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

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

190-01108-00 Rev. B

This manual reﬂects the operation of System Software version 0720.10 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

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

®

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 XM Satellite Radio, Inc.

October 2009 Printed in the U.S.A.

190-01108-00 Rev. B

Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix

i

LIMITED WARRANTY

This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this

period, Garmin will, at its sole option, 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 labor, provided that the customer shall be responsible for any transportation cost. This warranty

does not cover failures due to abuse, misuse, accident, or unauthorized alterations or repairs.

THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR 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 to you.

Garmin retains the exclusive right to repair or replace the unit or software, or to 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 a Service Center near you, visit

the Garmin Website at “http://www.garmin.com” or contact Garmin Customer Service at 800-800-1020.

Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix

190-01108-00 Rev. Bii

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.

190-01108-00 Rev. B

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:

For safety reasons, G1000 operational procedures must be learned on the ground.

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 anomalies 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 70° North latitude and south

of 70° South latitude. An area north of 65° North latitude between longitude 75º West and 120º West. An

area south of 55° South latitude between longitude 120º East and 165º East.

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.

Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix

190-01108-00 Rev. Biv

WARNINGS, CAUTIONS, AND NOTES

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.

190-01108-00 Rev. B

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

Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix

190-01108-00 Rev. Bvi

TABLE OF CONTENTS

SECTION 1 SYSTEM OVERVIEW

1.1 System Description ................................................. 1

1.2 Line Replaceable Units (LRU) ................................. 2

1.3 G1000 Controls ........................................................ 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 Display Inhibits .................................................... 96

CAS Messages and Prioritization .................................. 97

SECTION 4 AUDIO PANEL AND CNS

4.1 Overview .............................................................. 101

PFD Controls and Frequency Display ........................... 102

GMA 347 Audio Panel Controls .................................. 104

MFD/PFD Control Unit ............................................... 106

4.2 COM Operation .................................................... 108

COM Transceiver Selection and Activation ................... 108

COM Transceiver Manual Tuning ................................ 109

Quick-tuning and Activating 121.500 MHz .................. 110

Auto-tuning the COM Frequency ................................ 111

Frequency Spacing .................................................... 116

Automatic Squelch .................................................... 117

Volume .................................................................... 117

4.3 NAV Operation ..................................................... 118

NAV Radio Selection and Activation ........................... 118

NAV Receiver Manual Tuning ..................................... 119

Auto-tuning a NAV Frequency from the MFD ............... 121

Auto-tuning NAV Frequencies on Approach Activation . 125

190-01108-00 Rev. B

Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix

vii

TABLE OF CONTENTS

Marker Beacon Receiver ............................................ 126

DME Tuning ............................................................. 127

4.4 GTX 33 Mode S Transponder .............................. 128

Transponder Controls ................................................ 128

Transponder Mode Selection ...................................... 129

Entering a Transponder Code ..................................... 132

IDENT Function ........................................................ 133

Flight ID Reporting.................................................... 134

4.5 Additional Audio Panel Functions ..................... 135

Power-Up ................................................................. 135

Mono/Stereo Headsets .............................................. 135

Speaker ................................................................... 135

Intercom .................................................................. 136

Passenger Address (PA) System .................................. 138

Clearance Recorder and Player ................................... 138

Entertainment Inputs ................................................ 139

4.6 Audio Panel Preﬂight Procedure ....................... 140

4.7 Abnormal Operation ........................................... 141

Audio Panel Fail-safe Operation ................................. 141

Stuck Microphone ..................................................... 141

COM Tuning Failure ................................................... 141

SECTION 5 FLIGHT MANAGEMENT

5.1 Introduction ......................................................... 143

Navigation Status Box ............................................... 145

5.2 Using Map Displays ............................................. 146

Map Orientation ....................................................... 146

Map Range .............................................................. 148

Map Panning ............................................................ 151

Measuring Bearing and Distance ................................ 156

Topography .............................................................. 157

Map Symbols ........................................................... 160

Airways ................................................................... 166

Track Vector ............................................................. 168

Wind Vector ............................................................. 169

Nav Range Ring........................................................ 170

Fuel Range Ring ....................................................... 171

Field of View (SVS) .................................................... 172

5.3 Waypoints ............................................................. 173

Airports ................................................................... 174

Intersections ............................................................ 181

NDBs ....................................................................... 183

VORs ....................................................................... 185

User Waypoints ........................................................ 187

5.4 Airspaces .............................................................. 193

5.5 Direct-to-Navigation .......................................... 198

5.6 Flight Planning ..................................................... 204

Flight Plan Creation .................................................. 205

Adding Waypoints to an Existing Flight Plan ................ 210

Adding Airways to a Flight Plan ................................. 212

Adding Procedures to a Stored Flight Plan .................. 215

Flight Plan Storage ................................................... 222

Flight Plan Editing .................................................... 224

Along Track Offsets ................................................... 227

Parallel Track ............................................................ 229

Activating a Flight Plan Leg ....................................... 232

Inverting a Flight Plan ............................................... 233

Flight Plan Views ...................................................... 234

Closest Point of FPL .................................................. 236

5.7 Vertical Navigation ............................................. 237

Altitude Constraints .................................................. 239

5.8 Procedures ........................................................... 243

Departures ............................................................... 243

Arrivals ................................................................... 246

Approaches ............................................................. 248

5.9 Trip Planning ........................................................ 254

Trip Planning ............................................................ 254

Weight Planning ....................................................... 258

Weight Caution And Warning Conditions .................... 260

5.10 RAIM Prediction................................................... 261

5.11 Navigating a Flight Plan ..................................... 265

5.12 Abnormal Operation ........................................... 293

SECTION 6 HAZARD AVOIDANCE

6.1 XM Satellite Weather .......................................... 295

Using XM SATELLITE Weather Products ....................... 297

Weather Softkeys on the Weather Data Link Page ........ 300

6.2 Airborne Color Weather Radar .......................... 327

System Description ................................................... 327

Principles of Pulsed Airborne Weather Radar ............... 327

Safe Operating Distance ............................................ 332

Basic Antenna Tilt Setup ............................................ 332

Weather Mapping and Interpretation ......................... 334

Ground Mapping and Interpretation ........................... 347

Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix

190-01108-00 Rev. Bviii

TABLE OF CONTENTS

6.3 Stormscope .......................................................... 348

Setting Up Stormscope on the Navigation Map ........... 348

Selecting the Stormscope Page .................................. 352

6.4 Terrain Proximity ................................................. 355

Displaying Terrain Proximity Data ............................... 356

Terrain Proximity Page ............................................... 358

6.5 TERRAIN-SVS ........................................................ 360

Displaying TERRAIN-SVS Data .................................... 361

TERRAIN-SVS Page ................................................... 364

TERRAIN-SVS Alerts .................................................. 366

6.6 TAWS-B .................................................................371

Displaying TAWS-B Data ............................................ 372

TAWS-B Alerts .......................................................... 376

6.7 Trafﬁc Information Service (TIS) ........................ 387

Displaying TRAFFIC Data ........................................... 388

Trafﬁc Map Page ....................................................... 391

TIS Alerts ................................................................. 392

System Status ........................................................... 393

6.8 Trafﬁc Advisory System (TAS)............................. 397

TAS Symbology ......................................................... 397

Operation ................................................................ 398

Altitude Display ........................................................ 401

Trafﬁc Map Page Display Range ................................. 401

TAS Alerts ................................................................ 403

System Status ........................................................... 403

SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM

7.1 AFCS Controls ...................................................... 406

7.2 Flight Director Operation ................................... 409

Activating the Flight Director ..................................... 409

AFCS Status Box ....................................................... 410

Flight Director Modes ................................................ 411

Switching Flight Directors .......................................... 411

7.3 Vertical Modes ..................................................... 413

Pitch Hold Mode (PIT) ............................................... 414

Selected Altitude Capture Mode (ALTS) ....................... 415

Altitude Hold Mode (ALT) .......................................... 416

Vertical Speed Mode (VS) .......................................... 417

Flight Level Change Mode (FLC) ................................. 418

Vertical Navigation Modes (VPTH, ALTV) ..................... 420

Glidepath Mode (GP) ................................................ 425

Glideslope Mode (GS) ............................................... 427

Go Around Mode (GA) .............................................. 428

7.4 Lateral Modes ...................................................... 429

Roll Hold Mode (ROL) ............................................... 430

Low Bank Mode ....................................................... 430

Heading Select Mode (HDG) ...................................... 431

Navigation Modes (GPS, VOR, LOC) ............................ 432

Approach Modes (GPS, VAPP, LOC) ............................. 434

Backcourse Mode (BC) .............................................. 436

7.5 Autopilot and Yaw Damper Operation ............. 437

Flight Control ........................................................... 437

Engagement ............................................................. 438

Control Wheel Steering ............................................. 438

Disengagement ........................................................ 439

7.6 Example Flight Plan ............................................ 440

Intercepting a VOR Radial .......................................... 442

Flying a Flight Plan/GPS Course ................................. 443

Descent ................................................................... 444

Approach ................................................................. 448

Go Around/Missed Approach ..................................... 450

7.6 AFCS Annunciations and Alerts .........................452

AFCS Status Alerts .................................................... 452

Overspeed Protection ................................................ 453

SECTION 8 ADDITIONAL FEATURES

8.1 Synthetic Vision System (SVS) ........................... 456

SVS Operation .......................................................... 457

SVS Features ............................................................ 459

Field of View ............................................................ 467

8.2 SafeTaxi ................................................................ 469

SafeTaxi Cycle Number and Revision .......................... 472

8.3 ChartView ............................................................. 475

ChartView Softkeys ................................................... 475

ChartView Terminal Procedures Charts ........................ 476

Chart Options ........................................................... 484

Day/Night View ........................................................ 490

ChartView Cycle Number and Expiration Date ............. 492

8.4 FliteCharts ............................................................ 495

FliteCharts Softkeys .................................................. 495

FliteCharts Terminal Procedures Charts ....................... 496

Chart Options ........................................................... 503

Day/Night View ........................................................ 507

FliteCharts Cycle Number and Expiration Date ............. 509

8.5 AOPA Airport Directory ....................................... 512

AOPA Database Cycle Number and Revision ............... 512

190-01108-00 Rev. B

Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix

ix

TABLE OF CONTENTS

8.6 XM Radio Entertainment .................................... 515

Activating XM Satellite Radio Services ........................ 515

Using XM Radio ....................................................... 517

8.7 Scheduler .............................................................. 520

8.8 Flight Data Logging ............................................ 522

8.9 Abnormal Operation ........................................... 524

SVS Troubleshooting ................................................. 524

Reversionary Mode ................................................... 524

Unusual Attitudes ..................................................... 525

APPENDICES

Annunciations and Alerts ............................................. 529

CAS Messages .......................................................... 529

G1000 System Annunciations .................................... 534

G1000 System Message Advisories ............................. 537

AFCS Alerts .............................................................. 548

Terrain-SVS Alerts ..................................................... 549

Terrain-SVS System Status Annunciations .................... 549

TAWS ALERTS ........................................................... 550

Flight plan Import/Export Messages ........................... 551

SD Card Use ................................................................... 553

Jeppesen Databases .................................................. 553

Garmin Databases .................................................... 556

Glossary .......................................................................... 563

Frequently Asked Questions ........................................ 571

Map Symbols ................................................................. 575

INDEX

Index ................................................................................I-1

Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix

190-01108-00 Rev. Bx

TABLE OF CONTENTS

Bl a n k Pa g e

190-01108-00 Rev. B

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.

190-01108-00 Rev. B

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 WAAS 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.

190-01108-00 Rev. B

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.

190-01108-00 Rev. B

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.

190-01108-00 Rev. B

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.

190-01108-00 Rev. B

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/WAAS

G/S

AFCS Mode Logic

Flight Director

Servo Management

VHF COM

VHF NAV/LOC

GPS/WAAS

G/S

AFCS Mode Logic

Flight Director

Servo Management

(optional)

GRT10/GRC10

Figure 1-1 G1000 System (LRU Conﬁguration)

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