Garmin G1000: Quest Kodiak 100 Reference guide

Garmin International, Inc.

1200 East 151st Street

Olathe, KS 66062, U.S.A.

p:913.397.8200

f:913.397.8282

Garmin AT, Inc.

2345 Turner Road SE

Salem, OR 97302, U.S.A.

p:503.391.3411

f:503.364.2138

Garmin (Europe) Ltd.

Liberty House, Hounsdown Business Park

Southampton, Hampshire SO40 9LR U.K.

p:44 (0) 23 8052 4000

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

www.garmin.com

Quest KODIAK

®

100

G1000

®

Integrated Avionics System

Pilot’s Guide

G1000

®

Pilot’s Guide

Quest KODIAK

®

100

190-00590-07

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 Quest KODIAK

®

100

190-00590-08 Rev. A

This manual reﬂects the operation of System Software version 0552.23 or later for the Quest KODIAK

®

100. Some differences in

operation may be observed when comparing the information in this manual to earlier or later software versions.

Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.

Tel: 913/397.8200 Fax: 913/397.8282

Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.

Tel: 503/391.3411 Fax: 503/364.2138

Garmin (Europe) Ltd., Liberty House, Hounsdown Business Park, Southampton, SO40 9LR, U.K

Tel: 44 (0) 23 8052 4000 Fax: 44 (0) 23 8052 4004 Aviation Support:44 (0) 87 0850 1243

Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan

Tel: 886/02.2642.9199 Fax: 886/02.2642.9099

For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please

contact Garmin’s AOG Hotline at 913.397.0836.

Website Address: www.garmin.com

Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored

in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download

a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for

personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice

and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.

Garmin

®

and G1000

®

are registered trademarks of Garmin Ltd. or its subsidiaries. FliteCharts

®

, SafeTaxi

®

, and Garmin ESP

™

are trademarks

of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin.

Bendix/King

®

and Honeywell

®

are registered trademarks of Honeywell International, Inc.; NavData

®

is a registered trademark of Jeppesen,

Inc.; Stormscope

®

is a registered trademark of L-3 Communications; Avidyne

®

and TCAD

®

are registered trademarks of Avidyne Corporation;

and KODIAK

®

is a registered trademark of Quest Aircraft Compapny. 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.

July 2015 Printed in the U.S.A

190-00590-08 Rev. A

Garmin G1000 Pilot’s Guide for the Quest KODIAK

®

100

i

WARNINGS, CAUTIONS, AND NOTES

WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance

feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance

and does not relieve the pilot from the responsibility of being aware of surroundings during ﬂight. The

terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from

third party sources. Garmin is not able to independently verify the accuracy of the terrain data.

WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be

relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current

aeronautical charts for appropriate minimum clearance altitudes.

WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and

could vary signiﬁcantly from the altitude displayed by pressure altimeters, such as the GDC 74 Air Data

Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always

use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.

WARNING: Do not use outdated database information. Databases used in the G1000 system must be updated

regularly in order to ensure that the information remains current. Pilots using any outdated database do so

entirely at their own risk.

WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is

intended only to supplement other approved navigation data sources and should be considered as an aid to

enhance situational awareness.

WARNING: 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 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 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: 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.

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190-00590-08 Rev. Aii

WARNINGS, CAUTIONS, AND NOTES

WARNING:

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

WARNING:

The Garmin system, as installed in this aircraft, has a very high degree of functional integrity.

However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable

system failures is not practical.

WARNING:

The United States government operates the Global Positioning System and is solely responsible

for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy

and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic

NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be

misused or misinterpreted and, therefore, become unsafe.

WARNING:

To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000

Pilot’s Guide documentation and the G1000 Integrated Avionics System in the Airplane Flight Manual.

Thoroughly practice basic operation prior to actual use. During ﬂight operations, carefully compare indications

from the G1000 to all available navigation sources, including the information from other NAVAIDs, visual

sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation.

WARNING: Do not use the system to attempt to penetrate a thunderstorm. The illustrations in this guide are

only examples. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information

Manual (AIM) recommend avoiding any thunderstorm identiﬁed as severe of giving intense radar echo by

at least 20 miles.

WARNING

:

Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of

according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/

aboutGarmin/environment/disposal.jsp.

WARNING

:

Because of variation in the earth’s magnetic ﬁeld, operating the system within the following

areas could result in loss of reliable attitude and heading indications. North of 72° North latitude at all

longitudes; South of 70° South latitude at all longitudes; North of 65° North latitude between longitude

75° W and 120° W. (Northern Canada); North of 70° North latitude between longitude 70° W and 128° W.

(Northern Canada); North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia);

South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New

Zealand)

WARNING

:

Do not use GPS to navigate to any active waypoint identiﬁed as a ‘NON WGS84 WPT’ by a

system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that

may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned

in error as displayed.

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.

190-00590-08 Rev. A

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iii

WARNINGS, CAUTIONS, AND NOTES

CAUTION: The PFD and MFD displays use a lens coated with a special anti-reﬂective coating that is very

sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE

ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an

eyeglass lens cleaner that is speciﬁed as safe for anti-reﬂective coatings.

CAUTION:

The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by

an authorized Garmin service center. Unauthorized repairs or modiﬁcations could void both the warranty

and the pilot’s authority to operate this device under FAA/FCC regulations.

NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby

thunderstorms that can cause isolated discharge points in the strike display mode. However, clusters of

two or more discharge points in the strike display mode do indicate thunderstorm activity if these points

reappear after the screen has been cleared.

NOTE: 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 G1000 panel and

displays, are subject to change and may not reﬂect the most current G1000 system and aviation databases.

Depictions of equipment may differ slightly from the actual equipment.

NOTE

: This device complies with part 15 of the FCC Rules. Operation is subject to the following two

conditions: (1) this device may not cause harmful interference, and (2) this device must accept any

interference received, including interference that may cause undesired operation.

NOTE

: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of

attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards

away from the source of the interference should alleviate the condition.

NOTE

: Use of polarized eyewear may cause the ﬂight displays to appear dim or blank.

NOTE

: This product, its packaging, and its components contain chemicals known to the State of California

to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with

California’s Proposition 65. If you have any questions or would like additional information, please refer to

our web site at www.garmin.com/prop65.

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190-00590-08 Rev. Aiv

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 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 to

coordinate the revised DQRs.

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 ‘Report An Aviation Data Error Report.’

190-00590-08 Rev. A

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®

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v

REVISION INFORMATION

Record of Revision

Part Number Revision Date Page Range Description

190-00590-00

A

B

C

3/21/07

4/3/07

6/22/07

All

Initial Release

Added Print Speciﬁcation Reference to Cover Sheet

Revised AMPS Engine Gauge

190-00590-01 A 10/13/08 All Added GDU 8.20 parameters including gradient PFD

Added WAAS

Revised Flight Instruments/Annunciations

Added Weight Planning Page

Rewrote GPS Nav section to become Flight Management section

Added FliteCharts, ChartView, and SafeTaxi

Corrected various clerical errors

Changes for new book format

Added GDU 9.03 changes

Added SVS

190-00590-02 A 7/31/09 All Added GDU 9.1x changes

Added GDU 10.00 changes

Corrected various clerical errors

190-00590-03 A 5/7/10 All Added TKS Ice Protection Indications

Updated wind options

Enabled groundspeed and current track line on PFD

190-00590-04 A 11/5/10 All Updated Ice Protection display on the Engne System Page

Updated CAS messages

190-00590-05 A 1/6/12 All Added GWX 68

Added GTS 800

Updated CAS messages

- Remove Bleed Air On and Aux Bus On advisory annunciations

- Add AIR COND INH annunciation

Added Dynamic reference approach speed (green circle)

190-00590-06 A 3/12/14 All Added GDU 12.10, 13.0, & 14.01 changes

Added Garmin AFCS

Added Garmin ESP

Added Maintenance Log feature

Added AC-U-KWIK Airport Directory

Added User Deﬁned Holding Patterns

Added Temperature Compensated Altitudes

Added Weather Radar Overlay

Added Proﬁle View

Updated system messages

Garmin G1000 Pilot’s Guide for the Quest KODIAK

®

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190-00590-08 Rev. Avi

REVISION INFORMATION

190-00590-06 B 5/1/14 All Changed KODIAK

™

to KODIAK

®

Incorporated Quest comments on the Garmin AFCS

-

Removed automatic activation of Low Bank Mode

-

GA switch does not uncouple autopilot

-

Roll Trim does not uncouple autopilot

Corrections to USP and ESP

Added Database notes

Updated System Software Number for GDU 14.02

190-00590-07 A 8/29/14 All

Corrected Underspeed Protection CAS Warning

Added AFCS Conﬁg CAS Warning

Added AFCS Conﬁg alerts window message

Corrected CRG part number on Aux System Status Page

Updated System Software Number

190-00590-08 A 7/21/15 All

Updated to GDU 14.04

Updated to GDL 69A SXM

Updated Fuel Indications

Updated CAS Messages

Updated System Software Number

190-00590-08 Rev. A

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vii

TABLE OF CONTENTS

SECTION 1 SYSTEM OVERVIEW

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

1.2 Line Replaceable Units ........................................... 2

1.3 G1000 Controls ........................................................ 6

PFD/MFD Controls ........................................................ 6

Controls Associated With the MFD ................................. 8

Audio Panel Controls .................................................... 9

1.4 Secure Digital (SD) Cards .....................................11

1.5 System Power-Up .................................................. 12

1.6 System Operation .................................................. 13

Normal Display Operation ........................................... 13

Reversionary Mode ..................................................... 13

AHRS Operation ......................................................... 14

G1000 System Annunciations ...................................... 16

Softkey Function ......................................................... 17

GPS Receiver Operation .............................................. 23

1.7 Accessing G1000 Functionality............................ 28

Menus ....................................................................... 28

Data Entry.................................................................. 28

MFD Page Groups ....................................................... 29

System Setup and Status ............................................. 32

1.8 Display Backlighting ............................................. 49

SECTION 2 FLIGHT INSTRUMENTS

2.1 Flight Instruments ................................................. 54

Airspeed Indicator ...................................................... 54

Attitude Indicator ....................................................... 56

Altimeter ................................................................... 57

Vertical Speed Indicator (VSI) ....................................... 61

Vertical Deviation ....................................................... 61

Horizontal Situation Indicator (HSI) .............................. 62

Course Deviation Indicator (CDI) .................................. 67

2.2 Supplemental Flight Data .................................... 75

Temperature Displays .................................................. 75

Wind Data ................................................................. 76

Vertical Navigation (VNV) Indications ........................... 77

2.3 PFD Annunciations and Alerting Functions ........ 78

System Alerting .......................................................... 78

Marker Beacon Annunciations...................................... 79

Trafﬁc Annunciation .................................................... 80

TAWS Annunciations ................................................... 81

Altitude Alerting ......................................................... 81

Low Altitude Annunciation .......................................... 82

Minimum Descent Altitude/Decision Height Alerting ...... 82

2.4 Abnormal Operations ........................................... 84

Abnormal GPS Conditions ........................................... 84

Heading Failure Modes................................................ 85

Unusual Attitudes ....................................................... 85

SECTION 3 ENGINE INDICATION SYSTEM (EIS)

3.1 Engine Display ....................................................... 90

3.2 System Display ...................................................... 92

3.3 Fuel Display ............................................................ 94

SECTION 4 AUDIO PANEL AND CNS

4.1 Overview ................................................................ 97

MFD/PFD Controls and Frequency Display ..................... 98

Audio Panel Controls ................................................ 100

4.2 COM Operation .................................................... 102

COM Transceiver Selection and Activation ................... 102

COM Transceiver Manual Tuning ................................ 103

Quick-tuning and Activating 121.500 MHz .................. 104

Auto-tuning the COM Frequency ................................ 105

Frequency Spacing .................................................... 109

Automatic Squelch .................................................... 110

Volume .................................................................... 110

4.3 NAV Operation ..................................................... 111

NAV Radio Selection and Activation ........................... 111

NAV Receiver Manual Tuning ..................................... 112

Auto-tuning a NAV Frequency from the MFD ............... 114

Auto-tuning NAV Frequencies on Approach Activation . 118

Marker Beacon Receiver ............................................ 119

4.4 GTX 33 Mode S Transponder .............................. 120

Transponder Controls ................................................ 120

Transponder Mode Selection ...................................... 121

Entering a Transponder Code ..................................... 124

IDENT Function ........................................................ 125

4.5 Additional Audio Panel Functions ..................... 126

Power-up ................................................................. 126

Mono/Stereo Headsets .............................................. 126

Speaker ................................................................... 126

Intercom .................................................................. 127

Passenger Address (PA) System .................................. 129

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TABLE OF CONTENTS

Simultaneous COM Operation .................................... 129

Clearance Recorder and Player ................................... 130

Entertainment Inputs ................................................ 131

4.6 Audio Panels Preﬂight Procedure ...................... 132

4.7 Abnormal Operation ........................................... 134

Stuck Microphone ..................................................... 134

COM Tuning Failure ................................................... 134

PFD Failure, Dual System ........................................... 135

Audio Panel Fail-safe Operation ................................. 136

Reversionary Mode ................................................... 136

SECTION 5 FLIGHT MANAGEMENT

5.1 Introduction ......................................................... 137

Navigation Status Box ............................................... 138

5.2 Using Map Displays ............................................. 140

Map Orientation ....................................................... 140

Map Range .............................................................. 142

Map Panning ............................................................ 144

Measuring Bearing and Distance ................................ 148

Topography .............................................................. 149

Map Symbols ........................................................... 152

Airways ................................................................... 158

Track Vector ............................................................. 160

Wind Vector ............................................................. 161

Nav Range Ring........................................................ 162

Fuel Range Ring ....................................................... 163

Field of View (SVT) .................................................... 164

Selected Altitude Intercept Arc ................................... 165

5.3 Waypoints ............................................................. 166

Airports ................................................................... 167

Intersections ............................................................ 174

NDBs ....................................................................... 176

VORs ....................................................................... 178

User Waypoints ........................................................ 180

5.4 Airspaces .............................................................. 186

5.5 Direct-to-Navigation .......................................... 190

5.6 Flight Planning ..................................................... 195

Flight Plan Creation .................................................. 196

Adding Waypoints to an Existing Flight Plan ................ 201

Adding Airways to a Flight Plan ................................. 203

Adding Procedures to a Stored Flight Plan .................. 205

Flight Plan Storage ................................................... 212

Flight Plan Editing .................................................... 214

Along Track Offsets ................................................... 217

Parallel Track ............................................................ 219

Activating a Flight Plan Leg ....................................... 222

Inverting a Flight Plan ............................................... 223

Flight Plan Views ...................................................... 224

Closest Point of FPL .................................................. 226

User-Deﬁned Holding Patterns ................................... 226

5.7 Vertical Navigation ............................................. 231

Altitude Constraints .................................................. 233

5.8 Procedures ...........................................................237

Departures ............................................................... 238

Arrivals ................................................................... 241

Approaches ............................................................. 244

5.9 Trip Planning ........................................................ 252

Trip Planning ............................................................ 252

Weight Planning ....................................................... 256

Weight Caution And Warning Conditions .................... 258

5.10 RAIM Prediction................................................... 259

5.11 Navigating a Flight Plan ..................................... 262

5.12 Abnormal Operation ........................................... 290

SECTION 6 HAZARD AVOIDANCE

6.1 SiriusXM Weather ................................................ 294

Using SiriusXM Weather Products .............................. 296

6.2 Airborne Color Weather Radar .......................... 328

System Description ................................................... 328

Principles of Pulsed Airborne Weather Radar ............... 328

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

Basic Antenna Tilt Setup ............................................ 333

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

Ground Mapping and Interpretation ........................... 346

Weather Radar Overlay on the Navigation Map Page ... 347

System Status ........................................................... 349

6.3 WX-500 Stormscope ........................................... 350

Setting Up Stormscope on the Navigation Map ........... 350

Selecting the Stormscope Page .................................. 354

6.4 TAWS-B ................................................................. 355

TAWS-B Page ........................................................... 359

TAWS-B Alerts .......................................................... 360

System Status ........................................................... 367

6.5 Proﬁle View Terrain ............................................. 369

Proﬁle View Display .................................................. 370

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TABLE OF CONTENTS

6.6 Trafﬁc Information Service (TIS) ........................ 372

Displaying Trafﬁc Data .............................................. 373

Trafﬁc Map Page ....................................................... 375

TIS Alerts ................................................................. 376

System Status ........................................................... 377

6.7 Garmin GTS 800 Trafﬁc ....................................... 380

Theory of Operation .................................................. 380

TAS Alerts ................................................................ 382

System Test .............................................................. 383

Operation ................................................................ 384

System Status ........................................................... 390

6.8 SKY497 Trafﬁc ...................................................... 392

TAS Symbology ......................................................... 392

Operation ................................................................ 393

Altitude Display ........................................................ 396

Trafﬁc Map Page Display Range ................................. 396

TAS Alerts ................................................................ 398

System Status ........................................................... 398

SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM

7.1 Garmin AFCS ........................................................ 401

Basic Autopilot Operation .......................................... 402

Garmin AFCS Controls ............................................... 403

Flight Director Operation ........................................... 405

Vertical Modes ......................................................... 408

Lateral Modes .......................................................... 422

Autopilot and Yaw Damper Operation ........................ 428

Level Mode .............................................................. 430

Underspeed Protection .............................................. 431

Flap Conﬁguration Trim (FCT) ..................................... 433

Example Flight Plan .................................................. 433

AFCS Annunciations and Alerts .................................. 445

Abnormal Operation ................................................. 447

7.2 S-TEC Fifty Five X Autopilot (Optional) ............ 448

SECTION 8 ADDITIONAL FEATURES

8.1 Synthetic Vision Technology (SVT

™

) .................. 450

SVT Operation .......................................................... 451

SVT Features ............................................................ 453

Field of View ............................................................ 462

8.2 SafeTaxi ................................................................ 464

SafeTaxi Cycle Number and Revision .......................... 467

8.3 ChartView ............................................................. 470

ChartView Softkeys ................................................... 471

Terminal Procedures Charts ....................................... 472

Chart Options ........................................................... 480

Day/Night View ........................................................ 486

ChartView Cycle Number and Expiration Date ............. 488

8.4 FliteCharts ............................................................ 491

FliteCharts Softkeys .................................................. 492

Terminal Procedures Charts ....................................... 493

Chart Options ........................................................... 500

Day/Night View ........................................................ 504

FliteCharts Cycle Number and Expiration Date ............. 506

8.5 Airport Directory ................................................. 509

Airport Directory Database Cycle Number and Revision 510

8.6 SiriusXM Satellite Radio (Optional) .................. 512

Activating SiriusXM Satellite Radio Services ................ 512

Using SiriusXM Satellite Radio ................................... 514

8.7 Maintenance Logs ............................................... 517

8.8 Scheduler .............................................................. 522

8.9 Electronic Checklists ........................................... 524

8.10 Flight Data Logging ............................................ 527

8.11 Auxiliary Video ..................................................... 529

Video Setup .............................................................530

Display Selection ...................................................... 530

Input Selection ......................................................... 531

Zoom/Range ............................................................ 532

8.12 Electronic Stability & Protection (ESP

™

) ........... 533

Roll Engagement ...................................................... 534

Pitch Engagement..................................................... 536

High Airspeed Protection ........................................... 536

8.13 Abnormal Operation ........................................... 537

SVT Troubleshooting ................................................. 537

Reversionary Mode ................................................... 537

Unusual Attitudes ..................................................... 538

APPENDICES

Annunciations and Alerts ............................................. 541

Alert Level Deﬁnitions ............................................... 542

Aircraft Alerts ........................................................... 543

Comparator Annunciations ........................................ 546

G1000 System Annunciations .................................... 548

Garmin G1000 Pilot’s Guide for the Quest KODIAK

®

100

190-00590-08 Rev. Ax

TABLE OF CONTENTS

G1000 System Message Advisories ............................. 550

AFCS Alerts .............................................................. 564

TAWS-B ALERTS ........................................................ 565

TAWS-B System Status Annunciations ......................... 565

Flight Plan Import/Export Messages ........................... 566

Pilot Proﬁle Import/Export Messages .......................... 567

Database Management ................................................ 569

Jeppesen Databases .................................................. 570

Garmin Databases .................................................... 573

Garmin Aviation Glossary ............................................ 581

Frequently Asked Questions ........................................ 589

General TIS Information ............................................... 593

Introduction ............................................................. 593

TIS vs. TAS/TCAS ....................................................... 593

TIS Limitations.......................................................... 593

Map Symbols ................................................................. 595

INDEX

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

190-00590-08 Rev. A

Garmin G1000 Pilot’s Guide for the Quest KODIAK

®

100

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

1

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& cNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

SECTION 1 SYSTEM OVERVIEW

1.1 SYSTEM DESCRIPTION

This section is designed to provide an overview of the G1000 Integrated Flight Deck installed in the Quest

KODIAK

®

100. The G1000 is an integrated ﬂight deck system that presents ﬂight instrumentation, position,

navigation, communication, and identiﬁcation information to the pilot using ﬂat-panel color displays. The

system is distributed across the following Line Replaceable Units (LRUs):

•

GDU 1040

Primary Flight Display (PFD)/Multi

Function Display (MFD)

•

GMA 1347

Audio Panel with Integrated Marker

Beacon Receiver

•

GIA 63W

Integrated Avionics Units (IAU)

•

GDC 74A

Air Data Computer (ADC)

•

GEA 71

Engine/Airframe Unit

•

GTX 33

Mode S Transponder

•

GRS 77

Attitude and Heading Reference System

(AHRS)

•

GMU 44

Magnetometer

•

GDL 69A/69A SXM

Data Link Receiver (Optional)

•

GWX 68

Weather Radar (Optional)

•

GTS 800

Trafﬁc Avoidance System (Optional)

•

GMC 710

AFCS Control Unit (Optional)

•

GSA 80/81

AFCS Servos (Optional)

•

GSM 86

Servo Gearboxes (Optional)

A top-level G1000 system block digram is shown in Figure 1-1 (it does not include the GSM 86).

NOTE: Refer to the AFCS section for details on the Garmin AFCS.

The Garmin Automated Flight Control System (AFCS) provides the ﬂight director (FD) and autopilot (AP)

functions of the G1000 system.

Garmin G1000 Pilot’s Guide for the Quest KODIAK

®

100

190-00590-08 Rev. A

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

2

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

1.2 LINE REPLACEABLE UNITS

• GDU 1040 (3) – The GDU 1040 is conﬁgured as two Primary Flight Displays (PFD) and one Multi Function

Display (MFD). 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.

•

GMA 1347

(2) – 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.

•

GIA 63W

(2) – The Integrated Avionics Units (IAU) function as the main communications hub, linking all

LRUs with the PFD. Each IAU contains VHF COM/NAV/GS receivers and system integration microprocessors

and is paired with the on-side display via an HSDB connection. The IAUs are not paired together and do not

communicate with each other directly.

•

GDC 74A

(2) – The Air Data Computer (ADC) processes data from the pitot/static system and outside air

temperature (OAT) sensor. The ADC provides pressure altitude, airspeed, vertical speed, and OAT information

to the G1000 System, and it communicates with the primary IAU, displays, and AHRS using an ARINC 429

digital interface.

190-00590-08 Rev. A

Garmin G1000 Pilot’s Guide for the Quest KODIAK

®

100

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

3

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& cNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

•

GEA 71

(1) – The Engine Airframe Unit receives and processes signals from the engine and airframe sensors.

This unit communicates with both IAUs using an RS-485 digital interface.

•

GTX 33

(1) – The solid-state Transponder provides Modes A, C, and S capability and communicates with both

IAUs through an RS-232 digital interface.

•

GRS 77

(2) – The Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading

information via ARINC 429 to both the PFD and the primary IAU. The AHRS contains advanced sensors

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

information, with the ADC to obtain air data, and with both IAUs to obtain GPS information. AHRS operation

is discussed in Section 1.5, System Operation.

•

GMU 44

(2) – The Magnetometer measures local magnetic ﬁeld and sends data to the AHRS for processing to

determine aircraft magnetic heading. This unit receives power directly from the AHRS and communicates with

it via an RS-485 digital interface.

•

GDL 69A/69A SXM

(1) – The Data Link Satellite Radio Receiver provides real-time weather information to the

G1000 MFD and PFD Inset Map, as well as digital audio entertainment. The Data Link Receiver communicates

with the MFD via an HSDB connection. A subscription to XM Satellite Radio Service is required to enable the

GDL 69A capability.

Garmin G1000 Pilot’s Guide for the Quest KODIAK

®

100

190-00590-08 Rev. A

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

4

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

•

GWX 68

(1)(optional) – Provides airborne weather and ground mapped radar data to the MFD via HSDB

connection.

•

GTS 800

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

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

•

GSA 80

(2),

GSA 81

(2), and

GSM 86

(4) (optional) – The GSA 80 servos are used for the automatic control

of pitch and yaw. The GSA 81 servos are used for the automatic control of roll and pitch trim. These units

interface with each GIA 63W.

The GSM 86 servo gearboxes are responsible for transferring the output torque of the GSA 80/81 servo actuators

to the mechanical ﬂight-control surface linkage.

•

GMC 710

(1) (optional) – Provides the controls for the GFC 700 AFCS through an RS-232 digital interface

allowing communication with both PFDs.

190-00590-08 Rev. A

Garmin G1000 Pilot’s Guide for the Quest KODIAK

®

100

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

5

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& cNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

GMA 1347

Audio Panel #2

GTX 33

Transponder

GEA 71

Engine/

Airframe Unit

GDC 74A #1

Air Data

Computer

OAT

Airspeed

Altitude

Vertical Speed

GMU 44 #1

Magnetometer

Heading

GMA 1347

Audio Panel #1

GDU 1040

PFD #1

GDU 1040

MFD

GMC 710

AFCS Control Unit (optional)

GDU 1040

PFD #2

GRS 77 #1

AHRS

Attitude

Rate of Tu rn

Slip/Skid

GDC 74A #2

Air Data

Computer

OAT

Airspeed

Altitude

Vertical Speed

GMU 44 #2

Magnetometer

Heading

#

2

e

d

GRS 77 #2

AHRS

Attitude

Rate of Tu rn

Slip/Skid

GIA 63W #2

Integrated Avionics Unit

System Integration Processors

I/O Processors

VHF COM

VHF NAV/LOC

GPS

Glideslope

GPS Output

L-3 Skywatch

SKY497

Traffic

Advisory System

(optional)

L-3 WX-500

Stormscope

Lightning Sensor

(optional)

GDL 69A/

69A SXM

Data Link

Real-time Weather

and Digital Audio

Entertainment

(optional)

GWX 68

Weather Radar

Airborne Weather

and Ground Mapped

Radar Data

(optional)

GIA 63W #1

Integrated Avionics Unit

System Integration Processors

I/O Processors

VHF COM

VHF NAV/LOC

GPS

Glideslope

GPS Output

GD

V

G

M

G

R

We

Air

a

nd

GTS 800

Traffic Advisory

System

(optional)

GSA 80 (2)

GSA 81 (2)

Servos

(optional)

Figure 1-1 Basic G1000 System Block Diagram

Garmin G1000 Pilot’s Guide for the Quest KODIAK

®

100

190-00590-08 Rev. A

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

6

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

1.3 G1000 CONTROLS

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

The G1000 system controls are located on the PFD and MFD bezels and the 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/MFD Controls

1718

5

6

8

7

2

4

31 9

15

14

13

12

16

11

10

The NAV, CRS/BARO, COM, FMS, and ALT Knobs are concentric dual knobs, each having small (inner)

and large (outer) control portion. When a portion of the knob is not speciﬁed in the text, either may be used.

Large (Outer)

Knob

Small (Inner)

Knob

Figure 1-3 Dual Concentric Knob

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