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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
www.garmin.com
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, Houndsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
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f:44 (0) 23 8052 4004
Aviation Support:44 (0) 87 0850 1243
Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p:886/02.2642.9199
f:886/02.2642.9099
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
190-01889-01 Rev. A
Copyright © 2015, 2016 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 2164.07 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
Aircraft On Ground (AOG) Hotline: 913.397.0836
Aviation Dealer Technical Support: 888.606.5482
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
Tel: +44 (0) 238 052 4000
Fax: +44 (0) 238 052 4004
Aviation Support: +44 (0) 370 850 1243
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Tel: 503.581.8101
Fax 503.364.2138
Garmin Corporation
No. 68, Zhangshu 2nd Road
Xizhi District, New Taipei City, Taiwan
Tel: 34-93-357-2608
Fax: 34-93-429-4484
Website Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored
in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download
a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for
personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice
and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin
®
, G1000
®
, 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
®
is a registered trademark of Becker
Flugfunkwerk GmbH. NavData
®
is a registered trademark of Jeppesen, Inc.; Wi-Fi
®
is a registered trademark of the Wi-Fi Alliance;
SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, Inc.
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively “AOPA”) expressly disclaim all warranties,
with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties
of merchantability and fitness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any
representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any
incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if
AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to
the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual
or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for
incidental or consequential damages so the above limitations or exclusions may not apply to you.
AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”) expressly disclaim all warranties with
respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of
merchantability and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or
make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the
maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related
to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some jurisdictions
do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations
or exclusions may not apply to licensee.
Printed in the U.S.A.
190-01889-01 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
i
WARNINGS, CAUTIONS, AND NOTES
WARNING: Do not use terrain avoidance displays as the sole source of information for maintaining separation
from terrain and obstacles. Garmin obtains terrain and obstacle data from third party sources and cannot
independently verify the accuracy of the information.
WARNING: Always refer to current aeronautical charts and NOTAMs for verification of displayed aeronautical
information. Displayed aeronautical data may not incorporate the latest NOTAM information.
WARNING: Do not use geometric altitude for compliance with air traffic control altitude requirements. The
primary barometric altimeter must be used for compliance with all air traffic control altitude regulations,
requirements, instructions, and clearances.
WARNING: Do not use basemap information (land and water data) as the sole means of navigation. Basemap
data is intended only to supplement other approved navigation data sources and should be considered only
an aid to enhance situational awareness.
WARNING: Do not rely solely upon the display of traffic information to accurately depict all of the traffic
within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information
from aircraft or ground stations, traffic may be present that is not represented on the display.
WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous
weather. Information contained within data link weather products may not accurately depict current
weather conditions.
WARNING: Do not use the indicated data link weather product age to determine the age of the weather
information shown by the data link weather product. Due to time delays inherent in gathering and processing
weather data for data link transmission, the weather information shown by the data link weather product
may be significantly older than the indicated weather product age.
WARNING: The displayed minimum safe altitude (MSAs) are only advisory in nature and should not be relied
upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical
charts for appropriate minimum clearance altitudes.
WARNING: Always obtain qualified instruction prior to operational use of this equipment.
WARNING
:
Do not use a QFE altimeter setting with this system. System functions will not operate properly
with a QFE altimeter setting. Use only a QNH altimeter setting for height above mean sea level, or the
standard pressure setting, as applicable.
WARNING
:
Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a
system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that
may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned
in error as displayed.
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
190-01889-01 Rev. Aii
WARNINGS, CAUTIONS, AND NOTES
WARNING: When using the autopilot to fly an approach with vertical guidance, the autopilot will not level
the aircraft at the MDA/DH even if the MDA/DH is set in the altitude preselect.
WARNING: Do not rely solely upon the display of traffic information for collision avoidance maneuvering.
The traffic display does not provide collision avoidance resolution advisories and does not under any
circumstances or conditions relieve the pilot’s responsibility to see and avoid other aircraft.
WARNING
:
Because of variation in the earth’s magnetic field, do not rely on the accuracy of attitude and
heading indications (GRS 77 installations only) in the following geographic areas: North of 72° North
latitude at all longitudes; South of 70° South latitude at all longitudes; North of 65° North latitude between
longitude 75° W and 120° W. (Northern Canada); North of 70° North latitude between longitude 70° W and
128° W. (Northern Canada); North of 70° North latitude between longitude 85° E and 114° E. (Northern
Russia); South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and
New Zealand).
WARNING: Do not rely on information from a lightning detection system display as the sole basis for hazardous
weather avoidance. Range limitations and interference may cause the system to display inaccurate or
incomplete information. Refer to documentation from the lightning detection system manufacturer for
detailed information about the system.
WARNING:
Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance.
Garmin SVT is intended as an aid to situational awareness only and may not provide either the accuracy or
reliability upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic.
WARNING:
Intruder aircraft at or below 500 ft. AGL may not appear on the Garmin SVT display or may
appear as a partial symbol.
WARNING:
Do not use the Garmin SVT runway depiction as the sole means for determining the proximity of
the aircraft to the runway or for maintaining the proper approach path angle during landing.
WARNING: Do not operate the weather radar in a transmitting mode when personnel or objects are within
the MPEL boundary.
WARNING: Always position the weather radar gain setting to Calibrated for viewing the actual intensity of
precipitation. Changing the gain in weather mode causes precipitation intensity to be displayed as a color
not representative of the true intensity.
WARNING: Do not use TAWS information for primary terrain or obstacle avoidance. TAWS is intended only
to enhance situational awareness.
190-01889-01 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
iii
WARNINGS, CAUTIONS, AND NOTES
CAUTION: Do not clean display surfaces with abrasive cloths or cleaners containing ammonia. They will
harm the anti-reflective coating.
CAUTION:
Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or
modifications could void both the warranty and affect the airworthiness of the aircraft.
NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information.
Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control.
NOTE: All visual depictions contained within this document, including screen images of the system panel
and displays, are subject to change and may not reflect the most current system and aviation databases.
Depictions of equipment may differ slightly from the actual equipment.
NOTE: The United States government operates the Global Positioning System and is solely responsible for
its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and
performance of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation
AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or
misinterpreted and, therefore, become unsafe.
NOTE
: This device complies with part 15 of the FCC Rules. Operation is subject to the following two
conditions: (1) this device may not cause harmful interference, and (2) this device must accept any
interference received, including interference that may cause undesired operation.
NOTE
: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of
attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards
away from the source of the interference should alleviate the condition.
NOTE
: Use of polarized eyewear may cause the flight displays to appear dim or blank.
NOTE
: This product, its packaging, and its components contain chemicals known to the State of California
to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with
California’s Proposition 65. If you have any questions or would like additional information, please refer to
our web site at www.garmin.com/prop65.
NOTE: Operating the system in the vicinity of metal buildings, metal structures, or electromagnetic fields
can cause sensor differences that may result in nuisance miscompare annunciations during start up, shut
down, or while taxiing. If one or more of the sensed values are unavailable, the annunciation indicates no
comparison is possible.
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
190-01889-01 Rev. Aiv
WARNINGS, CAUTIONS, AND NOTES
NOTE: The system responds to a terminal procedure based on data coded within that procedure in the
Navigation Database. Differences in system operation may be observed among similar types of procedures
due to differences in the Navigation Database coding specific to each procedure.
NOTE
: The FAA has asked Garmin to remind pilots who fly with Garmin database-dependent avionics of the
following:
• It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory guidance and information
related to the use of databases in the National Airspace System.
• Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen. Databases
obtained from Garmin or Jeppesen 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.
NOTE: Garmin requests the flight crew report any observed discrepancies related to database information.
These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles
and fixes; or any other displayed item used for navigation or communication in the air or on the ground. Go
to FlyGarmin.com and select ‘Aviation Data Error Report’.
NOTE: Operate G1000 system power through at least one cycle in a period of four days of continuous
operation to avoid an autonomous system reboot.
NOTE: Lamp(s) inside this product 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
190-01889-01 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
v
WARNINGS, CAUTIONS, AND NOTES
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: The system supports approval of AC 120-76C Hardware Class 3, Software Type B Electronic Flight Bag
(EFB) electronic aeronautical chart applications. Possible additional requirements may make a secondary
source (traditional paper or additional electronic display) necessary onboard the aircraft. If the secondary
source is a Portable Electronic Device (PED), its use must be consistent with guidance in AC 120-76C.
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
190-01889-01 Rev. Avi
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
190-01899-01 A 12/28/16 All
Changes for GDU SW Version 15.12
Update CAS messages
Add GSR 56 Voice/Text only option
Add airway optional waypoints
Enable configuration of temperature units
190-01889-01 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
vii
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) ....................................... 64
Horizontal Situation Indicator (HSI) .............................. 65
Course Deviation Indicator (CDI) .................................. 70
2.2 Supplemental Flight Data .................................... 77
Temperature Displays .................................................. 77
Wind Data ................................................................. 78
Vertical Navigation (VNV) Indications ........................... 79
2.3 PFD Annunciations and Alerting Functions ........ 80
Marker Beacon Annunciations...................................... 80
Altitude Alerting ......................................................... 80
Low Altitude Annunciation .......................................... 81
Minimum Descent Altitude/Decision Height Alerting ...... 81
2.4 Abnormal Operations ........................................... 83
Abnormal GPS Conditions ........................................... 83
Heading Failure Modes................................................ 84
Unusual Attitudes ....................................................... 84
SECTION 3 ENGINE INDICATION SYSTEM
3.1 Engine Indication System (EIS) ............................ 89
Manifold Pressure Gauge ............................................ 90
Propeller RPM Gauge .................................................. 90
Turbine Inlet Temperature Gauge .................................. 90
Fuel Flow ................................................................... 91
Cylinder Head Temperature .......................................... 91
Oil Pressure and Temperature Gauges ........................... 91
Cabin Pressurization ................................................... 92
Pulse Oximeter ........................................................... 92
Fuel Quantity ............................................................. 93
Electrical .................................................................... 93
Flap Indicator ............................................................. 93
Landing Gear Indicator ................................................ 94
3.2 Engine Page............................................................ 95
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview ................................................................ 97
PFD Controls and Frequency Display ............................. 98
Audio Panel Controls ................................................ 100
MFD/PFD Control Unit ............................................... 102
4.2 COM Operation .................................................... 104
COM Transceiver Selection and Activation ................... 104
COM Transceiver Manual Tuning ................................ 105
Quick-tuning and Activating 121.500 MHz .................. 107
Auto-tuning the COM Frequency ................................ 108
Frequency Spacing .................................................... 113
Automatic Squelch .................................................... 114
Volume .................................................................... 114
4.3 NAV Operation ..................................................... 115
NAV Radio Selection and Activation ........................... 115
NAV Receiver Manual Tuning ..................................... 116
Auto-tuning a NAV Frequency from the MFD ............... 118
Auto-tuning NAV Frequencies on Approach Activation . 122
Marker Beacon Receiver ............................................ 122
ADF/DME Tuning ...................................................... 123
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
190-01889-01 Rev. Aviii
TABLE OF CONTENTS
4.4 GTX 33 ES Mode S Transponder(s) .................... 128
Transponder Controls ................................................ 128
Transponder Mode Selection ...................................... 129
Entering a Transponder Code ..................................... 131
IDENT Function ........................................................ 133
ADS-B TX ................................................................. 133
4.5 Additional Audio Panel Functions ..................... 134
Power-Up ................................................................. 134
Mono/Stereo Headsets .............................................. 134
Speaker ................................................................... 134
Passenger Address Mode (PA Mode) ........................... 134
Clearance Recorder and Player ................................... 134
Intercom System (ICS) .............................................. 135
Split COM Mode ....................................................... 140
Entertainment Inputs ................................................ 141
4.6 Audio Panels Preflight Procedure ...................... 142
Audio Panel Preflight ................................................ 142
4.7 Abnormal Operation ........................................... 143
Audio Panel Fail-safe Operation ................................. 143
Stuck Microphone ..................................................... 143
COM Tuning Failure ................................................... 143
PFD Failure, Dual System ........................................... 143
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 145
Navigation Status Box and Data Bar ........................... 146
5.2 Using Map Displays ............................................. 148
Map Orientation ....................................................... 148
Map Range .............................................................. 150
Map Panning ............................................................ 152
Measuring Bearing and Distance ................................ 158
Topography .............................................................. 159
Map Symbols ........................................................... 162
Airways ................................................................... 168
Track Vector ............................................................. 170
Wind Vector ............................................................. 171
Nav Range Ring........................................................ 172
Fuel Range Ring ....................................................... 173
Field of View (SVT) .................................................... 174
Selected Altitude Intercept Arc ................................... 175
5.3 Waypoints ............................................................. 176
Airports ................................................................... 177
Intersections ............................................................ 184
NDBs ....................................................................... 186
VORs ....................................................................... 188
VRPs ....................................................................... 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 ........................................... 307
SECTION 6 HAZARD AVOIDANCE
6.1 SiriusXM Weather ................................................ 310
Activating Services ................................................... 310
Using SiriusXM Weather Products .............................. 311
6.2 Garmin Connext Weather ................................... 345
Registering the system for Garmin Connext Weather .... 345
Accessing Garmin Connext Weather Products .............. 347
Connext Weather Data Requests ................................ 353
Garmin Connext Weather Products ............................. 357
Abnormal Operations ................................................ 369
190-01889-01 Rev. A
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
ix
TABLE OF CONTENTS
6.3 Airborne Color Weather Radar .......................... 371
System Description ................................................... 371
Principles of Pulsed Airborne Weather Radar ............... 371
NEXRAD and Airborne Weather Radar ....................... 372
Antenna Beam Illumination ....................................... 372
Safe Operating Distance ............................................ 375
Basic Antenna Tilt Setup ............................................ 376
Weather Mapping and Interpretation ......................... 378
Ground Mapping and Interpretation ........................... 388
Weather Radar Overlay on the Navigation Map Page ... 389
System Status ........................................................... 391
6.4 Stormscope Lightning ......................................... 393
Setting Up Stormscope on the Navigation Map ........... 394
Selecting the Stormscope Page .................................. 397
6.5 Terrain Proximity ................................................. 399
Displaying Terrain Proximity Data ............................... 400
Terrain Proximity Page ............................................... 403
6.6 Terrain-SVS ........................................................... 405
Displaying Terrain-SVS Data ....................................... 406
Terrain-SVS Page ...................................................... 408
Terrain-SVS Alerts ..................................................... 411
System Status ........................................................... 413
6.7 TAWS-B ................................................................. 415
Displaying TAWS-B Data ............................................ 416
TAWS-B Page ........................................................... 419
TAWS-B Alerts .......................................................... 421
System Status ........................................................... 427
6.8 Profile View Terrain ............................................. 429
Profile View Display .................................................. 429
Profile Path .............................................................. 431
6.9 Traffic Information Service (TIS) ........................ 433
Displaying TRAFFIC Data ........................................... 434
Traffic Map Page ....................................................... 436
TIS Alerts ................................................................. 437
System Status ........................................................... 439
6.10 TAS/TCAS I Traffic ................................................ 441
Theory of Operation .................................................. 441
Traffic Alerts ............................................................. 445
System Test .............................................................. 446
Operation ................................................................ 447
6.11 Garmin ADS-B Traffic ........................................... 455
ADS-B System Overview ............................................ 455
ADS-B with TAS ........................................................ 457
Conflict Situational Awareness & Alerting ................... 457
Airborne and Surface Applications .............................. 460
Traffic Description ..................................................... 461
Operation ................................................................ 461
System Status ........................................................... 470
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Controls ...................................................... 474
7.2 Flight Director Operation ................................... 476
Activating the Flight Director ..................................... 476
AFCS Status Box ....................................................... 477
Flight Director Modes ................................................ 478
Switching Flight Directors .......................................... 478
Command Bars ......................................................... 479
Underspeed Protection .............................................. 480
7.3 Vertical Modes ..................................................... 482
Pitch Hold Mode (PIT) ............................................... 483
Selected Altitude Capture Mode (ALTS) ....................... 484
Altitude Hold Mode (ALT) .......................................... 485
Vertical Speed Mode (VS) .......................................... 486
Flight Level Change Mode (FLC) ................................. 487
Glideslope Mode (GS) ............................................... 494
Take Off and Go Around Modes (TO/GA) ..................... 495
Level Mode (LVL) ...................................................... 496
7.4 Lateral Modes ...................................................... 497
Roll Hold Mode (ROL) ............................................... 498
Low Bank Mode ....................................................... 498
Heading Select Mode (HDG) ...................................... 499
Navigation Modes (GPS, VOR, LOC) ............................ 500
Approach Modes (GPS, VAPP, LOC) ............................. 501
Backcourse Mode (BC) .............................................. 503
Level Mode (LVL) ...................................................... 504
7.5 Autopilot and Yaw Damper Operation ............. 505
Flight Control ........................................................... 505
Engagement ............................................................. 506
Control Wheel Steering ............................................. 506
Disengagement ........................................................ 507
Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage
190-01889-01 Rev. Ax
TABLE OF CONTENTS
7.6 Example Flight Plan ............................................ 508
Intercepting a VOR Radial .......................................... 510
Flying a Flight Plan/GPS Course ................................. 511
Descent ................................................................... 512
Approach ................................................................. 516
Go Around/Missed Approach ..................................... 518
7.7 AFCS Annunciations and Alerts ......................... 520
AFCS Status Alerts .................................................... 520
Overspeed Protection ................................................ 521
Emergency Descent Mode ......................................... 521
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision Technology (SVT) ..................... 524
SVT Operation .......................................................... 525
SVT Features ............................................................ 527
Field of View ............................................................ 536
8.2 SafeTaxi ................................................................ 538
SafeTaxi Database Cycle Number and Revision ............ 541
8.3 ChartView ............................................................. 544
ChartView Softkeys ................................................... 545
Terminal Procedures Charts ....................................... 546
Chart Options ........................................................... 554
Day/Night View ........................................................ 560
ChartView Cycle Number and Expiration Date ............. 562
8.4 FliteCharts ............................................................ 565
FliteCharts Softkeys .................................................. 566
Terminal Procedures Charts ....................................... 567
Chart Options ........................................................... 574
Day/Night View ........................................................ 578
FliteCharts Cycle Number and Expiration Date ............. 580
8.5 Airport Directory ................................................. 583
Airport Directory Database Cycle Number and Revision 584
8.6 Satellite Telephone and SMS Messaging .......... 586
Registering With Garmin Connext .............................. 586
Contacts .................................................................. 587
Telephone Communication ........................................ 591
Text Messaging (SMS) ............................................... 598
8.7 SiriusXM Satellite Radio Entertainment ........... 610
Activating SiriusXM Satellite Radio Services ................ 610
Using SiriusXM Satellite Radio ................................... 612
8.8 Scheduler .............................................................. 615
8.9 Flight Data Logging ............................................ 617
8.10 Electronic Stability & Protection (ESP
™
) ........... 619
Roll Engagement ...................................................... 620
Pitch Engagement..................................................... 622
High Airspeed Protection ........................................... 622
8.11 Hypoxia Recognition & Automatic Descent Mode .. 623
Determining Pilot Alertness ....................................... 623
Automatic Descent Mode .......................................... 624
8.12 Abnormal Operation ........................................... 625
SVT Troubleshooting ................................................. 625
Reversionary Mode ................................................... 625
Unusual Attitudes ..................................................... 626
APPENDICES
Annunciations and Alerts ............................................. 629
CAS Messages .......................................................... 630
System Annunciations ............................................... 635
System Messages ..................................................... 637
Flight Plan Import/Export Messages ........................... 650
Pilot Profile Import/Export Messages .......................... 650
ADS-B Status Page Messages ..................................... 651
AFCS Alerts .............................................................. 652
Terrain-SVS Alerts ..................................................... 653
TAWS-B Alerts .......................................................... 654
TIS Annunciations ..................................................... 655
TAS/TCAS Annunciations ........................................... 656
ADS-B TAS Annunciations .......................................... 657
GDL 69A SXM .......................................................... 658
Weather Radar Annunciations .................................... 658
Database Management ................................................ 661
Navigation Databases ............................................... 662
Dual Navigation Database Feature ............................ 664
Garmin Databases .................................................... 666
Frequently Asked Questions ........................................ 685
Map Symbols ................................................................. 689
Hazard Avoidance Features ........................................ 691
INDEX
Index ................................................................................ I-1
190-01889-01 Rev. A
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 33/33D
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 SXM
Satellite Data Link Receiver • Becker RA-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.
190-01889-01 Rev. A
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.
190-01889-01 Rev. A
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 33/33D 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 SXM
(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.
190-01889-01 Rev. A
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 SXM
(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)
190-01889-01 Rev. A
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
190-01889-01 Rev. A
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)
/
