Garmin G1000 - Piper PA-46 M350 Mirage Reference guide

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

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)

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