Garmin G1000 NXi - Piper PA-28-181 Archer Reference guide

Piper PA-28-181 Archer

G1000

®

Integrated Flight Deck

Pilot’s Guide

G1000

®

Pilot’s Guide

Piper PA-28-181

Archer

190-02130-00

Revision A

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 AT, Inc.

2345 Turner Road SE

Salem, OR 97302, U.S.A.

Tel: 503.581.8101

Fax 503.364.2138

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 Corporation

No. 68, Zhangshu 2nd Road

Xizhi District,

New Taipei City, Taiwan

Tel: 34-93-357-2608

Fax: 34-93-429-4484

www.garmin.com

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-28-181 Archer

190-02130-00 Rev. C

This manual reﬂects the operation of System Software version 2698.00 or later for the Piper PA-28-181 Archer. 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

®

, FliteCharts

®

, and SafeTaxi

®

are registered trademarks of Garmin International, Inc. or its subsidiaries. Garmin SVT

™

,

SurfaceWatch

™

, and Connext

™

are trademarks of Garmin International, Inc. or its subsidiaries. These trademarks may not be used without

the express permission of Garmin.

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.

190-02130-00 Rev. C

Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer

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.

October 2016 Printed in the U.S.A.

Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer

190-02130-00 Rev. Civ

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 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.

190-02130-00 Rev. C

Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer

v

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: 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 use TAWS information for primary terrain or obstacle avoidance. TAWS is intended only

to enhance situational awareness.

WARNING

:

Because of variation in the earth’s magnetic ﬁeld, do not rely on the accuracy of attitude and

heading indications 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).

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.

Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer

190-02130-00 Rev. Cvi

WARNINGS, CAUTIONS, AND NOTES

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.

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.

190-02130-00 Rev. C

Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer

vii

WARNINGS, CAUTIONS, AND NOTES

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 that have a Type 2 Letter of Authorization (LOA) from the FAA are assured

compliance with all data quality requirements (DQRs). A copy of the Type 2 LOA is available for each applicable

database and can be viewed at http://ﬂy.garmin.com by selecting ‘Aviation Database Declarations.’

• 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: 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-28-181 Archer

190-02130-00 Rev. Cviii

REVISION INFORMATION

Record of Revisions

Part Number Revision Date Page Range Description

190-02130-00 A

B

C

10/11/16

10/12/16

10/31/16

i – I-6

Initial Release for GDU 20.02

Updated to ﬁx clerical errors

190-02130-00 Rev. C

Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer

ix

TABLE OF CONTENTS

SECTION 1 SYSTEM OVERVIEW

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

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

1.3 System Controls ........................................................ 4

PFD Controls ................................................................ 4

1.4 Secure Digital Cards ................................................. 6

1.5 System Power-up ....................................................... 7

1.6 System Operation ..................................................... 8

Normal Operation ......................................................... 8

Reversionary Mode ....................................................... 8

ADAHRS Operation ....................................................... 9

System Annunciations ................................................. 11

Softkey Function ......................................................... 11

GPS Receiver Operation .............................................. 18

1.7 Accessing System Functionality ............................ 23

Menus ....................................................................... 23

MFD Page Groups ....................................................... 24

MFD System Pages...................................................... 28

1.8 Display Backlighting ............................................... 42

SECTION 2 FLIGHT INSTRUMENTS

2.1 Flight Instruments ................................................... 46

Airspeed Indicator ...................................................... 46

Attitude Indicator ....................................................... 48

Altimeter ................................................................... 49

Vertical Speed Indicator (VSI) ....................................... 52

Vertical Deviation ....................................................... 52

Horizontal Situation Indicator (HSI) .............................. 54

Course Deviation Indicator (CDI) .................................. 58

2.2 Supplemental Flight Data ...................................... 65

Temperature Displays .................................................. 65

Wind Data ................................................................. 66

Vertical Navigation (VNV) Indications ........................... 67

2.3 PFD Annunciations and Alerting Functions .......... 68

System Annunciations ................................................. 68

Marker Beacon Annunciations...................................... 69

Altitude Alerting ......................................................... 69

Low Altitude Annunciation .......................................... 70

Minimum Descent Altitude/Decision Height Alerting ...... 70

2.4 Abnormal Operations ............................................. 72

Abnormal GPS Conditions ........................................... 72

Unusual Attitudes ....................................................... 73

SECTION 3 ENGINE INDICATION SYSTEM

3.1 Engine Display ......................................................... 76

Engine Page ............................................................... 78

Oil Pressure and Temperature Gauges ........................... 82

Fuel Quantity ............................................................. 82

EIS Display (Reversionary Mode) .................................. 83

SECTION 4 AUDIO PANEL AND CNS

4.1 Overview .................................................................. 85

PFD Controls and Frequency Display ............................. 86

GMA 1347 Audio Panel Controls .................................. 88

4.2 COM Operation........................................................ 90

COM Transceiver Selection and Activation ..................... 90

COM Transceiver Manual Tuning .................................. 91

Quick-tuning and Activating 121.500 MHz .................... 92

Auto-tuning the COM Frequency .................................. 93

Auto-tuning from the MFD .......................................... 94

Frequency Spacing ...................................................... 97

Automatic Squelch ...................................................... 98

Volume ...................................................................... 98

4.3 NAV Operation......................................................... 99

NAV Radio Selection and Activation ............................. 99

NAV Receiver Manual Tuning ..................................... 100

Auto-tuning a NAV Frequency from the MFD ............... 102

Auto-tuning NAV Frequencies on Approach Activation .106

Marker Beacon Receiver ............................................ 107

ADF/DME Tuning ...................................................... 108

4.4 GTX 345 Mode S Transponder ............................. 112

Transponder Controls ................................................ 112

Transponder Mode Selection ...................................... 113

Entering a Transponder Code ..................................... 115

IDENT Function ........................................................ 116

4.5 Additional Audio Panel Functions ....................... 117

Power-Up ................................................................. 117

Mono/Stereo Headsets .............................................. 117

Speaker ................................................................... 117

Intercom .................................................................. 117

Passenger Address (PA) System .................................. 120

Clearance Recorder and Player ................................... 120

Split COM Operation ................................................. 121

Entertainment Inputs ................................................ 122

4.6 Audio Panel Preﬂight Procedure ......................... 123

Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer

190-02130-00 Rev. Cx

TABLE OF CONTENTS

4.7 Abnormal Operation ............................................. 124

Stuck Microphone ..................................................... 124

COM Tuning Failure ................................................... 124

Audio Panel Fail-safe Operation ................................. 124

PFD Failure, Dual System ...........................................124

SECTION 5 FLIGHT MANAGEMENT

5.1 Introduction ........................................................... 127

Navigation Status Box ............................................... 128

5.2 Using Map Displays .............................................. 130

Map Orientation ....................................................... 130

Map Range .............................................................. 132

Map Panning ............................................................ 134

Measuring Bearing and Distance ................................ 138

Topography .............................................................. 139

Map Symbols ........................................................... 142

Airways ................................................................... 148

Track Vector ............................................................. 150

Wind Vector ............................................................. 151

Fuel Range Ring ....................................................... 152

Field of View (SVt) .................................................... 153

Selected Altitude Intercept Arc ................................... 154

5.3 Waypoints .............................................................. 155

Airports ................................................................... 157

Intersections ............................................................ 163

NDBs ....................................................................... 165

VORs ....................................................................... 167

VRPs ....................................................................... 169

User Waypoints ........................................................ 171

5.4 Airspaces ................................................................ 177

5.5 Direct-to-Navigation ........................................... 181

5.6 Flight Planning ...................................................... 187

Flight Plan Creation .................................................. 188

Adding Waypoints to an Existing Flight Plan ................ 197

Adding Airways to a Flight Plan ................................. 199

Adding Procedures to a Stored Flight Plan .................. 201

Flight Plan Storage ................................................... 208

Flight Plan Editing .................................................... 210

Along Track Offsets ................................................... 214

Parallel Track ............................................................ 215

Activating a Flight Plan Leg ....................................... 218

Inverting a Flight Plan ............................................... 219

Flight Plan Views ...................................................... 220

Closest Point of FPL .................................................. 222

User-Deﬁned Holding Patterns ................................... 222

5.7 Vertical Navigation ............................................... 228

Altitude Constraints .................................................. 230

5.8 Procedures ............................................................. 234

Departures ............................................................... 235

Arrivals ................................................................... 238

Approaches ............................................................. 240

5.9 Trip Planning .......................................................... 249

Trip Planning ............................................................ 249

Weight Planning ....................................................... 253

Weight Caution And Warning Conditions .................... 255

5.10 RAIM Prediction .................................................... 256

5.11 Navigating a Flight Plan ....................................... 259

5.12 Abnormal Operation ............................................. 286

SECTION 6 HAZARD AVOIDANCE

6.1 SiriusXM Weather .................................................. 290

Activating Services .................................................... 290

Using SiriusXM Weather Products .............................. 292

6.2 FIS-B Weather ........................................................ 328

Using FIS-B Weather Products .................................... 328

FIS-B Weather Status................................................. 352

6.3 Terrain Proximity ................................................... 353

Displaying Terrain Proximity Data ............................... 353

6.4 Vertical Situation Display (VSD) Terrain ............. 358

VSD Display ............................................................. 358

Track Mode Boundary ............................................... 360

6.5 Terrain-SVT ............................................................. 362

Displaying Terrain-SVT Data ....................................... 363

Terrain-SVT Page ...................................................... 366

Terrain-SVT Alerts ..................................................... 367

Forward Looking Terrain Avoidance ............................ 368

System Status ........................................................... 370

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

Relative Terrain Symbology ........................................ 372

TAWS-B Page ........................................................... 376

TAWS-B Alerts .......................................................... 377

System Status ........................................................... 382

190-02130-00 Rev. C

Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer

xi

TABLE OF CONTENTS

6.7 Trafﬁc Information Service (TIS) .......................... 384

Displaying TRAFFIC Data ........................................... 385

Trafﬁc Map Page ....................................................... 387

TIS Alerts ................................................................. 388

System Status ........................................................... 389

6.8 GTS 800 Trafﬁc ....................................................... 392

Theory of operation .................................................. 392

TAS Alerts ................................................................ 396

System Test .............................................................. 397

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

6.9 ADS-B Trafﬁc .......................................................... 405

ADS-B System Overview ............................................ 405

ADS-B with TAS ........................................................ 406

Conﬂict Situational Awareness & Alerting ................... 407

Airborne and Surface Applications .............................. 409

Trafﬁc Description ..................................................... 410

Operation ................................................................ 410

ADS-B System Status ................................................ 416

SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM

Automatic Flight Control System .................................. 419

SECTION 8 ADDITIONAL FEATURES

8.1 Synthetic Vision Technology (SVT) ...................... 422

SVT Operation .......................................................... 423

SVT Features ............................................................ 425

Field of View ............................................................434

8.2 SafeTaxi .................................................................. 436

SafeTaxi Cycle Number and Revision .......................... 439

8.3 FliteCharts .............................................................. 442

FliteCharts Softkeys .................................................. 443

Terminal Procedures Charts ....................................... 444

Chart Options ........................................................... 447

Day/Night View ........................................................ 447

FliteCharts Cycle Number and Expiration Date ............. 448

8.4 Airport Directory ................................................... 451

Airport Directory Database Cycle Number and Revision 451

8.5 WIFI Connections .................................................. 454

8.6 SiriusXM Radio Entertainment ............................ 457

Activating SiriusXM Satellite Radio Services ................ 457

Using SiriusXM Radio ................................................ 458

8.7 Scheduler ............................................................... 462

8.8 Flight Data Logging .............................................. 464

8.9 Connext Setup ....................................................... 466

8.10 Abnormal Operation ............................................. 468

SVT Troubleshooting ................................................. 468

Reversionary Mode ................................................... 468

Unusual Attitudes ..................................................... 468

GDL 59/69/69A SXM Troubleshooting ......................... 469

APPENDICES

Annunciations and Alerts ............................................... 471

CAS Message Prioritization ........................................ 473

CAS Annunciations ................................................... 475

System Annunciations ............................................... 476

System Message Advisories ....................................... 478

Flight Plan Import/Export Messages ........................... 489

Pilot Proﬁle Import/Export Messages .......................... 490

ADS-B Status Page Messages ..................................... 491

Terrain-SVT Alerts And Annunciations ......................... 492

TAWS-B Alerts And Annunciations .............................. 493

TIS Annunciations ..................................................... 495

TAS Annunciations .................................................... 496

ADS-B Alerts and Annunciations ................................. 497

GDL 69/69A SXM Data Link Receiver Messages ........... 498

Database Management .................................................. 499

Loading Updated Databases ...................................... 499

Magnetic Field Variation Database Update .................. 508

Garmin Aviation Glossary .............................................. 509

Frequently Asked Questions .......................................... 519

General TIS Information ................................................. 523

Map Symbols ................................................................... 525

INDEX

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

Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer

190-02130-00 Rev. Cxii

TABLE OF CONTENTS

Blank Page

190-02130-00 Rev. C

Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer

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 PA-

28-181 Archer. The system is an integrated system that presents ﬂight instrumentation, position, navigation,

communication, and identiﬁcation information to the pilot through large-format displays.

The optional Flight Stream 510 device provides a Bluetooth

®

connection between the system and a mobile

device. GPS, ADAHRS, ADS-B, trafﬁc, Sirius XM audio, and FIS-B weather data can then be shared with the

mobile device, and ﬂight plans can be transferred to or from the mobile device. Also, database updates may also

be performed using the Flight Stream 510 WiFi link.

The system consists of the following Line Replaceable Units (LRUs):

•

GDU 1050

Primary Flight Display (PFD)

•

GDU 1050

Multi Function Display (MFD)

•

GIA 63W

Integrated Avionics Unit

•

GMU 44

Magnetometer

•

GSU 75

Air Data, Attitude and Heading

Reference System (ADAHRS)

•

GEA 71

Engine/Airframe Unit

•

GMA 1347

Dual Audio System with Integrated

Marker Beacon Receiver

•

GTX 335R/345R

Extended Squitter Mode S

Transponder

•

GTP 59

Outside Air Temperature (OAT) Probe

Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are also shown in Figure 1-1.

The G1000 is capable of interfacing with the following optional equipment:

•

GDL 69A SXM

Data Link Receiver

•

GTS 800

Trafﬁc Advisory System

•

GDL 59

WiFi Data Link

• KN 63 DME

• KR 87 ADF or ADF 3504

• S-TEC 55X Autopilot

190-02130-00 Rev. C

Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer

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 1050

(2) – The GDUs are conﬁgured as a Primary Flight Display (PFD) and a Multi Function Display

(MFD). Both feature 10.4-inch LCD screens with 1024 x 768 resolution. The displays communicate with

each other through a High-Speed Data Bus (HSDB) Ethernet connection. Each display is also paired with an

Ethernet connection to an IAU.

•

GIA 63W

(2) – Functions as the main communication hub, linking all LRUs with the PFD and MFD. 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 PFD and MFD via HSDB connection. The GIA

63Ws are not paired together and do not communicate with each other directly.

•

GSU 75

(1) – Processes data from the pitot/static system as well as the OAT probe to provide pressure altitude,

airspeed, vertical speed and OAT information to the system. This unit also provides aircraft attitude and

heading information via ARINC 429 to the PFD, MFD, and GIA 63W. The GSU 75B contains advanced

sensors (including accelerometers and rate sensors) and interfaces with the GMU 44 to obtain magnetic ﬁeld

information, and with the GIA 63W to obtain GPS information. ADAHRS modes of operation are discussed

later in this document.

•

GTP 59

(1) – Provides Outside Air Temperature (OAT) data to the GSU 75B.

•

GEA 71

(2) – Receives and processes signals from the engine and airframe sensors. This unit communicates

with both GIA 63Ws using an RS-485 digital interface.

•

GMU 44

(1) – Measures local magnetic ﬁeld. Data is sent to the GSU 75B for processing to determine aircraft

magnetic heading. This unit receives power directly from the GSU 75B and communicates with the GSU 75B,

using an RS-485 digital interface.

•

GMA 1347

(1) – The Audio Panel integrates navigation/communication radio (NAV/COM) digital audio,

intercom, and marker beacon controls, and is installed between the displays. This unit also provides manual

control of display reversionary mode (red

DISPLAY BACKUP

Button; see Section 1.5, System Operation) and

communicates with both IAUs using an RS-232 digital interface.

•

GTX 335R/345R

(1) – Solid-state transponders that provide Modes A, C, S and ADS-B capability. The optional

GTX 345R also provides ADS-B In/Out. The transponder can be controlled from the PFD. The transponder

communicates with the both GIA 63Ws through an RS-232 digital interface.

•

GDL 69A SXM

(1) (Optional) – A satellite radio receiver that provides data link weather information to the

MFD (and, indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL 69A

SXM communicates with the MFD via HSDB connection. Subscriptions to the SiriusXM Weather or SiriusXM

Satellite Radio services are required to enable the GDL 69A SXM capability.

•

GDL 59

(1) (Optional) – GDL 59 operation is performed with the PFD through HSDB.

•

GTS 800

(Optional) – The GTS 800 Trafﬁc Advisory System (TAS) uses active interrogations of Mode S and

Mode C transponders to provide trafﬁc information to the pilot independent of the air trafﬁc control system.

190-02130-00 Rev. C

Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

3

SYSTEM OVERVIEW

GTX 345R

Or

#1

GDU 1050

(PFD)

GDL 69A SXM

(XM Weather/

Audio Datalink)

GMA 1347

(Audio

Panel)

KN-63

(DME)

#1 GIA 63W

(Integrated

Avionics

Unit)

VHF COM

GPS/SBAS

VOR/LOC

G/S

Flight

Director

AFCS Mode

Logic

Servo Logic

#2 GIA 63W

(Integrated

Avionics

Unit)

VHF COM

GPS/SBAS

VOR/LOC

G/S

Flight

Director

AFCS Mode

Logic

Servo Logic

#2

GDU 1050

(MFD)

Non-Garmin Equipment

KR-87 or ADF 3504

(ADF)

GEA 71 (Engine &

Airframe I/F)

GTX 335R

(Transponder)

GSU 75

(ADAHRS)

Optional

Garmin Equipment

Optional

Non-Garmin Equipment

GMA 44

(Magnetometer)

GTS 800

(TAS)

Garmin Equipment

GDL 59

(Data Link)

STEC 55X

(AFCS)

Figure 1-1 System (LRU Conﬁguration)

NOTE: For information on non-Garmin equipment, consult the applicable optional interface user’s guide.

This document assumes that the reader is already familiar with the operation of this additional equipment.

190-02130-00 Rev. C

Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

4

SYSTEM OVERVIEW

1.3 SYSTEM CONTROLS

NOTE: The Audio Panel (GMA 1347) is described in the CNS & Audio Panel section.

The system controls are located on the PFD and MFD bezels and audio panel. The controls for the PFD and

MFD are discussed within the following pages of this section.

PFD CONTROLS

Figure 1-2 PFD/MFD Controls

21 5

4

6

8

7

3

11

12

10

9

15

14

13

The following list provides an overview of the controls located on the PFD/MFD bezels (see Figure 1-2).

190-02130-00 Rev. C

Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

5

SYSTEM OVERVIEW

1

NAV VOL/ID Knob

– Controls NAV audio volume level. Press to toggle the Morse code identiﬁer audio ON

and OFF. Volume level is shown in the NAV frequency ﬁeld as a percentage.

2

NAV Frequency Transfer Key

– Toggles the standby and active NAV frequencies.

3

Dual

NAV Knob

– Tunes the standby frequencies for the NAV receiver (large knob for MHz; small knob for

kHz). Press to switch the tuning box (cyan box) between NAV1 and NAV2.

4

Joystick

– Changes the map range when rotated. Activates the map pointer when pressed.

5

BARO Knob

– Sets the altimeter barometric pressure. Press to enter standard pressure (29.92).

6

Dual COM Knob

– Tunes the standby frequencies for the COM transceiver (large knob for MHz; small

knob for kHz). Press to switch the tuning box (cyan box) between COM1 and COM2.

7

COM Frequency Transfer Key

– Toggles the standby and active COM frequencies. Press and hold this

key for two seconds to tune the emergency frequency (121.5 MHz) automatically into the active frequency

ﬁeld.

8

COM

VOL/SQ Knob

– Controls COM audio volume level. Volume level is shown in the COM frequency

ﬁeld as a percentage. Press to turn the COM automatic squelch ON and OFF.

9

Direct-to Key ( )

– Allows the user to enter a destination waypoint and establish a direct course to the

selected destination (the destination is either speciﬁed by the identiﬁer, chosen from the active route, or

taken from the map pointer position).

10

FPL Key

– Displays the active Flight Plan Page for creating and editing the active ﬂight plan.

11

CLR

Key

– Erases information, cancels entries, or removes page menus.

12

Dual FMS Knob

– Flight Management System Knob. Press the

FMS

Knob to turn the selection cursor

ON and OFF. When the cursor is ON, data may be entered in the applicable window by turning the small

and large

knobs. The large

knob moves the cursor on the page, while the small

knob selects individual

characters for the highlighted cursor location.

13

MENU Key

– Displays a context-sensitive list of options. This list allows the user to access additional

features or make setting changes that relate to particular pages.

14

PROC Key

– Gives access to IFR departure procedures (DPs), arrival procedures (STARs) and approach

procedures (IAPs) for a ﬂight plan. If a ﬂight plan is used, available procedures for the departure and/or

arrival airport are automatically suggested. These procedures can then be loaded into the active ﬂight plan.

If a ﬂight plan is not used, both the desired airport and the desired procedure may be selected.

15

ENT Key

– Validates or conﬁrms a menu selection or data entry.

190-02130-00 Rev. C

Garmin G1000 Pilot’s Guide for the Piper PA-28-181 Archer

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

6

SYSTEM OVERVIEW

1.4 SECURE DIGITAL CARDS

NOTE:

Refer to the Appendices for instructions on updating the aviation databases.

NOTE:

Ensure that the system is powered off before inserting the SD card.

The GDU 1050 data card slots use Secure Digital (SD) cards and are located on the top right portion of the

display bezels. Each display bezel is equipped with two SD card slots. SD cards are used for aviation database

and system software updates as well as terrain database storage. Also, ﬂight plans may be imported or exported

from an SD card in the MFD.

Install an SD card

Insert the SD card in the SD card slot, pushing the card in until the spring latch engages. The front of the card

should remain ﬂush with the face of the display bezel.

Remove an SD card

Gently press on the SD card to release the spring latch and eject the card.

Figure 1-3 PFD/MFD Display Bezel SD Card Slots

SD Card Slots

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