Profile Path .............................................................. 433
6.9 Traffic Information Service (TIS) ........................ 435
Displaying TRAFFIC Data ........................................... 436
Traffic Map Page ....................................................... 438
TIS Alerts ................................................................. 439
System Status ........................................................... 441
6.10 TAS/TCAS I Traffic ................................................ 443
Theory of Operation .................................................. 443
Traffic Alerts ............................................................. 447
System Test .............................................................. 448
Operation ................................................................ 449
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Controls ...................................................... 458
7.2 Flight Director Operation ................................... 460
Activating the Flight Director ..................................... 460
AFCS Status Box ....................................................... 461
Flight Director Modes ................................................ 462
Switching Flight Directors .......................................... 462
Command Bars ......................................................... 463
Underspeed Protection .............................................. 464
7.3 Vertical Modes ..................................................... 466
Pitch Hold Mode (PIT) ............................................... 467
Selected Altitude Capture Mode (ALTS) ....................... 468
Altitude Hold Mode (ALT) .......................................... 469
Vertical Speed Mode (VS) .......................................... 470
Flight Level Change Mode (FLC) ................................. 471
Glideslope Mode (GS) ............................................... 478
Take Off and Go Around Modes (TO/GA) ..................... 479
Level Mode (LVL) ...................................................... 480
7.4 Lateral Modes ...................................................... 481
Roll Hold Mode (ROL) ............................................... 482
Low Bank Mode ....................................................... 482
Heading Select Mode (HDG) ...................................... 483
Navigation Modes (GPS, VOR, LOC) ............................ 484
Approach Modes (GPS, VAPP, LOC) ............................. 485
Backcourse Mode (BC) .............................................. 487
Level Mode (LVL) ...................................................... 488
7.5 Autopilot and Yaw Damper Operation ............. 489
Flight Control ........................................................... 489
Engagement ............................................................. 490
Control Wheel Steering ............................................. 490
Disengagement ........................................................ 491
7.6 Example Flight Plan ............................................ 492
Intercepting a VOR Radial .......................................... 494
Flying a Flight Plan/GPS Course ................................. 495
Descent ................................................................... 496
Approach ................................................................. 500
Go Around/Missed Approach ..................................... 502
7.7 AFCS Annunciations and Alerts ......................... 504
AFCS Status Alerts .................................................... 504
Overspeed Protection ................................................ 505
Emergency Descent Mode ......................................... 505
190-01889-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
ix
TABLE OF CONTENTS
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision Technology (SVT) ..................... 508
SVT Operation .......................................................... 509
SVT Features ............................................................ 511
Field of View ............................................................ 520
8.2 SafeTaxi ................................................................ 522
SafeTaxi Database Cycle Number and Revision ............ 525
8.3 ChartView ............................................................. 528
ChartView Softkeys ................................................... 529
Terminal Procedures Charts ....................................... 530
Chart Options ........................................................... 538
Day/Night View ........................................................ 544
ChartView Cycle Number and Expiration Date ............. 546
8.4 FliteCharts ............................................................ 549
FliteCharts Softkeys .................................................. 550
Terminal Procedures Charts ....................................... 551
Chart Options ........................................................... 558
Day/Night View ........................................................ 562
FliteCharts Cycle Number and Expiration Date ............. 564
8.5 Airport Directory ................................................. 567
Airport Directory Database Cycle Number and Revision 568
8.6 Satellite Telephone and SMS Messaging .......... 570
Registering With Garmin Connext .............................. 570
Contacts .................................................................. 571
Telephone Communication ........................................ 575
Text Messaging (SMS) ............................................... 582
8.7 SiriusXM Satellite Radio Entertainment ........... 594
Activating SiriusXM Satellite Radio Services ................ 594
Using SiriusXM Satellite Radio ................................... 596
8.8 Scheduler .............................................................. 599
8.9 Flight Data Logging ............................................ 601
8.10 Electronic Stability & Protection (ESP
) ........... 603
Roll Engagement ...................................................... 604
Pitch Engagement..................................................... 606
High Airspeed Protection ........................................... 606
8.11 Hypoxia Recognition & Automatic Descent Mode .. 607
Determining Pilot Alertness ....................................... 607
Automatic Descent Mode .......................................... 608
8.12 Abnormal Operation ........................................... 609
SVT Troubleshooting ................................................. 609
Reversionary Mode ................................................... 609
Unusual Attitudes ..................................................... 610
APPENDICES
Annunciations and Alerts ............................................. 613
CAS Messages .......................................................... 614
G1000 System Annunciations .................................... 619
G1000 System Messages ........................................... 621
Flight Plan Import/Export Messages ........................... 634
Pilot Profile Import/Export Messages .......................... 634
AFCS Alerts .............................................................. 635
Terrain-SVS Alerts ..................................................... 636
Terrain-SVS System Status Annunciations .................... 636
TAWS-B ALERTS ........................................................ 637
TAWS-B System Status Annunciations ......................... 638
Database Management ................................................ 639
Jeppesen Databases .................................................. 640
Garmin Databases .................................................... 643
Frequently Asked Questions ........................................ 659
Map Symbols ................................................................. 663
INDEX
Index ................................................................................ I-1
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
190-01889-00 Rev. Bx
TABLE OF CONTENTS
Blank Page
190-01889-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
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 Mirage.
The G1000 system is an integrated flight control system that presents flight instrumentation, position, navigation,
communication, and identification information to the pilot through large-format displays. The system consists of
the following Line Replaceable Units (LRUs):
GDU 1040
Primary Flight Display (PFD)
GTX 33
Extended Squitter Mode S Transponder
GDU 1240A
Multi Function Display (MFD)
GCU 476
MFD/PFD Control Unit
GIA 63W
Integrated Avionics Unit
GMC 710
AFCS Control Unit
GDC 74A
Air Data Computer (ADC)
GTP 59
Outside Air Temperature (OAT) Probe
GEA 71
Engine/Airframe Unit
GSA 80/81
AFCS Servos
GMU 44
Magnetometer
GSM 86
Servo Gearboxes
GRS 77
Attitude and Heading Reference System
(AHRS)
GMA 350
Audio Panel with Integrated Marker
Beacon Receiver
A top-level G1000 system block diagram is shown in Figure 1-1 (it does not include the GSM 86). The G1000
is capable of interfacing with the following optional equipment:
GTX 33
Extended Squitter Mode S Transponder KN 63 DME
GDL 69
Satellite Data Link Receiver Becker 3504 ADF
GRC 10/GRT 10
Remote Control Transceiver ARTEX ELT
GWX 68
Weather Radar WX-500 Stormscope
GTS 825/855
Traffic Avoidance System
GSR 56
Iridium Transceiver
NOTE: Refer to the AFCS section for details on the Garmin AFCS.
In the Piper Mirage, the Garmin Automated Flight Control System (AFCS) provides the flight director (FD),
autopilot (AP), and yaw damper (YD) functions of the G1000 system.
190-01889-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
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 1040
(2) – Each unit is configured as a PFD that features a 10.4-inch LCD with 1024 x 768 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, the MFD, and with the on-side GIA 63W
Integrated Avionics Unit through a High-Speed Data Bus (HSDB) connection.
GDU 1240A
(1) – Features a 12-inch LCD with 1024 x 768 resolution and is configured as an MFD. This unit
is linked to both PFDs via HSDB connection.
GIA 63W
(2) – Functions as the main communication hub, linking all LRUs with the on-side PFD. 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 on-side PFD via HSDB connection. The GIA
63Ws are not paired together and do not communicate with each other directly.
GDC 74A
(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 G1000 system, and it communicates
with the on-side GIA 63W, on-side GDU 1040 and on-side GRS 77, using an ARINC 429 digital interface (it
also interfaces directly with the on-side GTP 59). The GDC 74A is designed to operate in Reduced Vertical
Separation Minimum (RVSM) airspace.
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.
GRS 77
(2) – Provides aircraft attitude and heading information via ARINC 429 to both the on-side GDU 1040
and the on-side GIA 63W. The GRS 77 contains advanced sensors (including accelerometers and rate sensors)
and interfaces with the on-side GMU 44 to obtain magnetic field information, with the GDC 74A to obtain air
data, and with both GIA 63Ws to obtain GPS information. AHRS modes of operation are discussed later in this
document.
GMU 44
(2) – Measures local magnetic field. Data is sent to the GRS 77 for processing to determine aircraft
magnetic heading. This unit receives power directly from the GRS 77 and communicates with the GRS 77,
using an RS-485 digital interface.
GMA 350
(1) – The Audio Panel integrates NAV/COM audio, intercom, telephone, and marker beacon controls
(refer to the Audio Panel & CNS Section). This unit communicates with both GIA 63Ws, using an RS-232
digital interface.
190-01889-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
3
SYSTEM OVERVIEW
GTX 33 ES
(1 or 2) – The GTX 33 ES is a solid-state transponder that provide Modes A, C, S and ADS-B
capability. Both transponders can be controlled from either PFD, and only one transponder can be active at a
time. Each transponder communicates with the on-side GIA 63W through an RS-232 digital interface.
GCU 476 (1) – The Control Unit provides MFD/PFD and radio tuning control through an RS-232 digital
interface.
GMC 710
(1) – Provides the controls for the Garmin AFCS through an RS-232 digital interface allowing
communication with both PFDs.
GTP 59
(2) – Provides Outside Air Temperature (OAT) data to the on-side GDC 74A.
GSA 80
(1),
GSA 81
(3) and
GSM 86
(4) – The GSA 80/81 servos are used for the automatic control of roll,
pitch, and yaw, and pitch trim. These units interface with each GIA 63W.
The GSM 86 servo gearbox is responsible for transferring the output torque of the GSA 81 servo actuator to the
mechanical flight-control surface linkage.
GWX 68
(1)(optional) – Provides airborne weather and ground mapped radar data to the MFD, through the
GDL 69, via HSDB connection.
GDL 69
(1)(optional) – A satellite radio receiver that provides real-time weather information to the G1000 MFD
(and, indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL 69 communicates
with the MFD via HSDB connection. A subscription to the XM Satellite Radio service is required to enable the
GDL 69 digital audio entertainment capability.
GRC 10 Remote Control (optional with GDL 69)
GRT 10
Remote Control Transceiver (optional with GDL 69)
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 56 is connected
to the #2 GIA 63W with an RS-232 digital interface.
GTS 825/855
(1)(optional)– The GTS 825 Traffic Advisory System (TAS), and the GTS 855 TCAS I, use active
interrogations of Mode S and Mode C transponders to provide traffic information to the pilot independent of
the air traffic control system.
190-01889-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
4
SYSTEM OVERVIEW
#1
GDU 1040
(PFD1)
KN-63
(DME)
#1 GIA 63W
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
AFCS Mode
Logic
Flight
Director
Servo
Management
#2 GIA 63W
(Integrated
Avionics
Unit)
VHF COM
GPS/SBAS
VOR/LOC
G/S
AFCS Mode
Logic
Flight
Director
Servo
Management
#2
GDU 1040
(PFD2)
Non-Garmin Equipment
RA-3504
(ADF)
WX-500
(Lightning
Detection)
ARTEX ELT
(ELT)
#1 GTX 33 w/ES or
GTX 33D w/ES
(Transponder)
#2 GTX 33 w/ES
(Transponder)
#3
GDU 1240A
(MFD)
GEA 71
(Engine & Airframe
I/F)
#1 GDC 74A
(Air Data
Computer)
#2 GDC 74A
(Air Data
Computer)
#1 GRS 77
(Attitude &
Heading)
#2 GRS 77
(Attitude &
Heading)
Optional
Garmin Equipment
Optional
Non-Garmin Equipment
#1 GMA 44
(Magnetometer)
#2 GMA 44
(Magnetometer)
GTS 825/855
(TAS/TCAS I)
Garmin Equipment
GCU 476
(Display
Controller)
GWX 68
(Weather
Radar)
GSA 80(1)/81(3)
(Garmin AFCS
Servos)
GMA 350
(Audio
Panel)
GDL 69
(XM Weather/
Audio Datalink)
GRT 10/GRC 10
(XM Remote
Control)
GSR 56
(Iridium)
Reversionary
Switch
Reversionary
Switch
GMC 710
(AFCS Mode
Controller)
Figure 1-1 G1000 System (LRU Configuration)
190-01889-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
5
SYSTEM OVERVIEW
1.3 G1000 CONTROLS
NOTE: The Audio Panel (GMA 350) and AFCS controls (GMC 710) are described in the CNS & Audio Panel
and AFCS sections respectively.
The G1000 system controls are located on the PFD bezels, MFD/PFD Control Unit, AFCS Control Unit 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 Controls
1718
5
6
8
7
2
4
31 9
12
16
11
10
15
14
13
1
NAV VOL/ID Knob
Turn to control NAV audio volume (shown in the NAV Frequency Box as a
percentage)
Press to toggle Morse code identifier audio ON/OFF
2
NAV Frequency
Transfer Key
Transfers the standby and active NAV frequencies
3
NAV Knob
Turn to tune NAV receiver standby frequencies (large knob for MHz; small for kHz)
Press to toggle cyan tuning box between NAV1 and NAV2
4
Heading Knob
Turn to manually select a heading
Press to display a digital heading momentarily to the left of the HSI and synchronize
the Selected Heading to the and current heading
190-01889-00 Rev. B
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
6
SYSTEM OVERVIEW
5
Joystick
Turn to change map range
Press to activate Map Pointer for map panning
6
CRS/BARO Knob
Turn large knob for altimeter barometric pressure setting
Turn small knob to adjust course (only when HSI is in VOR or OBS Mode)
Press to re-center the CDI and return course pointer directly TO bearing of active
waypoint/station
7
COM Knob
Turn to tune COM transceiver standby frequencies (large knob for MHz; small for
kHz)
Press to toggle cyan tuning box between COM1 and COM2
The selected COM (green) is controlled with the COM MIC Key (Audio Panel).
8
COM Frequency
Transfer Key
(EMERG)
Transfers the standby and active COM frequencies
Press and hold 2 seconds to tune the emergency frequency (121.5 MHz) automatically
into the active frequency field
9
COM VOL/SQ Knob
Turn to control COM audio volume level (shown as a percentage in the COM
Frequency Box)
Press to turn the COM automatic squelch ON/OFF
10
Direct-to Key ( )
Activates the direct-to function and allows the user to enter a destination waypoint
and establish a direct course to the selected destination (specified by identifier,
chosen from the active route)
11
FPL Key
Displays flight plan information
12
CLR Key
(DFLT MAP)
Erases information, cancels entries, or removes menus
Press and hold to display the MFD Navigation Map Page (MFD only).
13
MENU Key
Displays a context-sensitive list of options for accessing additional features or making
setting changes
14
PROC Key
Gives access to IFR departure procedures (DPs), arrival procedures (STARs), and
approach procedures (IAPs) for a flight plan or selected airport
15
ENT Key
Validates/confirms menu selection or data entry
16
FMS Knob
(Flight Management
System Knob)
Press to turn the selection cursor ON/OFF.
Data Entry: With cursor ON, turn to enter data in the highlighted field (large
knob moves cursor location; small knob selects character for highlighted cursor
location)
Scrolling: When a list of information is too long for the window/box, a scroll bar
appears, indicating more items to view. With cursor ON, turn large knob to scroll
through the list.
Page Selection: Turn knob on MFD to select the page to view (large knob selects a
page group; small knob selects a specific page from the group)
17
Softkey Selection
Keys
Press to select softkey shown above the bezel key on the PFD/MFD display
18
ALT Knob
Sets the Selected Altitude, shown above the Altimeter (the large knob selects the
thousands, the small knob selects the hundreds)
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Garmin G1000: Piper PA-46 M350 Mirage Reference guide

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Reference guide
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