Garmin G1000 User Manual

G1000® Integrated Flight Deck

Pilot’s Guide

Quest Kodiak 100

System Software 0552.05 or later

SYSTEM OVERVIEW

FLIGHT INSTRUMENTS

ENGINE INDICATION SYSTEM

AUDIO PANEL & CNS

FLIGHT MANAGEMENT

HAZARD AVOIDANCE

AUTOMATIC FLIGHT CONTROL SYSTEM

ADDITIONAL FEATURES

APPENDICES

INDEX

Copyright © 2006-2009 Garmin Ltd. or its subsidiaries. All rights reserved.

This manual reflects the operation of System Software version 0552.05 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: [phone]	Fax: [phone]
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: [phone]	Fax: [phone]
Garmin (Europe) Ltd., Liberty House, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB U.K.
Tel: [phone]	Fax: [phone]
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: [phone]	Fax: [phone]

Website Address: www.garmin.com

Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.

Garmin® is a registered trademark of Garmin Ltd. or its subsidiaries, and G1000® is a trademark of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin.

Bendix/King® and Honeywell® are registered trademarks of Honeywell International, Inc.; NavData® is a registered trademark of Jeppesen, Inc.; Stormscope® is a registered trademark of L-3 Communications;Avidyne® and TCAD® are registered trademarks of Avidyne Corporation; and XM® is a registered trademark of XM Satellite Radio, Inc.

July 2009

Printed in the U.S.A

Garmin G1000 Pilot’s Guide for the Quest Kodiak 100

190-00590-02 Rev. A

Limited Warranty

LIMITED WARRANTY

This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts and labor, provided that the customer shall be responsible for any transportation cost. This warranty does not cover failures due to abuse, misuse, accident, or unauthorized alterations or repairs.

THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO STATE.

IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not allow the exclusion of incidental or consequential damages, so the above limitations may not apply to you.

Garmin retains the exclusive right to repair or replace the unit or software, or to offer a full refund of the purchase price, at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY.

To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating a Service Center near you, visit the Garmin Web site at “http://www.garmin.com” or contact Garmin Customer Service at 800-800-1020.

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Warnings, Cautions, and Notes

WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from third party sources. Garmin is not able to independently verify the accuracy of the terrain data.

WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical charts for appropriate minimum clearance altitudes.

WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74A Air Data Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.

WARNING: Do not use outdated database information. Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current. Pilots using any outdated database do so entirely at their own risk.

WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness.

WARNING: Traffic information shown on system displays is provided as an aid in visually acquiring traffic. Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic.

WARNING: Use of the Stormscope is not intended for hazardous weather penetration (thunderstorm penetration). Stormscope information, as displayed on the G1000 MFD, is to be used only for weather avoidance, not penetration.

WARNING: GDL 69 Weather should not be used for hazardous weather penetration. Weather information provided by the GDL 69 is approved only for weather avoidance, not penetration.

Warning: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for short-range weather avoidance.

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Warnings, Cautions, and Notes

WARNING: The Garmin G1000, as installed in this aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000. It is thus the responsibility of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated information available in the cockpit.

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

WARNING: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be misused or misinterpreted and, therefore, become unsafe.

WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000 Pilot’s Guide documentation and the G1000 Integrated Avionics System in the Quest Kodiak 100 Airplane Flight Manual. Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the G1000 to all available navigation sources, including the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation.

WARNING: The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo.”

WARNING: Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/ aboutGarmin/environment/disposal.jsp.

WARNING: Because of variation in the earth’s magnetic field, operating the G1000 within the following areas could result in loss of reliable attitude and heading indications. North of 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)

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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: 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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Revision Information

Record of Revision

Part Number	Revision	Date	Page Range	Description
190-00590-00	1	3/13/06	All	Initial release
190-00590-00	A	3/21/07	All	Production Release
190-00590-00	B	4/3/07	All	Added Print Specification Reference to Cover Sheet
190-00590-00	C	6/22/07	All	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

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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............................	27
	Menus........................................................................	27
	Data Entry..................................................................	28
	MFD Page Groups.......................................................	28
	System Setup and Status..............................................	32
1.8	Display Backlighting..............................................	46
	Section 2 Flight Instruments
2.1	Flight Instruments..................................................	50
	Airspeed Indicator.......................................................	50
	Attitude Indicator........................................................	52
	Altimeter....................................................................	53
	Vertical Speed Indicator (VSI).......................................	57
	Vertical Deviation........................................................	57
	Horizontal Situation Indicator (HSI)...............................	58
	Course Deviation Indicator (CDI)...................................	63
2.2	Supplemental Flight Data.....................................	71
	Temperature Displays..................................................	71
	Wind Data..................................................................	72
	Vertical Navigation (VNV) Indications............................	73
2.3	PFD Annunciations and Alerting Functions.........	74
	System Alerting...........................................................	74
	Marker Beacon Annunciations......................................	75
	Traffic Annunciation.....................................................	76
	TAWS Annunciations...................................................	77

	Altitude Alerting..........................................................	78
	Low Altitude Annunciation...........................................	78
	Minimum Descent Altitude/Decision Height Alerting.......	79
2.4	Abnormal Operations............................................	80
	Abnormal GPS Conditions............................................	80
	Unusual Attitudes........................................................	81
	Section 3 Engine Indication System (EIS)
3.1	Engine Display........................................................	86
3.2	System Display.......................................................	88
3.3	Fuel Display............................................................	90
	Section 4 Audio Panel and CNS
4.1	Overview.................................................................	93
	MFD/PFD Controls and Frequency Display......................	94
	Audio Panel Controls...................................................	96
4.2	COM Operation......................................................	98
	COM Transceiver Selection and Activation......................	98
	COM Transceiver Manual Tuning...................................	99
	Quick-tuning and Activating 121.500 MHz...................	100
	Auto-tuning the COM Frequency.................................	101
	Frequency Spacing.....................................................	105
	Automatic Squelch....................................................	106
	Volume....................................................................	106
4.3	NAV Operation.....................................................	107
	NAV Radio Selection and Activation............................	107
	NAV Receiver Manual Tuning......................................	108
	Auto-tuning a NAV Frequency from the MFD...............	110
	Auto-tuning NAV Frequencies on Approach Activation..	114
	Marker Beacon Receiver............................................	115
4.4	GTX 33 Mode S Transponder..............................	116
	Transponder Controls.................................................	116
	Transponder Mode Selection......................................	117
	Entering a Transponder Code......................................	120
	IDENT Function.........................................................	121
	Flight ID Reporting....................................................	122
4.5	Additional Audio Panel Functions......................	123
	Power-up..................................................................	123
	Mono/Stereo Headsets...............................................	123
	Speaker....................................................................	123
	Intercom...................................................................	124
	Passenger Address (PA) System...................................	126

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Table of Contents

	Simultaneous COM Operation....................................	126
	Clearance Recorder and Player...................................	127
	Entertainment Inputs.................................................	128
4.6 Audio Panels Preflight Procedure......................		129
4.7	Abnormal Operation............................................	131
	Stuck Microphone.....................................................	131
	COM Tuning Failure...................................................	131
	PFD Failure, Dual System............................................	132
	Audio Panel Fail-safe Operation..................................	133
	Reversionary Mode....................................................	133
	Section 5 Flight Management
5.1	Introduction..........................................................	135
	Navigation Status Box...............................................	137
5.2	Using Map Displays.............................................	138
	Map Orientation.......................................................	138
	Map Range...............................................................	140
	Map Panning............................................................	143
	Measuring Bearing and Distance................................	147
	Topography..............................................................	148
	Map Symbols............................................................	151
	Airways....................................................................	157
	Track Vector..............................................................	159
	Wind Vector..............................................................	160
	Nav Range Ring........................................................	161
	Fuel Range Ring........................................................	162
	Field of View (SVS)....................................................	163
5.3	Waypoints.............................................................	164
	Airports....................................................................	165
	Intersections.............................................................	172
	NDBs.......................................................................	174
	VORs........................................................................	176
	User Waypoints.........................................................	178
5.4	Airspaces...............................................................	184
5.5 Direct-to-Navigation ..........................................		188
5.6	Flight Planning.....................................................	193
	Flight Plan Creation...................................................	194
	Adding Waypoints to an Existing Flight Plan................	199
	Adding Airways to a Flight Plan..................................	201
	Adding Procedures to a Stored Flight Plan...................	203
	Flight Plan Storage....................................................	209
	Flight Plan Editing.....................................................	212
	Along Track Offsets....................................................	215

	Parallel Track.............................................................	217
	Activating a Flight Plan Leg........................................	220
	Inverting a Flight Plan................................................	221
	Flight Plan Views.......................................................	222
	Closest Point of FPL...................................................	224
5.7	Vertical Navigation..............................................	225
	Altitude Constraints...................................................	227
5.8	Procedures............................................................	231
	Departures................................................................	231
	Arrivals ....................................................................	234
	Approaches .............................................................	236
5.9	Trip Planning.........................................................	242
	Trip Planning.............................................................	242
	Weight Planning.......................................................	246
	Weight Caution And Warning Conditions.....................	248
5.10	RAIM Prediction...................................................	249
5.11	Navigating a Flight Plan.....................................	252
5.12	Abnormal Operation............................................	280
	Section 6 Hazard Avoidance
6.1	XM Satellite Weather..........................................	283
	Activating Services....................................................	284
	Using XM Satellite Weather Products..........................	285
6.2	WX-500 Stormscope............................................	312
	Setting Up Stormscope on the Navigation Map............	312
	Selecting the Stormscope Page...................................	317
6.3	Terrain Awareness & Warning System...............	318
	Displaying TAWS Data...............................................	319
	TAWS-B Page............................................................	322
	TAWS Alerts..............................................................	324
	System Status...........................................................	330
6.4	Traffic Information Service (TIS)........................	332
	Displaying TRAFFIC Data............................................	333
	Traffic Map Page.......................................................	335
	TIS Alerts..................................................................	336
	System Status...........................................................	337
6.5	Traffic Advisory System (TAS).............................	340
	TAS Symbology.........................................................	340
	Operation.................................................................	341
	Altitude Display........................................................	344
	Traffic Map Page Display Range..................................	344
	TAS Alerts.................................................................	346
	System Status...........................................................	346

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Table of Contents

Section 7 Automatic Flight Control System
7.1	S-TEC Fifty Five X Autopilot (Optional).............	349
	Section 8 Additional Features
8.1	Synthetic Vision System (SVS)............................	352
	SVS Operation...........................................................	353
	SVS Features.............................................................	355
	Field of View.............................................................	363
8.2	SafeTaxi.................................................................	365
	SafeTaxi Cycle Number and Revision...........................	368
8.3	ChartView.............................................................	371
	ChartView Softkeys...................................................	371
	Terminal Procedures Charts........................................	372
	Chart Options...........................................................	380
	Day/Night View.........................................................	386
	ChartView Cycle Number and Expiration Date..............	388
8.4	FliteCharts.............................................................	391
	FliteCharts Softkeys...................................................	391
	Terminal Procedures Charts........................................	392
	Chart Options...........................................................	399
	Day/Night View.........................................................	403
	FliteCharts Cycle Number and Expiration Date.............	405
8.5	AOPA Airport Directory.......................................	408
	AOPA Database Cycle Number and Revision................	409
8.6	XM Radio Entertainment (Optional)..................	411
	Activating XM Satellite Radio Services........................	411
	Using XM Radio........................................................	412
8.7	Scheduler..............................................................	416
8.8	Electronic Checklists............................................	418
8.9	Flight Data Logging.............................................	421
8.10	Auxiliary Video.....................................................	423
	Video Setup..............................................................	424
	Display Selection.......................................................	424
	Input Selection..........................................................	426
	Zoom/Range.............................................................	426
8.11	Abnormal Operation............................................	427
	SVS Troubleshooting..................................................	427
	Reversionary Mode....................................................	427
	Unusual Attitudes......................................................	428

Appendices
Annunciations and Alerts..............................................	431
Alert Level Definitions................................................	432
Aircraft Alerts...........................................................	433
Comparator Annunciations.........................................	435
G1000 System Annunciations.....................................	437
G1000 System Message Advisories.............................	439
TAWS ALERTS...........................................................	450
TAWS System Status Annunciations............................	450
Flight Plan Import/Export Messages............................	451
SD Card Use....................................................................	453
Jeppesen Databases..................................................	453
Garmin Databases.....................................................	455
Glossary..........................................................................	463
Frequently Asked Questions.........................................	471
General TIS Information................................................	475
Introduction..............................................................	475
TIS vs. TAS/TCAS........................................................	475
TIS Limitations..........................................................	475
Map Symbols..................................................................	477
Index
Index .................................................................................	I-1

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system overview

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	• GEA 71 Engine/Airframe Unit
Function Display (MFD)	• GTX 33 Mode S Transponder
• GMA 1347 Audio Panel with Integrated Marker	• GRS 77 Attitude and Heading Reference System
Beacon Receiver	(AHRS)
• GIA 63W Integrated Avionics Units (IAU)	• GMU 44 Magnetometer
• GDC 74A Air Data Computer (ADC)	• GDL 69A Data Link Receiver (Optional)

A top-level G1000 system block digram is shown in figure 1-1.

HAZARD FLIGHT PANEL AUDIO EIS FLIGHT SYSTEM AVOIDANCE MANAGEMENT NSCc & INSTRUMENTS OVERVIEW

INDEX APPENDICES ADDITIONAL AFCS FEATURES

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system overview

HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

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.

AFCS	• 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 a HSDB connection. The IAUs are not paired together and do not
ADDITIONAL	communicate with each other directly.
FEATURES
APPENDICES
INDEX

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system overview

•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.

•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.

INDEX APPENDICES ADDITIONAL AFCS HAZARD FLIGHT PANEL AUDIO EIS FLIGHT SYSTEM FEATURES AVOIDANCE MANAGEMENT NSCc & INSTRUMENTS OVERVIEW

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system overview

ADDITIONAL HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM INDEX APPENDICES FEATURES AFCS AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

•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 (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 a HSDB connection. A subscription to XM Satellite Radio Service is required to enable the GDL 69A capability.

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system overview

GDU 1040

PFD #1

GIA 63W #1

Integrated Avionics Unit

System Integration Processors

I/O Processors

VHF COM

VHF NAV/LOC

GPS

Glideslope

GPS Output

GDU 1040				GDU 1040
MFD				PFD #2

GDL 69A

Data Link

Real-time Weather

and Digital Audio

Entertainment

(optional)

GDC 74A #1			GDC 74A #2
Air Data			Air Data
Computer			Computer
OAT			OAT
Airspeed			Airspeed
Altitude			Altitude
Vertical Speed			Vertical Speed

GRS 77 #1			GRS 77 #2
AHRS			AHRS
Attitude			Attitude
Rate of Turn			Rate of Turn
Slip/Skid			Slip/Skid

GMU 44 #1	GMU 44 #2
Magnetometer	Magnetometer
Heading	Heading
	GTX 33
	Transponder
	GEA 71
	Engine/
	Airframe Unit
	L-3 WX-500
	Stormscope
	Lightning Sensor
	(optional)
	L-3 Skywatch
	SKY497
	Traffic
	Advisory System
	(optional)

GIA 63W #2

Integrated Avionics Unit

System Integration Processors

I/O Processors

VHF COM

VHF NAV/LOC

GPS

Glideslope

GPS Output

Figure 1-1 Basic G1000 System Block Diagram

INDEX APPENDICES ADDITIONAL AFCS HAZARD FLIGHT PANEL AUDIO EIS FLIGHT SYSTEM FEATURES AVOIDANCE MANAGEMENT NSCc & INSTRUMENTS OVERVIEW

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system overview

ADDITIONAL HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM INDEX APPENDICES FEATURES AFCS AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

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

1

2

3

4

5

6

7

8

9

10	13
11	14
12	15
16

18

17

Figure 1-2 PFD/MFD Controls

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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Garmin G1000 Pilot’s Guide for the Quest Kodiak 100

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1 NAV VOL/ID Knob Turn to control NAV audio volume (shown in the NAV Frequency Box as a percentage)

Press to toggle Morse code identifier audio ON/OFF

2NAV Frequency Transfers the standby and active NAV frequencies

Transfer Key

3	NAV Knob	Turn to tune NAV receiver standby frequencies (large knob for MHz; small for kHz)
		Press to toggle light blue tuning box between NAV1 and NAV2
4	Heading Knob	Turn to manually select a heading
		Press to display a digital heading momentarily to the left of the HSI and synchronize
		the Selected Heading to the and current heading
5	Joystick	Turn to change map range
		Press to activate Map Pointer for map panning

6CRS/BARO Knob

7COM Knob

8COM Frequency Transfer Key (EMERG)

9COM VOL/SQ Knob

10Direct-to Key ()

11FPL Key

12CLR Key (DFLT MAP)

13MENU Key

Turn large knob for altimeter barometric pressure setting

Turn small knob to adjust course (only when HSI is in VOR or OBS Mode)

Press to re-center the CDI and return course pointer directly TO bearing of active waypoint/station

Turn to tune COM transceiver standby frequencies (large knob for MHz; small for kHz)

Press to toggle light blue tuning box between COM1 and COM2

The selected COM (green) is controlled with the COM MIC Key (Audio Panel). Transfers the standby and active COM frequencies

Press and hold two seconds to tune the emergency frequency (121.5 MHz) automatically into the active frequency field

Turn to control COM audio volume level (shown as a percentage in the COM Frequency Box)

Press to turn the COM automatic squelch ON/OFF

Activates the direct-to function and allows the user to enter a destination waypoint and establish a direct course to the selected destination (specified by identifier, chosen from the active route)

Displays flight plan information

Erases information, cancels entries, or removes menus

Press and hold to display the MFD Navigation Map Page (MFD only).

Displays a context-sensitive list of options for accessing additional features or making setting changes

14 PROC Key	Gives access to IFR departure procedures (DPs), arrival procedures (STARs), and
	approach procedures (IAPs) for a flight plan or selected airport

INDEX APPENDICES ADDITIONAL AFCS HAZARD FLIGHT PANEL AUDIO EIS FLIGHT SYSTEM FEATURES AVOIDANCE MANAGEMENT NSCc & INSTRUMENTS OVERVIEW

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system overview

HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

15	ENT Key	Validates/confirms menu selection or data entry
16	FMS Knob	Press to turn the selection cursor ON/OFF.
	(Flight Management Data Entry: With cursor ON, turn to enter data in the highlighted field (large
	System Knob)	knob moves cursor location; small knob selects character for highlighted cursor
		location)

Scrolling: When a list of information is too long for the window/box, a scroll bar appears, indicating more items to view. With cursor ON, turn large knob to scroll through the list.

Page Selection: Turn knob on MFD to select the page to view (large knob selects a page group; small knob selects a specific page from the group)

17Softkey Selection Press to select softkey shown above the bezel key on the PFD/MFD display

Keys

18 ALT Knob	Sets the Selected Altitude, shown above the Altimeter (the large knob selects the
	thousands, the small knob selects the hundreds)

Controls Associated With the MFD

The controls for the MFD are located on the MFD bezel. The bottom portion of the MFD bezel features 12 softkeys that are designed to perform various functions depending upon the specific page being displayed. These softkeys are discussed throughout the Pilot’s Guide documentation.

ADDITIONAL INDEX APPENDICES FEATURES AFCS

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Audio Panel Controls

1	2
3	4
5	6
7	8
9	10
11	12
13	14
15	16
17
18	19
20	21
22	23
	24

Figure 1-4 Audio Panel Controls (GMA 1347)

NOTE: When a key is selected, a triangular annunciator above the key is illuminated.

1COM1 MIC – Selects the #1 transmitter for transmitting. COM1 receive is simultaneously selected when this key is pressed allowing received audio from the #1 COM receiver to be heard. COM2 receive can be added by pressing the COM2 Key.

2COM1 – When selected, audio from the #1 COM receiver can be heard.

3COM2 MIC – Selects the #2 transmitter for transmitting. COM2 receive is simultaneously selected when this key is pressed allowing received audio from the #2 COM receiver to be heard. COM1 receive can be added by pressing the COM1 Key.

4COM2 – When selected, audio from the #2 COM receiver can be heard.

5COM3 MIC – Not used in Kodiak 100 aircraft.

INDEX APPENDICES ADDITIONAL AFCS HAZARD FLIGHT PANEL AUDIO EIS FLIGHT SYSTEM FEATURES AVOIDANCE MANAGEMENT NSCc & INSTRUMENTS OVERVIEW

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system overview

6COM3 – Not used in Kodiak 100 aircraft.

7COM 1/2 – Not used in Kodiak 100 aircraft.

8TEL – Not used in Kodiak 100 aircraft.

9PA – Selects the passenger address system. The selected COM transmitter is deselected when the PA Key is pressed.

10SPKR – Selects and deselects the cabin speaker. COM and NAV receiver audio can be heard on the speaker.

11MKR/MUTE – Selects marker beacon receiver audio. Mutes the currently received marker beacon receiver audio. Unmutes automatically when new marker beacon audio is received. Also, stops play of recorded COM audio.

12HI SENS – Press to increase marker beacon receiver sensitivity. Press again to return to low sensitivity.

13DME – Not used in Kodiak 100 aircraft.

14NAV1 – When selected, audio from the #1 NAV receiver can be heard.

15ADF – Not used in Kodiak 100 aircraft.

16NAV2 – When selected, audio from the #2 NAV receiver can be heard.

17AUX – Not used in Kodiak 100 aircraft.

18MAN SQ – Enables manual squelch for the intercom. When the intercom is active, press the PILOT Knob to illuminate SQ. Turn the PILOT/PASS Knobs to adjust squelch.

19PLAY – Press once to play the last recorded COM audio. Press again while audio is playing and the previous block of recorded audio is played. Each subsequent press plays each previously recorded block. Pressing the MKR/MUTE Key during play of a memory block stops play.

20PILOT – Selects and deselects the pilot intercom isolation.

21COPLT – Selects and deselects the copilot intercom isolation.

22PILOT Knob – Press to switch between volume and squelch control as indicated by illumination of VOL or SQ. Turn to adjust intercom volume or squelch. The MAN SQ Key must be selected to allow squelch adjustment.

23PASS Knob – Turn to adjust Copilot/Passenger intercom volume or squelch. The MAN SQ Key must be selected to allow squelch adjustment.

24DISPLAY BACKUP Button – Manually selects Reversionary Mode.

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Garmin G1000 Pilot’s Guide for the Quest Kodiak 100

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1.4 Secure Digital (SD) Cards

NOTE: Ensure the G1000 System is powered off before inserting an SD card.

NOTE: Refer to Appendix B for instructions on updating the aviation databases.

The PFD and MFD data card slots use Secure Digital (SD) cards and are located on the upper right side 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.

Installing an SD card:

1)Insert the SD card in the SD card slot (the front of the card should be flush with the face of the display bezel).

2)To eject the card, gently press on the SD card to release the spring latch.

SD Card Slots

Figure 1-5 Display Bezel SD Card Slots

INDEX APPENDICES ADDITIONAL AFCS HAZARD FLIGHT PANEL AUDIO EIS FLIGHT SYSTEM FEATURES AVOIDANCE MANAGEMENT NSCc & INSTRUMENTS OVERVIEW

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ADDITIONAL HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM INDEX APPENDICES FEATURES AFCS AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

1.5 System Power-Up

NOTE: See the Aircraft Flight Manual (AFM) for specific procedures concerning avionics power application and emergency power supply operation.

NOTE: Refer to Appendix A for system-specific annunciations and alerts.

The G1000 System is integrated with the aircraft electrical system and receives power directly from electrical busses. The G1000 PFD, MFD, and supporting sub-systems include both power-on and continuous built-in test features that exercise the processor, RAM, ROM, external inputs, and outputs to provide safe operation.

During system initialization, test annunciations are displayed, as shown in Figure 1-2. All system annunciations should disappear typically within the first minute of power-up. Upon power-up, key annunciator lights also become momentarily illuminated on the Audio Panel and the display bezels.

On the PFD, the AHRS begins to initialize and displays “AHRS ALIGN: Keep Wings Level”. The AHRS should display valid attitude and heading fields typically within the first minute of power-up. The AHRS can align itself both while taxiing and during level flight.

When the MFD powers up, the splash screen (Figure 1-5) displays the following information:

•System version

•Copyright

•Land database name and version

•Safe Taxi database information

•Terrain database name and version

•Airport Terrain database name and version

•Obstacle database name and version

•Navigation database name, version, and effective dates

•Airport Directory name, version and effective dates

•FliteCharts/ChartView database information

Current database information includes valid operating dates, cycle number, and database type. When this information has been reviewed for currency (to ensure that no databases have expired), the pilot is prompted to continue.

Pressing the ENT Key (or right-most softkey) acknowledges this information, and the Weight Planning Page is displayed. When the system has acquired a sufficient number of satellites to determine a position, the aircraft’s current position is shown on the Navigation Map Page.

Figure 1-6 PFD Initialization

Figure 1-7 MFD Power-Up Splash Screen

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Garmin G1000 Pilot’s Guide for the Quest Kodiak 100

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system overview

1.6 System Operation

NOTE: In normal operating mode, backlighting can only be adjusted from the PFD. In reversionary mode, it can be adjusted from the remaining display.

The displays are connected together via a single Ethernet bus for high-speed communication. Each IAU is connected to the on-side display. This section discusses normal and reversionary G1000 display operation, as well as the various AHRS modes and G1000 System Annunciations.

Normal Display Operation

In normal operating mode, the PFD presents graphical flight instrumentation (attitude, heading, airspeed, altitude, vertical speed), replacing the traditional flight instrument cluster (see the Flight Instruments Section for more information).

The MFD normally displays a full-color moving map with navigation information (see the Flight Management Section), while the left portion of the MFD is dedicated to the Engine Indication System (EIS; see the EIS Section).

All displays offer control for COM and NAV frequency selection.

Primary Flight Display #1

Multi-Function Display

Primary Flight Display #2

Figure 1-8 G1000 Normal Display Operation

Reversionary Mode

NOTE: The G1000 system alerts the pilot when backup paths are utilized by the LRUs. Refer to the Appendices for further information regarding system-specific alerts.

Reversionary mode is a mode of operation in which all important flight information is presented identically on at least one of the remaining displays (see Figure 1-10). Transition to reversionary mode should be straightforward for the pilot, for flight parameters are presented in the same format as in normal mode.

Reversionary mode can be activated manually by pressing the dedicated DISPLAY BACKUP Button at the bottom of the audio panel (see Figure 1-11 and refer to the Audio Panel section for further details). Pressing this button again deactivates reversionary mode.

INDEX APPENDICES ADDITIONAL AFCS HAZARD FLIGHT PANEL AUDIO EIS FLIGHT SYSTEM FEATURES AVOIDANCE MANAGEMENT NSCc & INSTRUMENTS OVERVIEW

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HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

Primary Flight Display #1

Multi-Function Display

Primary Flight Display #2

Figure 1-9 G1000 Reversionary Mode (Failed PFD #1)

Pressing the DISPLAY BACKUP

Button activates/deactivates reversionary mode for both the on-side PFD and the MFD.

Figure 1-10 DISPLAY BACKUP Button

Each display can be configured to operate in reversionary mode, as follows:

•PFD1 – By pressing the DISPLAY BACKUP Button on the left audio panel.

•MFD – By pressing the DISPLAY BACKUP Button on the left or the right audio panel.

•PFD2 – By pressing the DISPLAY BACKUP Button on the right audio panel.

Should the connection between a PFD and the on-side GIA 63W become inoperative, the on-side GIA 63W can no longer communicate with the remaining PFD (refer to Figure 1-1). As a result, the NAV and COM functions provided to the failed PFD by the on-side GIA 63W are flagged as invalid (red “X”) on the remaining PFD (see Figure 1-12).

ADDITIONAL INDEX APPENDICES FEATURES AFCS

Figure 1-11 Inoperative Input (NAV1 Shown)

AHRS Operation

NOTE: Refer to Appendix A for specific AHRS alert information.

NOTE: Aggressive maneuvering while AHRS is not operating normally may degrade AHRS accuracy.

The Attitude and Heading Reference System (AHRS) performs attitude, heading, and vertical acceleration calculations for the G1000 System, utilizing GPS, magnetometer, and air data in addition to information from its internal sensors. Attitude and heading information are updated on the PFD while the AHRS receives appropriate combinations of information from the external sensor inputs.

Loss of GPS, magnetometer, or air data inputs is communicated to the pilot by message advisory alerts. Any failure of the internal AHRS inertial sensors results in loss of attitude and heading information (indicated by red ‘X’ flags over the corresponding flight instruments).

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Garmin G1000 Pilot’s Guide for the Quest Kodiak 100

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GPS Data

				available
	Magnetometer Data
		available						unavailable
						Air Data
						available				unavailable
				AHRS noAHRS no-Mag/
	AHRS Normal
				Mag Mode					no-Air Mode
	Operation
							Heading Invalid

					unavailable
Magnetometer Data
			available				unavailable
	Air Data
	available					unavailable
AHRS
no-GPS					Attitude/Heading Invalid
Mode

Figure 1-12 AHRS Operation

GPS Input Failure

Two GPS inputs are provided to the AHRS. If GPS information from one of the inputs fails, the AHRS uses the remaining GPS input and an alert message is issued to inform the pilot. If both GPS inputs fail, the AHRS can continue to provide attitude and heading information to the PFD as long as magnetometer and airspeed data are available and valid.

Magnetometer Failure

If the magnetometer input fails, the AHRS continues to output valid attitude information; however, the heading output on the PFD is flagged as invalid with a red ‘X’.

Air Data Input Failure

Failure of the air data input has no effect on the AHRS output while AHRS is receiving valid GPS information. Invalid/unavailable airspeed data in addition to GPS failure results in loss of all attitude and heading information.

INDEX APPENDICES ADDITIONAL AFCS HAZARD FLIGHT PANEL AUDIO EIS FLIGHT SYSTEM FEATURES AVOIDANCE MANAGEMENT NSCc & INSTRUMENTS OVERVIEW

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system overview

HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM AFCS AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

G1000 System Annunciations

NOTE: For a detailed description of all annunciations and alerts, refer to Appendix A. Refer to the Aircraft Flight Manual (AFM) for additional information regarding pilot responses to these annunciations.

When an LRU or an LRU function fails, a large red ‘X’ is typically displayed over the instrument experiencing failed data (Figure 1-10 displays all possible flags and responsible LRUs). Upon G1000 power-up, certain instruments remain invalid as equipment begins to initialize. All instruments should be operational within one minute of power-up. If any instrument remains flagged, the G1000 should be serviced by a Garmin-authorized repair facility.

GIA 63W						GIA 63W
					GRS 77 or GMU 44

GEA 71

or GDC 74A GIA 63W

GIA 63W

								GTX 33 or GIA 63W
GDC 74A									GIA 63W
					Figure 1-13 G1000 System Failure Annunciations

ADDITIONAL INDEX APPENDICES FEATURES

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Garmin G1000 Pilot’s Guide for the Quest Kodiak 100

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Softkey Function

The softkeys are located along the bottoms of the displays. The softkeys shown depend on the softkey level or page being displayed. The bezel keys below the softkeys can be used to select the appropriate softkey. When a softkey is selected, its color changes to black text on gray background and remains this way until it is turned off, at which time it reverts to white text on black background.

Softkey On

Softkey Names (displayed)

Bezel-Mounted Softkeys (press)

Figure 1-14 Softkeys (Second-Level PFD Configuration)

PFD Softkeys

The CDI, IDENT, TMR/REF, NRST, and ALERTS Softkeys undergo a momentary change to black text on gray background and automatically switch back to white text on black background when selected. If messages remain after acknowledgement, the ALERTS Softkey is black on white.

The PFD softkeys provide control over flight management functions, including GPS, NAV, terrain, traffic, and lightning (optional). Each softkey sublevel has a BACK Softkey which can be pressed to return to the previous level. The ALERTS Softkey is visible in all softkey levels. For the top level softkeys and the transponder (XPDR) levels, the IDENT Softkey remains visible.

INSET	Displays Inset Map in PFD lower left corner
OFF	Removes Inset Map
DCLTR (3)	Selects desired amount of map detail; cycles through declutter levels:
	DCLTR (No Declutter): All map features visible
	DCLTR-1: Declutters land data
	DCLTR-2: Declutters land and SUA data
	DCLTR-3: Removes everything except for the active flight plan
TRAFFIC	Displays traffic information on Inset Map
	TRAFFIC: No Traffic displayed on Inset Map
	TRFC-1: Traffic displayed on Inset Map
	TRFC-2: Traffic Only display shown
TOPO	Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation scale
	on Inset Map
TERRAIN	Displays terrain information on Inset Map
STRMSCP	Displays Stormscope information on Inset Map (optional)
NEXRAD	Displays NEXRAD weather and coverage on Inset Map (optional)
XM LTNG	Displays XM lightning information on Inset Map (optional)
SENSOR	Displays softkeys for selecting the #1 and #2 AHRS and Air Data Computers
ADC1	Selects the #1 Air Data Computer
ADC2	Selects the #2 Air Data Computer

INDEX APPENDICES ADDITIONAL AFCS HAZARD FLIGHT PANEL AUDIO EIS FLIGHT SYSTEM FEATURES AVOIDANCE MANAGEMENT NSCc & INSTRUMENTS OVERVIEW

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ADDITIONAL HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM INDEX APPENDICES FEATURES AFCS AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

AHRS1	Selects the #1 AHRS
AHRS2	Selects the #2 AHRS
PFD	Displays second-level softkeys for additional PFD configurations
SYN VIS	Displays the softkeys for enabling or disabling Synthetic Vision features
PATHWAY	Displays rectangular boxes representing the horizontal and vertical flight path of the
	active flight plan
SYN TERR	Enables synthetic terrain depiction
HRZN HDG	Displays compass heading along the Zero-Pitch line
APTSIGNS	Displays position markers for airports within approximately 15 nm of the current aircraft
	position. Airport identifiers are displayed when the airport is within approximately 9 nm.
DFLTS	Resets PFD to default settings, including changing units to standard
WIND	Displays softkeys to select wind data parameters
OPTN 1	Headwind/tailwind and crosswind arrows with numeric speed components
OPTN 2	Wind direction arrow and numeric speed
OPTN 3	Wind direction arrow with numeric headwind/tailwind and crosswind speeds
OFF	Information not displayed
BRG1	Cycles the Bearing 1 Information Window through NAV1 or GPS/ waypoint identifier
	and GPS-derived distance information.
HSI FRMT	Displays the softkeys for selecting the two HSI formats
360 HSI	Displays HSI as a 360° compass rose
ARC HSI	Displays HSI as a 140° viewable arc
BRG2	Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier
	and GPS-derived distance information
ALT UNIT	Displays softkeys for setting the altimeter and BARO settings to metric units
METERS	When enabled, displays altimeter in meters
IN	Press to display the BARO setting as inches of mercury
HPA	Press to display the BARO setting as hectopacals
STD BARO	Sets barometric pressure to 29.92 in Hg (1013 hPa if metric units are selected)
OBS	Selects OBS mode on the CDI when navigating by GPS (only available with active leg)
CDI	Cycles through GPS, VOR1, and VOR2 navigation modes on the CDI
XPDR	Displays transponder mode selection softkeys
STBY	Selects standby mode (transponder does not reply to any interrogations)
ON	Selects Mode A (transponder replies to interrogations)
ALT	Selects Mode C – altitude reporting mode (transponder replies to identification and
	altitude interrogations)
GND	Manually selects Ground Mode, the transponder does not allow Mode A and Mode C
	replies, but it does permit acquisition squitter and replies to discretely addressed
	Mode S interrogations

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Garmin G1000 Pilot’s Guide for the Quest Kodiak 100

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