Garmin G1000 - Piper PA-46 Mirage/Matrix User guide

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User guide

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Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p:913.397.8200
f:913.397.8282
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
p:503.391.3411
f:503.364.2138
Garmin (Europe) Ltd.
Liberty House, Bulls Copse Road
Houndsdown Business Park
Southampton, SO40 9RB, U.K.
p:44/0870.8501241
f:44/0870.8501251
Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p:886/02.2642.9199
f:886/02.2642.9099
www.garmin.com
Piper PA-46 Mirage/Matrix
G1000
®
Integrated Flight Deck
Pilot’s Guide
G1000
®
Pilot’s Guide
Piper PA-46
Mirage/Matrix
190-01108-00
Revision B
Untitled-1 1 11/13/2007 9:15:37 AM
SYSTEM OVERVIEW
FLIGHT INSTRUMENTS
ENGINE INDICATION & CREW ALERTING 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/Matrix
190-01108-02 Rev. A
Copyright © 2009-2011 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0720.13 or later for the Piper Mirage/Matrix. 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, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB, U.K
Tel: 44/0870.8501241 Fax: 44/0870.8501251
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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and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin
®
is a registered trademark of Garmin Ltd. or its subsidiaries, and G1000
®
is a trademark of Garmin Ltd. or its subsidiaries. These
trademarks may not be used without the express permission of Garmin.
Bendix/King
®
and Honeywell
®
are registered trademarks of Honeywell International, Inc.; NavData
®
is a registered trademark of Jeppesen,
Inc.; and XM
®
is a registered trademark of 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.
July 2011 Printed in the U.S.A.
190-01108-02 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix
i
LIMITED WARRANTY
LIMITED WARRANTY
Within the warranty period, Garmin will, at its sole discretion, repair or replace any components that fail in normal use. Such repairs or
replacement will be made at no charge to the customer for parts and/or labor incidental to the direct repair of said product. Garmin may,
at its discretion with prior approval, reimburse an authorized Garmin Service Center for associated labor costs incurred for removal and
replacement of the panel mount product installed in an aircraft. The customer shall be responsible for any transportation or other cost. This
warranty does not apply to: (i) cosmetic damage, such as scratches, nicks and dents; (ii) consumable parts, such as batteries, unless product
damage has occurred due to a defect in materials or workmanship; (iii) damage caused by accident, abuse, misuse, water, flood, fire, or
other acts of nature or external causes; (iv) damage caused by service performed by anyone who is not an authorized service provider
of Garmin; or (v) damage to a product that has been modified or altered without the written permission of Garmin. In addition, Garmin
reserves the right to refuse warranty claims against products or services that are obtained and/or used in contravention of the laws of any
country.
THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES, WHETHER EXPRESS,
IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A
PARTICULAR PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM
STATE TO STATE.
IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER
RESULTING FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not
allow the exclusion of incidental or consequential damages, so the above limitations may not apply in every case.
Garmin retains the exclusive right to repair or replace (with a new or newly-overhauled replacement product) the product or offer a full
refund of the purchase price at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF
WARRANTY.
To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating the nearest Service Center, call
Garmin Customer Service at one of the numbers listed below.
Products sold through online auctions are not eligible for warranty coverage or rebates or other special offers from Garmin. Online auction
confirmations are not accepted for warranty verification. To obtain warranty service, an original or copy of the sales receipt from the original
retailer is required. Garmin will not replace missing components from any package purchased through an online auction.
Garmin International Inc.
1200 East 151st Street, Olathe, Kansas 66062
Telephone: (913)397-8200
Telephone Toll Free: (888)606-5482
Facsimile: (913)397-8282
Facsimile Toll Free: (800)801-4670
Garmin (Europe) Ltd.
Liberty House, Bulls Copse Road, Southampton, SO40
9RB, UK
Telephone: ++44 (0) 870-8501243
Telephone Toll Free: ++44 (0) 0808 238 0000
(option 5)
Facsimile: ++44 (0) 238052004
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix
190-01108-02 Rev. Aii
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: Traffic information shown on system displays is provided as an aid in visually acquiring traffic.
Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting
traffic.
WARNING: Use of the Stormscope is not intended for hazardous weather penetration (thunderstorm
penetration). Stormscope information, as displayed on the G1000 MFD, is to be used only for weather
avoidance, not penetration.
WARNING: GDL 69 Weather should not be used for hazardous weather penetration. Weather information
provided by the GDL 69 is approved only for weather avoidance, not penetration.
WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent
delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for
short-range weather avoidance.
WARNING:
For safety reasons, G1000 operational procedures must be learned on the ground.
190-01108-02 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix
iii
WARNINGS, CAUTIONS, AND NOTES
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 the G1000 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)
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-46 Mirage/Matrix
190-01108-02 Rev. Aiv
WARNINGS, CAUTIONS, AND NOTES
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: 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.
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.
190-01108-02 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix
v
REVISION INFORMATION
Record of Revisions
Part Number Revision Date Page Range Description
190-01108-00 A 9/29/09 - Initial Release with GDU SW Version 10.01
190-01108-00 B 10/21/09 All Complete Book Revision with GDU SW Version 10.01
190-01108-01 A 1/14/11 All Added Split COM
190-01108-02 A 7/14/11 All Complete Book Revision with GDU SW Version 12.01
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix
190-01108-02 Rev. Avi
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................. 1
1.2 Line Replaceable Units (LRU) ................................. 2
1.3 G1000 Controls ........................................................ 7
PFD Controls ................................................................ 7
MFD/PFD Control Unit ................................................. 10
AFCS Controls ............................................................ 12
Audio Panel Controls .................................................. 14
1.4 Secure Digital Cards.............................................. 16
1.5 System Power-up ................................................... 16
1.6 System Operation .................................................. 18
Normal Operation ....................................................... 18
Reversionary Mode ..................................................... 18
AHRS Operation ......................................................... 20
G1000 System Annunciations ...................................... 21
Softkey Function ......................................................... 22
GPS Receiver Operation .............................................. 28
1.7 Accessing G1000 Functionality............................ 33
Menus ....................................................................... 33
MFD Page Groups ....................................................... 33
MFD System Pages...................................................... 38
1.8 Display Backlighting ............................................. 50
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 54
Airspeed Indicator ...................................................... 54
Attitude Indicator ....................................................... 56
Altimeter ................................................................... 57
Vertical Speed Indicator (VSI) ....................................... 61
Vertical Deviation ....................................................... 61
Horizontal Situation Indicator (HSI) .............................. 62
Course Deviation Indicator (CDI) .................................. 67
2.2 Supplemental Flight Data .................................... 75
Temperature Displays .................................................. 75
Wind Data ................................................................. 76
Vertical Navigation (VNV) Indications ........................... 77
2.3 PFD Annunciations and Alerting Functions ........ 78
System Alerting .......................................................... 78
Traffic Annunciation .................................................... 79
Terrain Annunciations ................................................. 79
Altitude Alerting ......................................................... 80
Low Altitude Annunciation .......................................... 80
Minimum Descent Altitude/Decision Height Alerting ...... 81
Marker Beacon Annunciations...................................... 82
2.4 Abnormal Operations ........................................... 83
Abnormal GPS Conditions ........................................... 83
Unusual Attitudes ....................................................... 84
SECTION 3 ENGINE INDICATION AND CREW
ALERTING SYSTEM (EICAS)
3.1 Engine Indication System (EIS) ............................ 87
Manifold Pressure Gauge ............................................ 89
Propeller RPM Gauge .................................................. 89
Turbine Inlet Temperature Gauge .................................. 90
Fuel Flow Gauge ........................................................ 90
Cylinder Head Temperature .......................................... 91
Oil Pressure and Temperature Gauges ........................... 92
Cabin Pressurization (Mirage Only) .............................. 92
Oxygen Gauge (Matrix Only) ....................................... 93
Fuel Quantity ............................................................. 93
Electrical Information .................................................. 94
Vacuum Pressure ........................................................ 94
Flap Indicator ............................................................. 94
3.2 Crew Alerting System (CAS) ................................. 95
CAS Messages and Prioritization .................................. 96
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview ................................................................ 99
PFD Controls and Frequency Display ........................... 100
GMA 347 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 .................. 108
Auto-tuning the COM Frequency ................................ 109
Frequency Spacing .................................................... 114
Automatic Squelch .................................................... 115
Volume .................................................................... 115
4.3 NAV Operation ..................................................... 116
NAV Radio Selection and Activation ........................... 116
NAV Receiver Manual Tuning ..................................... 117
Auto-tuning a NAV Frequency from the MFD ............... 119
Auto-tuning NAV Frequencies on Approach Activation . 123
Marker Beacon Receiver ............................................ 124
DME Tuning ............................................................. 125
190-01108-02 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix
vii
TABLE OF CONTENTS
4.4 GTX 33 Mode S Transponder .............................. 126
Transponder Controls ................................................ 126
Transponder Mode Selection ...................................... 127
Entering a Transponder Code ..................................... 130
IDENT Function ........................................................ 131
Flight ID Reporting.................................................... 132
4.5 Additional Audio Panel Functions ..................... 133
Power-Up ................................................................. 133
Mono/Stereo Headsets .............................................. 133
Speaker ................................................................... 133
Intercom .................................................................. 134
Passenger Address (PA) System .................................. 136
Clearance Recorder and Player ................................... 136
Split COM ................................................................ 137
Entertainment Inputs ................................................ 138
4.6 Audio Panel Preflight Procedure ....................... 139
4.7 Abnormal Operation ........................................... 140
Audio Panel Fail-safe Operation ................................. 140
Stuck Microphone ..................................................... 140
COM Tuning Failure ................................................... 140
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 141
Navigation Status Box ............................................... 142
5.2 Using Map Displays ............................................. 144
Map Orientation ....................................................... 144
Map Range .............................................................. 146
Map Panning ............................................................ 149
Measuring Bearing and Distance ................................ 154
Topography .............................................................. 155
Map Symbols ........................................................... 158
Airways ................................................................... 164
Track Vector ............................................................. 166
Wind Vector ............................................................. 167
Nav Range Ring........................................................ 168
Fuel Range Ring ....................................................... 169
Field of View (SVS) .................................................... 170
Selected Altitude Intercept Arc ................................... 171
5.3 Waypoints ............................................................. 172
Airports ................................................................... 173
Intersections ............................................................ 180
NDBs ....................................................................... 182
VORs ....................................................................... 184
User Waypoints ........................................................ 186
5.4 Airspaces .............................................................. 192
5.5 Direct-to-Navigation ..........................................197
5.6 Flight Planning ..................................................... 203
Flight Plan Creation .................................................. 204
Adding Waypoints to an Existing Flight Plan ................ 209
Adding Airways to a Flight Plan ................................. 211
Adding Procedures to a Stored Flight Plan .................. 214
Flight Plan Storage ................................................... 221
Flight Plan Editing .................................................... 223
Along Track Offsets ................................................... 226
Parallel Track ............................................................ 228
Activating a Flight Plan Leg ....................................... 231
Inverting a Flight Plan ............................................... 232
Flight Plan Views ...................................................... 233
Closest Point of FPL .................................................. 235
5.7 Vertical Navigation ............................................. 236
Altitude Constraints .................................................. 239
5.8 Procedures ...........................................................242
Departures ............................................................... 242
Arrivals ................................................................... 245
Approaches ............................................................. 247
5.9 Trip Planning ........................................................ 253
Trip Planning ............................................................ 253
Weight Planning ....................................................... 257
Weight Caution And Warning Conditions .................... 259
5.10 RAIM Prediction................................................... 260
5.11 Navigating a Flight Plan ..................................... 264
5.12 Abnormal Operation ........................................... 293
SECTION 6 HAZARD AVOIDANCE
6.1 XM WX Satellite Weather ................................... 296
Activating Services .................................................... 296
Using XM WX SATELLITE Weather Products ................. 298
Weather Softkeys on the Weather Data Link (XM) Page 301
6.2 Airborne Color Weather Radar .......................... 328
System Description ................................................... 328
Principles of Pulsed Airborne Weather Radar ............... 328
Safe Operating Distance ............................................ 333
Basic Antenna Tilt Setup ............................................ 333
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix
190-01108-02 Rev. Aviii
TABLE OF CONTENTS
Weather Mapping and Interpretation ......................... 335
Ground Mapping and Interpretation ........................... 348
6.3 Stormscope Lightning ......................................... 349
Setting Up Stormscope on the Navigation Map ........... 349
Selecting the Stormscope Page .................................. 353
6.4 Terrain Proximity ................................................. 356
Displaying Terrain Proximity Data ............................... 357
Terrain Proximity Page ............................................... 359
6.5 Terrain-SVS ........................................................... 361
Displaying Terrain-SVS Data ....................................... 362
Terrain-SVS Page ...................................................... 365
Terrain-SVS Alerts ..................................................... 367
System Status ........................................................... 371
6.6 TAWS-B ................................................................. 372
Displaying TAWS-B Data ............................................ 373
TAWS-B Alerts .......................................................... 377
System Status ........................................................... 384
6.7 Traffic Information Service (TIS) ........................ 386
Displaying TRAFFIC Data ........................................... 387
Traffic Map Page ....................................................... 390
TIS Alerts ................................................................. 391
System Status ........................................................... 392
6.8 Traffic Advisory System (TAS)............................. 395
TAS Symbology ......................................................... 395
Operation ................................................................ 396
Altitude Display ........................................................ 399
Traffic Map Page Display Range ................................. 399
TAS Alerts ................................................................ 401
System Status ........................................................... 401
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Controls ...................................................... 404
7.2 Flight Director Operation ................................... 407
Activating the Flight Director ..................................... 407
AFCS Status Box ....................................................... 408
Flight Director Modes ................................................ 409
Switching Flight Directors .......................................... 409
7.3 Vertical Modes ..................................................... 411
Pitch Hold Mode (PIT) ............................................... 412
Selected Altitude Capture Mode (ALTS) ....................... 413
Altitude Hold Mode (ALT) .......................................... 414
Vertical Speed Mode (VS) .......................................... 415
Flight Level Change Mode (FLC) ................................. 416
Vertical Navigation Modes (VPTH, ALTV) ..................... 418
Glidepath Mode (GP) ................................................ 423
Glideslope Mode (GS) ............................................... 425
Go Around Mode (GA) .............................................. 426
7.4 Lateral Modes ...................................................... 427
Roll Hold Mode (ROL) ............................................... 428
Low Bank Mode ....................................................... 428
Heading Select Mode (HDG) ...................................... 429
Navigation Modes (GPS, VOR, LOC) ............................ 430
Approach Modes (GPS, VAPP, LOC) ............................. 432
Backcourse Mode (BC) .............................................. 434
7.5 Autopilot and Yaw Damper Operation ............. 435
Flight Control ........................................................... 435
Engagement ............................................................. 436
Control Wheel Steering ............................................. 436
Disengagement ........................................................ 437
7.6 Example Flight Plan ............................................ 438
Intercepting a VOR Radial .......................................... 440
Flying a Flight Plan/GPS Course ................................. 441
Descent ................................................................... 442
Approach ................................................................. 446
Go Around/Missed Approach ..................................... 448
7.7 AFCS Annunciations and Alerts ......................... 450
AFCS Status Alerts .................................................... 450
Overspeed Protection ................................................ 451
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision System (SVS) ........................... 454
SVS Operation .......................................................... 455
SVS Features ............................................................ 457
Field of View ............................................................ 465
8.2 SafeTaxi ................................................................ 467
SafeTaxi Cycle Number and Revision .......................... 470
8.3 ChartView ............................................................. 473
ChartView Softkeys ................................................... 473
ChartView Terminal Procedures Charts ........................ 474
Chart Options ........................................................... 482
Day/Night View ........................................................ 488
ChartView Cycle Number and Expiration Date ............. 490
8.4 FliteCharts ............................................................ 493
FliteCharts Softkeys .................................................. 493
FliteCharts Terminal Procedures Charts ....................... 494
Chart Options ........................................................... 501
190-01108-02 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix
ix
TABLE OF CONTENTS
Day/Night View ........................................................ 505
FliteCharts Cycle Number and Expiration Date ............. 507
8.5 AOPA Airport Directory ....................................... 510
AOPA Database Cycle Number and Revision ............... 511
8.6 SiriusXM Satellite Radio Entertainment ........... 513
Activating SiriusXM Satellite Radio Services ................ 513
Using SiriusXM Satellite Radio ................................... 515
8.7 Scheduler .............................................................. 518
8.8 Flight Data Logging ............................................ 520
8.9 Abnormal Operation ........................................... 522
SVS Troubleshooting ................................................. 522
Reversionary Mode ................................................... 522
Unusual Attitudes ..................................................... 523
APPENDICES
Annunciations and Alerts ............................................. 527
CAS Messages .......................................................... 527
G1000 System Annunciations .................................... 532
G1000 System Message Advisories ............................. 535
Flight plan Import/Export Messages ........................... 546
AFCS Alerts .............................................................. 547
Terrain-SVS Alerts ..................................................... 548
Terrain-SVS System Status Annunciations .................... 548
TAWS-B ALERTS ........................................................ 549
TAWS-B System Status Annunciations ......................... 550
Database Management ................................................ 551
Jeppesen Databases .................................................. 551
Garmin Databases .................................................... 555
Glossary .......................................................................... 561
Frequently Asked Questions ........................................ 569
Map Symbols ................................................................. 573
INDEX
Index ................................................................................ I-1
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix
190-01108-02 Rev. Ax
TABLE OF CONTENTS
Blank Page
190-01108-02 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix
1
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section provides an overview of the G1000 Integrated Flight Deck as installed in the Piper Mirage/Matrix.
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)
•
GDU 1500
Multi Function Display (MFD)
•
GIA 63W
Integrated Avionics Unit
•
GDC 74A
Air Data Computer (ADC)
•
GEA 71
Engine/Airframe Unit
•
GRS 77
Attitude and Heading Reference System
(AHRS)
•
GMU 44
Magnetometer
•
GMA 347
Audio Panel with Integrated Marker
Beacon Receiver
•
GTX 33
Mode S Transponder
•
GDL 69A
Satellite Data Link Receiver (optional)
GRC 10 Remote Control (optional with GDL 69A)
GRT 10
Remote Control Transceiver (optional
with GDL 69A)
•
GWX 68
Weather Radar (optional on Matrix)
•
GCU 476
MFD/PFD Control Unit
•
GMC 710
AFCS Control Unit
•
GTP 59
Outside Air Temperature (OAT) Probe
•
GSA 80/81
AFCS Servos
•
GSM 85A
Servo Gearboxes
A top-level G1000 system block diagram is shown in Figure 1-1 (it does not include the GSM 85A).
NOTE: Refer to the AFCS section for details on the GFC 700 AFCS.
In the Piper Mirage/Matrix, the GFC 700 Automated Flight Control System (AFCS) provides the flight director
(FD), autopilot (AP), and yaw damper (YD) functions of the G1000 system.
190-01108-02 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix
2
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
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 and the MFD through a High-Speed Data Bus
(HSDB) connection.
•
GDU 1500
(1) – Features a 15-inch LCD with 1024 x 768 resolution and is configured as an MFD. This unit
is linked to both PFDs, GIA #2, and the optional GWX 68 via HSDB connection.
•
GIA 63W
(2) – Functions as the main communication hub, linking all LRUs with PFD1 and the MFD. Each
GIA 63W contains a GPS SBAS receiver, VHF COM/NAV/GS receivers, a flight director (FD) and system
integration microprocessors. The GIA 63Ws are not paired together and do not communicate with each other
directly.
190-01108-02 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix
3
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
•
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 communicate with
both GIA 63Ws, the on-side PFD, the MFD (GDC2 only), and the 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 PFD, the
MFD (GRS2 only), and both GIA 63Ws. 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.
190-01108-02 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix
4
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
•
GMA 347
(1) – Integrates NAV/COM digital audio, intercom system and marker beacon controls. This unit
communicates with both GIA 63Ws, using an RS-232 digital interface.
•
GTX 33
(1 or 2) – Solid-state transponders that provide Modes A, C and S 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.
•
GWX 68
(1)(optional) – Provides airborne weather and ground mapped radar data to the MFD via HSDB
connection.
•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 GFC 700 AFCS through an RS-232 digital interface allowing
communication with PFD1 and the MFD.
190-01108-02 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix
5
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
•
GTP 59
(2) – Provides Outside Air Temperature (OAT) data to the on-side GDC 74A.
•
GSA 81
(3),
GSA 80
(1) and
GSM 85A
(4) – The GSA 81/80 servos are used for the automatic control of roll,
pitch, and yaw, and pitch trim. These units interface with each GIA 63W.
The GSM 85A servo gearbox is responsible for transferring the output torque of the GSA 81 servo actuator to
the mechanical flight-control surface linkage.
•
GDL 69A
(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 69A
communicates with PFD1 via HSDB connection. A subscription to the XM Satellite Radio service is required to
enable the GDL 69A capability.
•
GRT 10
(1, optional) – A transceiver that provides wireless functionality to the GDL 69A for use of the GRC 10
Remote Control.
•
GRC 10
(1, optional) – A wireless hand-held unit that provides remote control of the XM Radio functions.
190-01108-02 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix
6
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
GDU 1040
(PFD #1)
GDU 1040
(PFD #2)
GDU1500
(MFD)
GIA63W #2
GSA 80
(Pitch Trim)
GSA 81
(Roll)
GSA 81
(Pitch)
GSA 81
(Yaw)
GRS77#1
GIA 63W #1
GMC 710
GMU44#1
GEA 71
GDC 74A #1
GTP59#1
GMA 347
GTX 33 #1
(optional)
GTX 33 #2
GCU 476
(optional)
GWX 68
(optional)
GDL 69A
GRS77#2
GMU44#2
GDC 74A #2
GTP59#2
VHF COM
VHF NAV/LOC
GPS/SBAS
G/S
AFCS Mode Logic
Flight Director
Servo Management
VHF COM
VHF NAV/LOC
GPS/SBAS
G/S
AFCS Mode Logic
Flight Director
Servo Management
(optional)
GRT10/GRC10
Figure 1-1 G1000 System (LRU Configuration)
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Garmin G1000 - Piper PA-46 Mirage/Matrix User guide

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