Garmin Kodiak 100 Reference Guide

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Integrated Flight Deck

Cockpit Reference Guide

Quest

Kodiak 100

This manual reﬂects the operation of System Software version 0552.00 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., Unit 5, The Quadrangle, Abbey Park Industrial Estate, Romsey, Hampshire S051 9DL, U.K. Tel: 44/0870.851241 Fax: 44/0870.8501251

Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan Tel: 886/02.2642.9199 Fax: 886/02.2642.9099

Web Site 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. These trademarks may not be used without the express permission of Garmin.

NavData® is a registered trademark of Jeppesen, Inc.; Stormscope® is a registered trademark of L-3 Communications; and XM® is a registered trademark of XM Satellite Radio, Inc.

March 2007 190-00645-00 Rev. A Printed in the U.S.A.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

WARNINGS,

CAUTIONS, & NOTES

WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function. The G1000 Terrain Proximity 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 Proximity feature is only to be used as an aid for terrain avoidance and is not certiﬁed for use in applications requiring a certiﬁed terrain awareness system. 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 the G1000 Multi Function Display 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.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

WARNINGS,

CAUTIONS, & NOTES

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.

WARNING: The Garmin G1000, as installed in the Quest Kodiak 100 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 Quest Kodiak 100 Pilot’s Operating Handbook. 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 Airman’s Information Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identiﬁed as severe or giving an intense radar echo.”

CAUTION: The GDU 1040 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.

190-00645-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

WARNINGS,

CAUTIONS, & NOTES

CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modiﬁcations could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations.

NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode. However, clusters of two or more discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has been cleared.

NOTE: All visual depictions contained within this document, including screen images of the G1000 panel and displays, are subject to change and may not reﬂect the most current G1000 system. 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: 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.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

RECORD OF REVISIONS

Part Number Change Summary

190-00645-00 Initial release.

Revision Date of Revision Affected Pages Description

A March, 2007 i through Index-4 Production release

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Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

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RECORD OF REVISIONS

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Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

TABLE OF CONTENTS

SECTION 1: SYSTEM OVERVIEW .................................... 1-1

1.1 PFD/MFD Controls ................................................... 1-2

1.2 PFD Softkeys ............................................................ 1-4

1.3 MFD Softkeys ..........................................................1-7

1.4 MFD Page Groups ................................................... 1-8

1.5 Backlighting ............................................................. 1-8

1.6 Database Updates .................................................. 1-9

Aviation Database Update ........................................... 1-9

Terrain and Obstacle Database Updates ....................... 1-9

SECTION 2: FLIGHT INSTRUMENTS .............................. 2-1

2.1 Airspeed Indicator .................................................. 2-3

Speed Indication .........................................................2-3

Speed Ranges ............................................................. 2-3

Airspeed Trend Vector ................................................. 2-3

Vspeed References ...................................................... 2-3

2.2 Attitude Indicator ..................................................2-3

2.3 Altimeter .................................................................. 2-4

Altitude Select Bug ...................................................... 2-4

Altitude Trend Vector ................................................... 2-4

Barometric Setting Box ................................................ 2-4

Altitude Alerting .......................................................... 2-4

Barometric Minimum Descent Altitude .........................2-4

2.4 Vertical Deviation/Glideslope Indicator ............ 2-5

2.5 Marker Beacon Annunciations ............................2-5

2.6 Vertical Speed Indicator ....................................... 2-5

2.7 Horizontal Situation Indicator (HSI) ...................2-6

Arc HSI .......................................................................2-6

Turn Rate Indicator and Heading Trend Vector .............. 2-6

Course Pointer ............................................................ 2-7

Course Deviation Indicator (CDI) ..................................2-7

Bearing Pointers and Information Windows .................. 2-7

Navigation Source ....................................................... 2-8

SECTION 3: ENGINE INDICATION .................................. 3-1

Engine Display ............................................................3-1

Engine System Display .................................................3-1

Engine Fuel Display ..................................................... 3-2

SECTION 4: NAV/COM AND TRANSPONDER .......... 4-1

4.1 NaV/coM Description ...............................................4-1

4.1 Radio Status Indications ....................................... 4-3

4.2 Volume ......................................................................4-3

4.3 Automatic Squelch ................................................. 4-3

4.4 Quickly Activating 121.500 MHz .......................... 4-3

4.5 Frequency Auto-tuning ......................................... 4-3

Auto-tuning on the PFD .............................................. 4-3

Auto-tuning on the MFD .............................................4-3

4.5 Transponder Operation ........................................... 4-4

Mode Selection ........................................................... 4-4

Reply Status ................................................................ 4-4

Code Selection ............................................................ 4-4

Flight ID Reporting ...................................................... 4-5

SECTION 5: AUDIO PANEL ................................................5-1

5.1 COM Radio Selection ............................................. 5-2

5.2 Marker Beacon Receiver ....................................... 5-2

Marker Beacon Signal Sensitivity .................................5-2

5.3 Nav Radio Audio Selection ................................... 5-2

5.4 Intercom System (ICS) Isolation .......................... 5-3

5.5 Intercom Squelch Control ..................................... 5-3

5.6 Digital Clearance Recorder and Player .............5-4

5.7 Reversionary Mode .................................................. 5-4

SECTION 6: AUTOMATIC FLIGHT CONTROL ............. 6-1

SECTION 7: NAVIGATION .................................................. 7-1

7.1 Navigation Map Page ............................................ 7-1

Select the MAP Page Group ......................................... 7-1

7.2 Direct-to Navigation ..............................................7-1

Direct-to Navigation from the MFD .............................. 7-1

Direct-to Navigation from the PFD ............................... 7-2

7.3 Airport Information ............................................... 7-3

Select the Airport Information Page ............................. 7-3

7.4 Intersection Information ...................................... 7-4

Select the Intersection Information Page ...................... 7-4

7.5 NDB Information ..................................................... 7-4

Select the NDB Information Page .................................7-4

7.6 VOR Information ..................................................... 7-5

Select the VOR Information Page .................................7-5

7.7 User Waypoint Information Page .......................7-5

7.8 Nearest Airports ..................................................... 7-5

Nearest Airport Information on the MFD ...................... 7-5

Nearest Airports Information on the PFD ...................... 7-6

7.9 Nearest Intersections ............................................ 7-7

Select the Nearest Intersections Page ........................... 7-7

7.10 Nearest NDB ............................................................7-7

Select the Nearest NDB Page ....................................... 7-7

7.11 Nearest VOR .............................................................7-8

Select the Nearest VOR Page ....................................... 7-8

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Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

TABLE OF CONTENTS

7.12 Nearest User Waypoint ..........................................7-8

Select the Nearest User Waypoint Page ........................ 7-8

7.13 Nearest Frequencies .............................................. 7-9

Select the Nearest Frequencies Page ............................ 7-9

7.14 Nearest Airspaces ................................................... 7-9

Select the Nearest Airspaces Page ................................ 7-9

SECTION 8: FLIGHT PLANNING ...................................... 8-1

8.1 User Deﬁned Waypoints ........................................ 8-1

Select the User WPT Information Page ......................... 8-1

Create User Waypoints from the Navigation Map Page .8-2

8.2 Viewing the Active Flight Plan ............................ 8-2

8.3 Activate a Stored Flight Plan ............................... 8-2

8.4 Activate a Flight Plan Leg ....................................8-3

8.5 Stop Navigating a Flight Plan .............................. 8-3

8.6 Invert Active Flight Plan ....................................... 8-3

8.7 Create a New Flight Plan ...................................... 8-4

Create a New Flight Plan Using the MFD ..................... 8-4

Create a New Flight Plan Using the PFD ......................8-4

8.8 Load a Departure ...................................................8-5

8.9 Load an Arrival ........................................................ 8-5

8.10 Load an Approach ..................................................8-5

8.11 Remove a Departure, Arrival, or Approach

from a Flight Plan ...................................................8-5

8.12 Store a Newly Created Flight Plan ..................... 8-5

8.13 Edit a Stored Flight Plan ....................................... 8-5

8.14 Delete a Waypoint from the Flight Plan ............ 8-5

8.15 Invert and activate a Stored Flight Plan ...........8-6

8.16 Copy a Flight Plan ..................................................8-6

8.17 Delete a Flight Plan ............................................... 8-6

8.18 Graphical Flight Plan Creation ............................8-6

8.19 Trip Planning ............................................................8-6

8.20 Vertical Navigation (VNAV) Page ........................ 8-8

Create a Vertical Navigation Proﬁle .............................. 8-8

VNAV Page Menu Options ...........................................8-9

SECTION 9: PROCEDURES ................................................9-1

9.1 Arrivals and Departures ........................................ 9-1

Load and Activate a Departure Procedure ....................9-1

Load and Activate An Arrival Procedure ........................ 9-1

9.2 Approaches .............................................................. 9-2

Load and/or Activate an Approach Procedure ............... 9-2

Activate An Approach in the Active Flight Plan ............. 9-3

SECTION 10: HAZARD AVOIDANCE ...........................10-1

10.1 Customizing the Hazard Displays on the

Navigation Map .................................................... 10-1

10.2 STORMSCOPE® (Optional) ................................... 10-1

Displaying Stormscope Lightning Data on the

Navigation Map Page ................................................ 10-1

Stormscope Page ....................................................... 10-2

10.3 XM Weather (Optional) ....................................... 10-3

Displaying METAR and TAF information on the

Airport Information Page ........................................... 10-3

Displaying Weather on the Weather Data Link Page ... 10-4 Map Panning Information – Weather Data Link Page . 10-5

Weather Products and Symbols .................................10-5

Weather Product Age ................................................10-6

10.4 Trafﬁc Information Service (TIS) ....................... 10-7

Displaying Trafﬁc on the Trafﬁc Map Page ................... 10-7

Displaying Trafﬁc on the Navigation Map ................... 10-7

TIS Audio Alert ..........................................................10-7

10.5 Skywatch Trafﬁc Advisory System

(TAS)(Optional) ............................................................... 10-8

Displaying Trafﬁc on the Trafﬁc Map Page ................... 10-8

Displaying Trafﬁc on the Navigation Map ................... 10-8

10.6 Terrain And Obstacle Proximity ........................ 10-9

Displaying Terrain and Obstacles on the Terrain

Proximity Page .......................................................... 10-9

Displaying Terrain and Obstacles on the Navigation

Map .......................................................................... 10-9

10.7 Terrain Awareness & Warning System (TAWS)

Display (Optional) ..............................................10-10

Displaying Terrain on the TAWS Page ....................... 10-10

Enable/Disable Aviation Data ................................... 10-11

TAWS Inhibit ...........................................................10-11

Manual System Test ................................................. 10-12

Forward Looking Terrain Avoidance (FLTA) ................ 10-12

Premature Descent Alert (PDA) ................................ 10-12

Excessive Descent Rate Alert (EDR) .......................... 10-13

Negative Climb Rate After TakeoffAlert (NCR) .......... 10-13

“Five-Hundred” Aural Alert ...................................... 10-13

Pop-up Alerts .......................................................... 10-13

Displaying Terrain and Obstacles on the Navigation

Map ........................................................................ 10-14

Alert Annunciations ................................................. 10-14

TAWS Alerts Summary .............................................10-15

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 11: ABNORMAL OPERATION ..................... 11-1

11.1 Reversionary Mode .............................................. 11-1

11.2 Abnormal COM Operation .................................. 11-2

11.3 Unusual Attitudes ................................................. 11-2

11.4 Stormscope Operation with Loss of

Heading Input ........................................................ 11-2

11.5 Hazard Displays with Loss of GPS Position ....11-2

SECTION 12: ANNUNCIATIONS & ALERTS .............. 12-1

12.1 Alert Level Deﬁnitions ........................................ 12-2

12.2 Aircraft Alerts ........................................................12-3

WARNING Alerts ....................................................... 12-3

CAUTION Alerts ........................................................ 12-3

Annunciation Advisory ............................................... 12-4

Normal Operating Annunciation ................................ 12-4

Message Advisory Alerts ............................................ 12-4

12.4 G1000 System Annunciations ............................12-5

12.5 G1000 System Message Advisories .................. 12-7

MFD & PFD Message Advisories .................................12-8

Database Message Advisories .................................... 12-9

GMA 1347 Message Advisories ............................... 12-10

GIA 63 Message Advisories ..................................... 12-11

GEA 71 Message Advisories .................................... 12-13

GTX 33 Message Advisories .....................................12-13

GRS 77 Message Advisories ..................................... 12-14

GMU 44 Message Advisories ...................................12-14

GDL 69 Message Advisories .....................................12-15

GDC 74A Message Advisories .................................. 12-15

Miscellaneous Message Advisories ........................... 12-15

TABLE OF CONTENTS

INDEX ...................................................................................Index-1

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Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

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TABLE OF CONTENTS

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Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

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SECTION 1

SYSTEM OVERVIEW

SECTION 1: SYSTEM OVERVIEW

The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to ﬁnd operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide. Complete operating procedures for the complete system are found in the G1000 Pilot’s Guide for the Quest Kodiak 100 (19000590-00):

This guide gives the pilot abbreviated operating instructions for both Primary Flight Displays (PFD), Multi Function Display (MFD), and the GMA 1347 Audio Panel System.

NOTE: The pilot should read and thoroughly understand the Quest Kodiak 100 Pilot’s Operating Handbook (POH) for limitations, procedures and operational information not contained in this Cockpit Reference Guide. The Quest Kodiak 100 POH always takes precedence over the information found in this guide.

190-00645-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

1-1

SECTION 1

SYSTEM OVERVIEW

1.1 PFD/MFD CONTROLS

421 6

1-2

Figure 1-1 PFD/MFD Controls

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 1

SYSTEM OVERVIEW

The same controls and keys are found on both PFDs

and the MFD.

(1) NAV VOL/ID Knob – Controls the NAV audio level. Press to turn the Morse code identiﬁer ON and OFF. Volume level is shown in the ﬁeld as a percentage.

(2) NAV Frequency Transfer Key – Switches the standby and active NAV frequencies. (3) Dual NAV Knob – Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the NAV receiver. Press to move the tuning cursor (light blue box) between the NAV1 and NAV2 ﬁelds. (4) Heading Knob – Turn to manually select a heading on the HSI. When pressed, it synchronizes the heading bug with the compass lubber line. (5) Joystick – Changes the map range (distance top to bottom of map display) when rotated. Activates the map pointer when pressed. (6) CRS/BARO Knob – The large knob sets the altimeter barometric pressure and the small

knob adjusts the course. The course is only adjustable when the HSI is in VOR1, VOR2, or OBS/SUSP mode. Pressing this knob centers the CDI on the currently selected VOR. (7) Dual COM Knob – Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the COM transceiver. Pressing this knob moves the tuning cursor (light blue box) between the COM1 and COM2 ﬁelds. (8) COM Frequency Transfer Key – Switches the standby and active COM frequencies. Pressing and holding this key for two seconds automatically tunes the emergency frequency (121.5 MHz) in the active frequency ﬁeld. (9) COM VOL/SQ Knob – Controls COM audio level. Pressing this knob turns the COM automatic squelch ON and OFF. Audio volume level is shown in the ﬁeld as a percentage. (10) Direct-to Key – Allows the user to enter a destination waypoint and establish a direct course to the selected destination (speciﬁed by the identiﬁer, chosen from the

active route, or taken from the map pointer position). (11) FPL Key – Displays the active Flight Plan Page for creating and editing the active ﬂight plan, or for accessing stored ﬂight plans. (12) CLR Key (DFLT MAP) – Erases information, cancels an entry, or removes page menus. To display the Navigation Map Page immediately, press and hold CLR (MFD only). (13) Dual FMS Knob – Used to select the page to be viewed (only on the MFD). The large

knob selects a page group (MAP, WPT, AUX, NRST), while the small knob selects a speciﬁc page within the page group. Pressing the small knob turns the selection cursor ON and OFF. (14) MENU Key – Displays a context-sensitive list of options. This list allows the user to access additional features, or to make setting changes that relate to certain pages. (15) PROC Key – Selects approaches, departures and arrivals from the ﬂight plan. If a ﬂight plan is used, available procedures for the departure and/or arrival airport are automatically suggested. If a ﬂight plan is not used, the desired airport and the desired procedure may be selected. This key selects IFR departure procedures (DPs), arrival procedures (STARs) and approaches (IAPs) from the database and loads them into the active ﬂight plan. (16) ENT Key – Accepts a menu selection or data entry. This key is used to approve an operation or complete data entry. It is also used to conﬁrm selections and information entries. (17) Dual ALT Knob – Sets the reference altitude in the box located above the Altimeter. The large knob selects the thousands, while the small knob selects the hundreds.

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Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

1-3

SECTION 1

Press the BACK or OFF Softkey to return to the top-level softkeys.

ALERTS

SYSTEM OVERVIEW

1.2 PFD SOFTKEYS

Softkey ON

Figure 1-2 PFD Top Level Softkeys

INSET – Press to display the Inset Map in the lower

left corner of the PFD.

OFF

– Press to remove the Inset Map.

DCLTR

(3) – Press momentarily to select the desired amount of map detail. The declutter level appears adjacent to the DCLTR Softkey.

• No declutter: All map features are visible

• Declutter – 1: Declutters land data

• Declutter – 2: Declutters land and SUA data

• Declutter – 3: Removes everything except the active ﬂight plan

TRAFFIC TOPO

– Press to display trafﬁc on the inset map.

– Press to display topographical data (i.e., coastlines, terrain, rivers, lakes) and elevation scale on the Inset Map.

Softkey OFF

TERRAIN

– Press to display terrain information on

the Inset Map.

STRMSCP (optional)

– Press to display the Stormscope lightning data on the Inset Map (within a 200 nm radius of the aircraft).

NEXRAD (optional)

– Press to display NEXRAD

precipitation data on the Inset Map.

XM LTNG (optional)

– Press to display the XM Radio

lightning data on the Inset Map.

BACK

– Press to return to the previous level softkey

conﬁguration.

ALERTS

– Press to display the Alerts Window.

1-4

Figure 1-3 INSET Softkeys

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 1

Press the STD BARO or BACK Softkey to return to

the top-level softkeys

BRG2 (NAV2)

BRG2 (GPS)

BRG2 (OFF

)

BRG1 (NAV1

)

BRG1 (GPS)

BRG1 (OFF

)

ALERTS

METRIC

ARC HSI360 HSI

SYSTEM OVERVIEW

PFD – Press to display the additional softkeys for

additional conﬁguration of the PFD.

METRIC

– Press to display the current and reference altitudes in meters, in addition to feet. Pressing the metric softkey also changes the barometric setting to hectopascals.

DFLTS

– Press to reset default settings on the PFD.

BRG1 (bearing)

– Press to cycle through the

following information:

NAV1

– Displays NAV1 waypoint frequency or

identiﬁer in the BRG1 Information Window.

GPS

– Displays GPS waypoint identiﬁer and GPS distance information in the BRG1 Information Window.

OFF

– Removes the BRG1 In f o rmation

Window.

360 HSI ARC HSI BRG2 (bearing)

– Press to display the 360° compass rose.

– Press to display the 140° viewable arc.

– Press to cycle through the

following information:

NAV2

– Displays NAV2 waypoint frequency or

identiﬁer in the BRG2 Information Window.

GPS

– Displays GPS waypoint identiﬁer and GPS distance information in the BRG2 Information Window.

OFF

– Removes the BR G 2 Informat i o n

Window.

STD BARO

– Press to set the barometric pressure to

29.92 inches of mercury (1013 hPa by pressing the METRIC Softkey).

BACK

– Press to return to the previous level

softkeys.

ALERTS

– Press to display the Alerts Window.

190-00645-00 Rev. A

Figure 1-4 PFD Conﬁguration Softkeys

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

1-5

SECTION 1

Press the BACK Softkey to return to the top level softkeys

Press the BACK Softkey to retur

n to the top level softkeys

SYSTEM OVERVIEW

OBS – Press to select OBS mode on the CDI when

navigating by GPS (only available with active leg).

CDI – Press to change navigation mode on the CDI

between GPS, VOR1, and VOR2.

XPDR – Press to display the transponder mode

selection softkeys.

STBY

– Press to select standby mode.

– Press to select mode A.

ALT

– Press to select altitude reporting mode.

VFR

– Press to automatically squawk 1200 (only in the U.S.A., refer to ICAO standards for VFR codes in other countries).

CODE

– Press to display transponder code selection

softkeys 0-7.

0 through 7 IDENT

– Press numbers to enter code.

– Press to provide special aircraft position identiﬁcation to Air Trafﬁc Control (ATC).

BKSP

– Press to remove numbers entered one

at a time.

BACK

– Press to return to the previous level

softkeys.

IDENT

– Press to provide special aircraft position

identiﬁcation to Air Trafﬁc Control (ATC).

BACK

– Press to return to the previous level

softkeys.

ALERTS

– Press to display the Alerts Window.

IDENT – Press to provide special aircraft position

identiﬁcation to Air Trafﬁc Control (ATC).

TMR/REF – Press to display the Timer/References

Window.

NRST – Press to display the Nearest Airports

Window.

ALERTS – Press to display the Alerts Window.

1-6

Figure 1-5 XPDR (Transponder Softkeys

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 1

MAP

DCLTR

TRAFFIC

TOPO

TERRAIN

DCLTR-2

DCLTR-3

DCLTR-1

BACK

Press to return to the top softkey level

CHKLIST

EXIT

EMERGCY

ENGINE

DONE

The DONE Softkey changes to UNDO when the checklist item is already checked

STRMSCP

NEXRAD

XM LTNG

(optional)

(optional) (optional)

BACK

ENGINE

BACK

SYSTEM

Press the BACK Softkey on this level to return to the top softkey level

RST FUEL

DEC FUEL

INC FUEL

(optional)

FUEL

SYSTEM

FUEL

SYSTEM OVERVIEW

1.3 MFD SOFTKEYS

ENGINE – Pressing this softkey makes available the Engine

Display functions. Refer to the Engine Indication System section.

MAP – Pressing this softkey enables the following

softkeys:

TRAFFIC – Pressing this softkey displays/removes

Trafﬁc on the Navigation Map.

TOPO – Pressing this softkey displays or removes

topographic information on the Navigation Map.

TERRAIN – Pressing this softkey displays/removes

terrain and obstacle data on the Navigation Map.

STRMSCP (optional) – Pressing this softkey displays/

removes Stormscope lightning data on the Navigation Map.

NEXRAD (optional) – Pressing this softkey displays/

removes precipitation data on the Navigation Map.

XM LTNG (optional) – Pressing this softkey displays/

removes XM Radio lightning data on the Navigation Map.

BACK – Pressing this softkey displays the ENGINE and

MAP top level softkeys.

DCLTR (declutter) – Pressing this softkey removes map

information in three levels.

190-00645-00 Rev. A

Figure 1-6 MFD Softkeys

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

1-7

SECTION 1

SYSTEM OVERVIEW

1.4 MFD PAGE GROUPS

1) Turn the large

FMS

Knob until the desired page

group is selected.

FMS

2) Turn the small

Knob to select pages within

the group. See Figure 1-8.

Nearest Group

Auxiliary Page Group

Waypoint Page Group

Map Page Group

1.5 BACKLIGHTING

To manually adjust the backlight for the PFD and MFD:

1) Press the PFD Setup Menu Window.

MENU Key on the PFD to display the

Number of Pages in Current

Figure 1-7 Page Group Icon

Group

Selected Page

1-8

2) Press the small FMS Knob to activate the cursor. ‘PFD DSPL > AUTO’ is now highlighted.

3) Turn the small FMS Knob to display the selection window.

4) Turn the FMS Knob to select ‘MANUAL’, then press the ENT Key.

5) With the intensity value now highlighted, turn the small FMS Knob to select the desired backlighting.

6) Turn the large FMS Knob to highlight ‘MFD DSPL > AUTO’ and repeat steps 3 through 5.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Figure 1-8 PFD Setup Menu Window

190-00645-00 Rev. A

SECTION 1

SYSTEM OVERVIEW

1.6 DATABASE UPDATES

Aviation Database Update

NOTE: The display downloads the aviation database and stores it internally. The aviation database SD card is not required to remain in the display after the update.

1) With the G1000 System OFF, insert the aviation database update SD card into the top card slot of the PFD (Label of SD card facing left).

2) Turn the G1000 System ON. This prompt is displayed on the upper left corner of the PFD:

Figure 1-9 Database Update Prompt

3) Press the ENT Key to conﬁrm the database updated. This prompt is displayed:

7) Verify that the correct update cycle is loaded during startup of the MFD.

Terrain and Obstacle Database Updates

NOTE: The data contained in the terrain and obstacle databases comes from government agencies. Garmin accurately processes and cross-validates the data, but cannot guarantee the accuracy and completeness of the data.

NOTE: Obstacles 200’ and higher are included in the obstacle database. It is very important to note that not all obstacles are necessarily charted and therefore may not be contained in the obstacle database.

These databases are not stored internally in the MFD or PFD. Supplemental Data Cards containing identical database versions must be kept in both displays to retain terrain and obstacle data. A Supplemental Data Card should be inserted into the bottom card slot of the PFD and MFD.

Figure 1-10 Database Update Conﬁrmation

4) After the update completes, the PFD starts in normal mode. Remove the aviation database update SD card from the PFD.

5) Turn the G1000 System OFF.

6) Repeat steps 1 through 4 for the MFD. The MFD and PFD aviation databases are now updated.

190-00645-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

NOTE: If the Supplemental Data Card is

removed from the display, the TOPO and TERRAIN Softkeys are not functional and are

grayed out on the MFD Map Page.

1) Insert one card in the bottom card slot of the

MFD and one in the bottom card slot of the PFD.

2) Apply power to the G1000 System. View the

MFD power-up splash screen. Check that the Terrain and Obstacle databases are initialized and displayed on the scrolling window of the splash screen.

1-9

SECTION 1

SYSTEM OVERVIEW

3) Acknowledge the Power-up Page agreement by pressing the

ENT

Key or the right most

softkey.

4) At the MAP – NAVIGATION MAP page, select the

MAP

Softkey and check to make sure that

the

TOPO

and

TERRAIN

softkeys are functional

(not grayed out).

5) Power down the G1000.

1-10

Figure 1-11 Power-Up Splash Screen Window

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 2: FLIGHT INSTRUMENTS

The following discussions pertain to the Primary Flight Display, unless otherwise indicated.

SECTION 2

FLIGHT INSTRUMENTS

NAV Frequency Window

Airspeed Indicator

Turn Rate Indicator

Barometric Setting Box

190-00645-00 Rev. A

True Airspeed Box

Heading Box

Horizontal Situation Indicator

Outside Air Temperature Box

System Time Box

Transponder Status Bar

Figure 2-1 Default PFD Information

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Vertical Speed Indicator

Altimeter

Selected Altitude Box

COM Frequency Window

Navigation Status Window

Slip/Skid Indicator

Attitude Indicator

2-1

SECTION 2

FLIGHT INSTRUMENTS

Trafﬁc Annunciation

Selected Heading Box

Inset Map

BRG1 Information Window

BRG2 Information Window

Figure 2-2 Additional PFD Information

Alerts Window

Selected Course Box

Annunciation Window

Vertical Deviation/

Marker Beacon Annunciation

Glideslope Indicator

2-2

Distance to Next Waypoint

Next Waypoint

Desired Track to

Next Waypoint

Figure 2-3 PFD Navigation Status Window

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Current Track

190-00645-00 Rev. A

SECTION 2

FLIGHT INSTRUMENTS

2.1 AIRSPEED INDICATOR

Max Speed

for Approach

Flap Setting

Airspeed

Actual

Airspeed

True Airspeed

Box

Figure 2-4 Airspeed Indicator

Speed Indication

The indicated airspeed is displayed inside the black pointer. The pointer will become red upon reaching Vne.

Trend Vector

Speed

Ranges

Vspeed

References

Vspeed References

Vspeed References are turned on or off in the

Timer/References Window. Press the

TMR/REF Softkey to display the widow. When active (ON), the Vspeeds are displayed at their respective locations to the right of the airspeed scale. To activate the Vspeed References, display the Timer/Reference Window and turn the large FMS Knob to place the cursor in the ON/OFF ﬁeld. Turn the small FMS Knob to select ON or OFF.

2.2 ATTITUDE INDICATOR

The Slip/Skid Indicator is located under the roll pointer and moves laterally away from the pointer to indicate lateral acceleration. One Slip/Skid indicator displacement is equal to one ball displacement when compared to a traditional slip/skid indicator.

Figure 2-5 Red Pointer at Vne

Speed Ranges

The color coded speed range strip denotes ﬂaps operating range, normal operating range, and never exceed speed (Vne). A red range is also present for low speed awareness. Refer to the Pilot’s Operating Handbook (POH) for airspeed limitations and indicator markings.

Airspeed Trend Vector

The end of the trend vector displays approximately what the airspeed will be in 6 seconds if the current rate of acceleration/deceleration is maintained.

190-00645-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Roll Pointer

Roll Scale

Horizon Line

Aircraft Symbol

Land Representation

Figure 2-6 Attitude Indicator

Aircraft Wing Tips

Pitch Scale

Slip/Skid Indicator

Sky Representation

Roll Scale Zero

2-3

SECTION 2

FLIGHT INSTRUMENTS

2.3 ALTIMETER

Altitude Select Bug

Altitude Trend

Vector

Figure 2-7 Altimeter

Altitude Select Bug

The Altitude Select Bug is displayed at the Selected Altitude or the edge of the tape (whichever is closer to the current altitude) to provide increased altitude awareness and to set the desired hold altitude for the autopilot.

To set the Selected Altitude Bug:

ALT

Turn the

Bug. The the

large ALT

Knobs to set the Altitude Select

small ALT

Knob sets the hundreds and

Knob sets the thousands. This altitude also appears in the Selected Altitude Box above the Altimeter.

Altitude Trend Vector

The end of the trend vector displays approximately what the altitude will be in 6 seconds if the current rate of vertical speed is maintained.

Selected Altitude

Box

Current Altitude

Barometric Setting

Box

Altitude Alerting

Within 1000 ft

Figure 2-8 Altitude Alerting Visual Annunciations

Within 200 ft

Visual annunciations appear in the Selected Altitude Box. Whenever the Selected Altitude is changed, the Altitude Alerter is reset. The Altitude Alerter is independent of the Automatic Flight Control System.

An aural tone is heard when the aircraft is within 200 feet of acquiring the selected altitude or when deviating beyond 200 feet of the acquired selected altitude.

Deviation of ±200 ft

Barometric Minimum Descent Altitude

The desired barometric minimum descent altitude (MDA, or Decision Height, DH) can be set in the Timer/ References Window.

Visual annunciations alert the pilot when approaching the MDA:

• When the aircraft altitude descends to within 2500 feet of the MDA setting, the Barometric Minimum Box appears with the altitude in light blue text. The bug appears on the tape in light blue once in range.

• When the aircraft passes through 100 feet of the MDA, the bug and text turn white.

• Once the aircraft descends past the MDA, the bug and text turn yellow and the aural alert, “Minimums Minimums”, is generated.

2-4

Barometric Setting Box

To set barometric pressure, turn the BARO Knob to

select the desired setting.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Alerting is inhibited while the aircraft is on the ground. If the aircraft climbs after having reached the MDA, once it reaches 50 feet above the MDA, alerting is disabled.

190-00645-00 Rev. A

SECTION 2

FLIGHT INSTRUMENTS

Within 2500 ft

Barometric Mini-

mum Bug

Barometric

Minimum Box

Altitude Reached

Figure 2-9 Barometric Minimum Descent Altitude

Alerting Visual Annunciations

Within 100 ft

2.5 MARKER BEACON ANNUNCIATIONS

Marker Beacon

Annunciation

Vertical

Deviation/Glideslope

Indicator

Figure 2-10 Marker Beacon and Vertical Deviation

2.6 VERTICAL SPEED INDICATOR

2.4 VERTICAL DEVIATION/GLIDESLOPE INDICATOR

The Vertical Deviation/Glideslope Indicator appears

when an ILS is tuned in the active NAV ﬁeld.

190-00645-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Vertical Speed Pointer

Figure 2-11 Vertical Speed Indicator

The actual vertical speed is displayed inside the

pointer.

2-5

SECTION 2

FLIGHT INSTRUMENTS

2.7 HORIZONTAL SITUATION INDICATOR (HSI)

Turn Rate Indicator

Lateral Deviation Scale

Navigation Source

Aircraft Symbol

Course Deviation Indicator

Rotating Compass Rose

OBS Mode

TO/FROM Indicator

Heading Bug

Course Pointer

Flight Phase

Turn Rate and Heading Trend Vector

Heading

Lubber Line

Figure 2-12 Horizontal Situation Indicator (360˚)

Arc HSI

NOTE: When the Arc HSI is displayed the BRG1 and BRG2 Information Windows and pointers are disabled.

NOTE: If the pilot makes a heading change greater than 105˚ with respect to the course, the CDI switches to the opposite side of the deviation scale and displays reverse sensing.

The Arc HSI is a 140˚ expanded section of the compass rose. The Arc contains a course pointer arrow, the TO/ FROM indicator, a sliding deviation indicator (the TO/ FROM and sliding deviation indicators are one and the same), and a deviation scale. Upon station passage, the TO/FROM indicator ﬂips and points to the tail of the aircraft, just like the conventional TO/FROM ﬂag. Depending on the navigation source, the CDI on the Arc HSI can appear in two different ways:

• GPS, OBS, VOR – Arrowhead

• Localizer – Diamond

Lateral

Deviation

Scale

Course Deviation and

TO/FROM Indicator

Figure 2-13 Arc HSI

Turn Rate Indicator and Heading Trend Vector

Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. A magenta

2-6

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 2

FLIGHT INSTRUMENTS

turn rate trend vector shows the current turn rate. The end of the trend vector gives the heading predicted in six seconds, based on the present turn rate. At rates greater than 4 deg/sec, an arrowhead appears at the end of the magenta trend vector and the prediction is no longer valid.

Half-Standard Turn

Rate Tick Mark

Standard Turn

Rate Tick Mark

Figure 2-14 Turn Rate Indicator and Trend Vector

Figure 2-15 Standard-Rate Turn Indication

Turn Rate Trend Vector (rate > 4 deg/sec)

Turn Rate Trend Vector (standard rate)

Course Pointer

Course Deviation Indicator (CDI)

The CDI scale automatically adjusts to the current phase of ﬂight (enroute 5.0 nm, terminal area 1.0 nm, or approach 0.3 nm). Scaling may be selected manually from the MFD System Setup Page. See System Setup in the G1000 Pilot’s Guide for more details.

Bearing Pointers and Information Windows

Pressing the PFD Softkey provides access to the BRG1 and BRG2 Softkeys. The BRG1 pointer is a single line pointer. The BRG2 pointer is a double line pointer.

Bearing 1

Pointer

Bearing 2

Pointer

CDI

The course pointer is a single line arrow (GPS, VOR1 and LOC1) or double line arrow (VOR2 and LOC2) which points in the direction of the set course.

Figure 2-16 Course Pointer

190-00645-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Bearing 1

Information

Window

Figure 2-17 HSI with Bearing Information

Distance to

Bearing Source

Waypoint Identiﬁer

Bearing

Source

Figure 2-18 BRG1 Information Window

Pointer

Icon

Bearing 2

Information

Window

2-7

SECTION 2

FLIGHT INSTRUMENTS

Distance to

Bearing Source

Waypoint

Identiﬁer

Pointer

Icon

Figure 2-19 BRG2 Information Window

Bearing

Source

Navigation Source

To change between navigation sources:

1) Press the CDI Softkey to change from GPS to

VOR1/LOC1.

2) Press the CDI Softkey again to change from

VOR1/LOC1 to VOR2/LOC2.

3) Press the GPS.

When using GPS as the navigation source, the following

may appear:

• INTEG – GPS information is either not present or is invalid for navigation use

• WARN – GPS detects a position error

• SUSP – Displayed when in OBS Mode indicating GPS waypoint sequencing is suspended.

CDI

Softkey a third time to return to

Figure 2-20 GPS INTEG, GPS SUSP, LOC1 and VOR2

To enable/disable OBS mode while navigating with GPS:

1) Press the

OBS Softkey to select OBS Mode.

2) Turn the CRS Knob to select the desired course

TO/FROM the waypoint.

2-8

3) Press the OBS Softkey again to return to

normal operation.

NOTE: The OBS Softkey is only displayed when

navigating an active leg using GPS.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 3 – EICAS

SECTION 3: ENGINE INDICATION

Engine Display

In all cases green indicates normal operation, yellow

indicates caution, and red indicates warning.

Pressing the SYSTEM and FUEL softkeys which in turn provide access to the System Display and the Fuel Display, respectively.

Engine Torque

Inlet Turbine Temperature

Propeller

RPM

Gas Generator

RPM

Fuel Flow

(pounds per hour)

Oil Temperature

Indicator

ENGINE Softkey makes available the

Oil Pressure

Indicator

Engine System Display

Pressing the SYSTEM Softkey displays the System Display. This display presents a numerical indication of oil, fuel, and electrical parameters.

Ammeter

Voltmeter

Fuel Quantity

Indicator

Aileron and

Rudder Trim

Figure 3-1 Kodiak Default Engine Display

190-00645-00 Rev. A

Flap Position

Elevator Trim

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Figure 3-2 Kodiak SYSTEM Engine Display

3-1

SECTION 3 – EICAS

Engine Fuel Display

NOTE: Fuel calculations do not use the aircraft fuel quantity indicators, and are calculated from the last time the fuel was reset using fuel ﬂow.

Pressing the FUEL Softkey displays the System

Display.

The following softkeys allow for adjustment of the

remaining fuel quantity.

- DEC FUEL – Allows the pilot to decrease the fuel remaining (LB REM) in 10-pound increments

- INC FUEL – Allows the pilot to increase the remaining in 1-pound increments

- RST FUEL – Resets the fuel remaining to 2200 pounds.

Fuel used (LB USED), endurance (ENDUR), and range (RANGE NM) are all calculated based on the last adjustment of the fuel remaining (LB REM).

fuel

Figure 3-3 Kodiak FUEL Engine Display

3-2

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 4: NAV/COM AND

TRANSPONDER

4.1 NAV/COM DESCRIPTION

The Nav/Com controls and frequency boxes are located on the Primary Flight Display and the Multi-Function Display in the same locations.

SECTION 4 – NAV/COM &

TRANSPONDER

NAV

Controls

NAV Frequency Box COM Frequency Box

COM

Controls

190-00645-00 Rev. A

Figure 4-1 G1000 NAV/COM Control Location (PFD)

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

4-1

SECTION 4 – NAV/COM &

TRANSPONDER

Standby NAV

Frequency Field

Tuning Box

Selected NAV

Frequency

Active NAV

Frequency Field

Frequency Transfer Arrow

Figure 4-3 Frequency Transfer Arrow and Tuning Box

NAV Controls COM Controls

Figure 4-2 Frequency Fields

VOL/PUSH

ID Knob

VOL/PUSH

SQ Knob

Selected COM

Frequency

Tuning Box

Active COM

Frequency Field

Standby COM

Frequency Field

Tuning Box

4-2

Frequency Transfer Key

Dual NAV

Knob

• Turn to tune in desired frequencies.

• Press to change tuning box positions.

Figure 4-4 NAV/COM Controls

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Dual COM

Knob

190-00645-00 Rev. A

SECTION 4 – NAV/COM &

TRANSPONDER

4.1 RADIO STATUS INDICATIONS

• RX – When a COM signal is received, a white ‘RX’ appears by the active COM frequency during signal reception.

• TX – When a COM radio is transmitting, a white ‘TX’ indication appears to the right of the corresponding COM frequency.

• ID – When the Morse code identiﬁer is ON for a NAV radio, a white ‘ID’ indication appears to the left of the corresponding active NAV frequency. The Morse code identiﬁer can be heard if the corresponding NAV radio is selected on the

Figure 4-5 Radio Status Indications

audio panel.

4.2 VOLUME

‘VOLUME’ is displayed in place of the associated radio name (i.e., ‘COM1’ or ‘NAV2’) for two seconds after the volume level is last changed. The percentage of maximum volume is displayed in place of the standby frequency selected by the tuning box.

4.4 QUICKLY ACTIVATING 121.500 MHZ

Pressing and holding the COM Frequency Transfer Key for approximately two (2) seconds automatically tunes the selected COM radio to the emergency frequency.

4.5 FREQUENCY AUTO-TUNING

Auto-tuning on the PFD

Figure 4-7 Nearest Airports Window (PFD)

1) Select the Airports Window.

2) Turn either frequency.

3) Press the standby ﬁeld of the active COM.

4) Press the frequency in the active ﬁeld.

NRST

Softkey to display the Nearest

FMS

Knob to highlight the desired

ENT

Key to place the frequency in the

Frequency Transfer

Key to place the

Figure 4-6 COM Volume Level

4.3 AUTOMATIC SQUELCH

Automatic squelch can be disabled for a COM radio by pressing the COM Knob to place the tuning box on the desired COM’s standby frequency, then by pressing the VOL/PUSH SQ Knob.

190-00645-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

NAV frequencies are entered automatically in the active NAV frequency ﬁeld upon approach loading or approach activation.

Auto-tuning on the MFD

Auto-tuning on the MFD is done in much the same way as on the PFD. Use the FMS Knobs to select the desired frequency on any of the information pages. Pressing the ENT Key then loads the selected frequency in the tuning box as a standby frequency.

4-3

SECTION 4 – NAV/COM &

TRANSPONDER

4.5 TRANSPONDER OPERATION

Mode Selection

The STBY, ON, ALT, VFR, CODE, and IDENT

Softkeys can be accessed by pressing the

Ground Mode (Automatic)

GND is displayed when the aircraft is on the ground.

Figure 4-8 Ground Mode

Standby Mode (Manual)

Press the

STBY Softkey. In Standby Mode, the transponder does not reply to interrogations, but new codes can be entered.

STBY Mode (White

Code Number and

XPDR Softkey.

Mode)

Altitude Mode (Automatic or Manual)

Altitude Mode is automatically selected when the air

craft becomes airborne. Altitude Mode may also be selected manually by pressing the ALT Softkey.

All transponder replies requesting altitude information

are provided with pressure altitude information.

ALT Mode (Mode C

Altitude Reporting)

Figure 4-11 Altitude Mode

Reply Status

When the transponder sends replies to interrogations, an “R” indication appears momentarily in the reply status ﬁeld.

Indication

Figure 4-12 Reply Indication

4-4

Figure 4-9 Standby Mode

Manual ON Mode

Press the

ON Softkey. ON Mode generates Mode A and Mode S replies, but Mode C altitude reporting is inhibited.

ON Mode

(No Altitude

Reporting)

Figure 4-10 ON Mode

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Code Selection

VFR Code Selection

1) Press the transponder Mode Selection softkeys.

2) Press the Pressing the previous identiﬁcation code.

NOTE: The pre-programmed VFR Code is set at the factory to 1200.

Manual Code Entry

1) Press the transponder Mode Selection softkeys.

XPDR

Softkey to display the

VFR

Softkey to enter the VFR code.

VFR

Softkey again restores the

XPDR

Softkey to display the

190-00645-00 Rev. A

SECTION 4 – NAV/COM &

TRANSPONDER

2) Press the

CODE

Softkey to display the transponder Code Selection softkeys, which includes the digit softkeys.

3) Press the appropriate digit softkeys to enter the code in the four-digit code ﬁeld of the Transponder Status Box. Five seconds after the fourth digit has been entered, the transponder code becomes activated.

BKSP

When entering a code, press the

Softkey as needed to back up and change code digits.

Following is a list of important codes:

• 1200 – VFR code in the U.S. (please refer to the ICAO standards for VFR codes in other countries).

• 7000 – VFR code commonly used in Europe

(please

refer to the ICAO standards).

• 7500 – Hijack code.

• 7600 – Loss of communication code.

• 7700 – Emergency code.

• 7777 – Military interceptor operations code (NEVER ENTER THIS CODE).

• 0000 – Code for military use (in the U.S.).

Flight ID Reporting

If so conﬁgured, the Flight ID may be entered in the

Timer/Reference Window.

Flight ID

PFD Entry

Figure 4-13 Timer/References Window

1) Press the References Window.

2) Turn the large Flight ID ﬁeld.

3) Turn the small character.

4) Turn the large next desired ﬁeld.

5) Turn the small character.

6) Repeat steps 4 and 5 until the desired Flight ID is entered.

7) Press the the Flight ID is loaded into the system.

TMR/REF

ENT Key. ‘updating’ will be displayed as

Softkey to display the Timer/

FMS Knob to place the cursor in the

FMS Knob to enter the desired ﬁrst

FMS Knob to place the cursor in the

FMS Knob to enter the next desired

190-00645-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

4-5

SECTION 4 – NAV/COM &

TRANSPONDER

Blank Page

4-6

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 5: AUDIO PANEL

SECTION 5 – AUDIO PANEL

Transmitters

Disabled on Quest

Kodiak 100

Passenger Address

Marker Beacon/Mute

Disabled on Quest

Kodiak 100

Manual Squelch

Transceiver Audio

Disabled on Quest

Kodiak 100

Speaker

Marker Beacon Signal Sensitivity

Navigation Radio Audio

Digital Recording Playback

ICS Isolation

ICS Volume and Squelch Control

VOL Annunciation

Reversionary Mode for

PFD1 and MFD

190-00645-00 Rev. A

Master Volume Control

SQ Annunciation

Reversionary Mode for

Pilot Side Copilot Side

Figure 5-1 Front Panel Controls

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

PFD2 and MFD

5-1

SECTION 5 – AUDIO PANEL

5.1 COM RADIO SELECTION

Pressing the COM1 MIC or COM2 MIC Key selects the active transmitter (i.e., microphone). The associated receiver audio (COM1 or COM2) also becomes selected when the COM MIC Key is pressed.

To prevent deselecting the desired received audio when pressing another COM MIC Key, press the already selected COM1 or COM2 Key before pressing the other COM MIC Key.

Figure 5-2 Transceivers

5.2 MARKER BEACON RECEIVER

The marker beacon receiver is always on. Only the marker beacon audio can be turned off. Figure 5-3 shows the marker beacon annunciators on the PFD.

Outer Marker

Annunciator

Inner Marker

Annunciator

Figure 5-3 Marker Beacon Annunciators on the PFD

Middle Marker

Annunciator

Marker Beacon Signal Sensitivity

The HI SENS Key can be pressed for increased marker

beacon signal sensitivity.

5-2

When the

MKR/MUTE Key is pressed, the key annunciator is lit and the audio tone can be heard over the speaker or headsets during marker beacon reception.

When the tone is active, pressing the MKR/MUTE Key once mutes the audio but does not affect the marker annunciator. The audio returns when the next marker signal is received.

To turn off the marker beacon audio, press the

MKR/

MUTE Key once when there is no marker indication

present, or press twice when an indication is present. The key annunciator will be extinguished when the marker beacon audio is turned off.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Figure 5-4 Marker Beacon

5.3 NAV RADIO AUDIO SELECTION

Pressing NAV1, or NAV2 selects and deselects the radio source and activates the annunciator. Selected audio can be heard over the headset and the speakers. These twokeys can be selected individually or together.

Figure 5-5 Navigation Radios

190-00645-00 Rev. A

SECTION 5 – AUDIO PANEL

5.4 INTERCOM SYSTEM (ICS) ISOLATION

Press the PILOT and/or COPLT Key to select who is isolated from hearing the Nav/Com radios and music. Selection scenarios are addressed in Table 5-1.

Figure 5-6 ICS Isolation

Mode

PILOT KEY

ANNUNCIATOR

ALL OFF OFF

COPLT KEY

ANNUNCIATOR

5.5 INTERCOM SQUELCH CONTROL

Select manual squelch for intercom audio by pressing

the MAN SQ Key to light the annunciator.

Pressing the small between volume and squelch adjustment by lighting VOL or SQ respectively.

Figure 5-7 Volume/Squelch Control

Pilot Hears Copilot Hears

Selected radios; pilot; copilot; passengers; MUSIC 1

VOL/SQ Knob now switches

Passenger

Hears

Selected radios; pilot; copilot; passengers; MUSIC 2

PILOT

COPILOT

CREW ON ON

190-00645-00 Rev. A

Copilot; passengers; MUSIC 1

ON OFF

Selected radios; pilot

Selected radios;

OFF ON

pilot; passengers;

Copilot

MUSIC 1

Selected radios; pilot; copilot

Table 5-1 ICS Isolation Modes

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Selected radios; pilot; copilot

Copilot; passengers; MUSIC 2

Selected radios; pilot; passengers; MUSIC 2

Passengers; MUSIC 2

5-3

SECTION 5 – AUDIO PANEL

5.6 DIGITAL CLEARANCE RECORDER AND PLAYER

Each reception of primary active COM audio is automatically recorded in a memory block. When the next transmission is received, it is recorded in the next memory block, and so on. Once the 2.5 minutes of recording time has been reached, the recorder begins recording over the stored memory blocks, starting from the oldest block. Powering off the unit automatically clears all recorded blocks.

Figure 5-8 Clearance Recorder Play Key

• Pressing PLAY once plays the latest recorded memory block, then returns to normal operation.

• Pressing MKR/MUTE while playing a memory block stops play.

• Pressing the PLAY Key during play begins playing the previously recorded memory block. Each subsequent press of the PLAY Key will begin playing the next previously recorded block.

5.7 REVERSIONARY MODE

Figure 5-9 Reversionary Mode Button

The red DISPLAY BACKUP button selects the reversionary mode for all displays. Reversionary mode operation displays important ﬂight and engine information on both the PFD and MFD, in case of display failure.

The pilot side controls the pilot side PFD (PFD1) and the MFD. The copilot side controls the copilot side PFD (PFD2) and the MFD.

5-4

If a COM input signal is detected while playing, play is halted and the new COM input signal is recorded as the latest block.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 6: AUTOMATIC FLIGHT

CONTROL

Refer to the pilot’s guide for the installed autopilot system.

SECTION 6 – AUTOMATIC

FLIGHT CONTROL

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Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

6-1

SECTION 6 – AUTOMATIC

FLIGHT CONTROL

Blank Page

6-2

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 7 – NAVIGATION

SECTION 7: NAVIGATION

The following discussions pertain to the Multi Function Display, unless otherwise indicated.

7.1 NAVIGATION MAP PAGE

Select the MAP Page Group

1) Turn the large highlighted in the page group window in the lower right of the MFD display.

2) Turn the small page (indicated by a solid rectangular icon).

3) Press the for the available information which may be displayed on the map.

WARNING: The map display should only be used for situational awareness. Any map display indication should be compared with approved navigation sources.

FMS

Knob until ‘MAP’ is

FMS

Knob to select the ﬁrst MAP

MAP

Softkey to display softkeys

7.2 DIRECT-TO NAVIGATION

Direct-to Navigation from the MFD

Identiﬁer

Facility Name

Flight Plan Field

City

Map of the

Selected

Waypoint

Bearing

Distance

Direct-to

Course

Figure 7-2 MFD Direct-to Window

Enter a Direct-to Destination

1) Press the

2) Turn the small

Direct-to ( )

FMS

Knob to enter the ﬁrst letter

Key.

of the destination waypoint identiﬁer. Turn the

FMS

large

Knob to the right to move the cursor

to the next character position.

Symbol

Nearest Airport

Map Orientation

Map Range

Region

Latitude/

Longitude

Activate Field

Figure 7-1 Navigation Map Page

190-00645-00 Rev. A

3) Repeat step 2 to spell out the rest of the waypoint identiﬁer.

ENT

4) Press the

Key to conﬁrm the identiﬁer. The

‘Activate?’ ﬁeld is highlighted.

ENT

5) Press the

Key to activate.

Select a Direct-to Destination to a Flight Plan Waypoint or Nearest Airport

1) While navigating an active ﬂight plan, press the

Direct-to ( )

2) Turn the large

FMS

NRST WAYPOINT’ ﬁeld.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Key.

Knob to highlight the ‘FPL/

7-1

SECTION 7 – NAVIGATION

3) Turn the small

FMS

Knob to display a list of

waypoints or airports.

FMS

4) Continue turning the small

Knob to scroll through the list and highlight the desired waypoint or airport.

ENT

5) Press the Press

ENT

Key to conﬁrm the selection.

again to activate a Direct-to.

To Re-center the CDI to the Destination Waypoint

Press the Direct-to

by pressing the

( )

Key, followed

ENT

Key twice. If a missed approach point (MAP) is the current destination, the approach will be canceled.

To Manually Deﬁne the Direct-to Course

1) Press the

Direct-to ( )

Key and enter a waypoint as discussed in previous steps, or to edit the active direct-to.

FMS

2) Turn the large

Knob to highlight the

‘COURSE’ ﬁeld.

FMS

3) Turn the and press the

4) Press the

Knobs to select the desired course

ENT

Key.

ENT

Key again to begin navigation

using the selected destination and course.

Canceling Direct-to Navigation

1) Press the

2) Press the

Direct-to ( )

Key to display the Direct-to

Key.

options menu.

3) With ‘Cancel Direct-To NAV’ highlighted, press the

ENT

Key. If a ﬂight plan is still active, the G1000 resumes navigating the ﬂight plan along the closest leg.

Figure 7-3 Canceling Direct-to Navigation

Direct-to Navigation from the PFD

WPT Symbol

Identiﬁer

Facility Name

Flight Plan WPT

Bearing to WPT

Distance from WPT

Course to Selected WPT

Figure 7-4 PFD Direct-to Window

1) Press the Direct-to Key large

2) Turn the

FMS

the desired selection ﬁeld.

3) Turn the small

FMS

desired identiﬁer, location, etc.

ENT

4) Press the

Key.

5) The cursor is now ﬂashing on ‘ACTIVATE?’.

Press the

ENT

Key again to activate.

Cancelling Direct-to Navigation

1) Press the Direct-to

2) Press the

Window. The cursor will be ﬂashing on ‘Cancel Direct-to NAV’.

ENT

3) Press the

Key to cancel the direct-to.

( )

Knob to place the cursor in

Knob to begin selecting the

( )

Key.

Key to display the Options

WPT Location

Nearest WPT

Lat/Lon

7-2

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 7 – NAVIGATION

7.3 AIRPORT INFORMATION

Figure 7-5 Airport Information Page

Select the Airport Information Page

1) Turn the large page group.

2) Turn the small rectangular page icon.

Enter a Waypoint Facility Name or City Location

1) With the Airport Information Page displayed, press the

2) Turn the large name or location (city) ﬁeld.

3) Turn the small ﬁrst character.

4) Turn the large character ﬁeld.

5) Repeat steps 3 and 4 until the facility name or location is selected, then press If there are duplicate names in the database,

FMS

Knob to select the ‘WPT’

FMS

Knob to select the ﬁrst

FMS

Knob to activate the cursor.

FMS

Knob to select the facility

FMS

Knob to select the desired

FMS

Knob to select the next

the ENT Key.

a list is displayed from which to choose the desired location.

6) To remove the ﬂashing cursor, press the

FMS

Knob.

Access Runway Information

1) With the Airport Information Page displayed, press the

2) Turn the large

FMS

Knob to activate the cursor.

FMS

Knob to place the cursor

on the ‘RUNWAYS’ identiﬁer ﬁeld.

FMS

3) Turn the small

Knob to display the next

runway for the selected airport. Continue

FMS

turning the small

Knob to select the

desired runway.

4) To remove the ﬂashing cursor, press the

FMS

Knob.

Access Frequency Information

1) With the Airport Information Page displayed, press the

2) Turn the large

FMS

Knob to activate the cursor.

FMS

Knob to move the cursor to

the Frequencies Window.

FMS

3) Turn either

Knob to scroll through the list, placing the cursor on the desired frequency. If a listed frequency has sector or altitude restrictions, the frequency is preceded by an info (‘i’) designation. Press the

ENT

Key to view the information. The following may be displayed with the frequency:

• ‘TX’ – transmit only

• ‘RX’ – receive only

• ‘PT’ – part time frequency

4) Press the

ENT

Key to place the selected frequency in the standby ﬁeld of the COM or NAV window.

FMS

5) To remove the cursor, press the

Knob.

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Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

7-3

SECTION 7 – NAVIGATION

7.4 INTERSECTION INFORMATION

Select the Intersection Information Page

1) Turn the large page group.

2) Turn the small rectangular page icon.

FMS

Knob to select the ‘WPT’

FMS

Knob to select the second

7.5 NDB INFORMATION

Figure 7-7 NDB Information Page

Select the NDB Information Page

1) Turn the large page group.

FMS

Knob to select the ‘WPT’

7-4

Figure 7-6 Intersection Information Page

Access Information on an Intersection

1) With the Intersection Information Page displayed, press the cursor.

2) Turn the identiﬁer and press the

3) Press the cursor.

FMS

Knob to activate the

Knobs to enter a name for the

ENT

Key.

Knob to remove the ﬂashing

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

FMS

2) Turn the small rectangular page icon

View Information on a Speciﬁc NDB

1) With the NDB Information Page displayed, press the

2) Turn the large desired selection field (identifier, name or closest city).

3) Turn the or city and press the

4) Press the cursor.

FMS

Knob to select the third

Knob to activate the cursor.

FMS

Knob to highlight the

Knobs to enter an identiﬁer, name

ENT

Key.

Knob to remove the ﬂashing

190-00645-00 Rev. A

SECTION 7 – NAVIGATION

7.6 VOR INFORMATION

Figure 7-8 VOR Information Page

Select the VOR Information Page

1) Turn the large page group.

2) Turn the small rectangular page icon.

Access Information on a VOR

1) With the VOR Information Page displayed, press the

FMS

2) Turn the large desired selection field (identifier, name or closest city).

3) Turn the or city and press the

4) The ‘FREQUENCY’ ﬁeld is now highlighted. If desired, press the frequency in the NAV receiver standby ﬁeld.

5) Press the cursor.

FMS

Knob to select the ‘WPT’

FMS

Knob to select the fourth

Knob to activate the cursor.

FMS

Knob to highlight the

FMS

Knobs to enter an identiﬁer, name

ENT

Key.

ENT

Key to place the

FMS

Knob to remove the ﬂashing

7.7 USER WAYPOINT INFORMATION PAGE

See the Flight Planning section for a discussion on

creating and modifying user deﬁned waypoints.

7.8 NEAREST AIRPORTS

Figure 7-9 Nearest Airports Page

Nearest Airport Information on the MFD

Select the Nearest Airports Page

1) Turn the large page group.

2) Turn the small rectangular page icon.

Access Information on a Speciﬁc Airport

1) With the Nearest Airports Page displayed, press the ‘NEAREST AIRPORTS’ ﬁeld. The ﬁrst airport in the nearest airports list is highlighted.

2) Press the Knob to highlight the desired airport.

FMS

Knob to select the ‘NRST’

FMS

Knob to select the ﬁrst

APT

Softkey to place the cursor in the

FMS

Knob, then turn the large

FMS

190-00645-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

7-5

SECTION 7 – NAVIGATION

3) Press the

FMS

Knob to remove the ﬂashing

cursor.

Access Runway Information for the Selected Airport

1) With the Nearest Airports Page displayed, press the

RNWY

Softkey to place the cursor in the

‘RUNWAYS’ ﬁeld.

2) Turn the small

FMS

Knob to select the desired

runway.

FMS

3) Press the

Knob to remove the ﬂashing

cursor.

Quickly Tune the COM Transceiver to a Nearby Airport Frequency

1) With the Nearest Airports Page displayed, press the

FREQ

Softkey to place the cursor in the

‘FREQUENCIES’ ﬁeld.

FMS

2) Turn either

Knob to select the desired

frequency.

ENT

3) Press the

Key. The selected frequency is placed in the COM standby frequency tuning box.

4) Press the

Frequency Transfer

Key to place the

frequency in the active ﬁeld.

Nearest Airports Information on the PFD

Bearing TO

Airport Symbol

Identiﬁer

Primary COM Frequency

Figure 7-10 Nearest Airports Window

Press the

NRST

Nearest Airports Window.

View Information on a Speciﬁc Airport in the List

1) With the Nearest Airports Window displayed, turn either

FMS

the desired airport identiﬁer.

2) Press the

ENT

information.

ENT

3) Press the

Key again (cursor is on ‘BACK’)

to return to the list.

Distance

Runway Length

Softkey to display the PFD

Knob to place the cursor on

Key to display airpor t

7-6

5) Press the cursor.

FMS

Knob to remove the ﬂashing

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Load an Airport COM Frequency into the Active COM

1) With the Nearest Airports Window displayed, turn either

FMS

Knob to place the cursor on the desired airport frequency shown in the window.

ENT

2) Press the

Key and the selected frequency will be placed in the COM standby frequency ﬁeld.

3) Press the

Frequency Transfer

Key to make the

frequency the active frequency.

190-00645-00 Rev. A

SECTION 7 – NAVIGATION

7.9 NEAREST INTERSECTIONS

Figure 7-11 Nearest Intersections Page

Select the Nearest Intersections Page

1) Turn the large page group.

2) Turn the small rectangular page icon.

FMS

Knob to select the ‘NRST’

FMS

Knob to select the second

7.10 NEAREST NDB

Figure 7-12 Nearest NDB Page

Select the Nearest NDB Page

1) Turn the large page group.

2) Turn the small rectangular page icon.

FMS

Knob to select the ‘NRST’

FMS

Knob to select the third

View Information on the Nearest Intersection

1) With the Nearest Intersections Page displayed, press the

2) Turn either intersection.

3) Press the cursor.

190-00645-00 Rev. A

FMS

Knob to activate the cursor.

FMS

Knob to select the desired

FMS

Knob to remove the ﬂashing

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Access Information on a Speciﬁc NDB

1) With the Nearest NDB Page displayed, press the

FMS

Knob to activate the cursor.

FMS

2) Turn either The remaining information on the Nearest NDB Page pertains to the selected NDB.

3) Press the cursor.

Knob to select the desired NDB.

FMS

Knob to remove the ﬂashing

7-7

SECTION 7 – NAVIGATION

7.11 NEAREST VOR

Select the Nearest VOR Page

1) Turn the large page group.

2) Turn the small rectangular page icon.

FMS

Knob to select the ‘NRST’

FMS

Knob to select the fourth

2) Press the is placed in the NAV standby frequency ﬁeld.

3) Press the cursor.

ENT

Key. The selected VOR frequency

FMS

Knob to remove the ﬂashing

7.12 NEAREST USER WAYPOINT

Figure 7-14 Nearest User Waypoints Page

7-8

Figure 7-13 Nearest VOR Page

View Information on the Nearest VOR

1) With the Nearest VOR Page displayed, press the

VOR

Softkey to place the cursor in the

‘NEAREST VOR’ Window.

FMS

2) Turn either

3) Press the cursor.

Select and Load a VOR Frequency

1) With the Nearest VOR Page displayed, press the

FREQ

Softkey to highlight the VOR frequency

in the ‘FREQUENCY’ ﬁeld.

Knob to select a VOR.

FMS

Knob to remove the ﬂashing

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Select the Nearest User Waypoint Page

1) Turn the large page group.

2) Turn the small rectangular page icon.

Select a Nearest User Waypoint

1) With the Nearest User Waypoint Page displayed, press the any previously entered User Waypoints are within 200 nm, these will be displayed with the closest listed ﬁrst.

2) Turn either waypoint. The remaining information on the Nearest User Waypoint Page pertains to the selected Nearest User Waypoint.

FMS

Knob to select the ‘NRST’

FMS

Knob to select the ﬁfth

FMS

Knob to activate the cursor. If

FMS

Knob to select the desired

190-00645-00 Rev. A

SECTION 7 – NAVIGATION

3) Press the cursor.

FMS

Knob to remove the ﬂashing

7.13 NEAREST FREQUENCIES

Figure 7-15 Nearest Frequencies Page

Select the Nearest Frequencies Page

1) Turn the large page group.

2) Turn the small rectangular page icon.

Select and Load the Nearest ARTCC, FSS, or Weather Frequency

1) With the Nearest Frequencies Page displayed, press the the cursor in the appropriate ﬁeld.

2) Turn the or frequency.

3) Press the the COM frequency standby ﬁeld.

FMS

Knob to select the ‘NRST’

FMS

Knob to select the sixth

ARTCC, FSS, or Wx

FMS

Knobs to select the desired facility

ENT

Key to load the frequency into

Softkey to place

7.14 NEAREST AIRSPACES

Figure 7-16 Nearest Airspaces Page

Select the Nearest Airspaces Page

1) Turn the large page group.

2) Turn the small rectangular page icon.

Airspace Alerts Box

• If the projected course takes the aircraft inside an airspace within the next ten minutes, ‘Ahead’ is displayed.

• If the aircraft is within two nautical miles of an airspace and the current course takes the aircraft inside, ‘Ahead < 2 nm’ is displayed.

• If the aircraft is within two nautical miles of an airspace and the current course will not take the aircraft inside, ‘Within 2 nm’ is displayed.

• If the aircraft has entered an airspace, ‘Inside’ is displayed.

FMS

Knob to select the ‘NRST’

FMS

Knob to select the seventh

4) Press the cursor.

190-00645-00 Rev. A

FMS

Knob to remove the ﬂashing

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

7-9

SECTION 7 – NAVIGATION

View Additional Details for a Listed Airspace

1) With the Nearest Airspace Page displayed, press the

2) Turn the large

FMS

Knob to activate the cursor.

FMS

list, highlighting the desired airspace.

ALERTS

3) Press the

Softkey to place the cursor in

the ‘AIRSPACE ALERTS’ ﬁeld.

FMS

4) Turn either

Knob to select the desired

airspace.

FMS

5) Press the

Knob to remove the ﬂashing

cursor.

View and Quickly Load the Frequency for a Controlling Agency

1) With the Nearest Airspace Page displayed, press the

FREQ

Softkey to place the cursor in

‘FREQUENCIES’ ﬁeld.

Knob to scroll through the

7-10

FMS

2) Turn either

Knob to select the desired

frequency.

ENT

3) Press the

Key to load the frequency into

the COM frequency standby ﬁeld.

FMS

4) Press the

Knob to remove the ﬂashing

cursor.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 8 – FLIGHT PLANNING

SECTION 8: FLIGHT PLANNING

The following discussions pertain to the Multi Function

Display, unless otherwise indicated.

8.1 USER DEFINED WAYPOINTS

Figure 8-1 User WPT Information Page

Select the User WPT Information Page

4) Repeat steps 2 and 3 until the desired name is entered.

ENT

5) Press the

6) Press the waypoint identiﬁer.

7) The cursor is now in the ‘REFERENCE WAYPOINTS’ ﬁeld. If desired, the waypoint can be deﬁned by a reference waypoint. Turn the

FMS

Knobs to enter the position coordinates or the radial and distance from the reference waypoint.

8) Press the cursor.

Modify a User Waypoint

1) With the User Waypoint Information Page displayed, press the cursor.

2) Turn the large the desired ﬁeld and turn the small to make changes.

3) Press the

Key.

ENT

Key a again to accept the new

FMS

Knob to remove the ﬂashing

FMS

Knob to activate the

FMS

Knob to move the cursor to

FMS

ENT

Key to accept the changes.

Knob

1) Turn the large page group.

2) Turn the small rectangular page icon.

Create a New User Waypoint

1) With the User Waypoint Information Page displayed, press the is created at the current aircraft position.

2) Turn the small of the waypoint name.

3) Turn the large the next character ﬁeld.

190-00645-00 Rev. A

FMS

Knob to select the ‘WPT’

FMS

Knob to select the ﬁfth

NEW

Softkey. A waypoint

FMS

Knob to enter ﬁrst character

FMS

Knob to move the cursor to

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

FMS

4) Press the cursor.

Delete a User Waypoint

1) Select the User Waypoint Information Page and press Information Page Options or press the Softkey.

2) Turn the large Waypoint’ and press the ‘Would you like to delete the user waypoint’ is displayed. With ‘YES’ highlighted, press the

ENT

Key.

Knob to remove the ﬂashing

to display the User Waypoint

FMS

Knob to select ‘Delete User

ENT

Key. The message

DELETE

8-1

SECTION 8 – FLIGHT PLANNING

Create User Waypoints from the Navigation Map Page

1) With the Navigation Map Page displayed, push the

Joystick

The target pointer is displayed at the present aircraft position.

to activate the panning function.

2) Move the

Joystick

to place the pointer at the

desired position

ENT

3) Press the

Key. The User Waypoint Information Page is now displayed with the captured position.

FMS

4) Turn the

Knobs to select a waypoint

name.

ENT

5) Press the

Key to accept the selected name. The ﬁrst reference waypoint ﬁeld is highlighted.

FMS

6) If desired, turn the

Knobs to enter the identiﬁer of the reference waypoint and the radial and distance to the reference waypoint. Press the

7) Press the

ENT

Key to accept.

FMS

Knob to remove the ﬂashing

cursor.

8.2 VIEWING THE ACTIVE FLIGHT PLAN

Press the

FPL

Key.

Figure 8-3 Active Flight Plan Page on the MFD

8.3 ACTIVATE A STORED FLIGHT PLAN

1) Press the to display the Flight Plan Catalog Page.

FPL

Key and turn the small

FMS

Knob

8-2

Figure 8-2 Active Flight Plan Window on the PFD

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Figure 8-4 Flight Plan Catalog Page

2) Press the

3) Turn the large ﬂight plan and press the

FMS Knob

FMS

Knob to highlight the desired

to activate the cursor.

ACTIVE

Softkey.

4) With ‘OK’ highlighted, press the activate the ﬂight plan. To cancel the ﬂight plan activation, turn the large

FMS

highlight ‘CANCEL’ and press the

190-00645-00 Rev. A

ENT

Key to

Knob to

ENT

Key.

SECTION 8 – FLIGHT PLANNING

8.4 ACTIVATE A FLIGHT PLAN LEG

1) From the Active Flight Plan Page, press the Knob to activate the cursor and turn the large

FMS

Knob to highlight the desired destination

waypoint.

2) Press the

ACT LEG

Softkey (using MFD only).

3) Press the

Key, select the ‘Activate Leg’ option from the page menu and press the Key. This step must be used when activating a leg from the PFD.

4) With ‘Activate’ highlighted, press the Key.

Figure 8-5 Activate Flight Plan Leg Conﬁrmation

FMS

ENT

8.5 STOP NAVIGATING A FLIGHT PLAN

the ﬂight plan. This will not delete the stored ﬂight plan, only the active ﬂight plan.

Figure 8-7 Delete Flight Plan Conﬁrmation

8.6 INVERT ACTIVE FLIGHT PLAN

1) From the Active Flight Plan Page, press the

Key to display the Page Menu.

FMS

2) Turn the large Flight Plan’ and press the ﬂight plan remains intact in its ﬂight plan catalog storage location.

3) With ‘OK’ highlighted, press the invert the ﬂight plan.

Knob to highlight ‘Invert

ENT

Key. The original

ENT

Key to

1) Press the Plan Page.

2) Press the window.

Figure 8-6 Delete Flight Plan

3) Turn the large Flight Plan’ and press the highlighted, press the

190-00645-00 Rev. A

FPL

Key to display the Active Flight

Key to display the Page Menu

FMS

Knob to highlight ‘Delete

ENT

Key. With ‘OK’

ENT

Key to deactivate

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Figure 8-8 Invert Flight Plan

Figure 8-9 Invert Flight Plan Conﬁrmation

8-3

SECTION 8 – FLIGHT PLANNING

8.7 CREATE A NEW FLIGHT PLAN

Create a New Flight Plan Using the MFD

1) Press the to display the Flight Plan Catalog Page.

2) Press the ﬂight plan page for the ﬁrst empty storage location.

3) Turn the small Waypoint Information Window.

4) Turn the small character of the identiﬁer of the departure waypoint.

5) Turn the large the next character ﬁeld. Repeat steps 4 and 5 until the desired identiﬁer has been entered.

FPL

Key and turn the small

NEW

Softkey to display a blank

Figure 8-10 Create FPL on MFD

FMS

Knob to display the

FMS

Knob to enter the ﬁrst

FMS

Knob to move the cursor to

FMS

Knob

Catalog Page. The new ﬂight plan is now in the list.

Create a New Flight Plan Using the PFD

NOTE: A ﬂight plan cannot be entered using the

PFD if another ﬂight plan is active.

NOTE: After the ﬁrst leg is entered (using the

PFD only), it is immediately activated.

1) Press the activate the cursor.

2) Turn the small of the destination waypoint identiﬁer. Turn the large to the next character position.

3) Repeat step 2 to spell out the rest of the waypoint identiﬁer.

4) Press the for entering of the next ﬂight plan waypoint.

5) Repeat steps 2 through 4 to enter the identiﬁer for each additional ﬂight plan waypoint.

FPL

Key, then press the

FMS

Knob to enter the ﬁrst letter

FMS

Knob to the right to move the cursor

ENT

Key and the cursor is now ready

FMS

Knob to

8-4

Figure 8-11 Waypoint Info Window

6) Press the

ENT

Key.

7) Repeat steps 3 through 5 to enter the identiﬁer for each additional ﬂight plan waypoint.

8) When all waypoints have been entered, press

FMS

the

Knob to return to the Flight Plan

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

6) Once all waypoints have been entered, press

FMS

the

Knob remove the cursor. The new

ﬂight plan is now active.

Figure 8-12 Creating Flight Plan on the PFD

190-00645-00 Rev. A

8.8 LOAD A DEPARTURE

See the Procedures section for a discussion on loading

and activating departure procedures.

SECTION 8 – FLIGHT PLANNING

Figure 8-13 Store Flight Plan Conﬁrmation

8.9 LOAD AN ARRIVAL

See the Procedures section for a discussion on loading

and activating arrival procedures.

8.10 LOAD AN APPROACH

See the Procedures section for a discussion on loading

and activating approach procedures.

8.11 REMOVE A DEPARTURE, ARRIVAL, OR APPROACH FROM A FLIGHT PLAN

1) With the Active or Stored Flight Plan Page

displayed, press the FMS Knob to activate the cursor.

2) Turn the large FMS Knob to highlight the title

for the approach, departure or arrival to be deleted. Titles appear in white directly above the procedure’s waypoints.

3) Press the

window. With ‘OK’ highlighted, press the ENT Key to remove the selected procedure.

CLR Key to display a conﬁrmation

8.12 STORE A NEWLY CREATED FLIGHT PLAN

8.13 EDIT A STORED FLIGHT PLAN

1) Press the to display the Flight Plan Catalog Page.

2) Press the

3) Turn the large desired ﬂight plan and press the

4) Turn the large the desired locations for entering changes.

5) Turn the changes, then press the

6) Press the Catalog Page.

FPL

Key and turn the small

FMS Knob

FMS

FMS Knob

to activate the cursor.

FMS

Knob to highlight the

FMS

Knob to place the cursor in

Knobs to make the desired

ENT

Key.

to return to the Flight Plan

8.14 DELETE A WAYPOINT FROM THE FLIGHT PLAN

1) With either the Active or Stored Flight Plan displayed, press the cursor.

2) Turn the large to be deleted.

3) Press the Name)’ conﬁrmation window.

CLR

FMS

Knob to activate the

FMS

Knob to select the waypoint

Key to display a ‘REMOVE (Wpt

FMS

ENT

Knob

Key.

1) After creating a ﬂight plan on either the PFD or MFD, it may be saved by pressing the Key.

FMS

2) Turn the large Flight Plan’ and press the

3) With ‘OK’ highlighted, press the store the ﬂight plan.

190-00645-00 Rev. A

Knob to highlight ‘Store

ENT

Key.

ENT

Key to

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Figure 8-14 Remove Waypoint Conﬁrmation

4) With ‘OK’ highlighted, press the remove the waypoint. To cancel the delete request, turn the large ‘CANCEL’ and press the

FMS

Knob to highlight

ENT

Key.

ENT

Key to

8-5

SECTION 8 – FLIGHT PLANNING

5) Once all changes have been made, press the

FMS

Knob to remove the cursor.

8.15 INVERT AND ACTIVATE A STORED FLIGHT PLAN

1) From the Flight Plan Catalog Page, press the

FMS

Knob to activate the cursor.

FMS

2) Turn the large desired ﬂight plan.

3) Press the stored ﬂight plan?’ will be displayed.

4) With ‘OK’ highlighted, press the The selected ﬂight plan is now inverted and activated. The original ﬂight plan remains intact in its flight plan catalog storage location.

INVERT

Knob to highlight the

Softkey. ‘Invert and activate

ENT

Key.

8.16 COPY A FLIGHT PLAN

1) From the Flight Plan Catalog press the Knob to activate the cursor

2) Turn the large plan to be copied.

3) Press the

4) A ‘Copy to ﬂight plan #?’ conﬁrmation window is displayed. With ‘OK’ highlighted, press the

ENT

Key to copy the ﬂight plan. To cancel, turn the large press the

FMS

Knob to highlight the ﬂight

COPY

Softkey.

FMS

Knob to highlight ‘CANCEL’ and

ENT

Key.

FMS

3) Press the

4) A ‘Delete ﬂight plan #?’ conﬁrmation window is displayed. With ‘OK’ highlighted, press the

ENT

turn the large and press the

DELETE

Key to delete the ﬂight plan. To cancel,

Softkey.

FMS

Knob to highlight ‘CANCEL’

ENT

Key.

8.18 GRAPHICAL FLIGHT PLAN CREATION

1) Press the Plan Page.

2) Press the Use the desired point on the map to be inserted as a waypoint in the ﬂight plan.

3) Press the waypoint will be inserted at the end of the ﬂight plan. The default user waypoint naming is USR000, USR001, USR002 and so on.

4) If the selected waypoint is to be placed elsewhere in the ﬂight plan, press the Knob to activate the cursor. Waypoints are inserted

5) After placing the cursor at the desired point in the list of waypoints, press the Softkey.

6) To change the user waypoint name, follow the procedure for modifying a user waypoint.

FPL

Key to display the Active Flight

Joystick

ABOVE

to activate the map pointer.

to move the pointer to the

LD WPT

Softkey. The selected

the cursor.

FMS

LD WPT

8.19 TRIP PLANNING

8-6

8.17 DELETE A FLIGHT PLAN

1) From the Flight Plan Catalog Page, press the

FMS

Knob to activate the cursor.

2) Turn the large plan to be deleted.

FMS

Knob to highlight the ﬂight

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

1) Turn the large page group.

2) Turn the small rectangular page icon.

FMS

Knob to select the ‘AUX’

FMS

Knob to select the ﬁrst

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SECTION 8 – FLIGHT PLANNING

3) The current page mode is displayed at the top of the page: ‘AUTOMATIC’ or ‘MANUAL’. To change the page mode, press the

MANUAL

Starting WPT Ending WPT

Softkey.

Figure 8-15 Trip Planning Page

4) For Direct-to planning, press the

WPTS

AUTO

Softkey and verify that the starting waypoint field indicates ‘P.POS’ (present position). If necessary,

press the

Key and select ‘Set WPT to

Present Position’ to display ‘P.POS’. Press the

ENT

Key and the ﬂashing cursor moves to the

ending waypoint ﬁeld. Turn the

FMS

Knobs

to enter the identiﬁer of the ending waypoint

ENT

and press the

Key to accept the waypoint.

OR,

FMS

5) For point-to-point planning, turn the

Knobs to enter the identiﬁer of the starting waypoint. Once the waypoints identiﬁer is entered, press

ENT

the

Key to accept the waypoint. The ﬂashing cursor moves to the ending waypoint. Again, turn the the ending waypoint and press the

FMS

Knobs to enter the identiﬁer of

ENT

Key to

accept the waypoint. OR,

6) For ﬂight plan leg planning, press the

FPL

Softkey (at the bottom of the display) and turn the small

FMS

Knob to select the desired ﬂight plan

(already stored in memory), by number. Turn the

FMS

large turn the small

Knob to highlight the ‘LEG’ ﬁeld and

FMS

Knob to select the desired leg of the ﬂight plan, or select ‘CUM’ to apply trip planning calculations to the entire ﬂight plan. Selecting ‘FPL 00’ will display an active ﬂight plan. If an active ﬂight plan is selected, ‘REM’ will be an available option to display planning data for the remainder of the ﬂight plan.

NOTE: The Page Mode must be set to MANUAL to perform the following steps.

7) Turn the large

FMS

Knob to highlight the

departure time (DEP TIME) ﬁeld.

NOTE: The departure time on the Trip Planning Page is used for preﬂight planning. Refer to the Utility Page for the actual ﬂight departure time.

8) Turn the Press the

FMS

Knobs to enter the departure time.

ENT

Key when ﬁnished. (Departure time may be entered in local or UTC time, depending upon system settings).

FMS

9) Turn the Press the

Knobs to enter the fuel ﬂow.

ENT

Key when ﬁnished. Note that in automatic page mode, fuel ﬂow is provided by the system.

10) The ﬂashing cursor moves to the fuel on board

FMS

ﬁeld. Turn the on board. Press the

Knobs to modify the fuel

ENT

Key when ﬁnished. In ‘AUTOMATIC’ mode, fuel onboard is provided by the entry made in ‘GAL REM’ on the EIS System Page.

11) The ﬂashing cursor moves to the calibrated

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Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

8-7

SECTION 8 – FLIGHT PLANNING

airspeed ﬁeld. Turn the calibrated airspeed. Press the

FMS

Knobs to enter a

ENT

Key when

ﬁnished.

8.20 VERTICAL NAVIGATION (VNAV) PAGE

NOTE: An active ﬂight plan or Direct-to must be entered in order to utilize VNAV.

NOTE: VNAV is advisory only and cannot be coupled to the autopilot.

3) Press the

FMS

Knob to activate the cursor.

4) With the ‘TARGET POSITION’ distance ﬁeld

FMS

highlighted, turn the

Knobs to select the desired distance for Top Of Climb or Bottom Of Descent from the VNAV proﬁle endpoint. The default distance is 4 nm.

ENT

5) Press the

Key. The cursor is now positioned

over the ‘Before’ and ‘After’ ﬁeld.

FMS

6) Turn the small

Knob to select whether the previously set distance is ‘Before’ or ‘After’ the endpoint.

ENT

7) Press the

Key. The cursor is now placed

over the VNAV proﬁle endpoint ﬁeld.

8-8

Figure 8-16 Vertical Navigation (VNAV) Page

Create a Vertical Navigation Proﬁle

1) Press the

2) Turn the small page icon.

FPL

Key.

FMS

Knob to select the third

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

FMS

8) Turn the small

Knob to display a list possible VNAV proﬁle endpoints. When using a ﬂight plan, the target reference waypoint itself

190-00645-00 Rev. A

can be speciﬁed from the waypoints contained in the ﬂight plan. By default, the last waypoint in the ﬂight plan is selected. Highlight the desired waypoint.

ENT

9) Press the

Key.

10) With the ‘TARGET ALTITUDE’ ﬁeld highlighted,

FMS

turn the small and large

Knobs to select the target altitude. If the selected altitude is above the current aircraft altitude, a proﬁled climb is created. If the selected altitude is below the current aircraft altitude, a proﬁled descent will be created.

ENT

11) Press the

Key. The cursor is now placed in the ‘TARGET VERTICAL SPEED’ ﬁeld. The default proﬁle utilizes a 400 foot-per-minute descent rate.

FMS

12) To change the vertical speed, turn the Knobs to enter the desired vertical speed. Press the

ENT

Key when ﬁnished.

With the proﬁle set, the vertical speed required (VSR) is displayed. Expect the following to occur when using the vertical navigation feature:

At one minute prior to reaching the Bottom Of Climb or Top Of Descent point (gray arc), the message ‘APPR VPROF - Approaching VNAV Proﬁle’ is displayed as a PFD alert. The descent (or climb) angle also locks to prevent changes in speed from altering the proﬁle. If selected, the vertical speed required (VSR) readout on the default NAV and map pages shows the desired vertical speed to maintain the proper descent (or climb) angle. At 500 feet above (or below, for a climb) the target altitude (white arc), an ‘APPR TRG ALT’ - Approaching Target Altitude” message is provided. The VSR readout on the Navigation Map Page is blanked out at this point.

SECTION 8 – FLIGHT PLANNING

Figure 8-17 Approaching VNAV Proﬁle Message (PFD)

Figure 8-18 Approaching Target Altitude Message (PFD)

To display map data on the Vertical Navigation Map

Page, press the MAP Softkey. Press the TOPO, TERRAIN, or LTNG Softkey. Press the

same

softkey to remove the

displayed data from the Vertical Navigation Page.

VNAV Page Menu Options

The VNAV messages are not enabled until the ‘VNAV Messages On?’ option is enabled from the VNAV Page Menu Options. To display the page menu, press the MENU Key (with the VNAV Page displayed). The VNAV Page Options Menu also allows the pilot to restore VNAV page defaults.

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8-9

SECTION 8 – FLIGHT PLANNING

Blank Page

8-10

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 9: PROCEDURES

9.1 ARRIVALS AND DEPARTURES

Load and Activate a Departure Procedure

SECTION 9 – PROCEDURES

1) With the Navigation Map Page displayed, press the

FPL

Key.

LD DP

2) Press the

Softkey. If a ﬂight plan is active, the departure airport will be displayed as the default. A list of available departures is also displayed.

FMS

3) If no ﬂight plan is active, use the

Knobs to enter the identiﬁer of the desired airport. Press the

4) Turn the large Departure ﬁeld. Turn the small

ENT

Key.

FMS

Knob to highlight the

FMS

Knob to

display a list of available departures.

FMS

5) Turn either departure and press the

Figure 9-1 Select Departure

Knob to select the desired

ENT

Key.

6) A list of runways may be displayed for the

FMS

departure. Turn either desired runway and press the

Knob to select the

ENT

Key.

7) A list of available transitions is displayed for the

FMS

departure. Turn either

Knob to highlight

the desired transition waypoint and press the

ENT

Key.

Figure 9-2 Select Departure Transition

8) With ‘LOAD?’ highlighted, press the

ENT

The departure will be active when the ﬂight plan is active.

Load and Activate An Arrival Procedure

NOTE: If any portion of an arrival procedure is the active leg of a ﬂight plan, the existing arrival procedure must be deleted before changing to a different arrival procedure.

1) With the Navigation Map Page displayed, press the

FPL

Key.

2) Press the

LD STAR

active, the destination airport will be displayed as the default. A list of available arrivals is also displayed.

3) If no ﬂight plan is active, use the to enter the identiﬁer of the desired airport. Press the

ENT

4) Turn the large ﬁeld. Turn the small of available arrivals.

5) Turn either arrival and press the

Softkey. If a ﬂight plan is

FMS

Key.

FMS

Knob to highlight the Arrival

FMS

Knob to display a list

FMS

Knob to select the desired

ENT

Key.

Knobs

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Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

9-1

SECTION 9 – PROCEDURES

Figure 9-3 Select Arrival

6) A second window is displayed listing available transitions for the arrival. Turn either to highlight the desired transition waypoint and press the

ENT

Key.

FMS

Knob

9.2 APPROACHES

Not all approaches in the database are approved for GPS use. When selecting an approach, a “GPS” designation to the right of the procedure name indicates the procedure can be ﬂown using the GPS receiver. Some procedures will not have this designation, meaning the GPS receiver can be used for supplemental navigation guidance only. If the GPS receiver cannot be used for primary guidance, the appropriate navigation receiver must be used for the selected approach (e.g., VOR or ILS). The ﬁnal course segment of ILS approaches, for example, must be ﬂown by tuning the Nav receiver to the proper frequency and selecting that Nav receiver on the CDI.

Load and/or Activate an Approach Procedure

1) With the Navigation Map Page displayed, press the

FPL

Key.

9-2

Figure 9-4 Select Arrival Transition

7) A third window is displayed listing the available runways. Turn either desired runway and press the

Figure 9-5 Select Arrival Runway

8) With ‘LOAD?’ highlighted, press the

FMS

Knob to select the

ENT

Key.

ENT

Key. If a ﬂight plan is active, the selected arrival procedure is inserted after the destination airport and becomes part of the active ﬂight plan. If no ﬂight plan is active when the arrival is loaded, the arrival procedure will become the active ﬂight plan.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

2) Press the

LD APR

Softkey. If a ﬂight plan is active, the destination airport will be displayed as the default. A list of available approaches is also displayed.

3) If no ﬂight plan is active, use the to enter the identiﬁer of the desired airport. Press the

4) Turn the large Approach ﬁeld. Turn the small

ENT

Key.

FMS

Knob to highlight the

FMS

display a list of available approaches.

190-00645-00 Rev. A

FMS

Knobs

Knob to

Figure 9-6 Selecting an Approach Procedure

SECTION 9 – PROCEDURES

Selecting ‘Load?’ will add the procedure to the ﬂight plan without immediately using it for navigation guidance.

Activate An Approach in the Active Flight Plan

1) With the Navigation Map Page displayed, press the

PROC

Key.

FMS

2) Turn the large APPROACH’.

3) Press the

ENT

now active.

Knob to highlight ‘ACTIVATE

Key. The approach procedure is

5) Turn either approach. Press the

FMS

Knob to highlight the desired

ENT

Key.

6) The cursor will move to the TRANSITIONS

FMS

ﬁeld. Turn the large desired transition waypoint and press the

Knob to highlight the

ENT

Key. (The “Vectors” option assumes vectors will be received to the ﬁnal course segment of the approach and will provide navigation guidance relative to the ﬁnal approach course.)

Figure 9-7 Selecting an Approach Transition

7) Turn the large and press the

190-00645-00 Rev. A

FMS

Knob to highlight ‘Activate?’

ENT

Key to activate the approach.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

9-3

SECTION 9 – PROCEDURES

Blank Page

9-4

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 10 – HAZARD

AVOIDANCE

SECTION 10: HAZARD AVOIDANCE

10.1 CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP

1) With the Navigation Map Page displayed, press the

Key to display the Navigation Map Page Menu. The cursor ﬂashes on the ‘Map Setup’ option.

ENT

2) Press the displayed. Turn the small the ‘Weather’ or ‘Trafﬁc’ group to customize the display of weather features. Select ‘Trafﬁc’ to customize the display of trafﬁc.

3) Press the small Navigation Map Page.

Key. The Map Setup Menu is

FMS

Knob to select

FMS

Knob to return to the

10.2 STORMSCOPE® (OPTIONAL)

WARNING: Weather information on the G1000 MFD is approved for weather avoidance only, not weather penetration. Refer to the WX-500 Pilot’s Guide for detailed operation.

Displaying Stormscope Lightning Data on the Navigation Map Page

1) Press the

2) Press the Softkey again to remove Stormscope Lightning Data from the Navigation Map Page.

MAP

Softkey.

STRMSCP

Softkey. Press the

STRMSCP

Figure 10-2 Map Setup Menu

Figure 10-3 Map Setup Group List

190-00645-00 Rev. A

Figure 10-1 Page Menu

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Figure 10-4 In-Flight Navigation Map Page Displaying

Stormscope Lightning Data

Lightning Age Symbol

Strike is less than 6 seconds old

Strike is between 6 and 60 seconds old

Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old

10-1

SECTION 10 – HAZARD

AVOIDANCE

At a map range of less than 25 nm, Stormscope lightning data is not displayed, but can still be present. The presence of Stormscope lightning data is indicated by the annunciation ‘LTNG < 25 nm’ in the upper right corner.

Figure 10-5 Lightning Display Range Annunciation

To select ‘cell’ or ‘strike’ as the Stormscope lightning mode:

1) With the Weather Group selected, press the

ENT

Key. The cursor ﬂashes on ‘STRMSCP

LTNG’.

FMS

2) Turn the large

Knob to select ‘STRMSCP

MODE’.

FMS

3) Turn either

Knob to display the ‘Cell/Strike’

window.

FMS

4) Turn either Press the

5) Push the

Knob to select ‘Cell’ or ‘Strike’.

ENT

Key.

FMS

Knob to return to the Navigation

Map Page.

To clear Stormscope lightning data from the Navigation Map Page:

1) Press the

Key (with the Navigation Map

Page displayed).

FMS

2) Turn either Lightning Data’ ﬁeld and press the

Knob to highlight the ‘Clear

ENT

Key.

2) Turn the small

FMS

Knob until the Stormscope

Page is selected.

Figure 10-6 Stormscope Page

To change the Stormscope lightning mode between ‘cell’ and ‘strike’:

1) Select the Stormscope Page.

MODE

2) Press the

Softkey. The softkeys are displayed. Press the to display ‘CELL’ data or press the

CELL

and

CELL

STRIKE

Softkey

STRIKE

Softkey to display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’ is displayed in the mode box located in the upper left corner of the Stormscope Page.

NOTE: “Cell mode” uses a clustering program to identify clusters of electrical activity that indicate cells.

10-2

Stormscope Page

1) Turn the large group is selected.

To change the viewing mode between 360˚

and 120˚:

FMS

Knob until the Map Page

1) Select the Stormscope Page.

2) Press the

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

VIEW

Softkey. The

360

and

ARC

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SECTION 10 – HAZARD

AVOIDANCE

Softkeys are displayed. Press the 360 Softkey to display a 360˚ viewing are or press the ARC Softkey to display a 120˚ viewing area.

CLEAR

Press the

Softkey to remove all

Stormscope lightning data from the display.

10.3 XM WEATHER (OPTIONAL)

WARNING: Use of XM weather for hazardous weather penetration is not recommended. Weather information provided by XM Radio Service is approved only for weather avoidance, not penetration.

1) Press the

2) Press the display the desired weather. Press the applicable softkey again to remove weather data from the Navigation Map Page.

MAP

Softkey.

NEXRAD or XM LTNG

Softkey to

Displaying METAR and TAF information on the Airport Information Page

To display METAR and TAF text on the Airport Information Page:

FMS

1) Turn the large Group.

2) Turn the small Information Page.

3) Press the

WX Softkey to display METAR and

TAF text (METAR and TAF information is updated every 12 minutes).

Knob to select the WPT Page

FMS

Knob to select the Airport

METAR

Text

Figure 10-7 Navigation Map Page Displaying NEXRAD Weather

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Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

TAF Text

Softkey

Figure 10-8 METAR and TAF Text Displayed on the

Airport (Weather) Information Page

10-3

SECTION 10 – HAZARD

AVOIDANCE

Displaying Weather on the Weather Data Link Page

To select the Weather Data Link Page:

FMS

1) Turn the large Page Group.

2) Turn the small Data Link Page.

3) Press the available softkeys to select the desired XM weather product.

4) Press the

LEGEND

for the selected products. If necessary, turn either

FMS

Knob to scroll through the list. Press the small to return to the map.

Knob to select the Map

FMS

Knob to select the Weather

Softkey to view the legends

FMS

Knob or the

ENT

Softkey

NEXRAD Limitations

Certain limitations exist regarding the NEXRAD radar

displays. Some, but not all, are listed here:

• NEXRAD base reflectivity does not provide sufﬁcient information to determine cloud layers or precipitation characteristics (hail vs. rain, etc).

• An individual NEXRAD site cannot depict high altitude storms at close ranges, and has no information about storms directly over the site.

• The resolution of displayed NEXRAD data is 4 square kilometers. Therefore, when zoomed in on the display, each square block is 2 kilometers on each side. The intensity level reﬂected by the square will be the highest level sampled within the square area.

ECHO TOP – press the ECHO TOP Softkey to show

the location, elevation, and direction the highest radar echo. This may not indicate the top of a storm or clouds, only the highest radar return echo. ECHO TOPS cannot be displayed along with NEXRAD and CLOUD TOPS. When ECHO TOPS is activated, NEXRAD and CLOUD TOPS are removed. Refer to the Legend for a description of the ECHO TOPS coding. The display is updated every 7.5 minutes.

10-4

Figure 10-9 Weather Data Link Page

NEXRAD – press the NEXRAD Softkey to show

NEXRAD weather and radar coverage information. Areas where radar coverage is not available will be shown in grayish-purple. The display is updated every ﬁve minutes.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

CLD TOP – press the CLD TOP Softkey to show the

cloud top altitude determined from satellite imagery. The display is updated every 15 minutes.

LTNG – pressing the LTNG Softkey shows the location

of cloud-to-ground lightning strikes. The display is updated every ﬁve minutes.

NOTE: Strikes depicted represent cloud to ground strikes within a 2 kilometer radius of the actual strike location. Therefore, the exact location of the strike is not displayed.

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SECTION 10 – HAZARD

AVOIDANCE

CELL MOV – pressing the CELL MOV Softkey shows

storm cell movement by displaying an arrow. pointing in the direction of predicted movement. The display is updated every 12 minutes.

SIG/AIR – pressing the SIG/AIR Softkey shows

SIGMET and AIRMET information.

The display is

updated every 12 minutes.

METAR – press the METAR Softkey to graphically

display METARs. METARS are shown as colored ﬂags at airports providing METAR reports. The display is updated every 12 minutes.

MORE WX – press the MORE WX Softkey to display

the following group of softkeys for additional weather control:

SFC – pressing the SFC Softkey for Surface Analysis

shows current or forecast conditions. Forecasts are available for intervals of Current, 12, 24, 36, and 48 hours. Press the softkey corresponding to the desired forecast. The closest city forecast information is displayed in the legend. The display is updated every 12 minutes.

FRZ LVL – press the FRZ LVL Softkey to display

contour lines for freezing levels.

The display is

updated every 12 minutes.

WIND – press the WIND Softkey to show wind

speed and direction at a selected altitude from the ground up to 42,000 feet in 3,000 foot increments. After pressing the

WIND Softkey, press the softkey corresponding to the desired winds aloft altitude. The display is updated every 12 minutes.

COUNTY – pressing the COUNTY Softkey provides

speciﬁc public awareness and protection

weather warnings for Tornado, Severe Thunderstorm, and Flood conditions provided by the National Weather Service (NWS). The display is updated every 5 minutes.

CYCLONE – pressing the CYCLONE Softkey shows

the current location of cyclones (hurricanes and tropical storms) and their projected track at various time intervals. The update rate is every 12 minutes.

Map Panning Information – Weather Data Link Page

1) Push in the arrow.

2) Move the on AIRMETs, TFRs, METARs, or SIGMETs. Press the ENT Key to display pertinent information for the selected product.

Note that pressing the ENT Key when panning

over an AIRMET or a SIGMET displays an information box that displays the text of the report. Panning over an airport with METAR information does not display more information but allows the user to press the select that Airport’s Information Page to display the text of the report. Pressing the ENT Key when panning over a TFR displays TFR speciﬁc information.

Joystick

to display the panning

to place the panning arrow

ENT Key and

Weather Products and Symbols

Figure 10-10 depicts the symbol for each weather product (read from left to right). When a weather product is active, the product symbol is displayed in the lower right of the screen.

• NEXRAD

• Cloud Top/Echo Top

• XM Lightning

• Cell Movement

• SIGMETs/AIRMETs

• METARs

• City Forecast

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10-5

SECTION 10 – HAZARD

AVOIDANCE

• Surface Analysis

• Freezing Levels

• Winds Aloft

• County Warnings

• Cyclone Warnings

Echo Top (Cloud Top and Echo Top Mutually Exclusive)

Figure 10-10 Weather Product Symbols

The XM Information Page in the AUX Page Group will display the weather products available for the current subscription. A green box by the weather product means that it is available.

NOTE: The DONE Softkey on the AUX - XM INFORMATION page is used to save the GDL 69(A) activation data when the XM services are initially set up. It is not used during normal operation of the GDL 69(A), and it should have no adverse effects if inadvertently selected during ﬂight. Refer to the GDL 69/69A XM Satellite Radio Activation Instructions (190-00355-04, Rev E or later) for further information.

Weather Product Age

The age for each of the enabled products is displayed on the right side of the display. Times are based on Zulu time when the data was assembled on the ground, not the time the data was received by the XM receiver. When the age of a weather product has exceeded half of the expiration time, the product time will change from light blue to amber in color.

Weather Product Expires After

(minutes)

SIGMETs/AIRMETs 60 City Forecasts County Warnings Cyclone Warnings Echo Tops Freezing Levels METARs

60 60 60 30 60

90 Lightning 30 NEXRAD 30 Radar Coverage

30 Cell Movement 30 Surface Analysis

60 TFRs 60 Winds Aloft TAFs Clouds Tops

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Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

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SECTION 10 – HAZARD

AVOIDANCE

10.4 TRAFFIC INFORMATION SERVICE (TIS)

NOTE: If the G1000 is conﬁgured to use the optional Ryan 9900BX Trafﬁc Advisory System, TIS will not be available for use.

NOTE: Trafﬁc Information Service (TIS) is only available when the aircraft is within the service volume of a TIS capable terminal radar site.

Displaying Trafﬁc on the Trafﬁc Map Page

1) Turn the large Page Group.

2) Turn the small Map Page.

3) Press the trafﬁc. ‘TIS OPERATIING’ is displayed in the Trafﬁc mode ﬁeld.

4) Press the in the Standby mode. ‘TIS STANDBY’ will be displayed in the Trafﬁc mode ﬁeld.

5) Rotate the area or rotate counter-clockwise to display a smaller area.

If data is not received for a period longer than 6 seconds, the age of the present data will be displayed in the lower left of of the screen along with the annuciation that the system has entered Coast mode. The system will maintain the trafﬁc display (up to 60 seconds) until the next data reception. If no data is received after 60 seconds, trafﬁc will be removed from the display.

FMS

OPERATE

STANDBY

Joystick

Knob to select the Map

Knob to select the Trafﬁc

Softkey to begin displaying

Softkey to place the system

clockwise to display a larger

Trafﬁc Mode

Last data update

is older than 6

sec. resulting in

Coast mode

descending, moving in the direction of the line

Trafﬁc Advisory, aircraft is 400’ above &

Proximity Trafﬁc at same

altitude, level ﬂight & moving

in the direction of the line

Figure 10-11 Trafﬁc Map Page

Trafﬁc 1600’ above &

climbing, moving in the

Trafﬁc out of

range

direction of the line

Displaying Trafﬁc on the Navigation Map

1) Ensure TIS is operating. With the Navigation Map displayed, press the

2) Press the

TRAFFIC

Softkey. Trafﬁc will now be

MAP

Softkey.

displayed on the map.

TIS Audio Alert

When a Trafﬁc Advisory (TA) is displayed, an audio

alert “Trafﬁc” is given.

“Trafﬁc Not Available” will be heard whenever TIS

service becomes unavailable.

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Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

10-7

SECTION 10 – HAZARD

AVOIDANCE

10.5 SKYWATCH TRAFFIC ADVISORY SYSTEM (TAS)(OPTIONAL)

Refer to the SkyWatch pilot’s guide for a detailed

discussion of the SkyWatch system.

Displaying Trafﬁc on the Trafﬁc Map Page

1) Turn the large Page Group.

2) Turn the small Map Page.

3) Press the trafﬁc. ‘TAS OPERATING’ is displayed in the Trafﬁc mode ﬁeld.

4) Press the altitude volume. Select the desired altitude volume by pressing the the

ABOVE

, or selection is displayed in the Altitude mode ﬁeld.

5) Press the in the Standby mode. ‘TAS STANDBY’ will be displayed in the Trafﬁc mode ﬁeld.

6) Rotate the area or rotate counter-clockwise to display a smaller area.

FMS

OPERATE

ALT MODE

UREST

STANDBY

Joystick

Knob to select the Map

Knob to select the Trafﬁc

Softkey to begin displaying

Softkey to change the

BELOW, NORMAL

(unrestricted) Softkey. The

Softkey to place the system

clockwise to display a larger

Trafﬁc Mode

“Non-Bearing” Trafﬁc (system

is unable to determine bearing),

distance is 8.0 nm, 1190’ above

Altitude Mode

and descending

Trafﬁc Advisory,

aircraft is 400’ below

& climbing

Proximity Trafﬁc,

1000’ above &

descending

Figure 10-12 Trafﬁc Map Page

Trafﬁc, Out of

Displaying Trafﬁc on the Navigation Map

1) Ensure the SkyWatch system is operating. With the Navigation Map displayed, press the Softkey.

2) Press the displayed on the map.

TRAFFIC

Softkey. Trafﬁc will now be

Range

MAP

10-8

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 10 – HAZARD

1000'

Aircraft Altitude

100' Threshold

AVOIDANCE

Trafﬁc Advisory

Non-Bearing

Trafﬁc Advisories

Figure 10-13 TAS Trafﬁc on Navigation Map

Trafﬁc Off Scale

Banner

Non-Threat

Trafﬁc

10.6 TERRAIN AND OBSTACLE PROXIMITY

NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south.

4) Rotate the

Joystick

clockwise to display a larger area or rotate counter-clockwise to display a smaller area.

Figure 10-14 Terrain Proximity Page

Color Indication

RED

YELLOW

Terrain/Obstacle above or within 100’ below or above aircraft altitude.

Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude.

Displaying Terrain and Obstacles on the Terrain Proximity Page

1) Turn the large Page Group.

2) Turn the small rectangular page icon.

3) If desired, press the

ARC

and is pressed, a radar-like 120° view is displayed. Press the

190-00645-00 Rev. A

default display.

FMS

Knob to select the Map

FMS

Knob to select the last

VIEW

Softkey to access the

360

Softkeys. When the

360

Softkey to return to the 360°

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

ARC

Softkey

Displaying Terrain and Obstacles on the Navigation Map

1) With the Navigation Map displayed, press the

MAP

Softkey.

2) Press the

TERRAIN

proximity will now be displayed on the map.

Softkey. Terrain and obstacle

10-9

SECTION 10 – HAZARD

AVOIDANCE

Unlighted Obstacle (Height is less than 1000’ AGL)

Lighted Obstacle (Height is less than 1000’ AGL)

Figure 10-15 Obstacle Symbols

10.7 TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY (OPTIONAL)

NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south.

NOTE: TAWS operation is only available when the G1000 is conﬁgured for a TAWS-B installation.

Displaying Terrain on the TAWS Page

Unlighted Obstacle (Height is greater than 1000’ AGL)

Lighted Obstacle (Height is greater than 1000’ AGL)

10-10

1) Turn the large

FMS

Knob to select the Map

Page Group.

FMS

2) Turn the small

Knob to select the TAWS

Page.

VIEW

3) If desired, press the

ARC

and

360

Softkeys. When the

Softkey to access the

is pressed, a radar-like 120° view is displayed.

360

Press the

Softkey to return to the 360°

default display.

4) Rotate the

Joystick

clockwise to display a larger area or rotate counter-clockwise to display a smaller area.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

ARC

Figure 10-16 TAWS Page (360˚ View)

Softkey

Figure 10-17 TAWS Page (ARC View)

190-00645-00 Rev. A

Color Terrain/Obstacle Location

Potential Impact Point

Unlighted Obstacle

Projected Flight Path

1000'

100' Threshold

Red

Yellow

Black

Terrain/Obstacle above or within 100’ below or above aircraft altitude.

Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude.

Terrain/Obstacle is more than 1000’

below aircraft altitude.

SECTION 10 – HAZARD

AVOIDANCE

Enable/Disable Aviation Data

1) While the TAWS Page is displayed, press the

Key.

FMS

2) Turn the small Hide) Aviation Data”.

3) Press the

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Figure 10-18 TAWS Page Menu

ENT

Knob to select “Show (or

Key.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

TAWS Inhibit

Flying VFR into an area where unique terrain exists could cause the system to annunciate a nuisance alert. When TAWS is inhibited, only FLTA and PDA alerts are disabled.

To Inhibit TAWS:

1) While the TAWS Page is displayed, press the

Key.

FMS

2) Turn the small TAWS’.

ENT

3) Press the

Key.

To Enable TAWS:

1) While the TAWS Page is displayed, press the

Key.

2) Turn the small TAWS’.

ENT

3) Press the

Key.

Knob to select‘Inhibit

FMS

Knob to select ‘Enable

10-11

SECTION 10 – HAZARD

700

600

500

400

300

200

100

Height Above Terrain (Feet)

Distance From Destination Airport (nm)

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15

“Too Low, Terrain”“Too Low, Terrain”

Runway

Threshold

AVOIDANCE

Manual System Test

A system test is automatically performed at power-up. After sucessful completion of the test, “TAWS System Test, OK” will be heard.

The system test may also be initiated manually, but only when the aircraft is on the ground. To manually verify proper operation of the aural and visual annunciations of the system, perform the following steps.

1) While the TAWS Page is displayed, press the

Key.

FMS

2) Turn the small

Knob to select ‘Test

TAWS’.

ENT

3) Press the

Key. During the test ‘TAWS TEST’

is displayed in the center of the TAWS Page.

When all is in working order, “TAWS System

Test, OK” will be heard.

Forward Looking Terrain Avoidance (FLTA)

The Forward Looking Terrain Avoidance alert is

composed of two sub-functions:

Reduced Required Terrain Clearance (RTC) and Reduced Required Obstacle Clearance (

This provides alerts when the aircraft ﬂight path is above terrain and/or obstacles, yet is projected to come within minimum clearance values outlined in the following table. When an RTC or ROC alert is issued, a potential impact point is displayed on the TAWS Page as a yellow or red ‘X’.

ROC)

Phase of Flight Level Flight Descending

Enroute 700 ft. 500 ft.

Terminal 350 ft. 300 ft.

Approach 150 ft. 100 ft.

Departure 100 ft. 100 ft.

During the ﬁnal approach phase of ﬂight, RTC/ROC/ ITI/IOI alerts are automatically inhibited when the aircraft is below 200 feet AGL while within 0.5 nm of the approach runway or is below 125 feet AGL while within 1 nm of the runway.

Premature Descent Alert (PDA)

A Premature Descent Alert is issued when the system detects that the aircraft is signiﬁcantly below the normal approach path to a runway. The PDA alert mode functions only during descent to land.

PDA alerting begins when the aircraft is within 15 nm of the destination airport and ends when the aircraft is either 0.5 nm from the runway threshold OR is at an altitude of 125 feet AGL while within 1 nm of the threshold. During the ﬁnal descent, algorithms will set a threshold for alerting based on speed, distance, and other parameters.

Imminent Terrain Impact (

ITI) and Imminent

Obstacle Impact (IOI)

This provides alerts when the aircraft is below the

10-12

elevation of terrain in the aircraft’s projected path. ITI and IOI alerts are accompanied by a potential impact point displayed on the TAWS Page as a yellow or red ‘X’. The alert is given when the projected vertical ﬂight path is calculated to come within minimum clearance altitudes in the following table.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Figure 10-19 PDA Alerting

190-00645-00 Rev. A

Excessive Descent Rate Alert (EDR)

6000

5500

5000

4500

4000

3500

3000

2500

2000

1500

1000

500

2000 4000 6000 8000 10000 12000

"PULL UP""PULL UP"

"SINK RA

TE"

Descent Rate

Height Above Terrain (Feet)

1000

800

600

400

200

Height Above Terrain (Feet)

Altitude Loss (Feet)

0 20 40 60 80 100 120 140

“DON’T SINK”“DON’T SINK”

1000

900

800

700

600

500

400

300

200

100

Height Above Terrain (Feet)

Sink Rate (Feet Per Minute)

“DON’T SINK”“DON’T SINK”

500 1000 1500 2500 35002000 3000 4000

The purpose of the Excessive Descent Rate alert is to provide suitable alerts when the aircraft is determined to be closing (descending) upon terrain at an excessive speed. Figure 10-20 displays the correlation between height above terrain and descent rate, resulting in the two EDR alerts. EDR alerts have two levels of severity, caution (sink rate) and warning (pull-up).

SECTION 10 – HAZARD

AVOIDANCE

Figure 10-21 Negative Climb Rate

Figure 10-20 Excessive Descent Rate

Negative Climb Rate After Takeoff Alert (NCR)

The purpose of the Negative Climb Rate After Takeoff alert is to provide suitable alerts to the pilot when the system determines that the aircraft is losing altitude (closing upon terrain) after takeoff. The aural message “Don’t Sink” is given for NCR alerts, accompanied by an annunciation and a pop-up terrain alert on the display. Figure 10-21 illustrates the envelope for alerts.

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Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

“Five-Hundred” Aural Alert

The purpose of the aural alert message “Five-hundred” is to provide an advisory alert to the aircrew that the aircraft is ﬁve-hundred feet above terrain. When the aircraft descends within 500 feet of terrain, the aural message “Five-hundred” is heard. There are no display annunciations or pop-up alerts that accompany the aural message.

Pop-up Alerts

When the Navigation Map Page is displayed, and a terrain or obstacle alert is issued, a pop-up window is displayed with the appropriate alert.

10-13

SECTION 10 – HAZARD

AVOIDANCE

Figure 10-22 Alert Pop-Up

Press the ENT Key to display the TAWS Page, or press

the CLR Key to remain on the Navigation Map Page.

Alert Annunciations

Alert Annunciation

Figure 10-24 Alert Annunciation on the TAWS Page

Alert Annunciation

10-14

Displaying Terrain and Obstacles on the Navigation Map

1) With the Navigation Map displayed, press the

MAP

Softkey.

2) Press the

TERRAIN

proximity will now be displayed on the map.

Unlighted Obstacle (Height is less than 1000’ AGL)

Softkey. Terrain and obstacle

Lighted Obstacle (Height is less than 1000’ AGL)

Unlighted Obstacle (Height is greater than 1000’ AGL)

Figure 10-23 TAWS Symbols

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Figure 10-25 Alert Annunciation on the PFD

Lighted Obstacle

Potential Impact Points (Height is greater than 1000’ AGL)

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SECTION 10 – HAZARD

AVOIDANCE

TAWS Alerts Summary

The following table shows the possible TAWS alert types with corresponding annunciations and aural messages.

PFD/MFD TAWS

Alert Type

Page

Annunciation

Excessive Descent Rate Warning (EDR) “Pull Up”

Reduced Required Terrain Clearance Warning (RTC)

Imminent Terrain Impact Warning (ITI)

Reduced Required Obstacle Clearance Warning (ROC

Imminent Obstacle Impact Warning (IOI)

Reduced Required Terrain Clearance Caution (RTC)

Imminent Terrain Impact Caution (ITI)

Reduced Required Obstacle Clearance Caution (ROC)

Imminent Obstacle Impact Caution (IOI)

Premature Descent Alert Caution (PDA)

)

MFD

Pop-Up Alert

Aural Message

“Terrain, Terrain; Pull Up, Pull Up”

“Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”

Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”

“Terrain, Terrain; Pull Up, Pull Up”

“Obstacle, Obstacle; Pull Up, Pull Up”

“Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”

“Obstacle, Obstacle; Pull Up, Pull Up”

“Caution, Terrain; Caution, Terrain”

“Terrain Ahead; Terrain Ahead”

“Caution, Terrain; Caution, Terrain”

“Caution, Obstacle; Caution, Obstacle”

“Obstacle Ahead; Obstacle Ahead”

“Caution, Obstacle; Caution, Obstacle”

“Too Low, Terrain”

Altitude Callout “500”

Excessive Descent Rate Caution (EDR) “Sink Rate”

Negative Climb Rate Caution (NCR)

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Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

None None “Five-Hundred”

“Don’t Sink”

“Too Low, Terrain”

10-15

SECTION 10 – HAZARD

AVOIDANCE

The following system status annunciations may also be

issued.

PFD/MFD TAWS

Alert Type

Page

Annunciation

TAWS System Test Fail None “TAWS System Failure”

TAWS Alerting is disabled

No GPS position or excessively degraded GPS signal

System Test in progress None None

System Test pass

None None “TAWS System Test OK”

MFD

Pop-Up Alert

None None

None “TAWS Not Available”

“TAWS Availble” will be heard when sufﬁcient

Aural Message

GPS signal is re-established.

10-16

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 11 – ABNORMAL

OPERATION

SECTION 11: ABNORMAL

OPERATION

11.1 REVERSIONARY MODE

Should a system detected failure occur in either display, the G1000 automatically enters reversionary mode. In reversionary mode, critical ﬂight instrumentation is combined with engine instrumentation on the remaining display. Minimal navigation capability is available on the reversionary mode display.

Reversionary display mode can also be manually activated by the pilot if the system fails to detect a display problem. The reversionary mode is activated manually by pressing the red DISPLAY BACKUP button on the bottom of the audio panel (GMA 1347). Pressing the red DISPLAY BACKUP button again deactivates reversionary mode.

NOTE: The Quest Kodiak 100 Pilot’s Operating Handbook (POH) always takes precedence over the information found in this section.

190-00645-00 Rev. A

Normal PFD Display

MFD in Reversionary Mode

Figure 11-1 G1000 Reversionary Mode: Failed PFD1

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Normal MFD Display

11-1

SECTION 11 – ABNORMAL

OPERATION

11.2 ABNORMAL COM OPERATION

When a COM tuning failure is detected by the system, the emergency frequency (121.500 MHz) is automatically loaded into the active frequency ﬁeld of the COM radio for which the tuning failure was detected. In the event of a dual display failure, the emergency frequency (121.500 MHz) automatically becomes the active frequency to the pilot through the pilot headset.

11.3 UNUSUAL ATTITUDES

The PFD will ‘declutter’ when the aircraft enters an unusual attitude. Only the basic primary functions will be displayed in these situations.

Red extreme pitch warning chevrons pointing toward the horizon are displayed starting at 50 degrees above and 30 degrees below the horizon line.

11.5 HAZARD DISPLAYS WITH LOSS OF GPS POSITION

If GPS position is lost, or becomes invalid, selected hazards being displayed on the Navigation Map Page will be removed until GPS position is again established. The icons in the lower right of the screen, indicating the selected functions for display, will show an ‘X’, as shown in Figure 11-3.

Figure 11-3 Loss of Hazard Functions

with Loss of GPS Position

11-2

Figure 11-2 Extreme Pitch Indication

11.4 STORMSCOPE OPERATION WITH LOSS OF HEADING INPUT

If heading is lost, strikes and/or cells must be cleared manually after the execution of each turn. This is to ensure that the strike and/or cell positions are depicted accurately in relation to the nose of the aircraft.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 12 – ANNUNCIATIONS

& ALERTS

SECTION 12: ANNUNCIATIONS &

ALERTS

NOTE: The Airplane Flight Manual supersedes information found in this document.

System

Annunciation

Red ‘X’

Annunciation

Window

Alerts Window

from annunciations that are not yet acknowledged. Acknowledged annunciations are always above the line. Annunciations are displayed in order of priority from top to bottom. The highest priority annunciation is displayed at the top of the Annunciation Window.

• Alerts Window: The Alerts Window displays alert text messages. Up to 64 prioritized alerts can be displayed in the Alerts Window. Pressing the ALERTS Softkey displays the Alerts Window. Pressing the ALERTS Softkey again removes the Alerts Window from the display. When the Alerts Window is displayed, the pilot may use the large FMS Knob to scroll through the alert list. Higher priority alerts are displayed at the top of the window. Lower priority alerts are displayed at the bottom of the window. Active alerts are displayed in white text. Alerts that have become inactive will change to gray text. The ALERTS Softkey will ﬂash if the state of a displayed alert changes or a new alert is displayed. The inactive alerts can be removed from the Alerts Window by pressing the ﬂashing ALERTS Softkey.

ALERTS Softkey

Figure 12-1 G1000 Alerting System

Annunciation

The G1000 Alerting System conveys alerts to the pilot

using a combination of the following items:

• Annunciation Window: The Annunciation Window displays abbreviated annunciation text. The Annunciation Window is located to the right of the Altimeter and Vertical Speed Indicator on the PFD display (or the MFD if system is in Reversionary Mode). Up to 12 annunciations can be displayed simultaneously. A white horizontal line separates annunciations that are acknowledged

190-00645-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

• ALERTS Softkey Annunciation: When the Alerting System issues an alert, the ALERTS Softkey is used as a ﬂashing annunciation to accompany an alert. During the alert, the ALERTS Softkey assumes a new label consistent with alert level (WARNING, CAUTION, or ADVISORY). Pressing the softkey annunciation acknowledges that the pilot is aware of the alert. The softkey then returns to the previous ALERTS label. The pilot can then press the ALERTS Softkey again to view alert text messages.

• System Annunciations: Typically, a large red ‘X’ appears in a window when a related LRU fails or

12-1

SECTION 12 – ANNUNCIATIONS

& ALERTS

detects invalid data.

• Audio Alerting System: The G1000 system issues audio alert tones when speciﬁc system conditions are met. See the Alert Levels Deﬁnitions section for more information.

12.1 ALERT LEVEL DEFINITIONS

The G1000 Alerting System, as installed in Quest

Kodiak 100 aircraft, uses three alert levels.

• WARNING: This level of alert requires immediate pilot attention. A warning alert is accompanied by an annunciation in the Annunciation Window. Warning text appearing in the Annunciation Window is RED. A warning alert is also accompanied by a ﬂashing WARNING Softkey annunciation, as shown in Figure 12-2. Pressing the WARNING Softkey acknowledges the presence of the warning alert and stops the aural tone, if applicable.

• CAUTION: This level of alert indicates the existence of abnormal conditions on the aircraft that may require pilot intervention. A caution alert is accompanied by an annunciation in the Annunciation Window. Caution text appearing in the Annunciation Window is YELLOW. A caution alert is also accompanied by a ﬂashing CAUTION Softkey annunciation, as shown in Figure 12-3. Pressing the CAUTION Softkey acknowledges the presence of the caution alert.

of the message advisory alert and displays the alert text message in the Alerts Window.

Figure 12-2 WARNING Softkey

Annunciation

Figure 12-3 CAUTION Softkey

Annunciation

Figure 12-4 ADVISORY Softkey

Annunciation

12-2

• MESSAGE ADVISORY: This level of alert provides general information to the pilot. A message advisory alert does not issue annunciations in the Annunciation Window. Instead, message advisory alerts only issue a ﬂashing ADVISORY Softkey annunciation, as shown in Figure 12-4. Pressing the ADVISORY Softkey acknowledges the presence

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

SECTION 12 – ANNUNCIATIONS

& ALERTS

12.2 AIRCRAFT ALERTS

See the Airplane Flight Manual for information

regarding pilot responses.

WARNING Alerts

Annunciation Window Text Alerts Window Message Audio Alert/(Repeating)

BETA Beta operation is active while airborne. Chime

OIL PRES LO Oil pressure is below 40 psi. Chime

FUEL OFF Fuel cutoff switch is active. Chime

RESERVE FUEL Reserve fuel is in use. Chime

CO LVL HIGH Carbon Monoxide level is too high. Chime

OIL PRES LOW Low oil pressure. Chime

CAUTION Alerts

Annunciation Window Text Alerts Window Message Audio Alert

ALTERNATOR Alternator failed. Single Chime

CARGO DOOR Cargo door is not closed and locked. Single Chime

EMER PWR LVR Emergency power lever is active. Single Chime

FLAP FAIL TBD Single Chime FUEL LO L Left fuel quantity less than 67 lbs (10 gal). Single Chime

FUEL LO R Right fuel quantity less than 67 lbs (10 gal). Single Chime

FUEL LO L-R

FUEL PRES LO Fuel pressure less than 4 psi. Single Chime

GEN FAIL Generator failed. Single Chime

STBY PWR ON Standby power is active. Single Chime

VOLTAGE LO On-board voltage is below 24.0 V. Single Chime

190-00645-00 Rev. A

Left and right fuel quantities less than 67 lbs (10 gal) per tank.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Single Chime

12-3

SECTION 12 – ANNUNCIATIONS

& ALERTS

Annunciation Advisory

Annunciation Window Text Alerts Window Message Audio Alert

AUX PUMP ON Auxiliary fuel pump is on. None

BETA Beta operation is active. None

DE-ICE PR HI De-icing ﬂuid pressure is greater than TBD psi. None

FOD DOOR BP FOD door is in bypass position None

IGNITION ON Engine ignition is active. None

PITO FL L Left pitot heat is inoperative. None

PITO FL R Right pitot heat is inoperative. None

PITO FL L-R Left and right pitot heat are inoperative. None

STARTER ON Engine starter is active. None

Normal Operating Annunciation

Annunciation Window Text Alerts Window Message Audio Alert

FOD DOOR NRM

PITO OFF L

PITO OFF R

PITO OFF L-R

FOD door is in normal position. None

Left pitot heat is off. None

Right pitot heat is off. None

Left and right pitot heat are off. None

12-4

Message Advisory Alerts

Alerts Window Message Audio Alert

GIA FAN FAIL – The cooling fan for the GIAs is inoperative. PFD1 FAN FAIL – The cooling fan for PFD1 is inoperative. PFD2 FAN FAIL – The cooling fan for PFD2 is inoperative. MFD FAN FAIL – The cooling fan for the MFD is inoperative.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

None None None None

190-00645-00 Rev. A

12.4 G1000 SYSTEM ANNUNCIATIONS

When an LRU or an LRU function fails, a large red ‘X’ is typically displayed on windows associated with the failed data. The following section describes various system annunciations. Refer to the POH for additional information

regarding pilot responses to these annunciations.

System Annunciation Comment

Attitude and Heading Reference System is aligning.

SECTION 12 – ANNUNCIATIONS

& ALERTS

NOTE: Upon power-up of the G1000 system, certain windows remain invalid as G1000 equipment begins to initialize. All windows should be operational within one minute of power-up. Should any window continue to remain ﬂagged, the G1000 system should be serviced by a Garmin-authorized repair facility.

Display system is not receiving attitude information from the AHRS.

Display system is not receiving airspeed input from air data computer.

Display is not receiving altitude input from the air data computer.

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Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

12-5

SECTION 12 – ANNUNCIATIONS

& ALERTS

System Annunciation Comment

Display is not receiving vertical speed input from the air data computer.

Display is not receiving valid heading input from AHRS.

GPS information is either not present or is invalid for navigation use. Note that AHRS utilizes GPS inputs during normal operation. AHRS operation may be degraded if GPS signals are not present (see POH).

12-6

Other Various Red X Indications

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

Display is not receiving valid transponder information.

A red ‘X’ through any other display ﬁeld, such as engine instrumentation ﬁelds, indicates that the ﬁeld is not receiving valid data.

190-00645-00 Rev. A

A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 12-5 illustrates all possible ﬂags and the responsible LRUs.

SECTION 12 – ANNUNCIATIONS

& ALERTS

GIA 63 Integrated

Avionics Units

GEA 71 Engine

Airframe Unit

GIA 63 Integrated

Avionics Unit

GDC 74A Air Data

Computer

Figure 12-5 G1000 System Failure Annunciations

GIA 63 Integrated

Avionics Units

GDC 74A Air Data

Computer

GRS 77 AHRS

GMU 44

Magnetometer

GIA 63 Integrated

Avionics Units

GTX 33 Transponder

GIA 63 Integrated

Avionics Units

12.5 G1000 SYSTEM MESSAGE

ADVISORIES

This section describes various G1000 system message advisories. Certain messages are issued due to an LRU or an LRU function failure. Such messages are normally accompanied by a corresponding red ‘X’ annunciation as shown previously in the G1000 System Annunciation section.

190-00645-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

NOTE: This Section provides information regarding G1000 message advisories that may be displayed by the system. Knowledge of the aircraft, systems, ﬂight conditions, and other existing operational priorities must be considered when responding to a message. Always use sound pilot judgment. The Quest Kodiak 100 Pilot’s Operating Handbook (POH) takes precedence over any conﬂicting guidance found in this section.

12-7

SECTION 12 – ANNUNCIATIONS

& ALERTS

MFD & PFD Message Advisories

Message Comments

DATA LOST – Pilot stored data was lost. Recheck settings.

XTALK ERROR – A ﬂight display crosstalk error has occurred.

PFD1 SERVICE – PFD1 needs service. Return unit for repair.

PFD2 SERVICE – PFD2 needs service. Return unit for repair.

MFD1 SERVICE

service. Return unit for repair. PFD1 CONFIG – PFD1 conﬁguration

error. Conﬁg service req’d. PFD2 CONFIG – PFD2 conﬁguration

error. Conﬁg service req’d. MFD1 CONFIG – MFD1 conﬁguration

error. Conﬁg service req’d. SW MISMATCH – GDU software

mismatch. Xtalk is off. MANIFEST – PFD1 software mismatch.

Communication halted. MANIFEST – MFD1 software

mismatch. Communication halted. PFD1 COOLING – PFD1 has poor

cooling. Reducing power usage. PFD2 COOLING – PFD2 has poor

cooling. Reducing power usage. MFD1 COOLING – MFD1 has poor

cooling. Reducing power usage.

PFD1 “KEY” KEYSTK – Key is stuck. PFD2 “KEY” KEYSTK – Key is stuck. MFD1 “KEY” KEYSTK – Key is stuck. CNFG MODULE – PFD1 conﬁguration

module is inoperative.

– MFD1 needs

The pilot proﬁle data was lost. System reverts to default pilot proﬁle and settings. The pilot may reconﬁgure the MFD & PFD with preferred settings, if desired.

The MFD and PFD are not communicating with each other. The G1000 system should be serviced.

The PFD and/or MFD self-test has detected a problem. The G1000 system should be serviced.

The PFD and/or MFD conﬁguration settings do not match backup conﬁguration memory. The G1000 system should be serviced.

The MFD and PFD have different software versions installed. The G1000 system should be serviced.

The PFD and/or MFD has incorrect software installed. The G1000 system should be serviced.

The PFD and/or MFD is overheating and is reducing power consumption by dimming the display. If problem persists, the G1000 system should be serviced.

A key is stuck on the PFD and/or MFD bezel. Attempt to free the stuck key by press

ing it several times. The G1000 system should be serviced if the problem persists.

The PFD conﬁguration module backup memory has failed. The G1000 system should be serviced.

12-8

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

MFD & PFD Message Advisories (Cont.)

Message Comments

PFD1 VOLTAGE

age. Reducing power usage.

PFD2 VOLTAGE

age. Reducing power usage.

MFD1 VOLTAGE

age. Reducing power usage.

– PFD1 has low volt-

– PFD2 has low volt-

– MFD1 has low volt-

The PFD1 voltage is low. The G1000 system should be serviced.

The PFD2 voltage is low. The G1000 system should be serviced.

The MFD1 voltage is low. The G1000 system should be serviced.

Database Message Advisories

Alerts Window Message Comments

MFD1 DB ERR – MFD1 aviation database error exists.

PFD1 DB ERR – PFD1 aviation database error exists.

PFD2 DB ERR – PFD2 aviation database error exists.

MFD1 DB ERR – MFD1 basemap database error exists.

PFD1 DB ERR – PFD1 basemap database error exists.

PFD2 DB ERR – PFD2 basemap database error exists.

MFD1 DB ERR – MFD1 terrain database error exists.

PFD1 DB ERR – PFD1 terrain database error exists.

PFD2 DB ERR – PFD2 terrain database error exists.

DB MISMATCH – Aviation database version mismatch. Xtalk is off.

DB MISMATCH – Aviation database type mismatch. Xtalk is off.

The MFD and/or PFD detected a failure in the aviation database. Attempt to reload the aviation database. If problem persists, the G1000 system should be serviced.

The MFD and/or PFD detected a failure in the basemap database.

The MFD and/or PFD detected a failure in the terrain database. Ensure that the ter rain card is properly inserted in display. Replace terrain card. If problem persists, the G1000 system should be serviced.

The PFD and MFD have different aviation database versions installed. Crossﬁll is off. Install correct aviation database version in both displays.

The PFD and MFD have different aviation database types installed (Americas, Euro pean, etc.). Crossﬁll is off. Install correct aviation database type in both displays.

SECTION 12 – ANNUNCIATIONS

& ALERTS

190-00645-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

12-9

SECTION 12 – ANNUNCIATIONS

& ALERTS

Database Message Advisories (Cont.)

Alerts Window Message Comments

DB MISMATCH

– Basemap database

version mismatch. Xtalk is off.

DB MISMATCH

– Terrain database

version mismatch. Xtalk is off.

DB MISMATCH

– Terrain database

type mismatch. Xtalk is off.

DB MISMATCH

– Obstacle database

version mismatch. Xtalk is off

DB MISMATCH

– Airport Terrain

database mismatch. Xtalk is off

GMA 1347 Message Advisories

Alerts Window Message Comments

GMA1 FAIL – GMA1 is inoperative. Number 1 audio panel self-test has detected a failure. The audio panel is unavail

GMA2 FAIL – GMA2 is inoperative. Number 2 audio panel self-test has detected a failure. The audio panel is unavail

GMA1 CONFIG – GMA1 conﬁguration

error. Conﬁg service req’d. GMA2 CONFIG – GMA2 conﬁguration

error. Conﬁg service req’d. MANIFEST – GMA1 software

mismatch. Communication halted. MANIFEST – GMA2 software

mismatch. Communication halted.

GMA1 SERVICE

service. Return unit for repair.

GMA2 SERVICE

service. Return unit for repair.

BACKUP PATH – Audio panel 1 using backup data path.

– GMA1 needs

– GMA2 needs

The PFD and MFD have different basemap database versions installed. Crossﬁll is off. Install correct basemap database version in both displays.

The PFD and MFD have different terrain database versions installed. Crossﬁll is off. Install correct terrain database version in both displays.

The PFD and MFD have different terrain database types installed. Crossﬁll is off. Install correct terrain database type in both displays.

The PFD and MFD have different obstacle database versions installed. Crossﬁll is off. Install correct obstacle database version in both displays.

The PFD and MFD have different airport terrrain databases installed. Crossﬁll is off. Install correct airport terrain database in both displays.

able. The G1000 system should be serviced.

able. The G1000 system should be serviced. Number 1 audio panel conﬁguration settings do not match backup conﬁguration

memory. The G1000 system should be serviced. Number 2 audio panel conﬁguration settings do not match backup conﬁguration

memory. The G1000 system should be serviced. Number 1 audio panel has incorrect software installed. The G1000 system should be

serviced. Number 2 audio panel has incorrect software installed. The G1000 system should be

serviced. Number 1 audio panel self-test has detected a problem in the unit. Certain audio

functions may still be available, and the audio panel may still be usable. The G1000 system should be serviced when possible.

Number 2 audio panel self-test has detected a problem in the unit. Certain audio functions may still be available, and the audio panel may still be usable. The G1000 system should be serviced when possible.

The #1 audio panel is using a backup communication path. The G1000 system should be serviced when possible.

12-10

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

190-00645-00 Rev. A

GIA 63 Message Advisories

Alerts Window Message Comments

GIA1 CONFIG – GIA1 conﬁguration error. Conﬁg service req’d.

GIA2 CONFIG – GIA2 conﬁguration error. Conﬁg service req’d.

GIA1 COOLING – GIA1 temperature too low.

GIA2 COOLING – GIA2 temperature too low.

GIA1 COOLING – GIA1 over temperature.

GIA2 COOLING – GIA2 over temperature.

GIA1 SERVICE – GIA1 needs service. Return the unit for repair.

GIA2 SERVICE – GIA2 needs service. Return the unit for repair.

HW MISMATCH – GIA hardware mismatch. Communication halted.

MANIFEST – GIA1 software mismatch. Communication halted.

MANIFEST – GIA2 software mismatch. Communication halted.

COM1 TEMP – COM1 over temp. Reducing transmitter power.

COM2 TEMP – COM2 over temp. Reducing transmitter power.

COM1 SERVICE

service. Return unit for repair.

COM2 SERVICE

service. Return unit for repair.

– COM1 needs

– COM2 needs

SECTION 12 – ANNUNCIATIONS

& ALERTS

The GIA1 and/or GIA2 conﬁguration settings do not match backup conﬁguration memory. The G1000 system should be serviced.

The GIA1 and/or GIA2 temperature is too low to operate correctly. Allow units to warm up to operating temperature.

The GIA1 and/or GIA2 temperature is too high. If problem persists, the G1000 system should be serviced.

The GIA1 and/or GIA2 self-test has detected a problem in the unit. The G1000 system should be serviced.

There is a hardware mismatch between GIA1 and GIA2. The G1000 system should be serviced.

The GIA1 and/or GIA 2 has incorrect software installed. The G1000 system should be serviced.

The system has detected an over temperature condition in COM1 and/or COM2. The transmitter will operate at reduced power. If the problem persists, the G1000 system should be serviced.

The system has detected a failure in COM1 and/or COM2. COM1 and/or COM2 may still be usable. The G1000 system should be serviced when possible.

190-00645-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

12-11

SECTION 12 – ANNUNCIATIONS

& ALERTS

GIA 63 Message Advisories (Cont.)

Alerts Window Message Comments

COM1 PTT – COM1 push-to-talk key is stuck.

COM2 PTT – COM2 push-to-talk key is stuck.

COM1 RMT XFR – COM1 remote transfer key is stuck.

COM2 RMT XFR – COM2 remote transfer key is stuck.

RAIM UNAVAIL

available from FAF to MAP waypoints.

RAIM UNAVAIL

available. POSN ERROR – RAIM has determined

GPS position is in error.

DGRD GPS ACC

accuracy degraded & RAIM unavailable.

GPS1 FAIL – GPS1 is inoperative.

GPS2 FAIL – GPS2 is inoperative.

– RAIM is not

– GPS position

The COM1 and/or COM2 external push-to-talk switch is stuck in the enable (or “pressed”) position. Press the PTT switch again to cycle its operation. If the problem persists, the G1000 system should be serviced.

The COM1 and/or COM2 transfer switch is stuck in the enabled (or “pressed”) posi

tion. Press the transfer switch again to cycle its operation. If the problem persists, the G1000 system should be serviced.

GPS satellite coverage is insufﬁcient to perform Receiver Autonomous Integrity Monitoring (RAIM) from the FAF to the MAP waypoints.

GPS satellite coverage is insufﬁcient to perform Receiver Autonomous Integrity Monitoring (RAIM) for the current phase of ﬂight.

When a RAIM position error is detected, GPS is ﬂagged and the system no longer provides GPS-based guidance.

GPS position accuracy has been degraded and RAIM is not available.

A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver is unavailable. The G1000 system should be serviced.

12-12

GPS1 SERVICE – GPS1 needs service. Return unit for repair.

GPS2 SERVICE – GPS2 needs service. Return unit for repair.

NAV1 SERVICE – NAV1 needs service. Return unit for repair.

NAV2 SERVICE – NAV2 needs service. Return unit for repair.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still be available. The G1000 system should be serviced.

A failure has been detected in the NAV1 and/or NAV2 receiver. The receiver may still be available. The G1000 system should be serviced.

190-00645-00 Rev. A

GIA 63 Message Advisories (Cont.)

Alerts Window Message Comments

NAV1 RMT XFR – NAV1 remote transfer key is stuck.

The remote NAV1 and/or NAV2 transfer switch is stuck in the enabled (or “pressed”) state. Press the transfer switch again to cycle its operation. If the problem persists,

NAV2 RMT XFR – NAV2 remote

the G1000 system should be serviced.

transfer key is stuck.

G/S1 FAIL – G/S1 is inoperative. G/S2 FAIL – G/S2 is inoperative.

A failure has been detected in glideslope receiver 1 and/or receiver 2. The G1000 system should be serviced.

G/S1 SERVICE – G/S1 needs service. Return unit for repair.

G/S2 SERVICE – G/S2 needs service.

A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver may still be available. The G1000 system should be serviced when possible.

Return unit for repair.

GEA 71 Message Advisories

Alerts Window Message Comments

GEA1 CONFIG – GEA1 conﬁguration error. Conﬁg service req’d.

MANIFEST – GEA1 software mismatch. Communication halted.

BACKUP PATH

– EIS using backup

data path.

The GEA 71 conﬁguration settings do not match those of backup conﬁguration memory. The G1000 system should be serviced.

The GEA 71 has incorrect software installed. The G1000 system should be serviced.

The GEA 71 is using a backup communication path. The G1000 system should be serviced when possible.

SECTION 12 – ANNUNCIATIONS

& ALERTS

GTX 33 Message Advisories

Alerts Window Message Comments

XPDR1 CONFIG – XPDR1 conﬁg error. Conﬁg service req’d.

MANIFEST – GTX1 software mismatch. Communication halted.

BACKUP PATH

data path.

190-00645-00 Rev. A

– XPDR1 using backup

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

The transponder conﬁguration settings do not match those of backup conﬁguration memory. The G1000 system should be serviced.

The transponder has incorrect software installed. The G1000 system should be serviced.

The #1 transponder is using a backup communications path. The G1000 system should be serviced when possible.

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SECTION 12 – ANNUNCIATIONS

& ALERTS

GRS 77 Message Advisories

Alerts Window Message Comments

AHRS1 TAS – AHRS1 not receiving airspeed.

AHRS1 GPS – AHRS1 using backup GPS source.

AHRS1 GPS – AHRS1 not receiving any GPS information.

AHRS1 GPS – AHRS1 not receiving backup GPS information.

AHRS1 GPS – AHRS1 operating exclusively in no-GPS mode.

MANIFEST – GRS1 software mismatch. Communication halted.

BACKUP PATH – AHRS1 using backup data path.

AHRS1 SRVC – AHRS1 Magnetic-ﬁeld model needs update.

GEO LIMITS – AHRS1 too far North/ South, no magnetic compass.

The #1 AHRS is not receiving true airspeed from the air data computer. The AHRS relies on GPS information to augment the lack of airspeed. The G1000 system should be serviced.

The #1 AHRS is using the backup GPS path. Primary GPS path has failed. The G1000 system should be serviced when possible.

The #1 AHRS is not receiving any or any useful GPS information. Check AFMS limitations. The G1000 system should be serviced.

The #1 AHRS is not receiving backup GPS information. The G1000 system should be serviced.

The #1 AHRS is operating exclusively in no-GPS mode. The G1000 system should be serviced.

The AHRS has incorrect software installed. The G1000 system should be serviced.

The #1 AHRS is using a backup communications data path. The G1000 system should be serviced when possible.

The #1 AHRS earth magnetic ﬁeld model is out of date. Update magnetic ﬁeld model when practical.

The aircraft is outside geographical limits for approved AHRS operation. Heading is ﬂagged as invalid.

12-14

GMU 44 Message Advisories

Alerts Window Message Comments

HDG FAULT – AHRS1 magnetometer fault has occurred.

MANIFEST – GMU1 software mismatch. Communication halted.

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

A fault has occurred in the GMU 44. Heading is ﬂagged as invalid. The AHRS uses GPS for backup mode operation. The G1000 system should be serviced.

The GMU 44 has incorrect software installed. The G1000 system should be serviced.

190-00645-00 Rev. A

Garmin Kodiak 100 Reference Guide

Specifications and Main Features

Frequently Asked Questions

User Manual

SECTION 1: SYSTEM OVERVIEW

1.1 PFD/MFD CONTROLS

1.2 PFD SOFTKEYS

1.3 MFD SOFTKEYS

1.4 MFD PAGE GROUPS

1.5 BACKLIGHTING

1.6 DATABASE UPDATES

Aviation Database Update

Terrain and Obstacle Database Updates

SECTION 2: FLIGHT INSTRUMENTS

2.1 AIRSPEED INDICATOR

Speed Indication

Vspeed References

2.2 ATTITUDE INDICATOR

Speed Ranges

Airspeed Trend Vector

2.3 ALTIMETER

Altitude Select Bug

Altitude Trend Vector

Altitude Alerting

Barometric Minimum Descent Altitude

Barometric Setting Box

2.5 MARKER BEACON ANNUNCIATIONS

2.6 VERTICAL SPEED INDICATOR

2.4 VERTICAL DEVIATION/GLIDESLOPE INDICATOR

2.7 HORIZONTAL SITUATION INDICATOR (HSI)

Arc HSI

Turn Rate Indicator and Heading Trend Vector

Course Pointer

Course Deviation Indicator (CDI)

Bearing Pointers and Information Windows

Navigation Source

SECTION 3: ENGINE INDICATION

Engine Display

Engine System Display

Engine Fuel Display

4.1 NAV/COM DESCRIPTION

4.1 RADIO STATUS INDICATIONS

4.2 VOLUME

4.4 QUICKLY ACTIVATING 121.500 MHZ

4.5 FREQUENCY AUTO-TUNING

Auto-tuning on the PFD

4.3 AUTOMATIC SQUELCH

Auto-tuning on the MFD

4.5 TRANSPONDER OPERATION

Mode Selection

Reply Status

Code Selection

Flight ID Reporting

SECTION 5: AUDIO PANEL

5.1 COM RADIO SELECTION

5.2 MARKER BEACON RECEIVER

Marker Beacon Signal Sensitivity

5.3 NAV RADIO AUDIO SELECTION

5.4 INTERCOM SYSTEM (ICS) ISOLATION

5.5 INTERCOM SQUELCH CONTROL

5.6 DIGITAL CLEARANCE RECORDER AND PLAYER

5.7 REVERSIONARY MODE

SECTION 7: NAVIGATION

7.1 NAVIGATION MAP PAGE

Select the MAP Page Group

7.2 DIRECT-TO NAVIGATION

Direct-to Navigation from the MFD

Direct-to Navigation from the PFD

7.3 AIRPORT INFORMATION

Select the Airport Information Page

7.4 INTERSECTION INFORMATION

Select the Intersection Information Page

7.5 NDB INFORMATION

Select the NDB Information Page

7.6 VOR INFORMATION

Select the VOR Information Page

7.7 USER WAYPOINT INFORMATION PAGE

7.8 NEAREST AIRPORTS

Nearest Airport Information on the MFD

Nearest Airports Information on the PFD